as350b2 s/n 2364 se-jfl - cdn-3.thejameslist.com s/n 2364 se-jfl 1. ... as355f1, as355f2, as355n,...
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STATUS REPORT INDEX AS350B2 s/n 2364 SE-JFL
1. OVERVIEW STATUS AIRFRAME INSPECTIONS
2. AD, ASB, MOD AIRFRAME
3. STATUS! COMPONENT AIRFRAME
4. OVERVIEW STATUS ENGINE INSPECTIONS
5. AD, ASB, MOD ENGINE
6. STATUS! COMPONENT ENGINE
7. MODIFICATIONS – STC
8. BASIC WEIGHT & BALANCE
9. REMAINING REMARKS
10. REPETITIVE (NATIONAL) REQUIREMENTS
AIRFRAME INSP REF TOL Note Last perf. A/C TT Remaining time
SLL (various) 04-10-00 - See Binder tab No.3 -
Time Limits/Maintenace Checks
(various)04-20-00 - 5270,2FH / 34216TC -
Components subject to TBO
(various)05-10-00 - See Binder tab No.3 -
Components subject to OTL
(various)05-11-00 - See Binder tab No.3 -
Components subject to OC 05-12-00 - 5270,2FH / 34216TC -
BFF/ 0 -/ TA/ ALF 05-20-00 0 DAILY DAILY
10FH 05-20-01 1FH DAILY DAILY
10FH / 7D 05-20-02 0 DAILY DAILY
150FH / 12M insp 05-21-00 15FH/36D 5270,2FH / 2015-12-07 5420,2FH / 2016-12-07
150FH insp 05-21-01 15FH 5270,2FH 5420,2FH
12M insp 05-21-02 36D 2015-12-07 2016-12-07
600FH / 24M insp 05-22-00 60FH/73D 5270,2FH / 2015-12-07 5870,2FH / 2017-12-07
Scheduled Airframe Inspections
600FH / 24M insp 05-22-00 60FH/73D 5270,2FH / 2015-12-07 5870,2FH / 2017-12-07
600FH insp 05-22-01 60FH 5270,2FH 5870,2FH
24M insp 05-22-02 73D 2015-12-07 2017-12-07
1200FH / 48M insp 05-23-00 120FH/146D 5270,2FH / 2015-12-07 6470,2FH / 2019-12-07
1200FH insp 05-23-01 120FH 5270,2FH 6470,2FH
48M insp 05-23-02 146D 2015-12-07 2019-12-07
144M insp 05-24-02 180D 2015-12-07 2027-12-07
Specific periodic intervals (various) 05-25-00 -5270,2FH / 34216TC /
2015-12-07-
Punctual Intervals (various) 05-26-00 -5270,2FH / 34216TC /
2015-12-07-
ATA Appl.AD
classAD number
Issue
DateSubject
Appr. Holder / Type
Design.
Effective
date
Expire
datePerformed SB Rec.
65 N/A EADFAA 2015-22-53
(EASA 2015-0178)2015-10-30
Tail Rotor Control
SUPERSEDES FAA EAD 2015-22-52
Applicability: AS350B3 helicopters with a dual hydraulic
system installed, certificated in any category.
AIRBUS HELICOPTERS
AS 350
2015-11-02
N/A. AS350 B3
model only.
67.00.66
SIN 2944-
S-29
65 N/A EADFAA 2015-22-52
(EASA 2015-0178)2015-10-28
Tail Rotor Control
SUPERSEDED BY FAA EAD 2015-22-53
Applicability: AS350B3 helicopters with a dual hydraulic
system installed, certificated in any category.
AIRBUS HELICOPTERS
AS 350
2015-10-29
N/A. AS350 B3
model only.
67.00.66
SIN 2944-
S-29
65 Y AD 2015-0195 2015-09-23
Tail Rotor Drive – Drive Shaft Bearings – Inspection /
Replacement
SUPERSEDES AD F-1998-173-073
Applicability: AS 350 B, BA, BB, B1, B2, B3 and D helicopters,
and AS 355 E, F, F1, F2, N and NP helicopters, all serial
numbers, if equipped with tail rotor (TR) drive shaft bearings
as indicated in Table 1 of this AD.
AIRBUS HELICOPTERS
AS 350
AS 355
2015-10-07 165FH
New
driveshaft
bearings
installed 2015-
11-03. Next
insp: A/CTT
5435,2.
01.00.70 165FH
63 N/A AD FAA 2015-17-11 2015-09-29
Main Rotor System
Applicability: AS350B, AS350BA, AS350B1, AS350B2,
AS350B3,AS350C, AS350D, AS350D1, AS355E, AS355F,
AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2
helicopters with a swashplate assembly with rotating star,
part number (P/N) 350A371003-04, 350A371003-05,
350A371003-06, 350A371003-07, or 350A371003-08,
certificated in any category.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2015-09-29 165FH
2015-04-10
P/N affected,
but repair not
performed =
AD N/A. Test
iaw ASB
performed to
confirm.
62.00.34 No
- N/A AD 2015-0178 2015-08-26
Rotorcraft Flight Manual - Chapter Normal Procedures - Engine
prestart Check / Run-up Check / Engine and Rotor Shutdown -
Amendment
Applicability: AS 350 B3 helicopters, all serial numbers, if
equipped with a dual hydraulic system, production
modification (mod) OP 3082, or mod OP 3346.
AIRBUS HELICOPTERS
AS 3502015-08-31 2015-09-07
67.00.66
SIN 2944-
S-29
63 N/A PAD 15-104 2015-08-03
Rotor Drive - Main Gearbox Main and Bottom Casings -
Inspection/Replacement
Applicability: AS 350 B3 helicopters, all serial numbers, if
equipped with MGB main casing P/N 350A32-3156-21 (fitted
on assembly P/N 350A32-3156-01), or P/N 350A32-3156-22
(fitted on assembly P/N 350A32-3156-02), or P/N 350A32-
3121-04, or P/N 350A32-3121-06, or if equipped with MGB
bottom casing (sump) P/N 350A32-3119-05.
AIRBUS HELICOPTERS
AS 350- 165FH/6M - 01.00.68
63 Y PAD 15-105 2015-08-03
Rotor Drive - Main Gearbox Bottom Casing -
Inspection/Replacement
Applicability: AS 350 B1, B2 and AS 355 E, F, F1, F2, N
helicopters, all serial numbers, if equipped with MGB bottom
casing (sump) P/N 350A32-3119-03 or P/N 350A32-3119-05.
AIRBUS HELICOPTERS
AS 350
AS 355
- 165FH/6M
2015-12-04:
The recorded TC
on MGB sump is
34216 /FH is
5270,2. No
further action is
required until
TC has reached
93700 (PHAB
WO 17220006).
01.00.56
01.00.69
.05 y AD 2015-0132 2015-07-08
Time Limits / Maintenance Checks - Aitworthiness Limitations
/ Maintenance Requirements - Implementation
SUPERSEDES AD 2013-0088
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 D, AS
350 B1, AS 350 B2, AS 350 B3, EC 130 T2 and EC 130 B4
helicopters, all serial numbers.
AIRBUS HELICOPTERS
AS 350 / EC 1302015-07-22 2016-07-22
Perf iaw AMP
AS350B2 SE-
JFL 2015-11-
27 / PHAB
CAMO
SE.MG.0107
AS350B2
ALS
REVISION
005
67 N/A PAD 15-087 2015-06-24
Rotor Flight Control - Tail Rotor Control Stop Screws -
Modification
SUPERSEDES AD 2011-0164
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS
350 B2, AS 350 B3 and AS 350 D helicopters, all serial numbers
(s/n), if equipped with adjustable primary yaw stop in the
baggage compartment which corresponds to modification
(MOD) 071908, or MOD 171912, or MOD 073252, except
those helicopters that have incorporated MOD 074602.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
14 D after
Final AD
issue date.
110FH =>
660FH/13M
Only
applicable for
autopilot
05.00.64
67.00.61110FH
63 Y AD 2015-0094 2015-05-29
Main Rotor Drive - Cross-Bar - Inspection
Applicability: AS 350 B, BA, BB, B1, B2, B3 and D helicopters,
and AS 355 E, F, F1, F2, N and NP helicopters, and EC130 B4
and T2 helicopters, all serial numbers.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2015-06-12
Next
scheduled
MGB
removal
Perf 2015-11-
21 by PHAB
iaw WO
17220006.
Next insp:
9770,2FH /
94216TC.
05.00.84
4500F
H/
60000
TC
33 N AD 2013-0281R1 2015-01-30
Lights - Position Strobe Light - Inspection / Deactivation /
Modification
SUPERSEDES AD 2011-0244-E
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS
350 B2, AS 350 B3 and AS 350 D helicopters, all s/n, if modified
in production with (optional) modification OP0811 and
equipped with a Grimes-Honeywell power supply unit, Part
Number (P/N) 60-1431-3, in the baggage compartment as
part of that optional modification, except helicopters that have
embodied at least one of the modifications as listed in
Appendix1 of this AD.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2015-02-13 See AD
2015-04-10
N/A. MOD
OP0811 not
embodied.Ho
neywell pwr
suppl unit not
installed.
33.00.33R
1
25 N AD 2014-0279 2014-12-19
Equipment / Furnishing - Restraint System Rotary Buckle Sub-
Assembly - Identification / Replacement
Applicability: Romtex Anjou Aeronautique model 358 torso
restraint systems.
These restraint systems are known to be installed on, but not
limited to, Airbus Helicopters EC130 T2, AS 350 B2 and B3
helicopters.
ROMTEX ANJOU
AERONAUTIQUE
Torso Restraint
Systems
2015-01-022015-02-02
see AD
2015-04-10
N/A.
Equipment
not installed.
Another
brand
installed.
63 N AD 2014-0233 2014-10-23
Rotor Drive - Hydraulic Pump Bearing - Inspection /
Replacement
SUPERSEDES AD 2013-0284R1
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS
350 B2, AS 350 B3 and AS 350 D helicopters, all serial
numbers,
* if equipped with single hydraulic system (PRE MOD OP3346
or OP3082) and incorporating Airbus Helicopters, modification
079566 (hydraulic pump drive assembly part number (P/N)
350A35-0132-00 equipped with bearing P/N 704A33651243),
or
* modified in service by Airbus Helicopter Alert Service Bulletin
(ASB) No. 05.00.72 Rev.04 when the pump drive assembly is
equipped with bearing P/N 704A33651243,
except helicopters which embody modification 079568
(hydraulic pump drive assembly P/N 350A35-0132-01 fitted
with bearing P/N 704A33651269).
AIRBUS HELICOPTERS
AS 350 / EC 1302014-10-31 See AD
2015-04-10
N/A. Bearing
not installed.
H/C too old
63.00.24
20 N AD CF-2014-26 2014-08-25
Standard Practices - Helicopter External Transport System
(HETS) - Unapproved Parts, Inadequate Service Life Limits and
Maintenance Requirements
Applicability: Airbus Helicopters (formerly Eurocopter France)
model AS350 B, AS350 B1, AS350 B2, AS350 B3, AS350 BA and
AS350 D.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
BELL HELICOPTER
TEXTRON CANADA
(BHTC)
206
407
BELLIS INVESTMENTS
LTD
STC SH98-35
MD HELICOPTERS INC
(MDHI)
369
500N
2014-08-28
120D/12M/4
Y
see AD
2015-04-10
N/A. No
Canadian
parts
63 N AD 2013-0284R1 2014-07-25
SUPERSEDED BY EASA AD 2014-0233
SUPERSEDES AD 2013-0044-E
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS
350 B2, AS 350 B3 and AS 350 D helicopters, all serial
numbers,
- if equipped with single hydraulic system (PRE MOD OP3346
or OP3082) and incorporating Airbus Helicopters modification
079566 (hydraulic pump drive assembly part number (P/N)
350A35-0132-00),
- except pumps with a pump support P/N followed by the
letter "V", and
- except helicopters which embody modification 079568
(hydraulic pump drive assembly P/N 350A35-0132-01 fitted
with bearing P/N 704A33651269).
AIRBUS HELICOPTERS
AS 350 / EC 1302014-08-08 See AD N
05.00.72R
4
62 N AD2014-0132R1
FAA 2015-17-112014-06-02
Main Rotor - Rotating Star Swashplate - Inspection /
Replacement
Applicability: AS 350 B, BA, BB, B1, B2, B3 and D helicopters,
all serial numbers, if equipped with a swashplate assembly
comprising a rotating star with Part Number (P/N)
350A371003-04, P/N 350A371003-05, P/N 350A371003-06,
P/N 350A371003-07 , or P/N 350A371003-08.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2014-06-092014-07-09
see AD
2015-04-10
P/N affected,
but repair not
performed =
AD N/A. Test
iaw ASB
performed
2015-11-21
iaw PHAB
WO17220006
to confirm.
62.00.34
53 N/A EAD 2014-0076-E 2014-03-25
Fuselage - Rear Structure Junction Frame Reinforcement
Angles - Inspection
Applicability: AS 350 B, BA, BB, B1, B2, B3 and D helicopters,
all serial numbers,
- if incorporating modification (MOD) 07 3215, or
- if equipped with at least one reinforcement angle, Part
Number (P/N) 350A08.2493.21 or P/N 350A08.2493.23,
following the repair carried out in accordance with MRM Work
Card 53.10.22.772 or AMM Task 53-31-00, 8-5.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2014-03-2710FH ->
Every 165FH
N/A due to
PRE MOD
073215. See
ASB 05.00.43
05.00.70 165FH
23 Y IN 2670-I-23 2013-12-19VHF-AM Systems: European requirement concerning VHF 8.33
kHz channel spacing
AIRBUS HELICOPTERS
AS 350
AS 355
EC 120
EC 130
AS 365
EC 155
SA 330
AS 332
EC 225
2013-12-19 2018-01-01To be
performed.
- N/A AD 2013-0287 2013-12-05
Rotorcraft Flight Manual - Engine Digital Electronic Control
Unit Emergency Procedure - Amendment
Applicability: AS 350 B3 and EC 130 T2 helicopters, all serial
numbers, if equipped with ARRIEL 2D engine and THALES
FADEC Part Number (P/N) C13165DA00 or P/N C13165FA00.
AIRBUS HELICOPTERS
AS 350 / EC 1302013-12-12 See AD N 01.00.67
76 N/A EAD 2013-0191-E 2013-08-22
Engine controls - Switches 53Ka, 53Kb and 65K - Inspection /
Modification
SUPERSEDES AD 2013-0061
Applicability: AS 350 B3 helicopters, all serial numbers, if
equipped with an ARRIEL 2B1 engine incorporating the two-
channel FADEC (MOD 073254), and embodying modification
MOD 073261 (new twist grip).
AIRBUS HELICOPTERS
AS 350 / EC 1302013-08-23 See AD
2015-04-08
N/A. AS350 B3
model only.
80.00.09R
1
64 Y AD 2013-0133 2013-06-28
Tail Rotor - Tail Rotor Hub Pitch Horn - Inspection /
Replacement
Applicability: (B, BA, BB, B1, B2, B3, D) AS350/AS355
helicopters, all serial numbers, equipped with Tail Rotor Hub
(TRH) pitch horn assemblies P/N 350A121368.01, P/N
350A121368.02, P/N 350A121368.03, or P/N 350A121368.04,
incorporating TRH pitch horn P/N 350A121368.XX (where XX
stands for two digit dash number excluding 01, 02, 03, and 04
which are reserved for assemblies).
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2013-07-0310FH ->
Every 165FH
Perf 2015-12-
03 by PHAB,
WO17220006
at A/CTT
5270,2. Next
insp: A/CTT
5435,2.
05.00.74 165FH
67 N EAD 2013-0095-E 2013-04-16
Rotor Flight Controls - Main/Tail Rotor Servo-Control Bearings -
Inspection / Replacement
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS
350 B2, AS 350 B3 and AS 350 D, all serial numbers, equipped
with single hydraulic main and tail servo-controls
manufactured by “SAMM”, “TRW”, “GOODRICH”, or “UTAS”.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2013-04-18 10FH/7D
2015-11-12
N/A. Installed
Servo S/N
(6030, 6137,
3175) not
affected.
.05 N AD 2013-0088 2013-04-10
SUPERSEDED BY PAD 15-070
SUPERSEDES AD 2009-0011
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 D, AS
350 B1, AS 350 B2, AS 350 B3 and EC 130 B4 helicopters, all
serial numbers.
AIRBUS HELICOPTERS
AS 350 / EC 1302013-04-24 2013-04-24 N/A
76 N/A AD 2013-0061 2013-03-11
SUPERSEDED BY EASA EMERGENCY AD 2013-0191-E
SUPERSEDES AD 2009-0256
Applicability: AS 350 B3 helicopters, all serial numbers, if
equipped with an ARRIEL 2B1 engine incorporating the two-
channel FADEC (MOD 073254), and embodying modification
MOD 073261 (new twist grip), except helicopters that embody
modification 074263.
AIRBUS HELICOPTERS
AS 350 / EC 1302013-03-25 See AD N
05.00.61R
1
80.00.09
63 N EAD 2013-0044-E 2013-02-27
SUPERSEDED BY EASA EAD 2013-0284-E
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS
350 B2, AS 350 B3 and AS 350 D helicopters, all serial
numbers, if equipped with single hydraulic system (PRE MOD
OP3346 or OP3082) and incorporating Eurocopter
modification 079566 (new hydraulic pump drive).
AIRBUS HELICOPTERS
AS 350 / EC 1302013-03-01 See AD N 05.00.72
64 N/A AD 2013-0029 2013-02-08
Rotorcraft Flight Manual - Section Limitations - Amendment
Tail Rotor - Laminated Half-Bearings - Inspection /
Replacement / Modification
SUPERSEDES AD 2012-0217-E
Applicability: AS 350 B3 helicopters, all serial numbers, if
modified in production by incorporating Eurocopter
modification (MOD) 07 5601, except those helicopters that
have been modified by incorporating Eurocopter MOD 07 5606
in production.
AIRBUS HELICOPTERS
AS 350 / EC 1302013-03-01 See AD
2015-04-08
N/A. AS350 B3
model only.
01.00.65R
1
01.00.66
64 Y EAD 2012-0257-E 2012-12-05
Tail Rotor - Laminated Half-Bearings - Inspection /
Replacement
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS
350 B2 and AS 350 D helicopters, all serial numbers (s/n).
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2012-12-07Every day
(ALF)
Perf 2015-12-
03 by PHAB,
WO17220006
at A/CTT
5270,2. Next
insp: A/CTT
5280,2
05.00.71
R1
ALF /
10FH
67 N/A AD 2012-0252 2012-11-28
Rotor Flight Controls - Twist Grip Assembly - Adjustment /
Functional Check / Replacement / Modification
SUPERSEDES AD 2011-0237
Applicability: AS 350 B3 helicopters, all serial numbers, if
equipped with the ARRIEL 2B engines.
AIRBUS HELICOPTERS
AS 350 / EC 1302012-12-12 See AD
2015-04-07
N/A. B3
model only
05.00.49R
3
64 N/A EAD 2012-0217-E 2012-10-19
SUPERSEDED BY EASA AD 2013-0029
SUPERSEDES AD 2012-0207-E
Applicability: AS 350 B3 helicopters, all serial numbers, if
modified in production by incorporating Eurocopter
modification (MOD) 07 5601.
AIRBUS HELICOPTERS
AS 350 / EC 1302012-10-19 See AD N 01.00.65
64 N/A EAD 2012-0207-E 2012-10-05
SUPERSEDED BY EASA EAD 2012-0217-E
Applicability: AS 350 B3 helicopters, all serial numbers, if
modified in production by incorporating Eurocopter
modification (MOD) 07 5601.
AIRBUS HELICOPTERS
AS 350 / EC 1302012-10-05 See AD N 01.00.65
52 N AD 2012-0205 2012-10-01
Doors - Sliding Door Lower Ball-joint - Modification
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS
350 B2, AS 350 B3 and AS 350 D helicopters, all serial numbers
(s/n), if equipped with sliding doors, except those that embody
modification AL. 4262.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2012-10-15 165FH/13M
2015-04-10
N/A. No
sliding doors
52.00.34
26 N/A AD 2012-0033R1 2012-02-27
Fire Protection - Fire Detection System - Modification
Applicability: AS 350 B2 helicopters, all serial numbers, if
equipped with a Turbomeca ARRIEL 1D1 engine and
incorporating Eurocopter modification (mod) 73273, except
helicopters that incorporate mod 074346.
AIRBUS HELICOPTERS
AS 350 / EC 1302012-02-27 40FH/75D
MOD 073273
not
incorporated
26.00.02
33 N EAD 2011-0244-E 2011-12-22
SUPERSEDED BY EASA AD 2013-0281
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS
350 B2, AS 350 B3 and AS 350 D helicopters, all serial numbers
(s/n), if modified in production with (optional) modification
OP0811 and equipped with a Grimes-Honeywell power supply
unit, Part Number (P/N) 60-1431-3, in the baggage
compartment as part of that optional modification.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2011-12-23 See AD
2011-12-22
N/A to
configuration
05.00.66
34 N AD 2011-0239 2011-12-15
Navigation- Radio Altimeter Indicator- Modification
Applicability: Radio altimeter indicator IND201, Part Number
(P/N) 102-2100, all serial numbers. The affected radio
altimeter indicators are known to be installed on, but not
limited to, Eurocopter (formerly Eurocopter France,
Aerospatiale) EC 120 B, AS 350 B2, AS 350 B3 and AS 355 NP
helicopters .
SMS (trading as
Cobham Avionics)
IND201 Radio
Altimeter Indicators
2011-12-292012-06-29
see AD
2015-04-10
N/A.
Equipment
not installed
76 N/A AD 2011-0237 2011-12-14
SUPERSEDED BY EASA AD 2012-0252
SUPERSEDES AD 2006-0094
Applicability: AS 350 B3 helicopters, all serial numbers, if
equipped with the ARRIEL 2B engine.
AIRBUS HELICOPTERS
AS 350 / EC 1302011-12-28 See AD N 05.00.49
67 N AD 2011-0164 2011-08-31
Rotors Flight Control - Tail Rotor Control Stop Screws -
Inspection
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS
350 B2, AS 350 B3 and AS 350 D helicopters, all serial numbers
(s/n), if equipped with an Autopilot (AP).
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2011-09-14110FH ->
Every 110FH
2011-08-31
N/A. No
autopilot
installed
05.00.64
25 Y AD 2011-0103 2011-05-27
Equipment / Furnishings - Emergency Locator Transmitter
(ELT) Antenna - Modification / Replacement
SUPERSEDES AD 2011-093
Applicability: Tri-Band ELT antennas, Part Number (P/N) 21-41
( ) series, all serial numbers (s/n) up to 12999 inclusive, which
are used in combination with a large variety of ELT units; see
also Note below.
Chelton P/N 21-41 ( ) series antennas installed in combination
with the following ELT units are not affected by this AD:
*Chelton Avionics, Inc DBA Wulsberg Electronics (formerly
ARTEX) ELT model C406-N HM, P/N 453-5061,
*Chelton Avionics, INC DBA Wulsberg Electronics (formerly
ARTEX) ELT model C406-N, P/N 453-5060, and
*ELTA ELT model ADT406²AF/AP-H, P/N 01N65901 rev. (x)
The affected antennas are known to be installed on, but not
limited to, Eurocopter (formerly Eurocopter France,
Aerospatiale) AS 350, EC 155 and AS 332 series helicopters.
CHELTON LTD
(COBHAM ANTENNA
SYSTEMS)
Tri-Band ELT
Antennas
2011-06-03 See AD
2015-04-09
Verified
performed
Chelton
Limited
(trading
as
Cobham
Antenna
Systems)
SB
02/2011
Issue 1
65 N AD 2011-0104 2011-05-27
Tail Rotor Drive - Tail Gearbox (TGB) Casing Assembly -
Inspection / Replacement
Applicability: AS 350 B, BA, BB, B1, B2, B3 and D helicopters
and AS 355 E, F, F1, F2, N and NP helicopters, all serial
numbers.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2011-06-10 110FH/13M
2011-05-27
N/A to casing
P/N and S/N
(2015-04-08
N/A. P/N
350A33-1090-
01 installed)
65.00.46
25 N AD 2011-0093 2011-05-20
SUPERSEDED BY EASA AD 2011-0103
Applicability: Tri-Band ELT antennas, Part Number (P/N) 21-41
( ) series, all serial numbers (s/n) up to 12999 inclusive, which
are used in combination with a large variety of ELT units
without electro-static discharge (ESD) protection. ESD
protection is identified by a declaration of category A of
section 25 of RTCA, Inc. DO160 version D change 3 (or later
version) or EUROCAE ED-14D (or later version); see also Note
below.
Chelton P/N 21-41 ( ) series antennas installed in combination
with the following ELT units are not affected by this AD:
*Chelton Avionics, Inc DBA Wulsberg Electronics (formerly
ARTEX) ELT model C406-N HM, P/N 453-5061,
*Chelton Avionics, INC DBA Wulsberg Electronics (formerly
ARTEX) ELT model C406-N, P/N 453-5060, and
*ELTA ELT model ADT406²AF/AP-H, P/N 01N65901 rev. (x)
The affected antennas are known to be installed on, but not
limited to, Eurocopter (formerly Eurocopter France,
Aerospatiale) AS 350, EC 155 and AS 332 series helicopters.
CHELTON LTD
(COBHAM ANTENNA
SYSTEMS)
Tri-Band ELT
Antennas
2011-06-03 See AD N
Chelton
Limited
(trading
as
Cobham
Antenna
Systems)
SB
02/2011
Issue 1
25 N AD 2011-0072 2011-04-20
Equipment & Furnishings - Emergency Flotation Gear
Attachment Brackets - Inspection / Replacement
Applicability: AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS
350 B2, AS 350 B3 and AS 350 D helicopters, all serial
numbers, if equipped with fixed parts of the emergency
flotation gear.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2011-05-04 See AD
2011-05-27
N/A. Not
installed
05.00.63
- N AD US-2011-08-06 2011-04-13 Power Turbine Rotors - Identification / Replacement
HONEYWELL
INTERNATIONAL INC
LTP101
LTS101
2011-05-17 See AD
2015-04-08
N/A. Engine
type not
installed
N/A
65 N EAD 2011-0038-E 2011-03-04
[Correction] Tail Rotor Drive - Tail Gearbox (TGB) Control Lever
- Inspection / Rework / Replacement
SUPERSEDES AD 2010-0082-E
Applicability: AS 350 B, BA, BB, B1, B2, and D helicopters, all
serial numbers, all serial numbers, if equipped with TGB
control lever Part Number (P/N) 350A33-1058-00, P/N 350A33-
1058-01, P/N 350A33-1058-02, or P/N 350A33-1058-03.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2011-03-08 See AD
2010-06-17
N/A to
350A33-1526
Lever
05.00.62R
1
29 Y AD 2011-0033 2011-03-01
Hydraulic Power - Forward Hydraulic Servo Control Hoses /
Protection Installation
Applicability: AS 350 B, BA, BB, D, B1, B2, and B3 helicopters,
all serial numbers, with a single hydraulic power system and
the following forward (pitch) servo-control hydraulic hoses
installed:
- P/N 704A34-412-033 (other reference MP/N 675-102-05-
01);
- P/N 704A34-412-035 (other reference MP/N 675-102-06-
01).
AIRBUS HELICOPTERS
AS 350 / EC 1302011-03-15 2011-04-15
2011-04-04
Sleeves
installed
A/CTT 4658,3
29.00.13
25 N AD 2009-0122R1 2010-10-27
Equipment / Furnishings -Load Release Units - Inspection /
Modification / Limitation
Applicability: Eurocopter helicopter models:
EC 120 B, AS 350 B, BA, B1, B2, B3, BB and D, EC 130 B4, AS
355 E, F, F1, F2 and N, AS 365 N, N1, N2 and N3, EC 155 B and
B1, SA 330 F, G and J, AS 332 C, C1, L, L1 and L2, EC 225 LP, all
serial numbers, if equipped with any type of SIREN Load
Release Units.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
EC 120 B
SA 330 / AS 332 / EC
225
SA 365/366 / AS 365
/ EC 155
2010-11-10 See AD
2009-06-15
N/A.
Equipment
not installed
01.00.49
65 N EAD 2010-0082-E 2010-04-28
SUPERSEDED BY EASA EMERGENCY AD 2011-0038-E
Applicability: AS 350 B, BA, BB, B1, B2, and D helicopters, all
serial numbers, and AS 355 E, F, F1, F2 and N helicopters, all
serial numbers, if equipped with TGB control lever Part
Number (P/N) 350A33-1058-00, P/N 350A33-1058-01, P/N
350A33-1058-02, or P/N 350A33-1058-03, except those
marked with an “X”.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2010-04-29 See AD
2010-06-17
N/A to
350A33-1526
Lever
05.00.62R
1
25 N AD 2010-0014 2010-02-26
Equipment and Furnishings - Hoist Operator's Belt Snap Hook -
Replacement / Modification
SUPERSEDES AD 2006-0252
Applicability: EUROCOPTER helicopters:
- AS 350 B, BA, BB, B1, B2, B3 and D, before embodiment of
MOD 073299. All serial numbers (S/N) if equipped with an
operator’s belt (called "hoist operator’s belt") part number
(P/N) 330A87-0730-00, 330A87-2371-00, 341A84-1120-00,
350A84-0047-00, 360A84-0040-00, 360A84-0040-01 or
360A84-0040-02, fitted with a snap hook P/N GA343-95, and,
All S/N if equipped with a hoist operator’s belt P/N 3160S73-
08-200-1 fitted with a snap hook P/N 4100-80AT28.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 315/316/319
SA 330 / AS 332 / EC
225
SA 341/342
SA 365/366 / AS 365
/ EC 155
2010-02-09 See AD
2010-04-28
N/A. Hoist not
installed
25.00.89
25.00.93
25 N AD 2009-0183-CN 2010-02-11
CANCELLATION NOTICE - Equipment / Furnishings - D-Lok
Hook of the Rescue Hoist - Inspection / Removal from Service /
Replacement
SUPERSEDES AD 2009-0179-E
Applicability: Eurocopter model AS332, AS350, AS355, SA365,
AS365 and EC155 series and EC225 LP helicopters, all serial
numbers, if equipped with Lifesaving Systems D-Lok Hooks
with part numbers (P/N) 410-A or 410-F and identified as part
of lot number 208 or 1108.
AGUSTAWESTLAND
A109
AB 139
AW 139
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 330 / AS 332 / EC
225
SA 365/366 / AS 365
/ EC 155
AIRBUS HELICOPTERS
DEUTSCHLAND
EC135/635
MBB-BK 117
SIKORSKY
S-61
S-76
S-92
2010-02-11 2010-02-11
Ref.
Publicatio
ns: FAA
AD US-
2010-03-
02
26 N AD 2009-0277R1 2010-02-05
Fire Protection - Portable Halon 1211 Fire Extinguishers -
Identification / Replacement
Applicability: Eurocopter helicopter models:
EC 120 B, AS 350 B, BA, B1, B2, B3, BB and D, and EC 130 B4,
AS 355 E, F, F1, F2, N and NP, SA 341 G and SA 342 J if
equipped with P/N 863520-00 portable fire extinguishers,
serial numbers (s/n) as listed in L’Hotellier Service Bulletin (SB)
863520-26-001.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
EC 120 B
SA 341/342
2010-02-05 2010-08-05
2010-03-12
N/A to
General S/N
0640211
L’Hotellie
r SB
863520-
26-001
.05 Y AD 2010-0006 2010-01-07
Time Limits / Maintenance Checks - Tail Rotor (TR) Pitch-
Change Links - Inspection
Applicability: Models AS 350 B, AS 350 BA, AS 350 BB, AS 350
B1, AS 350 B2, AS 350 B3 and AS 350 D helicopters, all serial
numbers, if equipped with TR pitch-change links having Part
Number (P/N) 350A33-2100-00, 350A33-2100-01, 350A33-
2100-02, 350A33-2100-03, 350A33-2100-04, 350A33-2121-
00, 350A33-2121-01, 350A33-2121-02, 350A33-2143-00,
350A33-2145-00 or 350A33-2145-01 .
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2010-01-2130FH ->
Every 30FH
Performed
2015-11-30
iaw PHAB WO
17220006.
Next insp:
A/CTT 5300,2.
05.00.60 30FH
N AD US-2009-24-12 2009-12-03 Gas Generator Turbine Disc - Reduced Life Limit - Replacement
HONEYWELL
INTERNATIONAL INC
LTP101
LTS101
2010-01-04 See AD
2015-04-08
N/A. Engine
type not
installed
N/A
76 N AD 2009-0256 2009-12-02
SUPERSEDED BY EASA AD 2013-0061
Applicability: AS350 B3 and EC130 B4 helicopters, all serial
numbers, if equipped with the ARRIEL 2B1 engine associated
with the two-channel FADEC, and embodying modification
(MOD) 073254 (AS 350 B3) or MOD 073773 (EC 130 B4) (new
twist grip).
AIRBUS HELICOPTERS
AS 350 / EC 1302009-12-16 See AD N 05.00.61
25 N EAD 2009-0179-E 2009-08-11
SUPERSEDED BY EASA AD 2009-0183-E
SUPERSEDES AD 2009-0148-E
Applicability: Eurocopter model AS332, AS350, AS355, SA365,
AS365 and EC155 series and EC225 LP helicopters, all serial
numbers, if equipped with Lifesaving Systems D-Lok Hooks
with part numbers (P/N) 410-A or 410-F and identified as part
of lot number 208 or 1108.
AGUSTAWESTLAND
A109
AB 139
AW 139
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 330 / AS 332 / EC
225
SA 365/366 / AS 365
/ EC 155
AIRBUS HELICOPTERS
DEUTSCHLAND
EC135/635
MBB-BK 117
SIKORSKY
S-61
2009-08-12 See AD N
Goodrich
Service
Bulletin
42315-
489-01R1
25 N EAD 2009-0148-E 2009-07-09
SUPERSEDED BY EASA AD 2009-0179-E
SUPERSEDES AD 2009-0124
Applicability: Eurocopter model AS332, AS350, AS355, SA330,
SA365, AS365 and EC155 series, EC225 LP and SA360 C
helicopters, all serial numbers, if equipped with Lifesaving
Systems D-Lok Hooks with part numbers (P/N) 410-A or 410-F
and identified as part of lot number 208 or 1108.
AGUSTAWESTLAND
A109
AB 139
AW 139
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 330 / AS 332 / EC
225
SA 365/366 / AS 365
/ EC 155
AIRBUS HELICOPTERS
DEUTSCHLAND
BO 105
EC135/635
MBB-BK 117
SIKORSKY
S-61
2009-07-11 See AD N
Goodrich
Service
Bulletin
42315-
489-01R1
25 N AD 2009-0124 2009-06-12
SUPERSEDED BY EASA AD 2009-0148-E
Applicability: Eurocopter model AS332, AS365, AS350, AS355,
EC225, SA330, SA360 and EC155 series helicopters fitted with
Goodrich hook kit or rescue hoist assemblies as identified in
table 1 of Goodrich Service Bulletin 42315-489-01 revision 1,
dated 05 June 2009.
AGUSTAWESTLAND
A109
AB 139
AW 139
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 330 / AS 332 / EC
225
AIRBUS HELICOPTERS
DEUTSCHLAND
EC135/635
MBB-BK 117
2009-06-26 10FH
2009-06-18
N/A. Not
installed
Goodrich
Service
Bulletin
42315-
48901R1
64 N AD 2009-0039 2009-02-19
Tail Rotor - Tail Rotor Blades Skin - Inspection / Repair
SUPERSEDES AD 2007-0138R2
Applicability: EUROCOPTER helicopter models:
- AS 350 B, BA, BB, B1, B2, B3 and D
all serial numbers, if equipped with tail rotor blades, P/N:
- 355A12-0031-01/ -02/ -03/ -04/ -05/ -06/ -07/ -08/ -09/ -11/
-12/ -13/ -14.
- 355A12-0040-00/ -01/ -02/ -03/ -04/ -05/ -07/ -08.
- 355A12-0050-00/ -01/ -02/ -03/ -04/ -05.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2009-03-05
2015-09-24:
T/R Blades
P/N 355A12-
0040-14
installed.
2009-12-09
Perf A/CTT
4274,8
05.00.40R
3
Daily/A
LF
80 Y AD 2009-0027 2009-02-18
Engine Starting - Starter-Generator Damping Assembly -
Adjustment
SUPERSEDES AD 2009-0004
Applicability: AS 350 B, BA, BB, B1, B2, B3 and EC 130 B4
helicopters, all serial numbers, if equipped with ARRIEL
engines where Aircraft Parts Corporation (APC) starter-
generators with Part Number (P/N) 150SG122Q or P/N
200SGL130Q without “004” marking on their name plates are
installed.
AIRBUS HELICOPTERS
AS 350 / EC 1302009-03-04 110FH/3M
2009-05-10
Performed
A/CTT 4001,0
80.00.07R
1
55 Y AD 2009-0030 2009-02-12
Stabilizers - Upper and Lower Fin Attachment Fitting -
Inspection / Modification / Replacement
SUPERSEDES AD 2008-0121
Applicability: AS 350 B, B1, B2, B3, BA, BB and D helicopters,
all serial numbers if fitted with the following upper and lower
fins on which modification (MOD) 073330 has not been
embodied:
Upper fin assembly part number (P/N): 350A14-0020-00XX,
350A14-0020-01XX, 350A14-0020-02XX, 350A14-0020-03XX,
350A14-0020-08XX, 350A14-0020-09XX, 350A14-0020-10XX,
350A14-0020-17XX, 350A14-0020-18XX, 350A14-0020-19XX,
350A64-1144-00XX
Lower fin assembly P/N: 350A14-0021-00XX, 350A14-0021-
01XX, 350A14-0021-02XX, 350A14-0021-03XX, 350A14-0021-
04XX
AIRBUS HELICOPTERS
AS 350 / EC 1302009-02-26 See AD
2009-04-09
A/CTT 3914,4
55.00.13R
2
55.00.16R
1
MOD
073330
67 Y AD 2009-0019 2009-02-03
Rotors Flight Control - Collective Pitch Lever Locking Stud -
Inspection / Repair
SUPERSEDES AD 2008-0205-E
Applicability: All AS350 B, BA, BB, B1, B2, B3, D helicopters,
• Delivered before embodiment of modification 073175; or
• Helicopters on which the locking studs or the collective pitch
levers or the locking strips have been reworked or modified in
service; or
• Helicopters having accomplished Revision 0 or Revision 1 of
EUROCOPTER SB No. 67.00.37, corresponding to modification
073237; or
• Helicopters with a serial number equal to: 3972, 3973, 3982,
3987, 4003, 4023, 4046, 4050, 4086, 4120, 4122, 4132, 4143,
4152, 4172, 4194, 4259, 4314, 4324, 4378, 4392, 4447, 4452,
4477, 4489, 4490, 4501, 4523, 4546, 4560, 4589, 4594, 4599,
4632, 4659, 4666, 4671.
AIRBUS HELICOPTERS
AS 350 / EC 1302009-02-17 See AD
Perf 2015-11-
21 iaw PHAB
WO
17220006.
MOD 073237
implemented
iaw SB 67-00-
37. Next insp:
A/CTT 5930,2
/ 2017-11-21
EASB
05.00.58
660FH
/2Y
64 N AD 2007-0138R2 2009-02-03
SUPERSEDED BY EASA AD 2009-0039
SUPERSEDES AD 2006-0235-E
Applicability: EUROCOPTER helicopters models:
- AS 350 B, BA, BB, B1, B2, B3 and D - all serial numbers, if
equipped with tail rotor blades, Part Number (P/N) :
- 355A12-0031-01/ -02/ -03/ -04/ -05/ -06/ -07/ -08/ -09/ -11/
-12/ -13/ -14.
- 355A12-0040-00/ -01/ -02/ -03/ -04/ -05/ -07/ -08.
- 355A12-0050-00/ -01/ -02/ -03/ -04/ -05.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2007-05-18 See AD N05.00.40R
2
.05 N AD 2009-0011 2009-01-28
SUPERSEDED BY EASA AD 2013-0088
Applicability: AS 350B, BA, BB, B1, B2, B3 and EC 130B4
helicopters, all serial numbers.
AIRBUS HELICOPTERS
AS 350 / EC 1302009-02-11 See AD N N/A
80 N AD 2009-0004 2009-01-12
SUPERSEDED BY EASA AD 2009-0027
Applicability: AS 350 B, BA, BB, B1, B2, B3 and EC 130 B4
helicopters, all serial numbers if equipped with Aircraft Parts
Corporation (APC) 150SG and 200SGL-type starter-generators.
AIRBUS HELICOPTERS
AS 350 / EC 1302009-01-26 See AD N 80.00.07
25 N EAD 2008-0214-E 2008-12-08
Equipment & Furnishing - Emergency Flotation Gear -
Inspection / Limitation / Replacement
SUPERSEDES AD 2006-0248
Applicability: AS350 B, BA and D helicopters, all serial numbers
equipped with the emergency flotation gear installation.
AIRBUS HELICOPTERS
AS 350 / EC 1302008-12-10 See AD
2009-03-27
N/A to 350B201.00.59
67 N EAD 2008-0205-E 2008-12-02
SUPERSEDED BY EASA AD 2009-0019
Applicability: All AS350 B, BA, BB, B1, B2, B3, D helicopters,
• Delivered before embodiment of modification 073175; or
• Helicopters on which the locking studs or the collective pitch
levers or the locking strips have been reworked or modified in
service; or
• Helicopters having accomplished Revision 0 or Revision 1 of
EUROCOPTER SB No. 67.00.37, corresponding to modification
073237; or
• Helicopters with a serial number equal to: 3972, 3973, 3982,
3987, 4003, 4023, 4046, 4050, 4086, 4120, 4122, 4132, 4143,
4152, 4172, 4194, 4259, 4314, 4324, 4378, 4392, 4447, 4452,
4477, 4489, 4490, 4501, 4523, 4546, 4560, 4589, 4594, 4599,
4632, 4659, 4666, 4671.
AIRBUS HELICOPTERS
AS 350 / EC 1302008-12-04 See AD N 05.00.58
25 N AD 2008-0189 2008-10-10
Equipment and Furnishings - Emergency Flotation Gear -
Replacement
Applicability: All AS350 BA helicopters, all serial numbers fitted
with emergency flotation gear including the container
assemblies listed below and for which an operating time limit
extension has not been already granted by the equipment
manufacturer AERAZUR:
- Left hand (LH) container assembly P/N 158170 or P/N
158210-1 and
- Right hand (RH) container assembly P/N 158171 or P/N
158215-1.
AIRBUS HELICOPTERS
AS 350 / EC 1302008-10-24 2008-11-24
2015-04-08
N/A. AS350
BA only.
Emergency
Flotation Gear
not installed.
25.01.02
55 N AD 2008-0121 2008-06-27
SUPERSEDED BY EASA AD 2009-0030
SUPERSEDES AD 2006-0095 and AD 2006-0060-E
Applicability: AS 350 B, B1, B2, B3, BA, BB and D helicopters,
all serial numbers, fitted with the following upper and lower
fins to which modification (MOD) 073330 has not been
embodied:
- Upper fin assembly P/N: 350A14-0020 – 00XX; Upper fin
assembly P/N: 350A14-0020 – 01XX; Upper fin assembly P/N:
350A14-0020 – 02XX; Upper fin assembly P/N: 350A14-0020 –
03XX; Upper fin assembly P/N: 350A14-0020 – 08XX; Upper fin
assembly P/N: 350A14-0020 – 10XX; Upper fin assembly P/N:
350A14-0020 – 18XX; Upper fin assembly P/N: 350A14-0020 –
19XX.
- Lower fin assembly P/N: 350A14-0021 – 00XX; Lower fin
assembly P/N: 350A14-0021 – 01XX; Lower fin assembly P/N:
350A14-0021 – 02XX; Lower fin assembly P/N: 350A14-0021 –
04XX.
AIRBUS HELICOPTERS
AS 350 / EC 1302008-07-11 See AD N
55.00.16
55.00.13
25 Y AD 2008-0044 2008-02-27
Equipment / Furnishings - Rear Bench Seat and Sliding Doors -
Limitation / Removal / Modification.
Applicability: AS 350 helicopters models B, BA, BB, B1, B2, B3,
D and AS 355 helicopters models E, F, F1, F2, N, equipped with
rear bench seat, unless modified in
accordance with Modification (MOD) 073166 [AS 350 Service
Bulletin No.25.00.70 or AS 355 Service Bulletin No.25.00.66].
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2008-03-12 2001-03-21 25.00.70
67 N AD 2007-0289 2007-11-19
Rotor flight controls - Collective lever recess - Modification.
Applicability: EUROCOPTER helicopters models AS 350 B, AS
350 B1, AS 350 D, AS 355 E, AS 355 F, AS 355 F1 and AS 355
F2, all pre MOD 071995.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2007-12-03 See AD2008-02-25
N/A to B2
67.00.16R
2
25 N AD 2007-0256 2007-09-19
Equipment and Furnishing - Seat Restraint System Plastic
Rotary Buckle Handle - Inspection/Replacement
Applicability: All the Pacific Scientific rotary buckles p/n’s
1111430-XX and 1111475-XX used on restraint systems p/n’s:
2000029-01, 2000067-01, 2000115-101, 2000029-03,
2000115-121, 2000029-101, 2000029-121 manufactured from
November 2004 through May 2007 inclusive. These p/n’s are
known to be installed on, but not limited to, Eurocopter a/c
models AS 350, AS 355, EC120, EC 130, EC 155.
PACIFIC SCIENTIFIC
COMPANY
Seat Restraint System
2007-10-03 See AD
2008-03-05
N/A.
Equipment
not installed
05.00.55R
2
52 N AD 2007-0236 2007-08-31
Doors - Sliding Door Rear Roller Support Shaft and Rear Fitting -
Inspection / Replacement
SUPERSEDES AD 2006-0251R2
Applicability: Models AS 350 B, AS 350 BA, AS 350 BB, AS 350
B1, AS 350 B2, AS 350 B3 and AS 350 D, all serial numbers, if
fitted with sliding door(s) pre-MOD 073298 and/or pre-MOD
073308.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2007-09-14 2007-09-30
2008-03-05
N/A.
Equipment
not installed
05.00.47R
1
52.00.30R
1
.05
52N AD 2006-0251R2 2007-06-29
SUPERSEDED BY EASA AD 2007-0236
SUPERSEDES AD F-2005-136
Applicability: Helicopters: - AS 350 B, BA, BB, B1, B2, B3 and D,
fitted with sliding door(s) before embodiment of MOD 073298
and/or MOD 073308.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2006-09-01 See AD N
67 N EAD 2007-0141-E 2007-05-21
Rotor Flight Controls - Main & Tail Rotors Servo-Controls -
Inspection / Replacement.
Applicability: EUROCOPTER helicopters models: - AS 350 B, BA,
BB, B1, B2, B3 and D all serial numbers, and equipped with
GOODRICH main rotor servo-controls and tail rotor servo-
controls with no letter “C” marked in the inspection box of the
servo-control identification plate, and with the following Part
Numbers (P/N) and Serial Numbers (S/N):
- Main rotor servo-controls P/N SC5083 with S/N 270M, 272M,
409M, 423M, 452M or 1573, P/N SC5083-1 with S/N from
2902 to 2921 inclusive P/N SC5084 with S/N 30, 84, 104, 186,
438, 575 or 695, P/N SC5084-1 with S/N from 1462 to 1481
inclusive.
- Tail rotor servo-controls: P/N SC5072 with serial number
222M, 306M or 309 .
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2007-05-23 See AD
2015-11-12
N/A. Installed
Servo S/N
(6030, 6137,
3175) not
affected.
01.00.58R
1
53 N EAD 2007-0139-E 2007-05-15
[CORRECTED] Fuselage - Center cross-member under the cabin
floor - Inspection / Modification
Applicability: EUROCOPTER AS350 B, BA, BB, B1, B2, B3 and D,
all serial numbers delivered before January 1st, 2007 and
equipped with a collective-to-yaw control coupling with or
without an Automatic Flight Control System.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2007-05-18 10FH/1M
2008-03-05
N/A.
Equipment
not installed
53.00.37
67 N AD 2007-0099 2007-04-11
Rotors Flight Control - Main & Tail Rotors Servo-Controls -
Inspection / Modification
Applicability: - EC 130 B4, AS 350 B3
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 330 / AS 332 / EC
225
SA 365/366 / AS 365
/ EC 155
2007-04-25 See AD
2008-09-30
N/A. B3
model only
67.00.40
35 N AD 2006-0286R1 2007-03-22
Oxygen Reserve Cylinders- Removal/Emptying
SUPERSEDES AD 2006-0261-E
Applicability: Oxygen Reserve Cylinders having Part Number
(P/N) GLF(XXX)-(X), GLD(XXX)-(X), PC2300 and SLF300, which
are known to be installed on, but not limited to Airbus A300
series aircraft; Dassault Aviation (AMD-BA) Mystère-Falcon
20, Mystère-Falcon 50, Falcon 200 and Falcon 900 aircraft;
Pilatus aircraft; Eurocopter SA 315 B and AS 350 B3
helicopters; and Hindustan Aeronautics Limited helicopters.
ZODIAC AEROTECHNICS
Oxygen Cylinders2006-09-25 See AD
2008-03-05
N/A.
Equipment
not installed
05.00.54
67 N EAD 2006-0363-E 2006-12-01
Rotor Flight Controls - Load Compensator Lever - Check
Applicability: AS 350 B1 and AS 350 B2 helicopters, all serial
numbers
AIRBUS HELICOPTERS
AS 350 / EC 1302006-12-04 2006-12-04
2008-03-05
Affected P/N
not installed.
67.00.39R
1
24
80N AD 2006-0337 2006-11-07
Electrical Power - Starting - Starter Generator Limitation
Applicability: AS 350 B3 and EC 130 B4 helicopters fitted with
APC 200 A starter generators (P/N 200SGL130Q) before
embodiment of MOD 073345.
AIRBUS HELICOPTERS
AS 350 / EC 1302006-11-17 See AD
2008-03-05
N/A due to
A/C type
01.00.57
53 N AD 2006-0273 2006-09-04
Fuselage - RH Cabin Vibration Damper & Blade - Inspection /
Replacement / Modification
SUPERSEDES AD F-2005-102R1
Applicability: All Model AS 350 B, BA, BB, B1, B2, B3 and D
helicopters, all serial numbers; and All Model AS 355 E, F, F1,
F2 and N helicopters, all serial numbers, if equipped with RH
(right hand) cabin vibrator damper blades, all part numbers,
and with an automatic flight control system, all design
standards.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2006-09-14 See AD
2008-03-05
N/A.
Equipment
not installed
05.00.48R
1
? N AD US-2006-11-17 2006-09-04
Rotor Flight Controls - Cyclic Control Stick / Receptacle -
Replacement / Modification
Applicability: Model AS350B, BA, B1, B2, B3, C, D, and D1
helicopters, with a Geneva Aviation, Inc. (Geneva) P132
Console installed in accordance with Supplemental Type
Certificate No. SH4747NM, certificated in any category.
AIRBUS HELICOPTERS
AS 350 / EC 130
GENEVA AVIATION INC.
STC SH4747NM
2006-07-07 2006-09-07
2015-04-09.
N/A.
Equipment
not installed.
25 N AD 2006-0098 2006-08-31[Corrected] Equipment / Furnishings - Hoist Hooks
SUPERSEDES AD F-2004-046
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 315/316/319
SA 330 / AS 332 / EC
225
SA 341/342
SA 365/366 / AS 365
/ EC 155
SE 313 / SA 318
2006-05-05 2004-05-31
2008-09-30
N/A. Hoist not
installed.
01.00.54
34 Y
AD
SIB
LVD
2006-0265
2011-15R2
2-3368R1
2006-08-30
2013-07-19
2013-04-24
Navigation Systems – Mode S and C Transponders – Check
Applicability: Mode ‘C’ and Mode ‘S’ transponders, all types
and models utilising Gilham code altitude input.
ACSS
Transponders
BECKER
FLUGFUNKWERK GMBH
Transponders
FUNKWERK AVIONICS
GmbH
Transponders
GARMIN
INTERNATIONAL INC
Transponders
GARRECHT AVIONIK
GMBH
Transponders
HONEYWELL
INTERNATIONAL INC
Transponders
ROCKWELL COLLINS
Transponders
TRIG AVIONICS LTD
Transponders
2013-04-17 See AD
2015-12-08
perf by PHAB
iaw
WO17220006
at A/CTT
5270,2. Next
test: 2017-12
2Y
(recom
mende
d)
35 N EAD 2006-0261-E 2006-08-25
SUPERSEDED BY EASA EAD 2006-0286-E
Applicability: AS 350 B3 and SA 315 B helicopters, all serial
numbers, if equipped with Oxygen Cylinders having Part
Number (PN) GLF311-1, GLF312, GLF313, GLF316, GLF514 or
GLD511.
AIRBUS HELICOPTERS
AS 350 / EC 130
SA 315/316/319
2006-08-28 See AD N 05.00.54
.05
52N AD 2006-0249 2006-08-22
Doors- Sliding Door- Wear on Rollers and Rails
SUPERSEDES AD F-2002-344-093R1
Applicability: EUROCOPTER helicopters: - AS 350 B, BA, BB, B1,
B2, B3 and D equipped with sliding door(s) not modified per
MOD 073287 and/or MOD 073290 or in compliance with
EUROCOPTERService Bulletin No. 52. 00.29 or No. 52.00.22 .
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2006-09-01 See AD
2008-03-05
N/A.
Equipment
not installed
05.00.41R
2
25
.01N AD 2006-0248 2006-08-22
SUPERSEDED BY EASA AD 2008-0214-E
SUPERSEDES AD F-2004-085
Applicability: AS 350 BA helicopters equipped with an
AERAZUR emergency flotation gear comprising:
- LH side container assembly 158170 or 158210-1,
- RH side container assembly 158171 or 158215-1.
The containers referenced above are comprised in the
emergency flotation gear removable parts, P/N 350A82-8040-
00 or 350A82-8040-01.
AIRBUS HELICOPTERS
AS 350 / EC 1302006-09-01 See AD N
01.00.55R
1
67 N AD 2006-0247 2006-08-22
Rotor Flight Controls- Tail Servo-Control
SUPERSEDES AD F-2004-196
Applicability: EUROCOPTER AS 350 B3 helicopters fitted with a
GOODRICH tail servo-control P/No. SC5071-XX or SC5072,
except:
- tail servo-controls P/No. SC5072 with a serial number equal
to or above 1372,
- tail servo-controls overhauled or repaired in compliance with
GOODRICH Service Bulletin No. SC507X-67-39-01-3,
- tail servo-controls having never been removed since the
delivery of a new aircraft.
AIRBUS HELICOPTERS
AS 350 / EC 1302006-09-01 See AD
2008-09-30
N/A. B3
model only
67.00.30
25 N AD 2006-0252 2006-08-22
SUPERSEDED BY EASA AD 2010-0014
SUPERSEDES AD F-2004-096
Applicability: EUROCOPTER helicopters: - AS 350 B, BA, BB, B1,
B2, B3 and D, before embodiment of MOD 073299. Equipped
with an operator’s belt (called "hoist operator’s belt") PN
330A87-0730-00, 330A87-2371-00, 341A84-1120-00, 350A84-
0047-00, 360A84-0040-00, 360A84-0040-01 or 360A84-0040-
02, fitted with a snap hook PN GA343-95, or, equipped with an
operator’s belt (called "hoist operator’s belt") PN 3160S73-08-
200-1 fitted with a snap hook PN 4100-80AT28.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 315/316/319
SA 330 / AS 332 / EC
225
SA 341/342
SA 365/366 / AS 365
/ EC 155
2006-09-01 See AD N25.00.89
25.00.93
64 N EAD 2006-0235-E 2006-08-09
SUPERSEDED BY EASA AD 2007-0138-E
Applicability: Helicopters: - AS 350 B, BA, BB, B1, B2, B3 and D
equipped, according to the permitted assemblies, with tail
rotor blades, P/Ns.:
- 355A12-0031-01/ -02/ -03/ -04/ -05/ -06/ -07/ -08/ -09/ -11/
-12/ -13/ -14.
- 355A12-0040-00/ -01/ -02/ -03/ -04/ -05/ -07/ -08.
- 355A12-0050-00/ -01/ -02/ -03/ -04/ -05.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2006-08-10 See AD N05.00.40R
1
76 N EAD 2006-0183-E 2006-06-29
Engine Controls - Twist Grip Assembly -
Inspection/Replacement
SUPERSEDES AD F-2004-045
Applicability: AS 350 B3 helicopters equipped with twist grips
post-MOD 073084 and not modified per MOD 073222 (new
solenoid).
AIRBUS HELICOPTERS
AS 350 / EC 1302006-06-30 See AD
2008-09-30
N/A. B3
model only
05.00.44
25 N AD 2006-0164 2006-06-09
Equipment/Furnishings- Untimely Firing of Squibs on
GOODRICH Electric Hoists
Applicability: Helicopters: - AS 350 B, BA, BB, B1, B2, B3 and D,
Equipped with - GOODRICH electric hoists, PN 76370-XXX, (all
types of motors), and not modified per MOD 073318 (or per
Eurocopter AS 350 Alert Service Bulletin (ASB) No. 25.00.95 or
Eurocopter AS 355 Alert Service Bulletin No. 25.00.85) or, -
GOODRICH electric hoists, PN 76370–XXX, not equipped with
the AUXILEC motor.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2006-06-23 See AD
2008-09-30
N/A. Hoist not
installed.
25.00.94
55 N AD 2006-0095 2006-04-24
SUPERSEDED BY EASA AD 2008-0121
SUPERSEDES AD F-2005-010
Applicability: AS 350 B3 helicopters before application of
EUROCOPTER Alert Service Bulletin (ASB) 350 No. 55.00.13.
AIRBUS HELICOPTERS
AS 350 / EC 1302006-05-02 See AD N 05.00.46
76 N AD 2006-0094 2006-04-21
SUPERSEDED BY EASA AD 2011-0237
Applicability: AS 350 B3 helicopters, equipped with twist grips
before embodiment of MOD 073261 (new twist grip assembly
compatible with the ARRIEL 2B1 engine installation).
AIRBUS HELICOPTERS
AS 350 / EC 1302006-05-05 2006-04-12 N
05.00.49R
1
55 N EAD 2006-0060-E 2006-03-07
SUPERSEDED BY EASA AD 2008-0121
Applicability: 1 -AS 350 B, B1, B2, BA, BB and D helicopters,
equipped with: upper and lower fins pre-MOD 073288.
AIRBUS HELICOPTERS
AS 350 / EC 1302006-03-07 See AD
2010-07-20
perf A/CTT
4466,2
55.00.13
2.B.3
67 Y EAD 2006-0055-E 2006-03-01
Rotor Flight Controls - Main Servo-Controls
Applicability: AS 350 B, BA, BB, B1, B2, B3 and D, and AS 355 E
helicopters, equipped with main servo-controls, all part
numbers, not modified per MOD 073343, and on which the
tightening torque of the nut that secures the upper ball-end
has been increased following: - embodiment of MOD 073191,
Or, - compliance with MET Work Card 67.30.00.402 since MET
Revision 04-06 for AS 350 helicopters and Revision 04-08 for
AS 355 helicopters.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2006-03-01 See AD
2006-04-24
perf A/CTT
2230,6
05.00.51
65 N AD F-2005-158 2005-12-21
[Corrected] Tail Rotor Drive - Tail Rotor Drive Shaft
Maintenance
EFFECTIVITY: AS 350 B3 and EC 130 B4 helicopters.
AIRBUS HELICOPTERS
AS 350 / EC 1302005-10-01 See AD
2008-09-30
N/A. B3
model only
25 N AD F-2002-027-088R1 2005-09-14
Equipment/Furnishings - BREEZE 450-lb Electric Hoist Damper
Assembly
EFFECTIVITY: This Airworthiness Directive applies to AS 350 B3
helicopters equipped with BREEZE 450-lb electric hoist PN BL
29700-23.
AIRBUS HELICOPTERS
AS 350 / EC 1302005-09-24 See AD
2008-09-30
N/A. Hoist not
installed.
25.00.73
53 N AD F-2005-102R1 2005-08-03
SUPERSEDED BY EASA AD 2006-0273
EFFECTIVITY: Helicopters: - AS 350 B, BA, BB, B1, B2, B3 and D,
fitted with blades, all part numbers, of RH cabin vibration
dampers, and an automatic flight control system, all design
standards.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2005-08-13 See AD N05.00.48R
1
.05
52N AD F-2005-136 2005-08-03
SUPERSEDED BY EASA AD 2006-0251
SUPERSEDES AD F-2005-032
EFFECTIVITY: Helicopters: - AS 350 B, BA, BB, B1, B2, B3 and D,
fitted with sliding door(s).
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2005-08-03 See AD N
25 N AD F-2005-087 2005-06-22
SUPERSEDED BY EASA AD 2006-0164
EFFECTIVITY: Helicopters: - AS 350 B, BA, BB, B1, B2, B3, and
D, equipped with GOODRICH electric hoist 76370-XXX fitted
with any types of motor except AUXILEC motors.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2005-05-30 See AD N 25.00.94
.01
25
45
N AD F-2004-170R1 2005-03-16
Equipments/Furnishings - Hoist Hook - Operational
Procedures/Restriction
EFFECTIVITY: Helicopters: - AS 350 B, BA, B1, B2, B3, BB and D,
equipped with BREEZE hoists fitted with hook assembly PN BL-
7520-01, with hook PN BL-7520.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 330 / AS 332 / EC
225
SA 341/342
2005-03-26 See AD
2008-09-30
N/A. Hoist not
installed.
01.00.56
67 Y AD F-2005-042 2005-03-16
Rotor Flight Controls - Ball-type Yaw Controls - Replacement
EFFECTIVITY: AS 350 helicopter versions B, BA, BB, B1, B2 and
D, fitted with stainless steel-caged ball-type controls, PNos.:
- 704A 34-130-068 with automatic flight control system (pre-
MOD 072771),
- 704A 34-130-058 without automatic flight control system
(pre-MOD 072771).
AIRBUS HELICOPTERS
AS 350 / EC 1302005-03-26 See AD
2005-08-26
perf A/CTT
2184,7
67.00.26R
1
.05
52N AD F-2005-032 2005-02-16
SUPERSEDED BY DGAC FRANCE AD F-2005-136
EFFECTIVITY: AS 350 helicopter versions B, BA, BB, B1, B2, B3
and D, fitted with sliding door(s).
AIRBUS HELICOPTERS
AS 350 / EC 1302005-02-16 See AD N
67 N AD F-2004-196 2005-01-19
SUPERSEDED BY EASA AD 2006-0247
EFFECTIVITY: EUROCOPTER AS 350 B3 helicopters fitted with a
GOODRICH tail servo-control PN SC5071-XX or SC5072.
AIRBUS HELICOPTERS
AS 350 / EC 1302004-12-28 See AD N 67.00.30
.05
55N AD F-2005-010 2005-01-05
SUPERSEDED BY EASA AD 2006-0095
EFFECTIVITY: AS 350 B3 helicopters, all serial numbers.
AIRBUS HELICOPTERS
AS 350 / EC 1302005-01-05 See AD N 05.00.46
05
67N AD F-2001-580R2 2004-12-08
Rotor Flight Controls - Tail Servocontrols Eye End Fitting
Locking - Check
Effectivity: AS350 B, BA, B1, B2, B3, BB and D helicopters,
equipped with tail servocontrols, all part numbers and all
types, that have not been modified per MOD 073139 or per
EUROCOPTER AS350 Service Bulletin No. 67.00.22.
AIRBUS HELICOPTERS
AS 350 / EC 1302004-12-18
50FH ->
Every 550FH
2007-08-30
Verified A/CTT
3096,6
2015-04-07 SB
67.00.22
verified
performed
05.00.37R
1
29 Y AD F-2004-174 2004-11-10
Hydraulic Power - Rotorcraft Flight Manual - Hydraulic Power
Loss Procedure
EFFECTIVITY: AS 350 helicopter versions B, BA, B1, B2, B3, BB
and D.
AIRBUS HELICOPTERS
AS 350 / EC 1302004-11-20 See AD
Perf 2006-05-
03 A/CTT
2230,6
64 N AD F-2004-178 2004-11-10
Tail Rotor - Tail Rotor Blade Trailing Edge Tab - Modification
EFFECTIVITY: AS 350 helicopters, versions B, BA, BB, B1, B2, B3
and D, fitted with tail rotor blades PN 355A 12.0040 all dash
numbers and PN 355A 12.0050.04, with serial numbers from
8400 to 9224 inclusive, before embodiment of Repair Sheet FR
No. 238 or of Work Card 64.10.00.872 [refer to the equipment
log card (FME)].
AIRBUS HELICOPTERS
AS 350 / EC 1302004-11-20 See AD
2015-04-07
N/A to blades
S/N 18525
64.00.05R
2
.05
52N AD F-2002-344-093R1 2004-11-10
SUPERSEDED BY EASA AD 2006-0249
EFFECTIVITY: AS 350 helicopters, versions B, BA, BB, B1, B2, B3
and D fitted with sliding doors.
AIRBUS HELICOPTERS
AS 350 / EC 1302004-11-20 See AD N
05.00.41R
1
.05
64Y AD F-2000-222-079R1 2004-09-15
Tail Rotor Head Pitch Change Plate Bearing Spacer
EFFECTIVITY: AS 350 helicopters, versions B, B1, B2, B3, BA, BB
and D, fitted with tail rotor pitch change rotating plates all
part numbers, on which EUROCOPTER modification (MOD) 07
6554 has not been embodied.
AIRBUS HELICOPTERS
AS 350 / EC 1302004-09-25 See AD
Perf on Spider
S/N M1815
2001-11-19
05.00.33R
1
25 N AD G-2004-0019 2004-07-27
Equipment & Furnishings - Camera System Installation Floor-
mounted Platform Panel Hold-down Hook - Replacement
Applicability: Eurocopter Model AS350 and AS355 helicopters,
certificated in any category that have beenmodified in
accordance with MAG(E) modification 350-1521, 350-1680 or
350-1707. Installation of Cameraplatform.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
MANN AVIATION
GROUP
CAMERA SYSTEM
INSTALLATION
2004-08-05 2004-11-05
2015-04-09.
N/A.
Equipment
not installed.
25 N AD F-2004-096 2004-06-23
SUPERSEDED BY EASA AD 2006-0252
EFFECTIVITY: EUROCOPTER helicopters: - AS 350 B, BA, BB, B1,
B2, B3 and D, equipped with an operator's belt (called "hoist
operator's belt") PNs: 330A87-0730-00, 330A87-2371-00,
341A84-1120-00, 350A84-0047-00, 360A84-0040-00, 360A84-
0040-01 and 360A84-0040-02, fitted with a snap hook PN
GA343-95, or equipped with an operator's belt (called "hoist
operator's belt") PN 3160S73-08-200-1, fitted with a snap
hook PN 4100-80AT28.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 330 / AS 332 / EC
225
SA 341/342
SA 365/366 / AS 365
/ EC 155
2004-07-03 See AD N 25.00.89
25
.01N AD F-2004-085 2004-06-23
SUPERSEDED BY EASA AD 2006-0248
EFFECTIVITY: AS 350 BA helicopters equipped with an
AERAZUR emergency flotation gear comprising:
- LH side container assembly 158170 or 158210-1,
- RH side container assembly 158171 or 158215-1.
The containers are comprised in emergency flotation gear,
removable parts, PN 350A82-8040-00 or PN 350A82-8040-01.
AIRBUS HELICOPTERS
AS 350 / EC 1302004-06-11 See AD N 01.00.55
29 Y AD F-2004-089 2004-06-23
Hydraulic System - Hydraulic Cut-Off Function - Modification
EFFECTIVITY: AS 350 helicopter versions B, B1, B2, B3, BA, BB
and D, pre-MOD 073263.
AIRBUS HELICOPTERS
AS 350 / EC 1302004-07-03 See AD
2005-01-05
Verified A/CTT
1860,5
29.00.07
24 Y AD F-2003-260R1 2004-06-09
Electrical Power - Battery Lug Connection
EFFECTIVITY: AS 350 helicopter versions B, BA, BB, B1, B2, B3
and D, pre-MOD 073226 (subject of EUROCOPTER AS 350
Service Bulletin No. 24.00.11).
AIRBUS HELICOPTERS
AS 350 / EC 1302004-06-19 See AD
2004-06-03
Verified A/CTT
1597,1
24.00.10
67 Y AD F-2003-322R1 2004-05-26
Rotor Flight Controls - Double Locking of Stop Screws
Effectivity: before embodiment of MOD 073206 or MOD
073102.
Components affected: Roll, pitch and collective flight control
stops.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
EC 120 B
SA 365/366 / AS 365
/ EC 155
2004-06-05
1. 100FH
2.
500FH/12M
2004-10-14
Verified A/CTT
1860,5
67.00.25
2.B.1
.05
29Y AD F-2004-055 2004-04-28
Time Limits / Maintenance Checks - Replacement of Hydraulic
Fluid in Cold Weather
EFFECTIVITY: AS 350 helicopter versions B, BA, BB, B1, B2, B3
and D that operate in a flight envelope where the outside air
temperature (OAT) is below minus 15° Celsius (or below plus
5° Fahrenheit).
AIRBUS HELICOPTERS
AS 350 / EC 1302004-05-08 See AD
2012-07-02
Perf A/C TT
5070,6
05.00.45R
1
110FH
/1M
(only if
OAT is
below
15°
Celsius
)
25
.01
.04
N AD F-2004-046 2004-03-31
SUPERSEDED BY EASA AD 2006-0098
EFFECTIVITY: Helicopter versions: AS 350 B, BA, B1, B2, B3, BB
and D, equipped with GOODRICH (LUCAS – AIR EQUIPEMENT)
hoists, part numbers: 76300-xxx, 6340-xxx, 76360-xxx, 76360-
xxx-xx, 76363-xxx, 76365-xxx, 76368-xxx, 76370-xxx, 76375-
xxx, 76378-xxx, fitted with hooks, part numbers: 704160,
708223, 708931, 709866, 710177.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 315/316/319
SA 330 / AS 332 / EC
225
SA 341/342
SA 365/366 / AS 365
/ EC 155
SE 313 / SA 318
2004-03-31 See AD
76
.05N AD F-2004-045 2004-03-31
SUPERSEDED BY EASA EMERGENCY AD 2006-0183-E
EFFECTIVITY: AS 350 B3 helicopters fitted with twist grip post-
MOD 073084.
AIRBUS HELICOPTERS
AS 350 / EC 1302004-03-31 See AD
34 N AD F-2002-281R1 2004-03-17
Navigation - Horizontal Situation Indicator KI 525A - Wiring
Change
EFFECTIVITY: AS 350 helicopter versions B, BA, B1, B2, B3, BB
and D, equipped with HSI KI 525A.
AIRBUS HELICOPTERS
AS 350 / EC 1302004-03-27 See AD
2008-03-05
N/A.
Equipment
not installed
34.00.13
53 Y AD F-2004-035 2004-03-17
Fuselage - Rear Structure Junction Frame - Inspection /
Replacement
EFFECTIVITY: AS 350 helicopter versions B, BA, BB, B1, B2, B3
and D
- pre-MOD 073215, or
- not equipped with the four reinforcement angles, P/Nos.
350A08.2493.20 / .21 / .22 / .23, following the repair carried
out in accordance with MRM Work Card 53.10.22.772.
AIRBUS HELICOPTERS
AS 350 / EC 1302004-03-27 See AD
Perf 2015-11-
21 by PHAB
iaw WO
17220006.
Next insp:
A/CTT 5820,2.
05.00.43R
1550FH
28 Y AD F-2004-033 2004-03-17
Fuel - Fuel Bleed Lever - Modification
EFFECTIVITY: AS 350 helicopter versions B, BA, BB, B1, B2, B3
and D, pre-MOD 073239.
AIRBUS HELICOPTERS
AS 350 / EC 1302004-03-17 See AD
2004-10-14
Verified A/CTT
1860,5
28.00.16
67 Y AD F-2003-002R1 2004-02-18
Rotor Flight Controls - Cyclic Stick Bowl Lower Friction Cup -
Inspection/Replacement
EFFECTIVITY: AS 350 helicopter versions B, BA, B1, B2, B3, BB
and D, modified per MOD 070682 (this MOD forms the subject
of EUROCOPTER AS 350 Service Bulletin No. 67.09), and before
embodiment of MOD 073179.
The component affected is the lower friction cup P/N 350A27-
1612-20 of the cyclic stick.
AIRBUS HELICOPTERS
AS 350 / EC 1302004-02-28 See AD
Rev A perf
2001-12-10
A/CTT 1330,3
MOD 073179
67.00.24
67 N AD F-2002-314-092R1 2003-12-10
Rotor Flight Controls - "TRW-SAMM" Main Servo Controls -
Check
EFFECTIVITY: AS 350 B3 helicopters equipped with "TRW –
SAMM" main servocontrols, part numbers SC 8042 or SC 8043
that underwent their last complete overhaul or repair since
complete overhaul at "HAWKER PACIFIC AEROSPACE", USA,
before March 1, 2002.
AIRBUS HELICOPTERS
AS 350 / EC 1302003-12-20 See AD
2015-11-12
N/A. B3
model only.
67.00.23R
1
67 Y AD F-2003-406 2003-10-29
Rotor flight controls - Collective lever lock
EFFECTIVITY AS 350 helicopter versions B, BA, BB, B1, B2, B3
and D fitted with the pilot collective lever locking system:
Locks PN 350A77.1309.xx and 350A27.3155.20.
AIRBUS HELICOPTERS
AS 350 / EC 1302003-11-08 See AD
2004-10-14
§2.B.2 o 2.B.3
verified A/C
TT 1860,5
67.00.27
25 N AD G-2003-0008 2003-09-17
Equipment / Furnishings - Tail Rotor and Cyclic Control Cut-
Outs of Floor Mounted Camera System Installation Platform
Panel - Rework
Applicability: Eurocopter Model AS350 and AS355 helicopters,
certificated in any category that have been modified in
accordance with MAG(E) modification 350-1521 or 350-1680.
Installation of Camera platform.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
MANN AVIATION
GROUP
CAMERA SYSTEM
INSTALLATION
2003-09-18 2003-10-18
2015-04-09.
N/A.
Equipment
not installed.
71 N AD F-2003-208 2003-05-28
Power plant - Interference between the bleed valve air
exhaust duct and the engine fuel line
EFFECTIVITY AS 350 B3 helicopters equipped with optional
engine flushing system and modified per MOD 073098.
AIRBUS HELICOPTERS
AS 350 / EC 1302003-06-07 See AD
2008-09-30
N/A. System
not installed
71.00.16
62
63
64
65
N/A AD F-2002-452R1 2003-04-30
Main rotor and tail rotor dynamic component - Correction of
operating hours
EFFECTIVITY: Helicopters: - AS 350 B, BA, BB, B1, B2, B3 and D
equipped with dynamic components following overhaul (RG)
or repair (RE) at the EUROCOPTER helicopter maintenance and
overhaul facility (D.E.R.H.), listed in Tables 1 and 2 (as
applicable) in paragraph 4 "Appendix" of the Alert Service
Bulletins (ASBs) referenced below.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 330 / AS 332 / EC
225
SA 341/342
SA 365/366 / AS 365
/ EC 155
2003-05-10 See AD
2015-04-10
N/A. P/N and
S/N not
affected
.01
67N AD F-2003-099 2003-03-05
Mail and Tail TRW SAMM servocontrols
EFFECTIVITY: AS 350 helicopters, versions B, BA, B1, B2, B3, BB
and D equipped with the following main and tail TRW SAMM
servocontrols: SEE AD
AIRBUS HELICOPTERS
AS 350 / EC 1302003-03-05 See AD
2015-11-12
N/A. Installed
Servo S/N
(6030, 6137,
3175) not
affected.
25 N AD F-2002-585 2002-11-27
BREEZE or TRW (or LUCAS or AIR EQUIPEMENT)
EFFECTIVITY: The following helicopters: - AS 350 helicopters
versions B, BA, BB, B1, B2, B3 and D, equipped with the
optional BREEZE or TRW (or LUCAS or AIR EQUIPEMENT) 300
lb. electric hoist and hoist box 26 M part number 350A63-1136-
00 (AS 350) or 350A63-1136-01 (AS 355), not modified per
MOD 073190, and delivered before October 1st, 2002 .
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
2002-12-07 See AD
2008-09-30
N/A. Hoist not
installed.
25.00.79
.05
62N AD F-2001-557-086R3 2002-05-15
Main rotor - STARFLEX star
EFFECTIVITY: AS 350 version B, BA, B1, B2, B3, BB and D
helicopters equipped with STARFLEX stars P/N
350A31.1916.00, mounted on Main Rotor Hubs (MRH) prior to
the embodiment of MOD 076221.
AIRBUS HELICOPTERS
AS 350 / EC 1302002-05-15 See AD
2008-09-30
N/A to
Starflex P/N
62.00.24
MOD
076221
24 N AD F-2002-187-090 2002-04-03
Electrical power
EFFECTIVITY: AS 350 version B3 helicopters before
embodiment of MOD 073146, with the following serial
numbers: 3461, 3463, 3464, 3467, 3469, 3471, 3472, 3473,
3475, 3477, 3478, 3479, 3484, 3485, 3486, 3493, 3494, 3511
and 3522.
AIRBUS HELICOPTERS
AS 350 / EC 1302002-04-13 See AD
2008-09-30
N/A. B3
model only
24.00.09
.05
53N AD F-2000-340-080R2 2002-02-20
Tail rotor drive shaft forward fairing
EFFECTIVITY: AS 350 B3 helicopters equipped with tail rotor
drive shaft forward fairing P/Nos.: - 350A23.0032.09 pre MOD
073097 - 350A23.1075.00 post MOD 073097.
AIRBUS HELICOPTERS
AS 350 / EC 1302002-03-02 See AD
2010-08-23
N/A. 350B3
only
05.00.35R
2
.05
65N AD F-1999-085-076R3 2002-02-20
Tail rotor hub pitch-change plate bearing
EFFECTIVITY: AS 350 helicopters, versions: B, BA, B1, B2, B3,
BB and D fitted with tail rotor hub pitch change plate, P/Nos.
350A33-2004-00/-01/-02/-03/-05 or 350A33-2009-00/-01,
and which do not incorporate MOD 076551 [new generation
bearing P/No. 6010F234M16 (704A33.651.190) introduced by
EUROCOPTER AS 350 Service Bulletin No. 65.00.38 R1].
AIRBUS HELICOPTERS
AS 350 / EC 1302002-03-02 See AD
2008-09-30
N/A to
6010F234M16
bearings
05.00.29R
3
.05 N AD F-2002-044 2002-01-23
SIREN cargo hooks
EFFECTIVITY: This Airworthiness Directive applies to the
following helicopter models: - AS 350 B3, fitted with SIREN
cargo hooks P/N AS-21-5-7.
AIRBUS HELICOPTERS
AS 350 / EC 130
SA 365/366 / AS 365
/ EC 155
2002-01-23 See AD
2008-09-30
N/A. B3
model only
05.00.39
53 Y AD F-1997-147-072R1 2002-01-23
Tail boom-to-aircraft structure junction attachment screws
EFFECTIVITY: This Airworthiness Directive (AD) applies to AS
350 helicopters, versions B, BA, BB, B1, B2 and D equipped
with attachment screws P/N 22201BC060008L
(N5103337287), which ensure the tail boom-to-aircraft
structure junction attachment.
AIRBUS HELICOPTERS
AS 350 / EC 1302002-02-02 See AD
Perf 2001-10-
29 A/CTT
1330,3
01.00.46
76 N AD F-2001-548-084 2001-11-14
Engine controls - Switching unit
EFFECTIVITY: This Airworthiness Directive applies to AS 350 B3
helicopters delivered new before October 15, 2001 and
equipped with switching unit P/N 200192.
AIRBUS HELICOPTERS
AS 350 / EC 1302001-11-14 See AD
2008-09-30
N/A. B3
model only
76.00.16
77 N AD F-2001-319-083 2001-07-25
Engine indicating - ASU PCB
EFFECTIVITY: AS 350 B3 helicopters equipped with printed
circuit boards P/Nos. SE 03022 (704A47720110) (ASU No. 2
board) delivered before May 1st, 1999 and AS 350 B3
helicopters delivered new before May 1st, 1999.
AIRBUS HELICOPTERS
AS 350 / EC 1302001-08-04 See AD
2008-09-30
N/A. B3
model only
77.00.07
N AD CF-2000-06R1 2000-08-23
Left-Side Pilot Configuration - Modification
Applies to all Eurocopter Canada Limited (ECL) Left-Side Pilot
Configuration kits, Transport Canada Supplemental Type
Certificate (STC) SH96-32, Issues 1 through 5, installed in
Eurocopter France (Aerospatiale) AS 350 BA and B2
helicopters.
AIRBUS HELICOPTERS
AS 350 / EC 130
EUROCOPTER CANADA
LTD
STC SH96-32
2000-04-17 See AD
2015-04-10
N/A.
Equipment
not installed
28 N AD F-2000-302 2000-07-12
Ferry fuel tanks
APPLICABILITY: Helicopters of following models: - AS 350 B,
BA, B1, B2, B3, BB and D, equipped with metal ferry fuel tanks,
part number 330A 871310 .00, .01, .02, .03 and .04, - SA 316 B
and C, SA 3160 and SA 319 B, equipped with metal ferry fuel
tanks, part number 3160S 7375020 and 3160S 7375020-1.
AIRBUS HELICOPTERS
AS 350 / EC 130
AS 355
SA 315/316/319
SA 330 / AS 332 / EC
225
SA 365/366 / AS 365
/ EC 155
2000-07-12 See AD
2008-03-05
N/A.
Equipment
not installed
28.00.14
79 Y AD F-2000-268-078 2000-06-28
Engine oil pipe - Fire proofing
EFFECTIVITY: AS 350 helicopters, versions: B, B1, B2, BA, BB
and D on which MOD 07 2793 has not been embodied.
AIRBUS HELICOPTERS
AS 350 / EC 1302000-07-08 See AD
Perf 2001-10-
29 A/CTT
1330,3
79.00.11R
1
33 N AD F-1999-512-077 1999-12-29
"NR" indicator lighting
EFFECTIVITY: AS 350 B3 version helicopters, which do not
incorporate MOD 072810 or any other approved modification,
enabling full "NR" indicator lighting in normal mode and
emergency mode.
AIRBUS HELICOPTERS
AS 350 / EC 1302000-01-08 See AD
2008-09-30
N/A. B3
model only
33.00.17
- N AD F-1999-017-075 1999-01-13Climbing Speeds
EFFECTIVITY : AS 350 B3 helicopters.
AIRBUS HELICOPTERS
AS 350 / EC 1301999-01-13 See AD
2008-09-30
N/A. B3
model only
.01 N AD F-1998-511-074 1998-12-16
Single-pole circuit breakers
EFFECTIVITY: AS 350 helicopters, versions : B, BA, BB, B1, B2,
B3 and D equipped with single-pole CROUZET circuit breakers,
part numbers : SEE AD
AIRBUS HELICOPTERS
AS 350 / EC 1301998-12-16 See AD
2008-03-05
N/A.
Equipment
not installed
01.00.47
.05 N AD F-1998-173-073 1998-04-22
SUPERSEDED BY EASA AD 2015-0195
Tail Rotor Drive Shaft Bearings
AIRCRAFT CONCERNED: AS 350 helicopters, versions B, B1, B2,
D, BA, BB and B3 with tail rotor drive shaft rear section
bearing mountings, equipped with : non-regreasable bearings
P/N SKF 6007.2RS 1 MT 47CA (AS 704A33.651.010) or
regreasable bearings P/N KOYO 83A 85 1C3 (AS
704A33.651.143), FAFNIR P9107NPP7 (AS 704A33.651.111),
FAG 593404 (AS 704A33.651.181)
AIRBUS HELICOPTERS
AS 350 / EC 1301998-05-02 See AD
Perf 2012-07-
02 A/CTT
5070,6
05.00.08R
5
100FH
(VC)
.05 N AD F-1996-156-071R1 1997-04-06
MGB suspension bi-directional cross beam
This Airworthiness Directive applies to AS 350 helicopters,
versions B, BA, B1, B2 and D fitted with a MGB suspension bi-
directional cross beam P/N 350A38.1018 - all dash numbers,
installed on the complete cross beam assemblies P/No
350A38.0210 - all dash numbers (which are not modified per
MOD. 072720).
AIRBUS HELICOPTERS
AS 350 / EC 1301997-06-14 See AD
2008-03-05
N/A.
Equipment
not installed
05.00.28
.01 N AD F-1994-279-070R1 1995-01-18
Main rotor shaft
This Airworthiness Directive applies to AS 350 helicopters,
versions B, BA, B1, B2 and D, equipped with a "TIMKEN" main
rotor shaft P/N 350A37-0003- all dash numbers, that have
logged less than 100 operating hours since new or overhaul.
AIRBUS HELICOPTERS
AS 350 / EC 1301995-01-18 See AD
2008-03-05
N/A.
Equipment
not installed
01.00.44
.01 Y AD F-1994-180-069 1994-08-03
Cycle pitch change control rod
This Airworthiness Directive covers AS 350 helicopters,
versions B, BA, D, B1 and B2, fitted with cyclic pitch change
control rod P/N 704A34-113-279.
AIRBUS HELICOPTERS
AS 350 / EC 1301994-08-03 See AD
Perf 2001-10-
29 A/CTT
1330,3
01.00.42
.01 Y AD F-1994-087-068 1994-04-13
MGB oil pressure switch
The present Airworthiness Directive applies to AS 350 B, BA, D,
B1 and B2 helicopters fitted with MGB oil pressure switch P/N
704A37.721.082 (S 1130.021.082).
AIRBUS HELICOPTERS
AS 350 / EC 1301994-04-13 See AD
Perf 2001-10-
29 A/CTT
1330,3
01.00.43
.05 Y AD F-1984-064-037R3 1994-02-02
Tail rotor blade spars
The present AD applies to AS 350 helicopters, all versions fitted
with tail rotor blades assemblies P/N: -350A08.1011 all
dashnumbers, -350A12.0020 all dashnumbers, -350A12.0030
all dashnumbers, -350A12.0031 all dashnumbers, -
350A12.0040 all dashnumbers
AIRBUS HELICOPTERS
AS 350 / EC 1301994-02-12 See AD
Perf 2001-10-
29 A/CTT
1330,3
05.00.11R
5
.05 Y AD F-1993-090-067R1 1993-12-22
Door "clear vision" window
The present Airworthiness Directive applies to AS 350
helicopters, versions B, BA, B1, B2 and D fitted with "clear
vision" windows : Part Numbers : see AD
AIRBUS HELICOPTERS
AS 350 / EC 1301994-01-02 See AD
Perf 2015-12-
03 by PHAB
iaw
WO17220006
at A/CTT
5270,2. Next
insp: A/CTT
5370,2.
05.00.25R
1100FH
.01 N/A AD F-1988-184-052R1 1993-07-21
DUNLOP Servocontrols
This AD covers AS 350 B, B1, D helicopters fitted with the
following DUNLOP main and tail servocontrols: P/N: see AD
AIRBUS HELICOPTERS
AS 350 / EC 1301993-07-31 See AD
Perf 2001-10-
29 A/CTT
1330,3
2015-11-12
Goodrich M/R
servos
installed.
01.00.21R
1
- N AD F-1993-067-066 1993-05-12
Flight in falling snow
The present Airworthiness Directive applies to AS 350
helicopters, versions B, B1, B2 and BA.
AIRBUS HELICOPTERS
AS 350 / EC 1301993-05-22 See AD
2008-03-05
N/A. RFM
revised
62 Y AD F-1992-179-064R1 1993-03-31
Main rotor pitch change horn bushes
The present Airworthiness Directive applies to AS 350
helicopters, versions B, D, B1, B2 and BA on which the pitch
change horns P/N 350A31-1877-02 are not marked with an
"X" and have a serial number less than 100-000.
AIRBUS HELICOPTERS
AS 350 / EC 1301993-04-10 See AD
Perf 2001-10-
29 A/CTT
1330,3
62.00.21R
1
.01 Y AD F-1993-030-065 1993-03-03
Main rotor mast assembly
IThe present Airworthiness Directive applies to EUROCOPTER
AS 350 helicopters, versions B, BA, B1, B2 and D fitted with
rotor mast assembly Part Numbers : 350A37.0004.02,
350A37.0004.03, 355A37.0005.01
AIRBUS HELICOPTERS
AS 350 / EC 1301993-03-03 See AD
Perf 2001-10-
29 A/CTT
1330,3
01.00.41
.01
26N AD F-1992-159-063R2 1992-11-25
Engine bay fire detection
The present Airworthiness Directive applies to all
EUROCOPTER AS 350 helicopters, versions B1 and B2.
AIRBUS HELICOPTERS
AS 350 / EC 1301992-12-05 See AD
2006-05-03
N/A. MOD
072598
performed at
A/CTT 2230,6
01.00.38
26.00.01
25 N AD F-1992-144-061 1992-07-08
"JOLLIET" Emergency Locator Transmitter Antenna
This Airworthiness Directive applies to AS 350 helicopters,
versions B, BA, B1, B2 and D, fitted with the "JOLLIET"
emergency locator transmitter system, not modified per AMS
350A.07.2492.
AIRBUS HELICOPTERS
AS 350 / EC 1301992-07-18 See AD
2008-09-30
N/A. Jolliet
not installed.
25.00.45
.01 Y AD F-1992-145-062 1992-07-08
Hydraulic system
This Airworthiness Directive applies to AS 350 helicopters,
versions B, BA, B1, B2 and D, fitted with the hydraulic reservoir
P/N 350A75-1030-00.
AIRBUS HELICOPTERS
AS 350 / EC 1301992-07-18 See AD
Perf 2001-10-
29 A/CTT
1330,3
01.00.36
.01 Y AD F-1990-198-056R1 1991-11-27
Battery temperature probe
This AD is applicable to AEROSPATIALE helicopters AS 350 D,
B, B1 and B2 equipped with one or two SAFT 1606-1
battery(ies) not modified by amendment E.
AIRBUS HELICOPTERS
AS 350 / EC 1301991-12-07 See AD
Perf 2001-10-
29 A/CTT
1330,3
01.00.29R
1
25 N AD F-1991-165-058R1 1991-11-27
Electric hoist installation
The present AD applies to AEROSPATIALE AS 350 helicopters,
versions B, B1, B2, D, fitted with an AIR EQUIPMENT hoist P/N
76370.010, 76370.011 or 76370.030.
AIRBUS HELICOPTERS
AS 350 / EC 1301991-12-07 See AD
2008-09-30
N/A. Hoist not
installed.
25.00.42R
1
62 Y AD F-1989-155-054R4 1991-10-02
Swashplate
The present AD applies to AEROSPATIALE AS 350 helicopters
all S/N of versions B, B1, B2, D on which the swashplate is
fitted with bearings P/Ns: see AD.
AIRBUS HELICOPTERS
AS 350 / EC 1301991-10-12 See AD
Rev B perf
2001-10-29
A/CTT 1330,3
62.00.12R
2
.01 Y AD F-1991-159-060 1991-07-31
Tail rotor drive shaft bearings
The present AD applies to AEROSPATIALE AS 350 helicopters
versions B, D, B1,B2, L1 and AVEX equipped with FAFNIR tail
rotor drive shaft bearings P/N P.9107.NPP7 not marked with
"X" on sealing flanges and installed on those helicopters which
were acceptance tested by AEROSPATIALE Marignane, when
see AD.
AIRBUS HELICOPTERS
AS 350 / EC 1301991-07-31 See AD
Rev B perf
2001-10-29
A/CTT 1330,3
01.00.34
.01 Y AD F-1991-137-059 1991-07-01
Pitch control lever expansion pin - Tail rotor
This AD is applicable to AEROSPATIALE helicopters AS 350 D,
B, B1 AND B2.
AIRBUS HELICOPTERS
AS 350 / EC 1301991-07-01 See AD
Rev B perf
2001-10-29
A/CTT 1330,3
01.00.33
.01 N AD F-1989-081-053 1989-05-17
Spherical thrust bearings P/N 704A 33-633-1
This AD covers AEROSPATIALE AS 350 helicopters, versions B,
B1 and D.
AIRBUS HELICOPTERS
AS 350 / EC 1301989-05-27 See AD
2008-09-30
N/A to
bearings P/N
01.00.23
. 05 N AD F-1981-094-018R2 1988-07-20 Main gear boxAIRBUS HELICOPTERS
AS 350 / EC 1301988-07-20 See AD
2008-09-30
N/A to
helicopter S/N
05.00.06
.01 Y AD F-1987-161-051 1987-11-25 Spherical thrust bearing bolts - Service life limit reductionAIRBUS HELICOPTERS
AS 350 / EC 1301987-12-05 See AD
2001-10-29
Accomplished
A/CTT 1330,3
01.00.20
.01 Y AD F-1987-115-050 1987-08-19
Flight cycle calculation
This AD concerns AEROSPATIALE AS 350 helicopters, versions
B, B1 and D.
AIRBUS HELICOPTERS
AS 350 / EC 1301987-08-29 See AD
2001-10-29
Accomplished
A/CTT 1330,3
01.00.19
52 N/A AD F-1987-088-049 1987-06-24
Sliding doors
The present AD applies to AEROSPATIALE AS 350 helicopters
all versions, equipped with LH and/or RH sliding door(s).
AIRBUS HELICOPTERS
AS 350 / EC 1301987-06-24 See AD
2001-10-29
Accomplished
A/CTT 1330,3
52.00.18
28 Y AD F-1986-077-046R2 1986-12-10
Fuel filter
The AD is applicable to AEROSPATIALE AS 350 (ECUREUIL and
ASTAR) Helicopters fitted with a LEBOZEC and GAUTHIER fuel
filter P/N 432B12.3, .sC, .3D or a GUIOT fuel filter P/N
704A34620002, prior to compliance with modification 350A
071671.
AIRBUS HELICOPTERS
AS 350 / EC 1301986-12-10 See AD
2001-10-29
Accomplished
A/CTT 1330,3
28.00.07R
1
.01 Y AD F-1986-125-048R1 1986-10-15
Behaviour of the helicopter on the ground with rotor turning
Present AD applies to AEROSPATIALE AS 350 B, B1, C, D and
D1 helicopters.
AIRBUS HELICOPTERS
AS 350 / EC 1301986-10-15 See AD
2001-10-29
Accomplished
A/CTT 1330,3
01.00.17A
.05 Y AD F-1978-193-001R1 1986-10-01
Tail rotor
The AD applies to AEROSPATIALE AS 350B, C, D and D1
helicopters.
AIRBUS HELICOPTERS
AS 350 / EC 1301986-10-01 See AD
2001-10-29
Accomplished
A/CTT 1330,3
05.00.02
- N AD F-1986-057-044R1 1986-07-09
Main rotor head roving sleeve beams
The present AD applies to AEROSPATIALE AS 350 helicopters
models B and D, fitted with roving sleeve upper and lower
beams P/Ns 350A31-1830-00 and -01, 350A31-1831-00 and -
01, -04, -05, -06, -07, and AEROSPATIALE AS 350 helicopters
model B1, fitted with roving sleeve uper and lower beams
P/Ns 350A31-1831-04, -05, -06, -07.
AIRBUS HELICOPTERS
AS 350 / EC 1301986-07-16 See AD
2015-04-15
N/A. P/Ns not
installed
N/A
28 Y AD F-1986-097-047 1986-06-25
Fuel filter
The AD is applicable to AEROSPATIALE AS 350 (ECUREUIL and
ASTAR) Helicopters fitted with a LEBOZEC and GAUTHIER fuel
filter P/N 432B12.3, .sC, .3D or P/N 350A52-1070-00 (after
modification 350A 071671).
AIRBUS HELICOPTERS
AS 350 / EC 1301986-06-25 See AD
2001-10-29
Accomplished
A/CTT 1330,3
28.00.08
.01 Y AD F-1985-135-042 1985-07-31 Fuel filter and main gear box oil filterAIRBUS HELICOPTERS
AS 350 / EC 1301985-07-31 See AD
2001-10-29
Accomplished
A/CTT 1330,3
01.00.14A
.05 Y AD F-1985-095-040 1985-06-19
Main rotor shaft
Applicability: AEROSPATIALE helicopters AS 350 all versions
(ECUREUIL and ASTAR) - Main Rotor Shaft P/N 350A37-1076-
00 through -06.
AIRBUS HELICOPTERS
AS 350 / EC 1301985-06-26 See AD
2001-10-29
Accomplished
A/CTT 1330,3
05.00.15
.05 Y AD F-1985-068-038 1985-05-22Inspection of the bolted junction : bevel ring gear / Vertical
shaft of the bevel reduction gear module on the MGB
AIRBUS HELICOPTERS
AS 350 / EC 1301985-05-29 See AD
2001-10-29
Accomplished
A/CTT 1330,3
05.00.10R
1
.05 Y AD F-1983-173-036 1983-11-09 Main rotor mast shaft - Checking for cracksAIRBUS HELICOPTERS
AS 350 / EC 1301983-11-16 See AD
2001-10-29
Accomplished
A/CTT 1330,3
05.00.13R
1
.01 Y AD F-1983-075-033 1983-05-04
Tail rotor - Retiring from operation and replacing stainless
steel leading edges
The present AD applies to T/R assemblies P/N 350A12-0030-
01 to -05 from S/N 979 (inc) to 1150 (inc) excepting S/N 997 to
999, 1004, 1010, 1014, 1016, 1021 to 1026, 1028, 1029, 1033,
1044, 1136 which have been already reconditioned.
AIRBUS HELICOPTERS
AS 350 / EC 1301983-05-11 See AD
2001-10-29
Accomplished
A/CTT 1330,3
01.00.10
.05 Y AD F-1982-098-026 1982-07-28 Upper fin attachment fittingAIRBUS HELICOPTERS
AS 350 / EC 1301982-08-05 See AD
2001-10-29
Accomplished
A/CTT 1330,3
05.00.09
65 Y AD F-1982-175-029 1982-12-15 Main gear box - Oil monitoringAIRBUS HELICOPTERS
AS 350 / EC 1301982-12-22 See AD
2001-10-29
Accomplished
A/CTT 1330,3
65.00.20
55 Y AD F-1981-203-021 1981-12-02 Inproved installation of upper and lower finsAIRBUS HELICOPTERS
AS 350 / EC 1301981-12-09 See AD
1990-07-31
C/W by
factory A/CTT
0,0
55.00.02
ATA Appl ASB SB Rev. Issue date Subject Notes Ass. RequirmentsAD Due PerfEmbodiment
of MODRec.
33 Y - 33.00.40 0 2015-11-26
LIGHTING - Outer lighting - Improvement of wiring
protection in the stabilizer
EFFECTIVITY: (B2, B3) Helicopters PRE MOD 074720
Recommende
dN/A .074720
31 N/A - 31.00.64 0 2015-11-24
INDICATING AND RECORDING SYSTEMS - Modification to
the NR indicator electrical power supply
EFFECTIVITY: (B2, B3) Helicopters POST MOD 074222
and PRE MOD 074700.
Recommende
dN/A
N/A. PRE
MOD 074222.074700
67 N/A 67.00.57 1 2015-11-18
ROTOR FLIGHT CONTROLS - Optimization of the yaw
sheath routing
EFFECTIVITY: (B3)
Recommende
d
Applicable to
AS350 B3
.073422
AL 4738
67 N/A - 67.00.66 1 2015-10-22
ROTOR FLIGHT CONTROLS - Functional check procedure
for the tail rotor load compensator
EFFECTIVITY: (B3)
Recommende
d
Applicable to
AS350 B3
52 OPT - 52.00.25 1 2015-10-13
DOORS - Improved Closing System for the Side Baggage
Compartment Doors
Effectivity: (B, BA, BB, B1, B2, B3, D, L1)
OPTIONAL N/A 350A073016
31 N/A - 31.00.52 2 2015-10-06
INDICATING AND RECORDING SYSTEMS - VEMD version
2005
EFFECTIVITY: (B3) Helicopters equipped with VEMDs
"Vehicle & Engine Multifunction Display" listed in
paragraph 1.A.2. and with Global Positioning System
(GPS), compatible with ARINC 429 High Speed, and pre-
MOD 073195.
Recommende
d31.00.54
Applicable to
AS350 B3.073195
25 OPT - 25.02.60 0 2015-10-05
EQUIPMENT AND FURNISHINGS - Change of JAR
OPS3.745 first aid kit
Effectivity: (B, BA, BB, B1, B2, B3, D, L1) Helicopters -
with first aid kit P/N 7052A4256019 and POST MOD
OP3110 (Type 159 pilot and copilot crashworthy seats),
or - POST MOD 074338 (Sicma 198 seats with SRP210
for pilot and co-pilot), and PRE MOD 074687 (Change of
JAR OPS 3.745 first aid kit).
OPTIONAL N/A .074687
65 Y 01.00.70 - 1 2015-09-21
LIMITATIONS - Tail rotor drive - Tail rotor drive shaft
bearings
EFFECTIVITY: (B,BA,BB,B1,B2,B3,D) a) Helicopters
equipped with tail rotor drive shaft bearings with Part
Numbers (MP/Nos.):
- 6007-2RSMT47CA (P/N 704A33-651-010, non-
regreasable) manufactured by SKF,
- P9107NPP7 (P/N 704A33-651-111, regreasable)
manufactured by FAFNIR,
- 83A851BC3 and 83A851B-1C3 (P/N 704A33-651-143,
regreasable) manufactured by KOYO.
b) Helicopters equipped with tail rotor drive shaft
bearing with Part Number (MP/N):
- 593404 (P/N 704A33-651-181 , regreasable)
manufactured by FAG.
ASB 05.00.08 N/A 2015-0195 165FH
New
driveshaft
bearings
installed
2015-11-03.
Next insp:
A/CTT
5435,2.
- 165FH
34 N/A - 34.00.20 0 2015-09-16
NAVIGATION - Check of the altimeter
EFFECTIVITY: (B3) Helicopters POST MOD 07-3368 and
PRE MOD AL 4236 whose S/N:s are listed in SB
Recommende
dN/A
Applicable to
AS350 B3AL-4236
23 OPT - 23.00.06 0 2015-09-10
COMMUNICATION - VHF antenna sealing
EFFECTIVITY: (B, BA, BB, B1, B2, B3, D, L1) Helicopters
PRE MOD 074715 (VHF antenna tightness), POST MOD
OP4657 (New Garmin radio line - GNC255 VOR/VHF) or
OP0154 (COLLINS 251E VHF) or OP0625 (KING KY196
VHF) or 071979 (KY196A COPILOT VHF)
OPTIONAL N/A .074715
67 N/A - 67.00.66 0 2015-08-26
ROTOR FLIGHT CONTROLS - Functional check procedure
for the tail rotor load compensator
EFFECTIVITY: (B3)
Recommende
d
Applicable to
AS350 B3
71 OPT - 71.00.18 2 2015-07-30
POWER PLANT - Firewall reinforcement
EFFECTIVITY: (B, BA, B1, B2, B3, L1) Helicopters pre-
MOD 073219
OPTIONAL N/A .073219
63 y 01.00.69 - 1 2015-07-28
LIMITATIONS - Main Gearbox (MGB) Casings -
Limitations and follow-up of casings in torque cycles (TC)
EFFECTIVITY: (B1, B2) Helicopters equipped with a MGB
sump with a Part Number specified in paragraph 4.A.
MGB bottom
casing P/N
350A32-3119-
03 installed.
N/A PAD 15-105
165FH/6M
from 2015-06-
02
2015-12-04:
The recorded
TC on MGB
sump is
34216 /FH is
5270,2. No
further
action is
required until
TC has
reached
93700 (PHAB
WO
17220006).
63 N/A 01.00.68 - 1 2015-07-28
LIMITATIONS - Main Gearbox (MGB) Casings -
Limitations and follow-up of casings in torque cycles (TC)
EFFECTIVITY: (B3) Helicopters equipped with MGB
casings (main casing assembly and MGB sump) with Part
Numbers specified in paragraph 4.A.
Applicable to
AS350 B3N/A PAD 15-104
65 y - 65.00.43 1 2015-07-15
TAIL ROTOR DRIVE - Tail rotor pich change plate - four
contact bearing
EFFECTIVITY: (B, BA, BB, B1, B2, D, L1) Helicopters PRE
MOD 076550
Recommende
dN/A
Rev 0
performed
2009-02-19
.076550 NO
65 N/A - 65.00.41 3 2015-07-15
TAIL ROTOR DRIVE - Tail rotor pich change plate - four
contact bearing
EFFECTIVITY: (B3) Helicopters PRE MOD 076550
Recommende
dN/A
Applicable to
AS350 B3.076550
63 OPT - 63.00.23 0 2015-07-15
MAIN ROTOR DRIVE - Modification of material and
position of MGB intake O-ring
EFFECTIVITY: (B, B1, B2, B3, BA, BB, D, L1) Helicopters
PRE MOD 077240
OPTIONAL N/A .077240
32 OPT - 32.00.11 3 2015-06-24
LANDING GEAR - L/G skids - Reinforced wear plates for
skid L/G
EFFECTIVITY: (B, BA, BB, B1, B2, B3, D, L1) Helicopter(s)
equipped with L/G skids P/N 350A41-1016-XX or 350A41-
1079-XX PRE MOD 072610 or POST MOD 072610 (anti-
gravel paint on landings), PRE MOD 072111 or post
MOD 072111 (skids equipped with long wear plates),
with reinforced wear plates PRE MOD OP 3376
OPTIONAL N/A OP3376
- -159-036-
002015-06-22
Load Cell Torsional Fatigue Failure
Applicability: Helicopter models AS350, AS355, EC130,
Bell 206L and Bell 407 with an Onboard Systems
superseded load cell installed per Table 1 in Onboard
Systems SB 159-036-00.
Recommende
dN/A
N/A. STC
SR01164SE,
SR01393SE,
SH1262NW,
SR01812SE
not installed.
100FH
55 Y - 55.00.18 0 2015-06-22
STABILIZER - Horizontal stabilizer - Improvement of the
Stabilizer / Tail Boom Fittings interface
EFFECTIVITY: (B, BA, BB, B1, B2, B3, D, L1) Helicopters
PRE MOD 074643
Recommende
dN/A .074643
28 N/A - 28.00.21 0 2015-06-22
FUEL - DISTRIBUTION - Integration of a relay in the fuel
pump control circuit
EFFECTIVITY: (B2, B3) Helicopters POST MOD 073273
and PRE MOD 074280 and 350A084578.00
Recommende
dN/A
MOD 073273
not
embodied.
350A084578.00
25 N/A - 25.02.40 0 2015-06-18
EQUIPMENT AND FURNISHINGS - External load carrying -
Improved locking system of the LISI AS21-5-7 cargo hook
EFFECTIVITY: (B2, B3) Helicopters equipped with the
fixed parts of cargo hook assembly P/N 704A418110.29
(MP/N AS21-5-7)
Recommende
dN/A
No cargo
hook
installed.
67 N/A 05.00.64 - 1 2015-06-18
TIME LIMITS - MAINTENANCE CHECKS - Tail rotor control
- Checking the locking of the stop screws of the yaw
flight controls
EFFECTIVITY: (B, B1, B2, B3, BA, BB, D) AS350
helicopters equipped with adjustable primary yaw stop
in the luggage compartment. Which embody one of the
following modifications: 071908, 071912, 073252. But
do not embody modification 074602.
Compliance
with ASB
67.00.61
cancels the
inspections
issued by this
ASB.
N/A PAD 15-087 110FH - 110FH
67 N/A 67.00.61 - 0 2015-06-18
ROTOR FLIGHT CONTROLS - Installation of dual
mechanical safetying on primary yaw stops
EFFECTIVITY: (B, B1, B2, B3, BA, BB, D) AS350
helicopters equipped with adjustable primary yaw stop
in the luggage compartment. Which embody one of the
following modifications: 071908, 071912, 073252. But
do not embody modification 074602.
Compliance
with this ASB
cancels the
mandatory
scheduled
inspection
introduced by
ASB 05.00.64.
N/A PAD 15-087
660FH/13M
from 2015-06-
18
.074602
63 N/A - 63.00.22 0 2015-06-16
MAIN ROTOR DRIVE - Engine-to-MGB coupling - New
drive bearing of the hydraulic pump on dual hydraulic
helicopters
EFFECTIVITY: (B3) . Dual hydraulic helicopters (POST
MOD OP3346 or OP3082) POST MOD 079566 and PRE
MOD 079568
Recommended N/A 2016-07-16Applicable to
AS350 B3.079568 NO
76 N/A 05.00.77 - 1 2015-06-15
TIME LIMITS - MAINTENANCE CHECKS - Twist grip -
Checking and ensuring water-tightness of connectors on
microswitches 53Ka, 53Kb and 65K (IDLE/FLIGHT modes)
EFFECTIVITY: (B3) ARRIEL 2D engine (MOD 07-4302).
Applicable to
AS350 B3N/A 10FH/7D - .074699
76 N/A 05.00.61 - 3 2015-06-15
ENGINE CONTROLS- Twist grip - Functional check and
installation of a protection for microswitches 53Ka and
53Kb and 65K (IDLE/FLIGHT mode)
EFFECTIVITY: (B3) ARRIEL 2B1 engine associated with
the two-channel FADEC POST MOD 073261 (new twist
grip).
Applicable to
AS350 B3N/A 10FH/7D - .074699
25 N/ASIN 2829-
S-25- 2 2015-06-15
EQUIPMENT AND FURNISHINGS - REMINDER: Rupture of
the restraint system buckle cover
EFFECTIVITY: Type 198 & 284 ZODIAC seats
No Zodiac
Seats
installed.
2014-0127 2015-07-02
63 N/A 01.00.68 - 0 2015-06-02
LIMITATIONS - Main Gearbox (MGB) Casings - Limitation
and follow-up of casings in torque cycles (TC)
EFFECTIVITY: (B3) Helicopters equipped with a MGB
sump with a Part Number: 350A32-3156-21, 350A32-
3156-22, 350A32-3121-04, 350A32-3121-06 or 350A32-
3119-05
Applicable to
AS350 B3N/A -
63 N/A 01.00.69 - 0 2015-06-02
LIMITATIONS - Main Gearbox (MGB) Casings - Limitation
and follow-up of casings in torque cycles (TC)
SUPERSEDED BY REV 1
EFFECTIVITY: Helicopters equipped with a MGB sump
with a Part Number: 350A32-3119-03 or 350A32-3119-
05
MGB bottom
casing P/N
350A32-3119-
03 installed.
N/A -20000FH/
93700TC-
20000FH/
93700TC
63 Y 05.00.84 - 0 2015-05-21
TIME LIMITS - MAINTENANCE CHECKS - Main rotor drive -
Periodic inspection of bi-directional suspension cross-bar
P/Nos. 350A381040.20 and 350A381040.00
EFFECTIVITY: Helicopters equipped with a bi-directional
suspension cross-bar with one of the following Part
Numbers: 350A38-1040-20 or 350A38-1040-00.
MGB
suspension
cross bar P/N
350A38-1040-
20 installed.
N/A 2015-0094
Next MGB
removal ->
every
4500FH/
60000TC
Perf 2015-11-
21 by PHAB
iaw WO
17220006.
Next insp:
9770,2FH /
94216TC.
-4500FH/
60000TC
29 Y - 29.00.18 0 2015-05-11
HYDRAULIC POWER GENERATION - Collective Lever -
Installation or replacement of relay 47D.
EFFECTIVITY: (B, BA, BB, B1, B2, B3, D, L1) Single
hydraulic helicopters PRE MOD 074688
Recommende
dN/A .074688
25 N/A - 25.02.38 0 2015-05-11
EQUIPMENT AND FURNISHINGS - Front Seats - Restoring
conformity of ZODIAC AEROSPACE 198-series seat
buckets
EFFECTIVITY: (B2, B3)
Recommende
dN/A
150FH/ 3M
from 2015-04-
14
No Zodiac
Seats
installed.
- NO
33 N/A 33.00.33 - 1 2014-11-17
LIGHTS - Position lights - Protection of the power supply
unit of the optional equipment "position strobe lights" -
Corresponds to modification 074611
EFFECTIVITY: (B, BA, BB, B1, B2, B3, D) . Helicopters: -
which embody modification OP0811 (installation of
position strobe lights on the horizontal stabilizer) and -
equipped with GRIMES - HONEYWELL power supply unit
Part Number (MP/N) 60-1431-3 of the optional position
strobe light equipment and - which do not embody at
least one of the following modifications: - 074611
(installation of a protector assembly on the wires and
power supply unit of the optional position strobe light
equipment), - 350P085326 (installation and protection
of a Wulfsberg RT5000 AM/FM multi-band tactical wide
band radio), - 073274 (replacement of fuses with circuit-
breakers), - OP1882 (installation of air conditioning), -
OP2698 (replacement of Freon R12).
ASB
05.00.662013-0281R1
660FH/13M
from 2013-11-
20
2015-04-10
N/A. MOD
OP0811 not
embodied.Ho
neywell pwr
suppl unit
not installed.
.074611
63 N/A 63.00.24 - 0 2014-10-21
MAIN ROTOR DRIVE - Engine-to-MGB coupling - New
hydraulic pump drive bearing - Corresponds to
modification 079568
EFFECTIVITY: (B, BA, BB, B1, B2, B3, D) . Helicopters
equipped with a single hydraulic system and a hydraulic
pump drive assembly P/N 350A35-0132-00 (POST MOD
079566 and PRE MOD 079568).
N/A 2014-0233 2015-06-30
2015-04-10
N/A. Bearing
not installed.
H/C too old
.079568
25 N/A 25.00.79 - 1 2014-05-21
EQUIPMENT AND FURNISHINGS - BREEZE 300 lb. (136
kg) ELECTRIC HOIST INSTALLATION Failure of the
Pyrotechnic Squib Control to Operate - Corresponds to
MOD 07 3190
EFFECTIVITY: (B,BA,BB,B1,B2,B3,D) . Aircraft equipped
with optional BREEZE or TRW (or LUCAS or Air
Equipement) 300 lb. electric hoist and hoist operator's
control unit 26M, P/N 350A63-1136-00.
Aircraft
equipped
with
BREEZE or
TRW (or
LUCAS or
Air
Equipeme
nt) 300 lb.
electric
hoist fixed
parts pre
modificati
on 07
3190.
100FH/2M
550FH/12M
from 2014-05-
22
Hoist not
installed..073190
62 Y 62.00.34 - 0 2014-04-28
MAIN ROTOR - Swashplates - Check of the rotating star
EFFECTIVITY: (B, BA, BB, B1, B2, B3, D) . On helicopters
equipped with a swashplate assembly comprising a
rotating star with Part Number (MP/N) 350A371003-04, -
05, -06, -07 or -08.
N/A 2014-0132R1
165FH eller
senast 2014-
12-31
2015-04-10
P/N affected,
but repair
not
performed =
AD N/A. Test
iaw ASB
performed
2015-11-21
iaw PHAB
WO1722000
6 to confirm.
N/A
52 N/A 52.00.35 - 0 2014-04-03
DOORS - Crew doors - Check of the installation of the
crew door actuators
EFFECTIVITY: On crew door actuators on helicopters
equipped with the emergency flotation gear.
Emergency
flotation gearN/A
53 N/AEASB
05.00.70- 0 2014-03-24
TIME LIMITS - MAINTENANCE CHECKS - Rear structure -
Check of the rear frame reinforcement angles
EFFECTIVITY: Helicopters fitted with a rear structure /
tail boom junction frame, repaired or reinforced with at
least one reinforcement angle on the RH side as per
MRM Work Card 53.10.22.772 or AMM Task 53-31-00, 8-
5 or which embody MOD 073215.
PRE MOD
073215.N/A 2014-0076-E 165FH
73 N/A 01.00.67 - 2 2014-02-17
LIMITATION - FUEL SYSTEM AND CHECK - FADEC - Flight
manual procedure
EFFECTIVITY: AS350 B3 helicopters equipped with an
ARRIEL 2D engine and THALES FADEC P/N C13165DA00
or C13165DA00PC00 or C13165FA00, including all
amendments.
AS350 B3 N/A
71 N/A 71.00.36 - 0 2014-01-15
POWER PLANT - Air intake - Air intake draining on
helicopters equipped with the ARRIEL 1 engine -
Corresponds to modification 350A081080
EFFECTIVITY: Helicopters equipped with engine air
intakes with the following part numbers (MP/N): -
350A54-1080-00 (AS350 B), - 350A54-1080-01 (AS350 B,
B1 and L1), and which do not embody modification
071537 .
071537
embodied.N/A
67 N/A 67.00.43 - 2 2013-11-28
ROTOR FLIGHT CONTROLS - Modification to the electrical
operation of the twist grip for ARRIEL 2B engines -
Corresponds to modification 073357
EFFECTIVITY: Helicopters equipped with the Arriel 2B
engine and modification configuration combination in
accordance with table hereafter: see ASB
ARRIEL 1D1
installed.
H/Cs pre-
MOD
072817
shall
embody SB
33.00.19
previously.
33 N/A 33.00.33 - 0 2013-11-20
LIGHTS - Position lights - Protection of the power supply
unit of the optional equipment "position strobe lights" -
Corresponds to modification 074611
EFFECTIVITY: (B, BA, BB, B1, B2, B3, D) . Helicopters: -
embodying modification OP0811 and equipped with the
GRIMES - HONEYWELL power supply unit MP/N 60-1431-
3 of the optional equipment “position strobe lights”, and -
embodying neither modification 074611 nor
modification 350P085326 (installation and protection of
a Wulfsberg RT5000 multi-band AM/FM hyper-
broadband tactical radio, located in the baggage
compartment).
SUPERSEDED
BY REV 1
ASB
05.00.66
2015-04-10
N/A. MOD
OP0811 not
embodied.Ho
neywell pwr
suppl unit
not installed.
.074611
80 N/A 80.00.09 - 1 2013-08-13
ENGINE STARTING - Improving twist grip operational
logic - Corresponds to MOD 074263
EFFECTIVITY: (B3) . Helicopters equipped with ARRIEL
2B1 engine (MOD 073254), post-MOD 073261 and pre-
MOD 074263.
ARRIEL 1D1
installed.N/A
80
24Y - 05.00.75 0 2013-04-11
ENGINE STARTING - Starter control - Periodic adjustment
and check of the tensioning of the SKURKA (ex APC)
starter-generator damper system
EFFECTIVITY: Helicopters equipped with SKURKA (ex
APC) starter-generator part number (MP/N) 150SG122Q
or 200SGL130Q
N/A 600FH
Perf 2015-11-
30 iaw PHAB
WO1722000
6. Next insp:
A/CTT 5870,2
600FH
52 N/A 52.00.34 - 0 2012-07-09
DOORS - Sliding Door - Double locking of the sliding door
lower ball-joint bolt - Corresponds to modification AL.
4262
EFFECTIVITY: (B, B1, B2, B3, BA, BB, D) . Helicopters
equipped with sliding doors which do not embody
modification AL. 4262 .
N/A 2012-0205
165FH/13M
from 2012-07-
09
Sliding doors
not installed.AL. 4262
67 YEASB
05.00.58- 0 2008-12-01
Time Limits – Maintenance Checks - Collective pitch lever
locking stud
EFFECTIVITY: Helicopters delivered before modification
073175, or - helicopters on which work has been carried
out in service on the locking studs or on the collective
pitch levers or on the locking strips, or - helicopters
having been subject to compliance with Revision 0 or
Revision 1 of Service Bulletins No. 67.00.37 (AS350) or
No. 67.00.19 (AS550), corresponding to modification
073237, or - helicopters with a serial number equal to:
3972-3973-3982-3987-4003-4023-4046-4050-4086-
4120-4122-4132-4143-4152-4172-4194-4259-4314-
4324-4378-4392-4447-4452-4477-4489-4490-4501-
4523-4546-4560-4589-4594-4599-4632-4659-4666-
4671
SB 67.00.37
embodied by
PHAB
WO17220006
2015-11-21.
N/A
Performed
2015-11-21
iaw PHAB
WO
17220006.
Next insp:
A/CTT 5930,2
/ 2017-11-21
660FH /
2Y
53
55Y - 05.00.53 0 2007-05-25
TIME LIMITS - Maintenance Checks - Check of the upper
and lower fin spar attachment frame and screws
assembly
EFFECTIVITY: Upper and lower fin spar attachment
frame and screws assembly.
N/ANext T
inspection
Perf 2015-11-
30 iaw PHAB
WO1722000
6 at A/CTT
5270,2.
Every T
insp
67 YEASB
67.00.3967.00.39 1 2007-03-26
ROTOR FLIGHT CONTROLS - Load Compensator Lever
EFFECTIVITY: (B1, B2, BB) Helicopters equipped with a
load compensator fitted with a lever that was replaced
after delivery.
N/A
2015-12-03:
PHAB
WO1722000
6: Load
compensator
lever verfied
to be correct
during
inspection of
checking the
yaw control
travel.
-
53 y 05.00.43 - 0 2004-02-03
TIME LIMITS - MAINTENANCE CHECKS - REAR
STRUCTURE - Check of the Rear Frame
EFFECTIVITY: Rear structure / tail boom junction frame: -
pre-MOD 073215, or - not equipped with the four
reinforcement angles, P/Nos. 350A08.2493.20 /.21 /.22
/.23, following the repair carried out in accordance with
MRM Work Card 53.10.22.772.
PRE MOD
073215.N/A F-2004-035
Performed
2015-11-21
iaw PHAB
WO
17220006.
Next insp:
A/CTT 5820,2
550FH
29 Y29.00.04
R1- 1 2004-01-27
HYDRAULIC POWER - Lubrification of the Splines on the
Hydraulic Pump Drive Shaft (§ 2.B.3. Lubrication of the
drive shaft splines = recurrent)
Effectivity: (B,BA,BB,B1,B2,B3,D) Hydraulic pump drive
shaft.
N/A -Every
110FH/6M
Perf 2015-11-
21 iaw PHAB
WO1722000
6. Next insp:
A/CTT 5380,2
/ 2016-05-21
.079547 110FH/6M
.05 Y - 05.00.32 2000-08-01
TIME LIMITS - Corrosion check and corrosion prevention
at the lower bearing and on the splines of the main rotor
shaft.
EFFECTIVITY: Main rotor shafts P/N: 350A37-1076-00 to
12 pre and post MOD 076202, 350A37-1290-00 to 05
pre and post MOD 076201.
Shaft P/N
350A37-1290-
03 installed.
N/ANext planet
gear removal
Performed
2015-11-21
PHAB WO
17220006.
Next insp:
2021-11-21
6Y / Every
planet
gear
carrier
removal
62 Y 62.00.22 - 0 1994-03-18
MAIN ROTOR - Spring type vibration damper
Effectivity: AS 350 Helicopters, versions: B, BA, B1, B2, L1
PRE MOD 350A07-6199
N/A - 500FH
1995-03-16
perf on
Antivibration
damper S/N
M715. 2001-
10-29
Accomplishe
d A/CTT
1330,3
350A08-0720 NO
62 Y 62.00.21 - 1 1993-03-09
MAIN ROTOR - Pitch-change lever bushes
EFFECTIVITY: (B, BA, D, B1, B2, L1) PItch-change lever
P/N 350A31-1877-02 not marked wIth an X, and S/N
lower than 100.000.
N/A -
Perf 2015-12-
03 by PHAB,
WO1722000
2 at A/CTT
5270,2.
- NO
MOD A/CTT SB AD DATE Note
AL-4236 5270,2 34.00.20 2015-10-09 N/A. B3 model only.
AL.4262 5270,2 52.00.34 2015-10-09 N/A. Equipment not installed.
OP0124 0 1990-07-31
OP0136 0 1990-07-31
OP0177 0 1990-07-31
OP0223 0 1990-07-31
OP0235 0 1990-07-31
OP0237 0 1990-07-31
OP0303 0 1990-07-31
OP0370 0 1990-07-31
OP0403 0 1990-07-31
OP0419 0 1990-07-31
OP0464 0 1990-07-31
OP0471 0 1990-07-31
OP0472 0 1990-07-31
OP0544 0 1990-07-31
OP0626 0 1990-07-31
OP0649 0 1990-07-31
OP0650 0 1990-07-31
OP0651 0 1990-07-31
OP0664 0 1990-07-31
OP0699 0 1990-07-31
OP0710 0 1990-07-31
OP07200
2230,601.00.51
1990-07-31
2006-05-03
OP0910 0 1990-07-31
OP1045 0 1990-07-31
OP1751 0 1990-07-31
OP3376 32.00.11 2015-10-09 OPTIONAL. Not embodied.
350PO84960 2230,6 ASB25.00.80 2006-05-03
070001 0 1990-07-31
070002 0 1990-07-31
070003 0 1990-07-31
070004 0 1990-07-31
070007 0 1990-07-31
070009 0 1990-07-31
070010 0 1990-07-31
070011 0 1990-07-31
070012 0 1990-07-31
070013 0 1990-07-31
070014 0 1990-07-31
070015 0 1990-07-31
070016 0 1990-07-31
070017 0 1990-07-31
070018 0 1990-07-31
070019 0 1990-07-31
070020 0 1990-07-31
070021 0 1990-07-31
070022 0 1990-07-31
070023 0 1990-07-31
070024 0 1990-07-31
070025 0 1990-07-31
070027 0 1990-07-31
070028 0 1990-07-31
070029 0 1990-07-31
070030 0 1990-07-31
070031 0 1990-07-31
070032 0 1990-07-31
070033 0 1990-07-31
070034 0 1990-07-31
070035 0 1990-07-31
070036 0 1990-07-31
070037 0 1990-07-31
070038 0 1990-07-31
070039 0 1990-07-31
070040 0 1990-07-31
070042 0 1990-07-31
070043 0 1990-07-31
070044 0 1990-07-31
070045 0 1990-07-31
070047 0 1990-07-31
070048 0 1990-07-31
070049 0 1990-07-31
070050 0 1990-07-31
070051 0 1990-07-31
070052 0 1990-07-31
070053 0 1990-07-31
070054 0 1990-07-31
070055 0 1990-07-31
070056 0 1990-07-31
070057 0 1990-07-31
070058 0 1990-07-31
070059 0 1990-07-31
070060 0 1990-07-31
070061 0 1990-07-31
070064 0 1990-07-31
070065 0 1990-07-31
070066 0 1990-07-31
070068 0 1990-07-31
070070 0 1990-07-31
070071 0 1990-07-31
070072 0 1990-07-31
070073 0 1990-07-31
070075 0 1990-07-31
070076 0 1990-07-31
070078 0 1990-07-31
070079 0 1990-07-31
070080 0 1990-07-31
070081 0 1990-07-31
070083 0 1990-07-31
070084 0 1990-07-31
070085 0 1990-07-31
070086 0 1990-07-31
070088 0 1990-07-31
070090 0 1990-07-31
070092 0 1990-07-31
070093 0 1990-07-31
070094 0 1990-07-31
070100 0 1990-07-31
070101 0 1990-07-31
070102 0 1990-07-31
070103 0 1990-07-31
070104 0 1990-07-31
070107 0 1990-07-31
070109 0 1990-07-31
070110 0 1990-07-31
070112 0 1990-07-31
070113 0 1990-07-31
070114 0 1990-07-31
070115 0 1990-07-31
070117 0 1990-07-31
070119 0 1990-07-31
070120 0 1990-07-31
070121 0 1990-07-31
070123 0 1990-07-31
070125 0 1990-07-31
070126 0 1990-07-31
070129 0 1990-07-31
070130 0 1990-07-31
070131 0 1990-07-31
070133 0 1990-07-31
070135 0 1990-07-31
070138 0 1990-07-31
070141 0 1990-07-31
070142 0 1990-07-31
070147 0 1990-07-31
070148 0 1990-07-31
070156 0 1990-07-31
070158 0 1990-07-31
070160 0 1990-07-31
070161 0 1990-07-31
070162 0 1990-07-31
070164 0 1990-07-31
070165 0 1990-07-31
070181 0 1990-07-31
070183 0 1990-07-31
070184 0 1990-07-31
070185 0 1990-07-31
070186 0 1990-07-31
070187 0 1990-07-31
070188 0 1990-07-31
070189 0 1990-07-31
070193 0 1990-07-31
070194 0 1990-07-31
070197 0 1990-07-31
070198 0 1990-07-31
070199 0 1990-07-31
070200 0 1990-07-31
070201 0 1990-07-31
070207 0 1990-07-31
070208 0 1990-07-31
070212 0 1990-07-31
070213 0 1990-07-31
070214 0 1990-07-31
070215 0 1990-07-31
070230 0 1990-07-31
070232 0 1990-07-31
070241 0 1990-07-31
070260 0 1990-07-31
070262 0 1990-07-31
070265 0 1990-07-31
070267 0 1990-07-31
070269 0 1990-07-31
070273 0 1990-07-31
070277 0 1990-07-31
070279 0 1990-07-31
070280 0 1990-07-31
070281 0 1990-07-31
070285 0 1990-07-31
070286 0 1990-07-31
0702890
2230,601.00.51
1990-07-31
2006-05-03
070290 0 1990-07-31
070291 0 1990-07-31
070292 0 1990-07-31
070293 0 1990-07-31
070294 0 1990-07-31
070298 0 1990-07-31
070299 0 1990-07-31
070300 0 1990-07-31
070301 0 1990-07-31
070302 0 1990-07-31
070306 0 1990-07-31
070309 0 1990-07-31
070314 0 1990-07-31
070316 0 1990-07-31
070318 0 1990-07-31
070320 0 1990-07-31
070323 0 1990-07-31
070324 0 1990-07-31
070325 0 1990-07-31
070326 0 1990-07-31
070327 0 1990-07-31
070332 0 1990-07-31
070333 0 1990-07-31
070334 0 1990-07-31
070335 0 1990-07-31
070336 0 1990-07-31
070337 0 1990-07-31
070338 0 1990-07-31
070342 0 1990-07-31
070343 0 1990-07-31
070344 0 1990-07-31
070345 0 1990-07-31
070346 0 1990-07-31
070348 0 1990-07-31
070349 0 1990-07-31
070351 0 1990-07-31
070352 0 1990-07-31
070357 0 1990-07-31
070358 0 1990-07-31
070362 0 1990-07-31
070363 0 1990-07-31
070364 0 1990-07-31
070365 0 1990-07-31
070367 0 1990-07-31
070368 0 1990-07-31
070376 0 1990-07-31
070377 0 1990-07-31
070378 0 1990-07-31
070379 0 1990-07-31
070380 0 1990-07-31
070381 0 1990-07-31
070382 0 1990-07-31
070383 0 1990-07-31
070388 0 1990-07-31
070390 0 1990-07-31
070392 0 1990-07-31
070394 0 1990-07-31
070398 0 1990-07-31
070399 0 1990-07-31
070400 0 1990-07-31
070401 0 1990-07-31
070404 0 1990-07-31
070405 0 1990-07-31
070406 0 1990-07-31
070407 0 1990-07-31
070408 0 1990-07-31
070409 0 1990-07-31
070410 0 1990-07-31
070411 0 1990-07-31
070412 0 1990-07-31
070413 0 1990-07-31
070414 0 1990-07-31
070415 0 1990-07-31
070417 0 1990-07-31
070420 0 1990-07-31
070421 0 1990-07-31
070422 0 1990-07-31
070423 0 1990-07-31
070427 0 1990-07-31
070428 0 1990-07-31
070429 0 1990-07-31
070430 0 1990-07-31
070433 0 1990-07-31
070434 0 1990-07-31
070438 0 1990-07-31
070440 0 1990-07-31
070441 0 1990-07-31
070442 0 1990-07-31
070443 0 1990-07-31
070444 0 1990-07-31
070446 0 1990-07-31
070447 0 1990-07-31
070449 0 1990-07-31
070451 0 1990-07-31
0704520
2230,601.00.51
1990-07-31
2006-05-03
070455 0 1990-07-31
070456 0 1990-07-31
070457 0 1990-07-31
070458 0 1990-07-31
070459 0 1990-07-31
070460 0 1990-07-31
070461 0 1990-07-31
070469 0 1990-07-31
070470 0 1990-07-31
070473 0 1990-07-31
070474 0 1990-07-31
070475 0 1990-07-31
070476 0 1990-07-31
070477 0 1990-07-31
070479 0 1990-07-31
070482 0 1990-07-31
070483 0 1990-07-31
070484 0 1990-07-31
070485 0 1990-07-31
070486 0 1990-07-31
070488 0 1990-07-31
070489 0 1990-07-31
070490 0 1990-07-31
070491 0 1990-07-31
070494 0 1990-07-31
0704980
2230,601.00.51
1990-07-31
2006-05-03
070499 0 1990-07-31
070500 0 1990-07-31
070503 0 1990-07-31
070504 0 1990-07-31
070509 0 1990-07-31
070511 0 1990-07-31
070515 0 1990-07-31
070516 0 1990-07-31
070518 0 1990-07-31
070522 0 1990-07-31
070523 0 1990-07-31
070524 0 1990-07-31
070525 0 1990-07-31
070527 0 1990-07-31
070530 0 1990-07-31
070531 0 1990-07-31
070532 0 1990-07-31
070533 0 1990-07-31
070534 0 1990-07-31
070535 0 1990-07-31
070538 0 1990-07-31
070541 0 1990-07-31
070542 0 1990-07-31
070549 0 1990-07-31
070550 0 1990-07-31
070551 0 1990-07-31
070557 0 1990-07-31
070558 0 1990-07-31
070559 0 1990-07-31
070564 0 1990-07-31
070566 0 1990-07-31
070569 0 1990-07-31
070572 0 1990-07-31
070582 0 1990-07-31
070583 0 1990-07-31
070584 0 1990-07-31
070585 0 1990-07-31
070586 0 1990-07-31
070590 0 1990-07-31
070591 0 1990-07-31
070592 0 1990-07-31
070600 0 1990-07-31
070601 0 1990-07-31
070602 0 1990-07-31
070608 0 1990-07-31
070609 0 1990-07-31
070611 0 1990-07-31
070612 0 1990-07-31
070613 0 1990-07-31
0706150
2230,601.00.51
1990-07-31
2006-05-03
070616 0 1990-07-31
070620 0 1990-07-31
070621 0 1990-07-31
070622 0 1990-07-31
070667 0 1990-07-31
070669 0 1990-07-31
070675 0 1990-07-31
070677 0 1990-07-31
070679 0 1990-07-31
070682 0 1990-07-31
070683 0 1990-07-31
070689 0 1990-07-31
070695 0 1990-07-31
070697 0 1990-07-31
070698 0 1990-07-31
070700 0 1990-07-31
070706 0 1990-07-31
070708 0 1990-07-31
070709 0 1990-07-31
070717 0 1990-07-31
070719 0 1990-07-31
070721 0 1990-07-31
070732 0 1990-07-31
0707330
2230,601.00.51
1990-07-31
2006-05-03
070744 0 1990-07-31
070745 0 1990-07-31
070747 0 1990-07-31
070748 0 1990-07-31
070750 0 1990-07-31
070756 0 1990-07-31
070762 0 1990-07-31
070766 0 1990-07-31
070773 0 1990-07-31
070780 0 1990-07-31
070781 0 1990-07-31
070782 0 1990-07-31
070787 0 1990-07-31
070792 0 1990-07-31
070795 0 1990-07-31
070796 0 1990-07-31
070799 0 1990-07-31
070802 0 1990-07-31
0708040
2230,601.00.51
1990-07-31
2006-05-03
070805 0 1990-07-31
070810 0 1990-07-31
070812 0 1990-07-31
070815 0 1990-07-31
070817 0 1990-07-31
070818 0 1990-07-31
070821 0 1990-07-31
070823 0 1990-07-31
070826 0 1990-07-31
070832 0 1990-07-31Partial installation of SBR type SARMA rod. - Drawing
embodied. 350P08336922. - Aft transmission flange installed
flange AU4G1T6. 350A34102320. Called out by AMS 079029.
070838 0 1990-07-31
070854 0 1990-07-31
070858 0 1990-07-31
070859 0 1990-07-31
070862 0 1990-07-31
070863 0 1990-07-31
070866 0 1990-07-31
070868 0 1990-07-31
070887 0 1990-07-31
070893 0 1990-07-31
070895 0 1990-07-31
0709000
2230,601.00.51
1990-07-31
2006-05-03
070918 0 1990-07-31
070921 0 1990-07-31
070922 0 1990-07-31
070923 0 1990-07-31
070927 0 1990-07-31
070929 0 1990-07-31
070944 0 1990-07-31
070948 0 1990-07-31
070949 0 1990-07-31
070952 0 1990-07-31
070955 0 1990-07-31
070959 0 1990-07-31
070963 0 1990-07-31
070971 0 1990-07-31
070979 0 1990-07-31
071000 0 1990-07-31
071007 0 1990-07-31
071008 0 1990-07-31
071011 0 1990-07-31
071017 0 1990-07-31
071025 0 1990-07-31
0710460
2230,601.00.51
1990-07-31
2006-05-03
0710470
2230,601.00.51
1990-07-31
2006-05-03
0710500
2230,601.00.51
1990-07-31
2006-05-03
071051 0 1990-07-31
071058 0 1990-07-31
071063 0 1990-07-31
071065 0 1990-07-31
071068 0 1990-07-31
071073 0 1990-07-31
071083 0 1990-07-31
071093 0 1990-07-31
071096 0 1990-07-31
071098 0 1990-07-31
071103 0 1990-07-31
071113 0 1990-07-31
071115 0 1990-07-31
071138 0 1990-07-31
0711560
2230,601.00.51
1990-07-31
2006-05-03
071175 0 1990-07-31
071182 0 1990-07-31
071209 0 1990-07-31
071210 0 1990-07-31
0712110
2230,601.00.51
1990-07-31
2006-05-03
Bevel reduction gear M1624 1990-04-27
TGB M907 2008-10-06
071222 0 1990-07-31 Main Rotor Mast M456 1990-04-27
071243 0 1990-07-31
071244 0 1990-07-31
071269 0 1990-07-31
071270 0 1990-07-31
071278 0 1990-07-31
071286 0 1990-07-31
071295 0 1990-07-31
071306 0 1990-07-31
0713180
2230,601.00.51
1990-07-31
2006-05-03
0713230
2230,601.00.51
1990-07-31
2006-05-03
071324 0 1990-07-31
071344 0 1990-07-31
071348 0 1990-07-31
071354 0 1990-07-31
071357 0 1990-07-31
071364 0 1990-07-31
071365 0 1990-07-31
071392 0 1990-07-31
071393 0 1990-07-31
071395 0 1990-07-31
071398 0 1990-07-31
071412 0 1990-07-31
071413 0 1990-07-31
071414 0 1990-07-31
071417 0 1990-07-31
071429 0 1990-07-31
071437 0 1990-07-31
071438 0 1990-07-31
0714470
2230,601.00.51
1990-07-31
2006-05-03
071474 0 1990-07-31
071502 0 1990-07-31
071504 0 1990-07-31
071506 0 1990-07-31
071520 0 1990-07-31
071534 0 1990-07-31
0715370
2230,601.00.51
1990-07-31
2006-05-03
071539 0 1990-07-31
071549 0 1990-07-31
071570 0 1990-07-31
071580 2230,601.00.51
01.00.502006-05-03
071581 0 1990-07-31
071583 0 1990-07-31
0715910
2230,601.00.51
1990-07-31
2006-05-03
071602 0 1990-07-31
071609 0 1990-07-31
0716160
2230,601.00.51
1990-07-31
2006-05-03
071624 0 1990-07-31
0716270
2230,601.00.51
1990-07-31
2006-05-03
071629 0 1990-07-31
071651 0 1990-07-31
071659 0 1990-07-31
071660 0 1990-07-31
071665 2230,601.00.51
01.00.502006-05-03
0716670
2230,601.00.51
1990-07-31
2006-05-03
071671
0
1330,3
2230,6
.
28.00.07R1
01.00.51
1990-07-31
2001-10-29
2006-05-03
071674 0 1990-07-31
0716780
2230,601.00.51
1990-07-31
2006-05-03
0716860
2230,601.00.51
1990-07-31
2006-05-03
071688 0 1990-07-31
071691 0 1990-07-31
071699 2230,6 01.00.51 2006-05-03
0717010
2230,601.00.51
1990-07-31
2006-05-03
071703 2230,6
01.00.35
53.00.18
01.00.51
2006-05-03
071704 0 1990-07-31
071705 0 1990-07-31
071709 2230,601.00.35
01.00.512006-05-03
0717130
2230,601.00.51
1990-07-31
2006-05-03
071719 0 1990-07-31
0717210
2230,601.00.51
1990-07-31
2006-05-03
071726 0 1990-07-31
071727 0 1990-07-31
071733 0 1990-07-31
071735 0 1990-07-31
071736 0 1990-07-31
071737 0 1990-07-31
0717400
2230,601.00.51
1990-07-31
2006-05-03
071753 2230,601.00.51
01.00.502006-05-03
0717550
2230,601.00.51
1990-07-31
2006-05-03
071773 0 1990-07-31
071778 0 1990-07-31
071781 0 1990-07-31
071782 0 1990-07-31
0717980
2230,601.00.50
1990-07-31
2006-05-03
071806 0 1990-07-31
0718130
2230,601.00.51
1990-07-31
2006-05-03
071814 0 1990-07-31
071815 0 1990-07-31
071818 0 1990-07-31
071820 0 1990-07-31
071822 0 1990-07-31
0718260
2230,601.00.51
1990-07-31
2006-05-03
071830 0 1990-07-31
071834 0 1990-07-31
071835 0 1990-07-31
071841 0 1990-07-31
071842 2230,628.00.10
01.00.512006-05-03
071848 0 1990-07-31
071852 0 1990-07-31
071855 0 1990-07-31
071865 0 1990-07-31
071883 0 1990-07-31
071884 0 1990-07-31
071891 0 1990-07-31
071894 0 1990-07-31
071900 0 1990-07-31
071902 0 1990-07-31
071907 0 1990-07-31
071922 0 1990-07-31
071923 0 1990-07-31
071927 0 1990-07-31
0719340
2230,601.00.51
1990-07-31
2006-05-06
071941 0 1990-07-31
071942 0 1990-07-31
071952 0 1990-07-31
0719530
2230,601.00.51
1990-07-31
2006-05-06
071954 0 1990-07-31
071955 2230,6 01.00.51 2006-05-03
071966 2230,639.00.04
01.00.512006-05-03
071967 0 1990-07-31
071969 0 1990-07-31
071971 0 1990-07-31
071973 0 1990-07-31
071978 0 1990-07-31
071980 0 1990-07-31
071981 0 1990-07-31
071982 0 1990-07-31
071986 2230,601.00.51
52.00.212006-05-03
071988 0 1990-07-31
071989 0 1990-07-31
0719950
.
.
67.00.16R2
.
2007-0289
1990-07-31
2008-02-25
.
N/A to B2
072016 0 1990-07-31
072056 2230,6 01.00.51 2006-05-03
072058 2230,6 01.00.50 2006-05-03
072201 2230,6 01.00.51 2006-05-03
072204 2230,601.00.51
52.00.212006-05-03
072205 0 1990-07-31
072208 2230,601.00.51
01.00.502006-05-03
072213 0 1990-07-31
072214 2230,601.00.51
01.00.502006-05-03
072225 0 1990-07-31
072226 0 1990-07-31
072230 2230,601.00.51
01.00.502006-05-03
072239 2230,639.00.04
01.00.512006-05-03
072243 0 1990-07-31
072246 2230,601.00.50
01.00.512006-05-03
072248 0 1990-07-31
072255 0 1990-07-31
072259 0 1990-07-31
072270 0 1990-07-31
072276 0 1990-07-31
072279 0 1990-07-31
072385 2230,6 39.00.04 2006-05-03
072407 2230,601.00.51
01.00.502006-05-03
072460 2230,652.00.21
01.00.512006-05-03 SBT 52.00.21 NOTE: Upper striking plates removed
072475 2230,601.00.51
39.00.062006-05-03
072490 2230,6 01.00.35 2006-05-03
0725982230,6
2230,6
01.00.51
26.00.01
2006-05-03
2006-05-03
072660 2230,6 01.00.35 2006-05-03
072717 JAPAN Belt and Harness strip
072720 0 63.00.07 1990-07-31 FCW 2015-11-20 by PHAB.
072793 79.00.11 JAPAN
072840 33.00.17 2008-09-30 N/A. B3 model only.
073012 1330,3 05.00.31R1 2001-10-29 Accomplished.
073029 1729,1 05.00.36 2004-08-07 Verified.
0731183164
.
2008-01-28
2008-10-06
Bevel reduction gear M1624 2008-01-28
Oil Pump M1653 2008-01-28
TGB M907 2008-10-06
073139 1520,7 67.00.222003-04-23
2015-04-07
Verified.
SB performed. Verified by PHAB (JA)
073161 1520,7 53.00.31 2003-05-09 Verified.
073179 1330,3 67.00.24 F-2003-002(A) 2001-12-10 Accomplished.
073190 25.00.79 2015-10-09 N/A. Equipment not installed.
073195.
5270,2
31.00.52R1
31.00.52R2
2008-09-30
2015-10-09
N/A. B3 model only.
N/A. B3 model only.
073215 2015-11-30 Applicable. Not incorporated.
073219 71.00.18 2015-10-09 OPTIONAL. Not embodied.
073222 67.00.33 2008-09-30 N/A. B3 model only.
073226 24.00.11R1 2008-09-30 N/A to 1606-1 battery.
073237 5270,205.00.58
67.00.372015-11-21 Implemented by PHAB WO17220006.
073273 2012-02-27 Not incorporated.
073287 52.00.29 2008-08-22 N/A. Not installed.
073288 2420 55.00.12 2006-07-17
073290 52.00.29 2008-08-22 N/A. Not installed.
073298 52.00.30R1 2008-03-05 N/A. Equipment not installed.
073308 52.00.30R1 2008-03-05 N/A. Equipment not installed.
073325 53.00.34 2008-03-05 N/A. Equipment not installed.
073354 31.00.54 2008-09-30 N/A. B3 model only.
073370 24.00.13 2008-09-30 N/A. VEMD not installed.
073380 25.01.01 2008-09-30 N/A. Not installed.
073330 3914,4 55.00.16R1 2009-0030 2009-04-09
074346 26.00.02 2012-02-27 N/A. Mod 073273 not incorporated.
074602 67.00.61 2015-10-09 N/A
074611 33.00.33 2015-10-09 N/A
074643 55.00.18 2015-10-09 Applicable. Not incorporated.
074688 29.00.18 2015-10-09 Applicable. Not incorporated.
07469905.00.77
05.00.612015-10-09 N/A. B3 model only.
074715 23.00.06 2015-10-09 OPTIONAL. Not embodied.
075001 0 1990-07-31
075002 0 1990-07-31
075004 0 1990-07-31
075005 0 1990-07-31
075007 0 1990-07-31
075008 0 1990-07-31
075009 0 1990-07-31
075010 0 1990-07-31
075012 0 1990-07-31
075013 0 1990-07-31
075014 0 1990-07-31
075015 0 1990-07-31
075016 0 1990-07-31
075020 0 1990-07-31
075027 0 1990-07-31
075028 0 1990-07-31
075032 0 1990-07-31
075043 0 1990-07-31
075045 0 1990-07-31
075046 2230,6 01.00.51 2006-05-03
075051 0 1990-07-31
075500 0 1990-07-31
075501 0 1990-07-31
075502 0 1990-07-31
075503 0 1990-07-31
075504 0 1990-07-31
075505 0 1990-07-31
075506 0 1990-07-31
075507 0 1990-07-31
075508 0 1990-07-31
075509 0 1990-07-31
075512 0 1990-07-31
075513 0 1990-07-31
075515 0 1990-07-31
075516 0 1990-07-31
075519 0 1990-07-31
075521 0 1990-07-31
075522 0 1990-07-31
0755240
2230,601.00.51
1990-07-31
2006-05-03
075525 0 1990-07-31
075526 0 1990-07-31
075527 0 1990-07-31
075532 0 1990-07-31
075535 0 1990-07-31
075536 0 1990-07-31
075537 0 1990-07-31
0755380
2230,601.00.51
1990-07-31
2006-05-03
075540 0 1990-07-31
075541 0 1990-07-31
075544 0 1990-07-31
075547 0 1990-07-31
0755480
2230,601.00.51
1990-07-31
2006-05-03
075549 0 1990-07-31
075551 0 1990-07-31
075552 0 1990-07-31
075555 2230,6 01.00.51 2006-05-03
075557 0 1990-07-31
075563 0 1990-07-31
075564 0 1990-07-31
075577 0 1990-07-31
075578 0 1990-07-31
075580 5270,2 2015-10-01 Due to inst of TR Blades with P/N 355A12-0040-14
075587 ?
076000 0 1990-07-31
076001 0 1990-07-31
076002 0 1990-07-31
076003 0 1990-07-31
076004 0 1990-07-31
076005 0 1990-07-31
076006 0 1990-07-31
076008 0 1990-07-31
076010 0 1990-07-31
076012 0 1990-07-31
076013 0 1990-07-31
076014 0 1990-07-31
076015 0 1990-07-31
076017 0 1990-07-31
076018 0 1990-07-31
076019 0 1990-07-31
076021 0 1990-07-31
076022 0 1990-07-31
076025 0 1990-07-31
076026 0 1990-07-31
076027 0 1990-07-31
076029 0 1990-07-31
076030 0 1990-07-31
076032 0 1990-07-31
076034 0 1990-07-31
076035 0 1990-07-31
076036 0 1990-07-31
076037 0 1990-07-31
076038 0 1990-07-31
076039 0 1990-07-31
076040 0 1990-07-31
076041 0 1990-07-31
076042 0 1990-07-31
076043 0 1990-07-31
076044 0 1990-07-31
076045 0 1990-07-31
076046 0 1990-07-31
076047 0 1990-07-31
076048 0 1990-07-31
076049 0 1990-07-31
076050 0 1990-07-31
076051 0 1990-07-31
076052 0 1990-07-31
076053 0 1990-07-31
076055 0 1990-07-31
076056 0 1990-07-31
076057 0 1990-07-31
076058 0 1990-07-31
076059 0 1990-07-31
076060 0 1990-07-31
076061 0 1990-07-31
0760630
2230,601.00.51
1990-07-31
2006-05-03
076064 0 1990-07-31
076065 0 1990-07-31
076068 0 1990-07-31
076069 0 1990-07-31
076070 0 1990-07-31
076072 0 1990-07-31
076074 0 1990-07-31
076076 0 1990-07-31
0760780
2230,601.00.51
1990-07-31
2006-05-03
076080 0 1990-07-31
076085 0 1990-07-31
076087
0
1330,3
2230,6
.
65.00.26R1
01.00.51
1990-07-31
2001-10-29
2006-05-03
0760880
2230,601.00.51
1990-07-31
2006-05-03
076089 0 1990-07-31
076090 0 1990-07-31
076095 0 1990-07-31
076098 0 1990-07-31
076100 0 1990-07-31
076103 0 1990-07-31
076105 0 1990-07-31
076107 0 1990-07-31
076108 0 1990-07-31
076109 0 1990-07-31
076110 0 1990-07-31
076112 0 1990-07-31
076113 0 1990-07-31
076114 0 1990-07-31
0761170
2230,601.00.51
1990-07-31
2006-05-03
076120 0 1990-07-31
076124 0 1990-07-31
076125 0 1990-07-31
076129 0 1990-07-31 Main Rotor Mast M456 1990-04-27
076132 0 1990-07-31
076138 0 1990-07-31 MRH M807 1990-11-15
076142 0 1990-07-31
076143 0 1990-07-31 Vibration damper M715 1990-04-27
0761440
2230,601.00.51
1990-07-31
2006-05-03
076145 0 1990-07-31 Main Rotor Mast M456 1990-04-27
076148 0 1990-07-31 Vibration damper M715 1990-04-27
076150 0 1990-07-31
MRH M807 1990-11-15
Vibration damper M715 1990-04-27
Main Rotor Mast M456 1990-04-27
076152 0 1990-07-31 Main Rotor Mast M456 1990-04-27
076156 0 1990-07-31 Main Rotor Mast M456 1990-04-27
076159 0 1990-07-31
076163 0 1990-07-31 Main Rotor Mast M456 1990-04-27
076167 0 1990-07-31 Main Rotor Mast M456 1990-04-27
076169 0 1990-07-31 Main Rotor Mast M456 1990-04-27
076172 2230,601.00.35
01.00.512006-05-03
076174 2230,601.00.51
62.00.132006-05-03
0761750
2230,601.00.51
1990-07-31
2006-05-03MRH M807 1990-11-15
076176 0 1990-07-31 Main Rotor Mast M456 1990-04-27
076187 5070,6 2012-07-02 Mast S/N M456 (new type of swashplate bearing)
076188 5070,6 2012-07-02 Mast S/N M456 (new type of swashplate bearing)
076221 62.00.24 F-2001-557-086(A)R3 2008-09-30 N/A to Starflex P/N
076227 62.00.26 2008-09-30 N/A to M/R Hub P/N
076306 5270,2 2015-10-30 O-ring installed = MOD performed.
076500 0 1990-07-31
076502 0 1990-07-31
076504 0 1990-07-31
076505 0 1990-07-31
076506 0 1990-07-31
076507 0 1990-07-31
076508 0 1990-07-31
0765100
2230,601.00.51
1990-07-31
2006-05-03
076511 0 1990-07-31
0765130
2230,601.00.51
1990-07-31
2006-05-03
076514 0 1990-07-31
076515 0 1990-07-31
076516 0 1990-07-31
076517 0 1990-07-31
0765190
2230,601.00.51
1990-07-31
2006-05-03
0765210
2230,601.00.51
1990-07-31
2006-05-03
076522 0 1990-07-31
0765230
2230,601.00.51
1990-07-31
2006-05-03
076525 0 1990-07-31
076526 0 1990-07-31
076527 0 1990-07-31
076528 0 1990-07-31
0765290
2230,601.00.51
1990-07-31
2006-05-03
0765350
2230,601.00.51
1990-07-31
2006-05-03
0765360
2230,601.00.51
1990-07-31
2006-05-03
076543 2015-11-03 TRH. Found performed.
076544 1330,3 65.00.35 2001-10-29
076550
.
5270,2
3739,1
65.00.41R2
65.00.41R3
65.00.43R0
2008-09-30
2015-10-09
2009-02-19
N/A. B3 model only.
N/A. B3 model only.
Perf. 704A33651210 NR3931
076551 1330,3 65.00.38R1 2001-10-29
076554 05.00.33R1 F-2000-222-079(A) 2001-11-19 Performed on Spider M1815
077000 0 1990-07-31
077001 0 1990-07-31
077002 0 1990-07-31
077003 0 1990-07-31
077004 0 1990-07-31
077005 0 1990-07-31
077008 0 1990-07-31
077009 0 1990-07-31
077011 0 1990-07-31
077012 0 1990-07-31
077014 0 1990-07-31
077016 0 1990-07-31
077017 0 1990-07-31
077018 0 1990-07-31
077019 0 1990-07-31
077020 0 1990-07-31
077021 0 1990-07-31
077022 0 1990-07-31
077023 0 1990-07-31
077024 0 1990-07-31
077026 0 1990-07-31 Bevel reduction gear M1624 1990-04-27
0770270
2230,601.00.51
1990-07-31
2006-05-03
077028 0 1990-07-31
077029 0 1990-07-31
077034 0 1990-07-31
077037 0 1990-07-31 Bevel reduction gear M1624 1990-04-27
077042 2230,6 01.00.51 2006-05-03
077043 0 1990-07-31
077051 0 1990-07-31 Bevel reduction gear M1624 1990-04-27
077057 0 1990-07-31
077061 0 1990-07-31 Bevel reduction gear M1624 1990-04-27
077070 0 1990-07-31
077072 0 1990-07-31 Epicyclic reduction gear M594 1990-04-27
077083 0 1990-07-31
077092 0 1990-07-31
077096 0 1990-07-31
0770980
2230,601.00.51
1990-07-31
2006-05-03 Bevel reduction gear M1624 1990-04-27
077102 0 1990-07-31 Bevel reduction gear M1624 1990-04-27
077108 0 1990-07-31
077109 0 1990-07-31
0771110
2230,601.00.51
1990-07-31
2006-05-03
077114 2230,6 01.00.51 206-05-03
077117 0 1990-07-31 Epicyclic reduction gear M594 1990-04-27
077118 0 1990-07-31
Bevel reduction gear M1624 1990-04-27
Oil Pump M1653 1990-04-27
Epicyclic reduction gear M594 1990-04-27
077120 0 1990-07-31 Bevel reduction gear M1624 1990-04-27
077121 2230,601.00.51
63.00.122006-05-03 MGB spin-on filter
077125 0 1990-07-31
077133 3164 2008-01-28 Bevel reduction gear M1624
077157 3164 2008-01-28 Bevel reduction gear M1624
077162
63.00.12
63.00.18
63.00.09
Not implemented. Oil Filter P/N CH48108 installed.
077174Not implemented. Old Oil Filter P/N CH48108 installed. P/N
FA01315A AFTER MOD 077174.
077175 63.00.09R1 2001-11-30
Bevel reduction gear M1624
Oil Pump M1653 2001-11-30
Epicyclic reduction gear M594
077188 3164 2008-01-28 Bevel reduction gear M1624
077203 3164 2008-01-28 Bevel reduction gear M1624
0772043164
.
.
63.00.13 2.B3
2008-01-28
2008-09-30
Bevel reduction gear M1624
N/A. B3 model only.
077207 5270,2 2015-10-01 Reduction gear bevel S/N M1624. Performed by PHAB.
077240 63.00.23 2015-10-09 OPTIONAL. Not embodied.
078500 0 1990-07-31
078501 0 1990-07-31
078502 0 1990-07-31
078503 0 1990-07-31
078504 0 1990-07-31
078505 0 1990-07-31
078507 0 1990-07-31
078508 0 1990-07-31
078509 0 1990-07-31
078510 0 1990-07-31
078511 0 1990-07-31
078512 0 1990-07-31
078513 0 1990-07-31
078514 0 1990-07-31
0785150
2230,601.00.51
1990-07-31
2006-05-03
078517 0 1990-07-31
0785190
2230,601.00.51
1990-07-31
2006-05-03
078520 0 1990-07-31
078521 0 1990-07-31
0785220
2230,601.00.51
1990-07-31
2006-05-03
0785230
2230,601.00.51
1990-07-31
2006-05-03
0785240
2230,601.00.51
1990-07-31
2006-05-03TGB M907 2008-10-06
078525 0 1990-07-31
078526 0 1990-07-31 TGB M907 2008-10-06
078527 0 1990-07-31
078528 0 1990-07-31 TGB M907 2008-10-06
078532 0 1990-07-31 TGB M907 2008-10-06
078533 0 1990-07-31 TGB M907 2008-10-06
078534 0 1990-07-31 TGB M907 2008-10-06
0785350
2230,601.00.51
1990-07-31
2006-05-03TGB M907 2008-10-06
078536 0 1990-07-31 TGB M907 2008-10-06
078537 5270,2 2015-11-03 Aft T/R drive shaft PPT01299
078538 2008-10-06 TGB M907 2008-10-06
078543 1330,3 65.00.36 2001-10-29 TGB M907 2008-10-06
078547 2008-10-06 TGB M907 2008-10-06
078552 5270,2 2014-06-03 TGB M907 2014-06-03
079000 0 1990-07-31
079002 0 1990-07-31
079003 0 1990-07-31
079005 0 1990-07-31
079006 0 1990-07-31
079008 0 1990-07-31
079011 0 1990-07-31
0790170
2230,601.00.51
1990-07-31
2006-05-03
079020 0 1990-07-31
079023 0 1990-07-31
0790250
2230,601.00.51
1990-07-31
2006-05-03
0790290
2230,601.00.51
1990-07-31
2006-05-03
079057 5270,2 2015-11-03 Aft T/R drive shaft PPT01299 (partially perf)
079059 5270,2 2015-11-03 Aft T/R drive shaft PPT01299
079501 0 1990-07-31
079504 0 1990-07-31
079505 0 1990-07-31
079506 0 1990-07-31
079507 0 1990-07-31
0795080
2230,601.00.51
1990-07-31
2006-05-03
079510 0 1990-07-31
079512 0 1990-07-31
079514 0 1990-07-31
079522 0 1990-07-31
079524 0 1990-07-31
079526 0 1990-07-31
079533 0 1990-07-31
0795370
2230,601.00.51
1990-07-31
2006-05-03
079539 0 1990-07-31
079541 0 1990-07-31
079547 1860,5 29.00.04R1 2004-10-14 Verified.
079552 5270,2 2015-11-06 Shaft P/N 350A35-1100-21 installed.
079558Hydraulic pump - drive bearing, inst 2015-10 iaw PHAB
WO17220002
079563 63.00.14 2008-09-30 N/A. Poly V not installed.
079566 2015-04-10 Not implemented.
07956863.00.22
63.00.24
2015-10-09
2015-10-09
N/A. B3 model only.
N/A. Equipment not installed.
080720.
1330,362.00.22
1995-03-16
2001-10-29Vibration damper M715
350A084578.00 5270,2 28.00.21 2015-10-09 N/A (MOD 073273 not embodied.)
350A08-0720 1330,3 62.00.22 1995-03-16 Verified.
ATA Name P/N S/N SLL (04-10/05-12) TBO (05-10) CHK (04-20) Inst A/CTT Inst CTT Inst. DateCurrent
timeTime left Maintenance
Helicopter AS350 B2 2364 - - - - - 1990-07-315271,3FH/
34227TC-
24.31 Battery (SAFT) 1606-1 H03093 OC 24M VC 5270,2 UNK 2015-11-20 1,1FH (TSO)2017-11-20
(24M OH)
VC before installation (04-
20). Periodical: DI every
12M (05-21-02/CMM CHK
2.B), OH (RS FT) every
24M (05-22-02/CMM CHK
3). Specific periodical: DI
every 6M. (05-25-
00/CMM CHK 2.A).
Component Overhauled
2015-11-20.
25.00 First Aid Kit 70028 692/70028 N/A 12M N/A 5270,2 0 2015-11-27 1,1FH aug-1612M insp (JAR-OPS) NEW
2015-08.
25.00Belt crew
Amsafe/AUTOFLUG704A41123012 - OC N/A N/A
Manu.date:
belt 2002-02
/ harness
2011-04
25.00Belt crew
Amsafe/AUTOFLUG704A41123012 - OC N/A N/A
Manu.date:
belt 2002-04
/ harness
2011-04
25.00 Belt pass ANJOU 3491107-12-070 - OC N/A N/AManu.date:
25.00 Belt pass ANJOU 3491107-12-070 - OC N/A N/AManu.date:
2004-06
25.00 Belt pass ANJOU 3491107-12-070 - OC N/A N/AManu.date:
2010-05
25.00 Belt pass ANJOU 3491108-12-070 - OC N/A N/AManu.date:
2011-02
25.00 Belt pass ANJOU 3491109-12-070 - OC N/A N/AManu.date:
2011-05
25.66 ELT Kannad ELT406AF S1821502-02 P1273-0028 N/A N/A N/A 2234 0 2006-05-04 3037,32016-01-16
(1M insp)
600FH/24M (05-22-00),
1M (05-25-00), MM
KANNAD Periodical (6Y)
25.66 ELT Battery S1820506-01 1105016 6Y N/A N/A 4721,7 0 2011-09-01 549,6
Exp date:
2017-09-01.
WO JFL-48
26.22 Cabin fire extinguisher 704A32810008 640211 N/A 120M (OTL) 2886,4 0 2007-06-28 2384,9 2017-06-28
28.20 Fuel Pump P94B12-209 (704A44510042) B65524 OC N/A N/A 2230,6 0 2006-05-03 3040,7
2398,9FH
(MSM 05-25-
00)
DI every 2400FH (05-25-
00) Perf 2015-11-05 A/CTT
5270,2
62.10Unequipped blade pin
(Yellow)350A31-1771-21 M48086 INF N/A N/A 0 0 1990-04-01 5271,3 INF
LUB 600FH/6M (05-25-00)
Perf 2015-11 A/CTT
5270,2
62.10Unequipped blade pin
(Yellow)350A31-1771-21 M48169 INF N/A N/A 0 0 1990-04-01 5271,3 INF
LUB 600FH/6M (05-25-00)
Perf 2015-11 A/CTT
5270,2
62.10Unequipped blade pin
(Red)350A31-1771-21 M48333 INF N/A N/A 0 0 1990-04-01 5271,3 INF
LUB 600FH/6M (05-25-00)
Perf 2015-11 A/CTT
5270,2
62.10Unequipped blade pin
(Red)350A31-1771-21 M48353 INF N/A N/A 0 0 1990-04-01 5271,3 INF
LUB 600FH/6M (05-25-00)
Perf 2015-11 A/CTT
5270,2
62.10Unequipped blade pin
(Blue)350A31-1771-21 M48343 INF N/A N/A 0 0 1990-04-01 5271,3 INF
LUB 600FH/6M (05-25-00)
Perf 2015-11 A/CTT
5270,2
62.10Unequipped blade pin
(Blue)350A31-1771-21 M48288 INF N/A N/A 0 0 1990-04-01 5271,3 INF
LUB 600FH/6M (05-25-00)
Perf 2015-11 A/CTT
5270,2
62.10 Main Rotor Blade (R ) 355A11-0030-04 27926 20000FH N/A N/A 2230,6 0 2006-04-20 3040,716959,3FH
(SLL)
62.10 Main Rotor Blade (Y) 355A11-0030-04 27914 20000FH N/A N/A 2230,6 0 2006-04-20 3040,716959,3FH
(SLL)
62.10 Main Rotor Blade (B) 355A11-0030-04 27862 20000FH N/A N/A 2230,6 0 2006-04-20 3040,716959,3FH
(SLL)
62.20 MRH 355A31-0001-06 M807 OC N/A GVI 4378,1 5925,3 2010-06-24 6818,5 OC
GVI when removed (04-
20). GVI every 30FH (05-
25-00, PRE MOD 076153).
TCK when installed 2FH
(05-26-00). All tasks
performed 2015-11 A/CTT
5270,2.
62.20 *Blade horn 350A31-1877-02 M8973 80000FH N/A VC (Other H/C) 0 1990-10-01 6818,573181,5FH
(SLL)
VC (04-20). Perf 2015-11
A/CTT 5270,2
62.20 *Blade horn 350A31-1877-02 M8987 80000FH N/A VC (Other H/C) 0 1990-10-01 6818,573181,5FH
(SLL)
VC (04-20). Perf 2015-11
A/CTT 5270,2
62.20 *Blade horn 350A31-1877-02 M9065 80000FH N/A VC (Other H/C) 0 1990-10-01 6818,573181,5FH VC (04-20). Perf 2015-11
62.20 *Blade horn 350A31-1877-02 M9065 80000FH N/A VC (Other H/C) 0 1990-10-01 6818,573181,5FH
(SLL)
VC (04-20). Perf 2015-11
A/CTT 5270,2
62.20 *Star, Starflex 350A31-1917-01 M3243 2400FH N/A 10FH (Other H/C) 0 2007-08-24 1529 871FH (SLL)GVI 10FH (04-20). Perf
2015-11 A/CTT 5270,2
62.20*Pin, Spherical Thrust
Bearing (Y)350A31-1854-21 23841 3000FH N/A N/A (Other H/C) 0 2005-03-15 2399,8
600,2FH
(SLL)
62.20*Pin, Spherical Thrust
Bearing (Y)350A31-1854-21 24155 3000FH N/A N/A (Other H/C) 0 2005-03-15 2399,8
600,2FH
(SLL)
62.20*Pin, Spherical Thrust
Bearing (R )350A31-1854-21 24137 3000FH N/A N/A (Other H/C) 0 2005-03-15 2399,8
600,2FH
(SLL)
62.20*Pin, Spherical Thrust
Bearing (R )350A31-1854-21 24129 3000FH N/A N/A (Other H/C) 0 2005-03-15 2399,8
600,2FH
(SLL)
62.20*Pin, Spherical Thrust
Bearing (B)350A31-1854-21 23301 3000FH N/A N/A (Other H/C) 0 2005-03-15 2399,8
600,2FH
(SLL)
62.20*Pin, Spherical Thrust
Bearing (B)350A31-1854-21 24146 3000FH N/A N/A (Other H/C) 0 2005-03-15 2399,8
600,2FH
(SLL)
62.20 *Spherical thrust bearing 579107-00 J (704A33633211) N20461 6400FH N/A 10FH 4598,9 0 2011-02-03 672,45727,6FH
(SLL)
GVI 10FH (04-20) Perf
2015-11 A/C TT 5270,2
62.20 *Spherical thrust bearing 579107-00 J (704A33633211) N20463 6400FH N/A 10FH 4598,9 0 2011-02-03 672,45727,6FH
(SLL)
GVI 10FH (04-20) Perf
2015-11 A/C TT 5270,2
62.20 *Spherical thrust bearing 579107-00 J (704A33633211) N20477 6400FH N/A 10FH 4598,9 0 2011-02-03 672,45727,6FH
(SLL)
GVI 10FH (04-20) Perf
2015-11 A/C TT 5270,2
62.20*Upper sleeve flange
(Straight)350A31-1850-03 M10767 6600FH N/A N/A (Other H/C) 0 2005-03-15 2399,8
4200,2FH
(SLL)
62.20*Upper sleeve flange
(Straight)350A31-1850-03 M10830 6600FH N/A N/A (Other H/C) 0 2005-03-15 2399,8
4200,2FH
(SLL)
62.20*Upper sleeve flange
(Straight)350A31-1850-03 M10937 6600FH N/A N/A (Other H/C) 0 2005-03-15 2399,8
4200,2FH
(SLL)
62.20*Lower sleeve flange
(Straight)350A31-1850-02 M10804 6600FH N/A N/A (Other H/C) 0 2005-03-15 2399,8
4200,2FH
(SLL)
62.20*Lower sleeve flange
(Straight)350A31-1850-02 M10803 6600FH N/A N/A (Other H/C) 0 2005-03-15 2399,8
4200,2FH
(SLL)
62.20*Lower sleeve flange
(Straight)350A31-1850-02 M10831 6600FH N/A N/A (Other H/C) 0 2005-03-15 2399,8
4200,2FH
(SLL)
62.20*Frequency adapter
YellowE4165F01 (704A33640088) .0277 N/A N/A 10FH (Other H/C) 0 2003-11-20 2907,1 N/A
GVI 10FH (04-20) Perf
2015-11 A/C TT 5270,2
62.20 *Frequency adapter Red E4165F01 (704A33640088) .0264 N/A N/A 10FH (Other H/C) 0 2003-11-20 2907,1 N/AGVI 10FH (04-20) Perf
2015-11 A/C TT 5270,2
62.20 *Frequency adapter Blue E4165F01 (704A33640088) .0267 N/A N/A 10FH (Other H/C) 0 2003-11-20 2907,1 N/AGVI 10FH (04-20) Perf
2015-11 A/C TT 5270,2
62.20Vibration damper, spring
type350A31-0033-03 M715 OC N/A N/A 0 0 1990-06-01 5271,3 OC
62.30 Main rotor mast 350A37-0004-02 M456 OC N/A N/A 0 0 1990-06-01 5271,3 OC
62.30 *Non-rotating swashplate 350A37-1002-05 M1799 INF N/A 100FH 0 0 1990-04-01 5271,3 INF
LUB 100FH (04-20) POST
MOD 076188. Perf 2015-
11 A/CTT 5270,2
62.30 *Rotating swashplate 350A37-1003-07 M1340 INF N/A 100FH 0 0 1990-04-01 5271,3 INF
LUB 100FH (04-20) POST
MOD 076188. Perf 2015-
11 A/CTT 5270,2
62.30 *Scissor drive adapter 350A37-1119-21 M1819 INF N/A N/A 0 0 1990-04-01 5271,3 INF62.30 *Scissor drive adapter 350A37-1119-21 M1819 INF N/A N/A 0 0 1990-04-01 5271,3 INF
62.30 *Scissor link, upper 350A37-1126-01 PMA107 INF N/A N/A 0 0 1990-04-01 5271,3 INF
62.30 *Scissor link, upper 350A37-1126-01 PMA195 INF N/A N/A 0 0 1990-04-01 5271,3 INF
62.30 *Scissor link, lower 350A37-1127-01 PMA770 INF N/A N/A 0 0 1990-04-01 5271,3 INF
62.30 *Scissor link, lower 350A37-1127-01 PMA825 INF N/A N/A 0 0 1990-04-01 5271,3 INF
62.30 *MRH attachment bolt 350A37-1244-20 84035 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)
62.30 *MRH attachment bolt 350A37-1244-20 84040 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)
62.30 *MRH attachment bolt 350A37-1244-20 85048 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)
62.30 *MRH attachment bolt 350A37-1244-20 84049 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)
62.30 *MRH attachment bolt 350A37-1244-20 85318 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)
62.30 *MRH attachment bolt 350A37-1244-20 85358 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)
62.30 *MRH attachment bolt 350A37-1244-20 75394 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)
62.30 *MRH attachment bolt 350A37-1244-20 75585 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)
62.30 *MRH attachment bolt 350A37-1244-20 75835 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)
62.30 *MRH attachment bolt 350A37-1244-20 76737 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)
62.30 *MRH attachment bolt 350A37-1244-20 76795 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)
62.30 *MRH attachment bolt 350A37-1244-20 76913 3000FH N/A 100FH 4378,1 481,5 2010-06-24 1374,7 1625,3TCK 100FH (04-20)
62.30 *Main rotor shaft 350A37-1290-03 M3642 160000TC N/A N/A 0 0 1990-04-015271,3FH
/34227TC125773TC
SB 05.00.32 6Y corr check.
Performed 2015-11-21
A/CTT 5270,2
62.30 *Rotor shaft upper casing 350A37-1291-00 PMA523 INF N/A N/A 0 0 1990-04-01 5271,3 INF
62.30 *Rotor shaft lower casing 350A37-1292-00 PMA496 INF N/A N/A 0 0 1990-04-01 5271,3 INF
62.30 *Swashplate bearing 704A33651158 NR10004 OTL 6300FH N/A 10FH 5070,6 0 2012-07-02 200,7 6099,3FHGVI 10FH (04-20) DI
600FH (05-22-01). Perf
2015-11 A/CTT 5270,2
63.10 Hydraulic pump - Belt FILONTYPEFO (704A33690004) - OTL 1200FH N/A N/A 4663,4 0 2011-05-16 607,9592,1FH
(OTL)
63.10Hydraulic pump - Drive
bearing593733 (704A33651206) R/NA10785 OTL 3600FH/72M N/A N/A 5270,2 0 2015-11-02 1,1
3598,9FH/20
21-11-02
63.20 Bevel reduction gear 350A32-0300-05 M1624 N/A 3500FH/288M N/A 0 0 1990-06-012107,3
(TSO)
1392,7FH/20
32-01-28
63.20 *Main casing 350A32-3121-04 MA15620 INF N/A N/A 0 0 1990-06-01 5271,3 INF
63.20 *MGB bottom casing 350A32-3119-03 M3540 20000FH / 93700TC N/A N/A 3164 0 2008-01-28 2107,3
17892,7FH /
59473TC
(SLL)
63.20 *Bevel gear 350A32-3173-20 L979 20000FH N/A N/A 3164 0 2008-01-28 2107,317892,7FH
(SLL)
63.20 *Bevel wheel 350A32-3165-20 M791 20000FH N/A N/A 3164 0 2008-01-28 2107,317892,7FH
63.20 *Bevel wheel 350A32-3165-20 M791 20000FH N/A N/A 3164 0 2008-01-28 2107,317892,7FH
(SLL)
63.20 Epicyclic reduction gear 350A32-0110-00 M594 N/A 3500FH/288M N/A 0 0 1990-06-012107,3
(TSO)
1392,7FH/20
32-01-28
63.20 *Sun gear 350A32-1075-20 ZF4466 INF N/A N/A 0 0 1990-06-01 5271,3 INF
63.20 *Fixed ring gear 350A32-1051-20 ZF1987 N/A N/A N/A 0 0 1990-06-01 5271,3 N/ANO SLL, enligt mail Airbus
2015-10-29
63.20 *Planet gear 350A32-1082-03 ZF7523 20000FH N/A N/A 3164 0 2008-01-28 2107,317892,7FH
(SLL)
63.20 *Planet gear 350A32-1082-03 ZF7564 20000FH N/A N/A 3164 0 2008-01-28 2107,317892,7FH
(SLL)
63.20 *Planet gear 350A32-1082-03 ZF7710 20000FH N/A N/A 3164 0 2008-01-28 2107,317892,7FH
(SLL)
63.20 *Planet gear 350A32-1082-03 ZF7778 20000FH N/A N/A 3164 0 2008-01-28 2107,317892,7FH
(SLL)
63.20 *Planet gear 350A32-1082-03 ZF8175 20000FH N/A N/A 3164 0 2008-01-28 2107,317892,7FH
(SLL)
63.20 *Planet gear cage 350A32-1089-21 ZF635 68700TC N/A N/A 3164 18984TC 2008-01-28 34227TC34473TC
(SLL)
63.20 Oil pump 350A32-0400-00 M1653 N/A 3500FH/288M N/A 0 0 1990-06-01 2107,3 TSO1392,7FH/20
32-01-28
63.30 MGB suspension cross bar 350A38-1040-20 AF238598 INF N/A N/A 0 0 1990-06-01 5271,3 INF
64.10 Tail Rotor Blades 355A12-0040-14 18525 4000FH N/A 30FH 5270,2 0 2015-11-05 1,1 3998,9FH
GVI 30FH (04-20).
Component new 2015-11-
05.
64.10 *Tail rotor blade horn 350A12-1368-04 SND1402 INF N/A N/A 5270,2 0 2015-11-05 1,1 INF
64.10 *Tail rotor blade horn 350A12-1368-04 SND1403 INF N/A N/A 5270,2 0 2015-11-05 1,1 INF
65.10Front Shaft Assy (short
shaft)350A34-0150-03 M3909 N/A N/A N/A 4569,3 2337,8 2010-11-19 3039,8 N/A
65.10Rear Section, Rear
Transm.350A34-0210-06 PPT01299 OC N/A N/A 5270,2 0 2015-11-05 1,1 OC
Ny komponent, levererad
PHAB 2015-11-03
65.10 *Aft shaft (long shaft) 350A34-1012-05 PPT01299 10500FH N/A N/A 5270,2 0 2015-11-05 1,1 10498,9FHNy komponent, levererad
PHAB 2015-11-03
65.10T/R drive shaft - lub
bearing593404 (704A33651181) - OTL 3600FH/60M N/A 600FH 5270,2 0 2015-11-05 1,1
3598,9FH/
2020-10
DI every 600FH (04-20-
00). 150FH GVI (05-21-
01). LUB 600FH/24M (05-
22-00). New inst 2015-11-
05, A/CTT 5270,2.
65.10T/R drive shaft - lub
bearing593404 (704A33651181) - OTL 3600FH/60M N/A 600FH 5270,2 0 2015-11-05 1,1
3598,9FH/
2020-10
DI every 600FH (04-20-
00). 150FH GVI (05-21-
01). LUB 600FH/24M (05-
22-00). New inst 2015-11-
05, A/CTT 5270,2.
65.10T/R drive shaft - lub
bearing593404 (704A33651181) - OTL 3600FH/60M N/A 600FH 5270,2 0 2015-11-05 1,1
3598,9FH/
2020-10
DI every 600FH (04-20-
00). 150FH GVI (05-21-
01). LUB 600FH/24M (05-
22-00). New inst 2015-11-
05, A/CTT 5270,2.
T/R drive shaft - lub 3598,9FH/
DI every 600FH (04-20-
00). 150FH GVI (05-21-
65.10T/R drive shaft - lub
bearing593404 (704A33651181) - OTL 3600FH/60M N/A 600FH 5270,2 0 2015-11-05 1,1
3598,9FH/
2020-10
00). 150FH GVI (05-21-
01). LUB 600FH/24M (05-
22-00). New inst 2015-11-
05, A/CTT 5270,2.
65.10T/R drive shaft - lub
bearing593404 (704A33651181) - OTL 3600FH/60M N/A 600FH 5270,2 0 2015-11-05 1,1
3598,9FH/
2020-10
DI every 600FH (04-20-
00). 150FH GVI (05-21-
01). LUB 600FH/24M (05-
22-00). New inst 2015-11-
05, A/CTT 5270,2.
65.20 Tail Gear Box 350A33-0200-05 M907 N/A 3000FH/288M N/A 5270,2 1880,2 2015-11-06 4265,71118,7FH
/2032-10-06
65.20 *Casing 350A33-1090-01 MA0047 20000FH N/A 1200FH/24M (Other H/C) 0 2008-10-06 1881,318118,7FH
(SLL)
GVI 1200FH/24M (05-25-
00) Perf 2015-11-06 at
CTT 1880,0, A/CTT 5270,2.
65.20 *Tail rotor shaft 350A33-1092-01 MA2318 20000FH N/A N/A 5270,2 3286,5 2014-06-03 3287,616712,4FH
(SLL)
65.20 *Bevel gear 350A33-1000-21 L10803 7500FH N/A N/A (Other H/C) 0 2008-10-06 1881,35618,7FH
(SLL)
65.20 *Bevel wheel 350A33-1001-21 L8972 20000FH N/A N/A (Other H/C) 0 2008-10-06 1881,318118,7FH
(SLL)
65.20 *Control lever 350A33-1526-00 MA84921 20000FH N/A N/A 5270,2 0 2015-11-06 1,119998,9FH
(SLL)
DI every 1200FH/24M (05-
25-00). Component new
2015-11-06.
65.20 Pitch Change Rod 350A33-2145-01 S25983 N/A N/A 30FH 5270,2 0 2015-11-10 1,1 N/A
DI every 30FH (04-20-00)
Component NEW 2015-11
A/CTT 5270,2
65.20 Pitch Change Rod 350A33-2145-01 S25425 N/A N/A 30FH 5270,2 0 2015-11-10 1,1 N/A
DI every 30FH (04-20-00)
Component NEW 2015-11
A/CTT 5270,2
65.20 Spider Assy, Pitch Change 350A33-2030-00 M1815 OC N/A N/A 1330,5 1333,2 2001-11-30 5274 OCDI 150FH (05-21-01) Perf
2015-11 A/CTT 5270,2
65.20*TRH pitch change
bearing704A33-651-210 4050 OTL 3000FH N/A N/A 4828,3 353,4 2011-12-31 796,4
2203,6FH
(OTL)
67.30 Main servocontrol SC5083-1 (704A44831161) 6130 N/A 3000FH/240M N/A 5270,2 0 2015-11-01 1,12998,9FH/20
35-11-01 New 2015-11
67.30 Main servocontrol SC5083-1 (704A44831161) 6137 N/A 3000FH/240M N/A 5270,2 0 2015-11-01 1,12998,9FH/20
35-11-01 New 2015-11
67.30 Main servocontrol SC5084-1 (704A44831162) 3175 N/A 3000FH/240M N/A 5270,2 0 2015-11-01 1,12998,9FH/20
35-11-01 New 2015-11
67.30 Tail rotor servo control AC67032 (704A44831115) BY448 INF 1800FH/240M N/A 3835,9 0 2009-03-18 1435,4364,6FH/202
8-07-26
(GVI 500FH (04-20)PRE
MOD 073139) N/A: MOD
embodied.
80.00 Starter-Generator 150SG122Q 6464 N/A 900FH N/A 4948,4 462,8 2012-04-10 785,7 114,3FH
DI every 300FH (05-25-
00), 600FH (SB 05.00.75)
Perf 2015-11 A/CTT
5270,2
MGB Oil Mobil 254
Eng Oil Mobil 254
Hyd Oil Fluid 31Hyd Oil Fluid 31
Fett Grease 7
ENGINE INSP REF TOL Note Last perf. ENG TT Remaining time
ENG SLL (various) (05-10-01-200-801) N/A See Binder tab No.6 -
ENG DAILY (05-10-10-200-801) - DAILY DAILY
ENG TBO/OC (various) (05-15-00-201-801) - See Binder tab No.6 -
ENG Use-Limited Parts (05-15-00-201-802) - See Binder tab No.6 -
ENG 15FH/7D insp (05-20-10-201-810) - DAILY DAILY
ENG 30FH insp (05-20-10-201-815) 3
Performed together
with AS350B2 MSM Ch
05-20-02
5270,2FH 5300,2FH
ENG 50FH insp (05-20-10-201-817) 5 Not to be performed - -
ENG 100FH insp (05-20-10-201-820) 10 7527,5 98,90FH
ENG 150FH insp (05-20-10-201-825) 15 7464,65 86,05FH
ENG 200FH insp (05-20-10-201-830) 20 7464,65 136,05FH
ENG 300FH insp (/12M) (05-20-10-201-835) 30H/1M 7492,35263,75FH/2016-
02-17
Scheduled Engine Inspections
ENG 300FH insp (/12M) (05-20-10-201-835) 30H/1M 7492,3502-17
ENG 400FH insp (05-20-10-201-840) 40 Not to be performed - -
ENG 500FH insp (05-20-10-201-846) 50 7362,6 334,00FH
ENG 600FH insp (05-20-10-201-850) 50 7068,85 140,25FH
ENG 750FH insp (/2Y) (05-20-10-201-852) 50H/2M 7362,6584,00FH/ 2016-
06-20
ENG 800FH insp (05-20-10-201-855) - Not to be performed - -
ENG 1000FH insp (05-20-10-201-860) 50 6967,7 439,10FH
ENG 1500FH insp (05-20-10-201-870) 50 7464,65 1436,05FH
ENG 3000FH insp (05-20-10-201-880) 50 Not to be performed - -
ENG 3600FH insp (05-20-10-201-886) 50 5995,8 2067,20FH
ENGOil Change,
750FH/24MMobil 254 7464,65
686,05FH /2016-
10-02
ATA Appl.AD
classAD nr FAA AD
Issue
DateSubject
Approval
Holder /
Type
Designation
Effective
date
Expire
datePerformed SB Repetetive
77 N/A AD 2015-0175 2015-08-24Engine Indicating - Tachometer Boxes - Replacement
Applicability: ARRIEL 1E2 engines, all serial numbers.
TURBOMECA
ARRIEL 12015-09-07 1600FH
N/A to Arriel
1D1
MSB 292 77
0844
72 N/A AD 2015-0064R1 2015-07-29
Engine – Front Support Pins – Inspection / Replacement
Applicability: ARRIEL 1E2 turbo-shaft engines, all serial
numbers.
TURBOMECA
ARRIEL 12015-07-29 15FH
N/A to Arriel
1D1
MSB 292 72
0842
72 Y AD 2014-0036 2015-13-04 2014-02-11
Engine - Accessory Gear Box (M01) - 41/23 Tooth Bevel Gear
Assembly - Check / Replacement
Applicability: ARRIEL 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1,
1E2, 1K, 1K1, 1S and 1S1 turbo-shaft engines, all serial
numbers.
TURBOMECA
ARRIEL 1
ARRIEL 2
2014-02-25 2016-10-25MSB 292 72
0839
During every
qualifying shop
visit
72 N/A AD 2013-0120 2013-06-04
Engine - Free Turbine Bearing Plug - Inspection / Rework
Applicability: ARRIEL 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1,
1E2, 1K, 1K1, 1S, 1S1, all serial numbers.
TURBOMECA
ARRIEL 12013-06-18 50FH
M04 S/N
10274 not
affected.
A292.72.083
8
72 N/A AD 2012-0187R2 2012-12-06
Engine - Airworthiness Limitation Section - Cycle Counting Aid
System - Modification/Amendment
Applicability: ARRIEL 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1,
1E2, 1K, 1K1, 1S and 1S1 turbo-shaft engines, all serial
numbers.
TURBOMECA
ARRIEL 12012-12-13 See AD
Engine not
affected. Cycl
count aid
system not
used.
ALF
72 Y AD 2010-0101R32010-19-06
DCA/TUR/70D2012-09-05
Engine - Module M03 (Gas Generator) - Post-TU347 Second
Stage Turbine Disc - Reduced Life Limit
Applicability: Arriel 1A, 1A1, 1B, 1C, 1C1, 1C2, 1D, 1D1 and
1S1 turbo-shaft engines, all serial numbers, if modified by
Turboméca TU347, except those with Gas Generator 2nd
stage Turbine Discs modified by Turboméca Modification
TU365 in production, or modified by Turboméca Service
Bulletin (SB) 292 72 0365 in-service.
TURBOMECA
ARRIEL 12012-09-19 6500 Ng Cycl
Complied With
2010-09-21
A.292.72.083
1
6500 Ng Cycl
(MM 05-10-01-
200-801-A01 )
72 N/A AD 2012-0143 2012-08-01
Engine - Gas Generator Second Stage Turbine - Inspection /
Replacement
Applicability: All ARRIEL 1B post-mod TU 148, ARRIEL 1D,
ARRIEL 1D1 and ARRIEL 1S1 turboshaft engines, all serial
numbers, except those with Gas Generator 2nd stage turbine
wheels installed that have incorporated Turbomeca
modification TU347 in production, or have been modified by
Turbomeca Service Bulletin (SB) 292 72 0347 in-service.
TURBOMECA
ARRIEL 12012-08-15 See AD
N/A. TU 347
incorporated
A292.72.080
7
72 Y AD 2012-0117 2012-07-03
Engine - Gas Generator Rotating Assembly and Rear Bearing -
Check / Replacement
Applicability: ARRIEL 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1,
1E2, 1K, 1K1, 1S and 1S1 turbo-shaft engines, all serial
numbers.
TURBOMECA
ARRIEL 12012-07-17
Whenever
M03 is
removed
MM X 292 G2
452 2 Issue
14
Yes
72N/A
(S)AD 2009-0236R1 2010-10-09 2012-06-22
SUPERSEDED BY EASA AD 2012-0143
Applicability: All ARRIEL 1B post-mod TU 148, ARRIEL 1D,
ARRIEL 1D1 and ARRIEL 1S1 turboshaft engines, with gas
generator second stage turbine wheels Part Numbers (P/N)
listed in Appendix 2 of this AD.
TURBOMECA
ARRIEL 12012-06-29 See AD N/A
A292.72.080
7
72 Y AD 2012-00712003-12-14
DCA/TUR/822012-04-26
Engine - Axial Compressor, Gas Generator Hollow Shaft and
Rear Bearing - Identification / Inspection / Cleaning /
Replacement
Applicability: ARRIEL 1A, 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1,
1E2, 1K, 1K1, 1S and 1S1 turbo-shaft engines, all serial
numbers, except those incorporating Turboméca TU360
modification.
TURBOMECA
ARRIEL 12012-05-10
Engine
history
checked: not
op in dusty
environment
= not
repetetive
2012-08-23A292.72.023
0Not repetetive
73 N/A AD 2012-0063 2012-04-17
Engine Fuel & Control - Fuel Control Unit (FCU) 3-way Union
Plug - Inspection
Applicability: ARRIEL 1E2, 1S and 1S1 turboshaft engines, all
serial numbers.
TURBOMECA
ARRIEL 12012-05-01 See AD
N/A to 1D1
engines292.73.0817
72 N/A AD 2010-0273R1 2011-02-16
Engine - Module M03 (Gas Generator) - Second Stage
Turbine Nozzle Guide Vane - Inspection/Replacement
Applicability: Arriel 1B turboshaft engines, if modified by
TU76 or TU202, and not modified by TU148, and fitted with
repaired second stage Nozzle Guide Vane.
TURBOMECA
ARRIEL 12011-03-02 See AD
N/A to 1D1
engines
A292.72.082
9
73 N/A EAD 2011-0023-E 2011-02-10
[Correction] Engine Fuel & Control - Low Pressure Fuel
System / Ejector Assembly - Inspection / Replacement
Applicability: Arriel 1E2, 1S and 1S1 turboshaft engines, all
serial numbers, on which Turbomeca Internal Consign (IC)
No. 298468 or Turbomeca Service Bulletin (SB) No. 292 73
0826 version A has been accomplished.
TURBOMECA
ARRIEL 12011-02-11 See AD
N/A to 1D1
engines
A292.73.083
4
292.73.0826
72 N/A AD 2010-0118 2010-06-18
SUPERSEDED BY EASA AD 2010-0273
Applicability: Arriel 1B turboshaft engines, if modified by
TU76 and not modified by TU148 and fitted with repaired
second stage Nozzle Guide Vane.
TURBOMECA
ARRIEL 12010-07-02 See AD
N/A to 1D1
engines
A292.72.082
9
72 N/A EAD 2009-0245-E 2009-26-07 2009-11-10
Engine - Module M05 (Reduction Gear Box) Lubrication Duct -
Inspection / Repair
Applicability: Arriel 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2,
1K, 1K1, 1S and 1S1 turbo-shaft engines, all serial numbers if
modified by TU332 and fitted with Modules M05 (Reduction
Gear Box) as identified in figure 1 of Turboméca Mandatory
Service Bulletin (MSB) A292 72 0825 version B.
TURBOMECA
ARRIEL 12009-11-12 2010-02-12 N/A 292.72.0825
72 N/A AD 2009-0112R1 2009-08-08 2009-07-30
Engine - Module M04 (Power Turbine) Power Turbine Blades -
Life Limit / Replacement
Applicability: Variant Arriel 1B, 1D and 1D1 turboshaft
engines, fitted with Modules M04 (Power Turbine) as
identified in figure 1 of Turboméca Mandatory Service
Bulletin (MSB) A292 72 0827 version C, and Variant Arriel 2B,
2B1 and 2B1A turboshaft engines, fitted with Modules M04
as identified in figure 1 of Turboméca MSB A292 72 2833
version C.
TURBOMECA
ARRIEL 1
ARRIEL 2
2009-06-01 See ADN/A to MO4
S/N 10274
A292.72.082
7
72N/A
(S)EAD 2009-0117-E 2009-26-07 2009-06-02
SUPERSEDED BY EASA EAD 2009-0245-E
Applicability: Arriel 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2,
1K, 1K1, 1S and 1S1 turbo-shaft engines, all serial numbers if
modified by TU332 and fitted with Modules M05 (Reduction
Gear Box) as identified in figure 1 of Turboméca Mandatory
Service Bulletin (MSB) A292 72 0825.
TURBOMECA
ARRIEL 12009-06-04 2010-02-04 N/A 292.72.0825
72N/A
(S)EAD 2009-0068-E 2009-08-08 2009-03-25
SUPERSEDED BY EASA AD 2009-0112
Applicability: Variant Arriel 1B, 1D and 1D1 turboshaft
engines, fitted with Modules M04 (Power Turbine) as
identified in fig 1 of Turboméca Mandatory Service Bulletin
(MSB) A292 72 0827 version A.
TURBOMECA
ARRIEL 1
ARRIEL 2
2009-03-27 See AD N/AA292.72.082
7
72 N/A AD 2009-0002 2010-02-01 2009-01-07
Engine - Reduction Gear Box Intermediate Pinion -
Modification
Applicability: Arriel 1B, 1D and 1D1 turboshaft engines, all
serial numbers.
TURBOMECA
ARRIEL 12009-01-21 2011-02-28 N/A
292.72.0276
B
73 S AD 2008-0014 2008-01-17
SUPERSEDED BY EASA AD 2012-0063
Applicability: Arriel 1E2, 1S and 1S1 turboshaft engines, all
serial numbers.
TURBOMECA
ARRIEL 12008-01-31 See AD
N/A to 1D1
engines292.73.0817
72N/A
(S)AD 2007-0018R1 2010-10-09 2007-08-14
SUPERSEDED BY EASA AD 2009-0236 DATED 29 OCTOBER
2009
Applicability: all ARRIEL 1B post-mod TU 148, ARRIEL 1D,
ARRIEL 1D1 and ARRIEL 1S1 turboshaft engines, not modified
with Turbomeca modification TU347 or Service Bulletin (SB)
292 72 0347 [Installation of turbine Part Number (P/N) 0 292
25 039 0].
TURBOMECA
ARRIEL 12007-01-29 See AD N/A
A292 72
0807 E
72 N/A AD 2007-0045 2007-02-21
Return to Service for Civil Use from an Operator Not
Controlled by a Civil Authority
Applicability: ARRIEL 1A,1A1,1A2,1B, 1C, 1C1, 1C2, 1D, 1D1,
1E2, 1K, 1K1, 1S, 1S1 turboshaft engines originally assembled
by TURBOMECA and having previously been used by an
operator who is not under the control of a civil Authority
(Military, Paramilitary…).
TURBOMECA
ARRIEL 12007-03-08 2007-03-08
N/A to this
engine.292.72.0806
72 Y AD 2007-0002 2006-06-17 2007-01-05
Engine - 2nd Stage Nozzle Guide Vane (NGV2) - Inspection
Applicability: TURBOMECA ARRIEL 1B, 1D and 1D1 models
turboshaft engines, modified TU 202, except to those having
2nd stage nozzle guide vanes of which serial numbers or
specific marks are identified in Service Bulletin No. 292 72
0231 update No 5.
TURBOMECA
ARRIEL 12004-08-04 See AD
Found
Embodied
2010-09-21
A292.72.023
1Not repetetive
72 Y AD 2006-0068 2007-02-17 2006-03-24Engine - Fuel Leaks on the Start Electro Valve - Inspection
Applicability: Arriel 1 Series
TURBOMECA
ARRIEL 12006-04-07 See AD
Complied With
2010-09-21
A292.72.025
1Not repetetive
72N/A
(S)AD
F-2004-
047R12010-10-09 2005-10-26
SUPERSEDED BY EASA AD 2007-0018
EFFECTIVITY: This Airworthiness Directive (AD) applies to the
following turboshaft engine variants: ARRIEL 1B which have
been modified per TU 148, ARRIEL 1D, ARRIEL 1D1 and
ARRIEL 1S1 (not incorporating TU347).
TURBOMECA
ARRIEL 12005-11-05 See AD N/A
A292 72
0807 E
72 S ADF-2004-
088R12006-06-17 2004-08-04
SUPERSEDED BY EASA AD 2007-0002
EFFECTIVITY: This Airworthiness Directive (AD) applies to
TURBOMECA ARRIEL 1B, 1D and 1D1 models turboshaft
engines, modified TU 202, except to those having 2nd stage
nozzle guide vanes of which serial numbers or specific marks
are identified in Service Bulletin No. 292 72 0231 Revision 5.
TURBOMECA
ARRIEL 12004-08-04 See AD
Found
Embodied
2010-09-21
292 72 0231
R5
72 N/A AD 2003-16-03 2003-09-18
Second Stage Turbine Disk - Inspection of gas generator 2nd
Stage NGV
Applicability: Arriel 1 A, 1 A1, 1 A2, 1 B, 1 C, 1 C1, 1 C2, 1 D, 1
D1, 1 E2, 1 K, 1 K1, 1 S, and 1 S1 that have not incorporated
modification TU 202
TURBOMECA
ARRIEL 12003-09-18 See AD N/A
A292 72
0181 R3 and
A292 72
0212 R5
72 N/A AD 2003-11-08 2003-07-03
2nd stage gas generator - Replacement of 2nd stage turbine
blades (post TU204)
Applicability: Arriel -1B, -1D, and -1D1
TURBOMECA
ARRIEL 12003-07-03 See AD N/A
72 Y AD 2003-03-12 2003-03-07
Bleed Valve - Centrifugal impeller blade rupture. Bleed valve
boss sleeve (TU300 and 316)
Applicability: Arriel 1 A2, 1 C, 1 C1, 1 C2, 1 D, 1 D1, 1 E2, 1 K,
1 K1, 1 S, 1 S1 and Arriel 2 B, 2 B1, 2 C, 2 C1, 2 S1
TURBOMECA
ARRIEL 12003-03-07 See AD
Complied With
2010-09-21Not repetetive
72 Y AD 2002-14-26 2002-08-06
Containment Shield Rings - Installation of containment shield
(TU215 or 254 or 255) and supports (TU259)
Applicability: Arriel Models 1A, 1A1, 1B, 1D, and 1D1
TURBOMECA
ARRIEL 12002-08-06 2002-09-20
Found
Embodied
2010-09-21
Not repetetive
72 S ADF-1990-
064R12003-12-14 2001-03-21
SUPERSEDED BY EASA AD 2012-0071
APPLICABILITY: ARRIEL 1 turboshaft engines all variants
installed on single or twin-engine helicopters.
TURBOMECA
ARRIEL 12001-03-31 See AD
Complied With
2008-10-07
A292 72
0230
72 Y AD 2000-20-01 2000-10-17
Rear Bearing Oil Return System - Electrical mag plug for gas
generator rear bearing
Applicability: Arriel 1 A, -1 A1, -1 A2, -1 B, -1 C, -1 C1, -1 C2, -
1 D, -1 D1, -1 K, -1 K1, -1 S, and -1 S1
TURBOMECA
ARRIEL 12000-10-17 See AD
Found
Embodied
2010-09-21292 72 0163
R1 (TU208)
Not repetetive
72 N/A AD 94-25-08 1995-01-17
Gearboxes - Inspection of reduction gearbox chip plug every
8H not modified TU232
Applicability: Arriel Model 1B, 1D, 1D1, 1A with TU13, and
1A1 with TU13 Engines
TURBOMECA
ARRIEL 11995-01-17 See AD N/A
72 N/A AD 91-24-02 1992-02-21
Main Rotor Drive Shaft - Free Wheel Shaft with S/N 793 or
higher not modified TU211 or TU212
Applicability: Arriel 1B, 1D, Arriel 1D, and Arriel 1D1 Engines
TURBOMECA
ARRIEL 11992-02-21 See AD N/A
AD SB TU Description Compliance Date Eng hrs Perf by Rec Module
1 Fitting of a power output shaft made of a tube (3 mm thick) Included in the definition package 2002-06-27 0 Turbomeca
2 Compressor casing. Fitting of cast stators .. Included in the definition package 2002-06-27 0 Turbomeca
4 Combustion chamber. Addition of a positioning dowel device Included in the definition package 2002-06-27 0 Turbomeca
5 Fitting of removable gas generator rear bearing Included in the definition package 2002-06-27 0 Turbomeca
6 Free turbine bearing support fitted with enlarged sealing ring Included in the definition package 2002-06-27 0 Turbomeca
7 1st and 2nd stage diffuser assemblies of centrifugal compressor. Included in the definition package 2002-06-27 0 Turbomeca
8 Free turbine nozzle guide vane. Included in the definition package 2002-06-27 0 Turbomeca
9 Front and rear bearings of axial compressor. Included in the definition package 2002-06-27 0 Turbomeca
11 Injectors supply electric cock. Included in the definition package 2002-06-27 0 Turbomeca
12 Accessory box. Addition of a support for the anticipator control Included in the definition package 2002-06-27 0 Turbomeca
13 Suppression of the free turbine overspeed device Included in the definition package 2002-06-27 0 Turbomeca
14 Axial compressor wheel. Thicking of blades profile on their root Included in the definition package 2002-06-27 0 Turbomeca
15 FCU. Installation of a strainer .. Previously Embodied 2010-09-09 FCU S/N C500B
16
Single engine output for helicopter tail rotor drive.
Previously Embodied 2010-09-21 Free Wheel Shaft
Assy S/N 3182B
19 Power shaft. Suppression of the blanker stop shoulder .. Included in the definition package 2002-06-27 0 Turbomeca
20 Inst of fire detector on the front face of reduction gear box.. Included in the definition package 2002-06-27 0 Turbomeca
21 Lubricating system. Addition of a strainer .. Included in the definition package 2002-06-27 0 Turbomeca
23 FCU. Principal cock of Fuel control unit. Previously Embodied 2010-09-09 FCU S/N C500B
24 Oil pump inlet union and swivel union hollow bolt Included in the definition package 2002-06-27 0 Turbomeca
25 Common oil tapping on the accessory box .. Included in the definition package 2002-06-27 0 Turbomeca
26 Detection of min oil press in gas gen bearings supply circuit Included in the definition package 2002-06-27 0 Turbomeca
27 Free turbine nozzle guide vane. Inserted turbine ring .. Included in the definition package 2002-06-27 0 Turbomeca
28 FCU. Suppression of the tin plating .. Previously Embodied 2010-09-09 FCU S/N C500B
29 Accessory box. Included in the definition package 2002-06-27 0 Turbomeca
30 FCU. Fine adjustment of max Ng stop .. Included in the definition package 2002-06-27 0 Turbomeca
31 Free turbine sealing ring diameter Included in the definition package 2002-06-27 0 Turbomeca
33 Installation of module identification plates Included in the definition package 2002-06-27 0 Turbomeca
37 Combustion chamber outer part. Included in the definition package 2002-06-27 0 Turbomeca
38 Free turbine nozzle guide vane .. Included in the definition package 2002-06-27 0 Turbomeca
92.078(B)R2 39M05. Turbine reduction gear.
N/A to this engine 2010-11-18MO5 S/N 9975
40 Turbine reduction gear. Included in the definition package 2002-06-27 0 Turbomeca
41 Axial compressor. Inst of a wheel shrink fitted on its shaft Included in the definition package 2002-06-27 0 Turbomeca
42 1st and 2nd stage diffusers. Included in the definition package 2002-06-27 0 Turbomeca
43 Turbine reduction gear. Included in the definition package 2002-06-27 0 Turbomeca
44 Accessory drive. Installation of a tail type pinion .. Included in the definition package 2002-06-27 0 Turbomeca
45 Inst of check valve at connection of oil return pipe to oil cooler Included in the definition package 2002-06-27 0 Turbomeca
46 Main output drive. Addition of ducts … Included in the definition package 2002-06-27 0 Turbomeca
47 Engine front support. Addition of a drain Included in the definition package 2002-06-27 0 Turbomeca
48 Electro-valve support. Mounting of a reinforced support Included in the definition package 2002-06-27 0 Turbomeca
49 Installation of a magnetic plug with indication on the panel Included in the definition package 2002-06-27 0 Turbomeca
51 FCU. Pump pressure relief valve .. Previously Embodied 2010-09-09 FCU S/N C500B
52 Integral injection wheel Included in the definition package 2002-06-27 0 Turbomeca
53 Combustion chamber outer part. Included in the definition package 2002-06-27 0 Turbomeca
56
Improvement of the starting bleed valve sealing
Previously Embodied 2010-08-19 Starting Drain
Valve S/N 1165M
58 FCU. Installation of "D.U." rings in the pump unit bearings Previously Embodied 2010-09-09 FCU S/N C500B
60 Reduction gear. Roller bearings inner races.. Included in the definition package 2002-06-27 0 Turbomeca
61
Rear drive. Installation of magnetic seal
Previously Embodied 2010-09-21 Free Wheel Shaft
Assy S/N 3182B
62 Torquemeter. Inst of the transmitter on accessory box casing Included in the definition package 2002-06-27 0 Turbomeca
63 Suppression of the alternator drive in the module MO5 Included in the definition package 2002-06-27 0 Turbomeca
64 Assembly of the compressor casing and of the accessory box. Included in the definition package 2002-06-27 0 Turbomeca
65 Torquemeter. Installation of an oblique double contact bearing.. Included in the definition package 2002-06-27 0 Turbomeca
67 "Le Bozec & Gautier" bleed valve. Addition of a close limit .. Included in the definition package 2002-06-27 0 Turbomeca
68 Fuel injection union. Installation of two "o'rings .. Included in the definition package 2002-06-27 0 Turbomeca
69 Bearings of the reduction gear drive pinion. Included in the definition package 2002-06-27 0 Turbomeca
70 Free turbine rear bearing. Addition of an axial load device Included in the definition package 2002-06-27 0 Turbomeca
71 Free turbine bearing. Inst of a bearing support.. Included in the definition package 2002-06-27 0 Turbomeca
72 Starter generator drive. Installation of MRC 1905 S bearings Included in the definition package 2002-06-27 0 Turbomeca
73 Installation of an intermediate casing made of INCONEL 625 Included in the definition package 2002-06-27 0 Turbomeca
74 Combustion chamber outer part. Included in the definition package 2002-06-27 0 Turbomeca
75 Installation of an injection wheel made from a forging blank Included in the definition package 2002-06-27 0 Turbomeca
76 Installation of a 2nd stage nozzle guide vane with a flexible hub Included in the definition package 2002-06-27 0 Turbomeca
77 Reduction gear. Toothing ratio 30/98 becomes 29/99 Included in the definition package 2002-06-27 0 Turbomeca
79 Cover of the centrifugal compressor. Included in the definition package 2002-06-27 0 Turbomeca
80 Drain valve of the fuel injection system. Included in the definition package 2002-06-27 0 Turbomeca
82 2nd stage gas generator turbine. Included in the definition package 2002-06-27 0 Turbomeca
85 FCU. Fuel pump bearings with Teflon flanks Included in the definition package 2002-06-27 0 Turbomeca
86 Reduction gear casing. Front part reinforced Included in the definition package 2002-06-27 0 Turbomeca
87 Fuel injection manifold. Included in the definition package 2002-06-27 0 Turbomeca
88 Combustion chamber outer part. Included in the definition package 2002-06-27 0 Turbomeca
89 External section of combustion chamber. Included in the definition package 2002-06-27 0 Turbomeca
92 FCU. New adjustment of the deceleration unit Included in the definition package 2002-06-27 0 Turbomeca
95 FCU. Change of material of Ng and Ntl springs .. Previously Embodied 2010-09-09 FCU S/N C500B
99 Replaced by TU215 Included in the definition package 2002-06-27 0 Turbomeca
100 Installation of a 2nd stage turbine nozzle guide vane .. Included in the definition package 2002-06-27 0 Turbomeca
101 Addition of a ring for curviccoupling sealing .. Included in the definition package 2002-06-27 0 Turbomeca
102 Fuel distributor of the main injection system. Included in the definition package 2002-06-27 0 Turbomeca
105 Free turbine rear bearing. Included in the definition package 2002-06-27 0 Turbomeca
292.72.0069 106 M05. Reduction gear rear casing. Embodied 2010-11-18 MO5 S/N 9975
107 Fuel injection distributor. Fuel pipe and sleeve .. Included in the definition package 2002-06-27 0 Turbomeca
108 Combustion chamber inner part. Included in the definition package 2002-06-27 0 Turbomeca
109 1st and 2nd stage turbine nozzle guide vane.. Included in the definition package 2002-06-27 0 Turbomeca
110 Injector electro-valve. Suppression of emergency manual ctrl Included in the definition package 2002-06-27 0 Turbomeca
111 FCU. Inst of reinforced spring to hold metering valve diaphragm Previously Embodied 2010-09-09 FCU S/N C500B
112 Free turbine front bearing. Installation of a labyrinth .. Included in the definition package 2002-06-27 0 Turbomeca
113 Installation of "Le Bozec" compressor bleed valve with axial outlet Included in the definition package 2002-06-27 0 Turbomeca
116 Engine control and indicating harness. Installation of a plug.. Included in the definition package 2002-06-27 0 Turbomeca
117 1 st stage gas generator turbine wheel. Addition of "chamfer".. Included in the definition package 2002-06-27 0 Turbomeca
118 2nd stage gas generator turbine wheel. Addition of "chamfer".. Included in the definition package 2002-06-27 0 Turbomeca
119 Rotating assembly. Fitting of turbine bolt in INCO 718 material Included in the definition package 2002-06-27 0 Turbomeca
120 Gas generator rear bearing oil return pipe of 0.8 mm thickness Included in the definition package 2002-06-27 0 Turbomeca
121 FCU. Installation of a reinforced spring Previously Embodied 2010-09-09 FCU S/N C500B
125 FCU. Addition of a 0.5 mm jet on the metering valve .. Previously Embodied 2010-09-09 FCU S/N C500B
292.72.0209 126 Axial compressor. Installation of NC19FeNb axial bolt Included in the definition package 2002-06-27 0 Turbomeca
129 Free turbine bearing. Improvement of the lubrication .. Included in the definition package 2002-06-27 0 Turbomeca
130 1st stage turbine nozzle guide vane. Vanes made of KCN 22 W Included in the definition package 2002-06-27 0 Turbomeca
132 Turbine casing. Plate sheets and bosses made of NC 22 CNb. Included in the definition package 2002-06-27 0 Turbomeca
134 Free turbine bearing pressurisation. Inst of P2 pipe (pre TU 59) Included in the definition package 2002-06-27 0 Turbomeca
135 Module M05 (reduction gear). Improvement .. Included in the definition package 2002-06-27 0 Turbomeca
140 Oil filter. Addition of a stop in front of the by-pass plug Included in the definition package 2002-06-27 0 Turbomeca
142 Introduction of retainers on the oil transfer tubes .. Included in the definition package 2002-06-27 0 Turbomeca
143 Accessory gear box. Installation of 2 SNFA bearings .. Included in the definition package 2002-06-27 0 Turbomeca
144 Gas generator rear bearing lubricating oil pipe. Included in the definition package 2002-06-27 0 Turbomeca
145 Min oil pressure switch supply pipe. Installation of a clamp .. Included in the definition package 2002-06-27 0 Turbomeca
146 Oil return pipe of the gas generator rear bearing. New routing Included in the definition package 2002-06-27 0 Turbomeca
147 Front bearing lubricating pipe. Addition of a clamp .. Included in the definition package 2002-06-27 0 Turbomeca
292.72.0108 149 M02. Inst of generator 1st & 2nd stage turbine with sealed roots Embodied 2010-11-18 MO2 S/N 3741
292.72.0094 150 Identification plate of module M03 Included in the definition package 2002-06-27 0 Turbomeca
151
Free Wheel Shaft Assy
Previously Embodied 2010-09-21 Free Wheel Shaft
Assy S/N 3182B
292.72.0109 152 M03. Intro of sealing segment between 1st & 2nd stage gas gen.. Embodied 2010-11-18 MO3 S/N 9936
153
Free Wheel Shaft Assy
Previously Embodied 2010-09-21 Free Wheel Shaft
Assy S/N 3182B
154 Heat shield securing. Repl of 2 mounting tabs by securing strap Included in the definition package 2002-06-27 0 Turbomeca
155 Gas generator rear bearing. Inst of bearing with reduced.. Included in the definition package 2002-06-27 0 Turbomeca
158 FCU. Constant AP device equipped with matched valve & guide Embodied on non-modular elements 2002-06-27 0 Turbomeca
158 FCU. Constant AP device equipped with matched valve & guide Embodied on complete engine 2002-06-27 0 Turbomeca
162 Increase of the clearance on the free turbine bearing support Included in the definition package 2002-06-27 0 Turbomeca
163 M03. 2nd stage generator nozzle guide vane. Embodied 2010-11-18 MO3 S/N 9936
164 Accessory gearbox. Fitting of a magnetic plug Included in the definition package 2002-06-27 0 Turbomeca
165 Replaced by TU259 Included in the definition package 2002-06-27 0 Turbomeca
166 Free turbine/reduction gear coupling sleeve.. Included in the definition package 2002-06-27 0 Turbomeca
292.72.0122 167 Power shaft. Press fitting of the 52 tooth-pinion Included in the definition package 2002-06-27 0 Turbomeca
168 Gas generator 1st stage turbine blades. Included in the definition package 2002-06-27 0 Turbomeca
170 M05. Reduction gearbox. Replacement of a normal screw.. Included in the definition package 2002-06-27 0 Turbomeca
171 Compressor bleed valve. Addition of a 3 way union.. Included in the definition package 2002-06-27 0 Turbomeca
292.72.0130 173 Protection of 1st stage turbine blades Embodied 2010-11-18 MO3 S/N 9936
292.72.0127 174 M03. Injection manifold Embodied 2010-11-18 MO3 S/N 9936
292.72.0124 175M02. M03. Rotating assy. Addition of a curvic-coupling sealing ring..
Embodied 2010-11-18MO2 S/N 3741,
MO3 S/N 9936
292.72.0124 175 M03. Rotating assy. Addition of a curvic-coupling sealing ring.. Embodied 2010-11-18 MO3 S/N 9936
292.73.0121 176 FCU flyweight assembly. Replacement of bearing Previously Embodied 2010-09-09 FCU S/N C500B
292.73.0133 183 FCU. Replacement of the thermal compensating capsule Previously Embodied 2010-09-09 FCU S/N C500B
292.75.0132 184 M03. Unions of the clean P2 air tapping points for the FCU.. Embodied 2010-11-18 MO3 S/N 9936
292.72.0135 188 Compressor bleed valve. Opening threshold at Ng = 93% Embodied on non-modular elements 2002-06-27 0 Turbomeca
292.72.0135 188 Compressor bleed valve. Opening threshold at Ng = 93% Embodied on complete engine 2002-06-27 0 Turbomeca
292.72.0136 189 Accessory gearbox. 23 tooth bevel gear Embodied 2010-11-18 MO1 S/N 9845
292.72.0139 195 Gas Generator rear bearing Embodied 2010-11-18 MO3 S/N 9936
A292.72.0212 197 Inspection of 2nd stage turbine NGV2 mod to TU197 standard Engine not concerned 2010-09-21 MO3 S/N 9936
292.73.0147 198 FCU. Conic section of the constant delta P valve Previously Embodied 2010-09-09 FCU S/N C500B
292.73.0160 199
Fuel system. Improvement of the start drain valve
Previously Embodied 2010-08-19 Starting Drain
Valve S/N 1165M
292.73.0148 200 FCU. Staked housing sleeve Previously Embodied 2010-09-09 FCU S/N C500B
292.72.0149 201 New routing of pipe Embodied 2010-11-18 MO1 S/N 9845
A292.72.0150 202 2nd stage NGV of the gas generator Previously Embodied 2010-11-18 MO3 S/N 9936
F-2002-
258(A)292.72.0265 204 Cancellation of incorporation of TU204 Engine not concerned 2010-11-18
MO3 S/N 9936
98.394(A) 292.72.0163 208 Installation of a chip detector with electric warning Embodied 2010-11-18 MO1 S/N 9845
90.105(B)R1 292.72.0140 211Free wheel shaft assy - inst of a free wheel flange..
Cancelled by TU 221
90.105(B)R1 292.72.0141 212
Freewheel Shaft Assy. New manufacture
Previously Embodied 2010-09-21 Free Wheel Shaft
Assy S/N 3182B
292.77.0154 214A Indicating and control harness Embodied on non-modular elements 2002-06-27 0 Turbomeca
292.77.0154 214A Indicating and control harness Embodied on complete engine 2002-06-27 0 Turbomeca
1995.069
(A)R3292.72.0175 215
M04. U-shaped INCO 625 containment shieldEmbodied 2010-11-18
MO4 S/N 10274
292.71.0155 216A Permanent installation of the vibration pick up Embodied on non-modular elements 2002-06-27 0 Turbomeca
292.71.0155 216A Permanent installation of the vibration pick up Embodied on complete engine 2002-06-27 0 Turbomeca
292.73.0176 217 FCU. Addition of a second sealing ring Previously Embodied 2010-09-09 FCU S/N C500B
91.156(B)R1 292.72.0146 221
Freewheel shaft assy. Limitation of dynamic deflection
Previously Embodied 2010-09-21 Free Wheel Shaft
Assy S/N 3182B
292.75.0171 231 Installation of a strainer union for P2 air tapping Embodied 2010-11-18 MO3 S/N 9936
2009-0002 292.72.0276 232 Reduction gearbox intermediate pinion Embodied 2010-11-18 MO5 S/N 9975
292.72.0172 234A Intermediate pinion. Increase of the minimum value Embodied 2010-11-18 MO5 S/N 9975
NO SB 240A M05. Reduction gearbox front casing. Inst. magn. plug Embodied 2010-11-18 MO5 S/N 9975
292.77.0164 241A Accessory gearbox. Installation of torquemeter pickup Embodied 2010-11-18 MO1 S/N 9845
292.72.0167 244 Combustion chamber outer part Embodied 2010-11-18 MO3 S/N 9936
292.72.0196 245 Power shaft provided with an oil collector Embodied 2010-11-18 MO1 S/N 9845
292.75.0193 247A Installation of an attachment bracket for the reinforced.. Embodied 2010-11-18 MO5 S/N 9975
292.72.0191 250 2nd stage turbine. Diameter increase of turbine housing Embodied 2010-11-18 MO3 S/N 9936
A292.72.0207 255 M04. Incorporation of mod TU255 Engine not concerned 2010-09-21
292.72.0204 257A Washer assembly. Increase of outer diameter Embodied 2010-11-18 MO3 S/N 9936
1995.069
(A)R3292.72.0208 259
Reduction gear. Installation of double supportEmbodied 2010-11-18
MO5 S/N 9975
292.72.0189 262 Injection system drain. Return to tank Embodied on non-modular elements 2002-06-27 0 Turbomeca
292.72.0189 262 Injection system drain. Return to tank Embodied on complete engine 2002-06-27 0 Turbomeca
292.73.0205 266A FCU. Improvement of sealing Previously Embodied 2010-09-09 FCU S/N C500B
292.72.0214 267 M03. Rear bearing. Installation of bearing Embodied 2010-11-18 MO3 S/N 9936
292.72.0219 268A M05. Angular off setting of anti torque washers Embodied 2010-11-18 MO5 S/N 9975
292.74.0203 271A Igniters with separated cables Embodied 2010-11-18 MO3 S/N 9936
292.73.0220 272 NTL bearing of the FCU. Increased lubrication Previously Embodied 2010-09-09 FCU S/N C500B
292.74.0221 273 Installation of HE generator of thyristor type Embodied on non-modular elements 2002-06-27 0 Turbomeca
292.74.0221 273 Installation of HE generator of thyristor type Embodied on complete engine 2002-06-27 0 Turbomeca
292.72.0215 274 Gas generator rear bearing. Installation of deflector Embodied 2010-11-18 MO3 S/N 9936
292.72.0217 275 M02. Tighter fit between cover and casing Embodied 2010-11-18 MO2 S/N 3741
292.72.0211 276 Axial compressor nut with a long base Embodied 2010-11-18 MO3 S/N 9936
292.72.0222 277A M03. 1st and 2nd stage diffuser Embodied 2010-11-18 MO3 S/N 9936
292.72.0223 278 M03. Injection manifold Embodied 2010-11-18 MO3 S/N 9936
292.77.0216 280 Control and indicating harness. Embodied on non-modular elements 2002-06-27 0 Turbomeca
292.77.0216 280 Control and indicating harness. Embodied on complete engine 2002-06-27 0 Turbomeca
292.72.0215 281 Transfer of lubricating jet Embodied 2010-11-18 MO3 S/N 9936
292.72.0227 282 Cancellation of TU282. Modif of manifold and injection wheel
292.72.0215 283 Internal diameter of oil scavange tube Embodied 2010-11-18 MO3 S/N 9936
292.72.0215 284 Gas generator rear bearing. Increased area Embodied 2010-11-18 MO3 S/N 9936
292.72.0228 286 M03. Injection wheel designed from Arriel 2 part Embodied 2010-11-18 MO3 S/N 9936
292.73.0240 289 Installation of protection box Embodied on non-modular elements 2002-06-27 0 Turbomeca
292.73.0240 289 Installation of protection box Embodied on complete engine 2002-06-27 0 Turbomeca
292.72.0241 290A Start and electrovalve bracket Embodied 2010-11-18 MO3 S/N 9936
292.72.0239 291A 1st stage gas generator turbine Embodied 2010-11-18 MO3 S/N 9936
292.74.0242 292A Igniters with separated cables Embodied 2010-11-18 MO3 S/N 9936
292.72.0243 293A Indicating magnetic plug Embodied on non-modular elements 2002-06-27 0 Turbomeca
292.72.0243 293A Indicating magnetic plug Embodied on complete engine 2002-06-27 0 Turbomeca
292.73.0250 299A Optimisation of starting drain valve sealing Previously Embodied 2010-08-19 Starting Drain
Valve S/N 1165M
F-2002-
126(A)292.72.0261 300 Compressor module. Installation of sleeve Embodied 2010-11-18
MO2 S/N 3741
292.72.0267 302A M01. Installation backlash of bevel gear Embodied 2010-11-18 MO1 S/N 9845
292.72.0199 306A Gas generator module. 1st and 2nd stage diffuser Embodied 2010-11-18 MO3 S/N 9936
292.73.0271 307 Fuel system. Ignition solenoid valve Embodied on non-modular elements 2002-06-27 0 Turbomeca
292.73.0271 307 Fuel system. Ignition solenoid valve Embodied on complete engine 2002-06-27 0 Turbomeca
292.72.0272 308A M01. Installation of one INFLEX mechanical magnetic plug Embodied 2010-11-18 MO1 S/N 9845
292.72.0279 314A M05. Installation of one INFLEX mechanical magnetic plug Embodied 2010-11-18 MO5 S/N 9975
F-2002-
126(A)292.72.0275 316A M02 compressor module. Bonding of sleeve Embodied 2010-11-18
MO2 S/N 3741
292.75.0326 326 Integration of an anti-contamination device at bleed valve inlet Konstaterat ej genomförd. 2015-09-03 SE.MG.0107
292.73.0327 327A FCU. Shoe of acceleration control unit Previously Embodied 2010-09-09 FCU S/N C500B
292.73.0329 329A FCU. Plasma coating on NTL flyweight support shaft Previously Embodied 2010-09-09 FCU S/N C500B
292.77.0331 331A Equipment/accessory. Thermocouple harness Embodied on non-modular elements 2007-05-15 Turbomeca
292.72.0332 332B M05. Replacement of the TRIPLEX ball bearing Embodied 2010-11-18 MO5 S/N 9975
292.73.0337 337 FCU. To ensure proper installation of constant delta P … Previously Embodied 2010-09-09 FCU S/N C500B
292.73.0344 344 FCU. Pressure reducing valve with improved sealing Embodied 2010-09-09 FCU S/N C500B
292.72.0347 347 M03. Modified 2nd stage turbine Embodied 2010-11-18 MO3 S/N 9936
292.72.0355 355 M03. Shortening of power turbine NGV lip Embodied 2010-11-18 MO3 S/N 9936
292.72.1357 357 M03. Small labyrinth with increased clearance Rev A embodied 2010-11-18 MO3 S/N 9936
292.72.0359 359 M01. Fastening of two spring strips Embodied 2010-11-18 MO1 S/N 9845
292.05.0103 Recording of operating hours/cycles N/A to 1D1 engines
292.72.0157 a) M05. Inspection of the magnetic plug N/A to POST TU 232
292.72.0157 b) Incorporating of TU39 N/A to POST TU 232
1990.064
(A)R1A292.72.0230
Checking of axial compressor erosion and cleaningEmbodied. Superseeded by AD 2012-0071 2008-10-07
MO3 S/N 9936
2012-0071 A292.72.0230Checking of axial compressor erosion and cleaning
Embodied (DCA/TUR/82) 2012-08-23MO2 S/N 3741,
MO3 S/N 9936
2007-0002 A292.72.0231 Position inspection of secondary air ducts - NGV2 Embodied 2010-11-18 MO3 S/N 9936
292.72.0237 Check and possible replacement of coupling sleeve Embodied 2010-11-18 MO5 S/N 9975
292.72.0246 Ultrasonic frequency inspection of centrifugal compressorEmbodied. Rev E: Integrated in Overhaul
Manual 2015-07-012010-11-18
MO3 S/N 9936
2006-0068 A292.73.0251 Check of the installation of the fuel unions Embodied 2010-09-21
2007-0045 292.75.0806 Military/paramilitary engines N/A to this engine
2009-0236 A292.72.0807 Gas Generator 2nd Stage Turbine - Inspection/replacement Found N/A. Superseded by 2012-0143 2010-11-18 MO3 S/N 9936
2012-0143 A292.72.0807 Gas Generator 2nd Stage Turbine - Inspection/replacement Found N/A. 2015-09-01 SE.MG.0107 MO3 S/N 9936
2007-
0018R1A292.72.0809
Relative position check of 2nd stage turbine bladesSuperseeded by 72.A292.0807
2009-0236 A292.72.0810 Gas Generator 2nd Stage Turbine - Inspection/replacement Found N/A. Superseded by 2012-0143 2010-11-18 MO3 S/N 9936
2008-0014 292.73.0817 FCU 3-way uniion plug N/A to 1D1 engines
292.73.0818 FCU. Check and replacement of the constant delta P … N/A to POST TU 337 engine
2009-0117-E 292.72.0825M05. Insp/repair of post TU332 lubrication ducts
Superseded by 2009-0245-E 2010-11-18MO5 S/N 9975
2009-0245-E 292.72.0825M05. Securement of post TU332 lubrication ducts
Embodied 2010-11-18MO5 S/N 9975
2009-
0112R1A292.72.0827
M04. Restricted use limit of the FT bladesN/A to M04 S/N 10274 2010-11-18
MO4 S/N 10274
2010-
0101R1A292.72.0831 M03. POST TU347 2nd Stg Turbine Disc - Reduced Life Limit
Embodied. Re-inforced Eddy Current Insp -
CFR applied2010-11-18 MO3 S/N 9936
2010-
0101R2A292.72.0831 M03. POST TU347 2nd Stg Turbine Disc - Reduced Life Limit
Embodied. Re-inforced Eddy Current Insp -
CFR applied2010-11-18 MO3 S/N 9936
2010-
0101R3A292.72.0831 M03. POST TU347 2nd Stg Turbine Disc - Reduced Life Limit
Embodied. Re-inforced Eddy Current Insp -
CFR applied2010-11-18 MO3 S/N 9936
2012-0117M03. High Ng Rating Vib Check after M03 deep maintenance
To be performed after M03 deep
maintenanceYes
2012-
0187R1 Cycle counting aid system - Modification/AmendmentFound embodied 2013-03-27
292.72.0836POST TU 360 engines. Operation in a dusty atmosphere. Determination of the limit
for first cleaning of the gas generator rotating assembly. Determination of the
optimal cleaning frequency for the gas generator rotating assy
TU 360 not embodied.
292.73.0837 FCU. Updated log card reflecting the TBO extension to 3,600 hrs Embodied 2014-06-20 FCU S/N C500B
2013-0120 A292.72.0838Module M04 (Free Turbine). Check of the presence, positioning and bonding of the
free turbine bearing plugM04 S/N 10274 not affected. MO4 S/N 10274
2014-0036 292.72.0839 41/23 bevel gear of accessory gearbox (Moduel M01) During every qualifying shop visit MO1 S/N 9845
292.72.0841Fuel injection manifold chemical cleaning. Method 2: Injection with a special tool
inserted through the start injectors and igniter plugsNot performed.
292.71.0843 Creation of a configuration applicable to ARRIEL 1A1, 1A2, 1B, 1C, 1C1, 1C2, 1D,
1D1, 1E2, 1K, 1K1, 1S and 1S1 turboshaft engines during overhaul
Not performed.
292.72.0845 Visual check of power turbine (PT) blades Not performed.
ENG Engine Arriel 1D1 9835 5270,2 7527,5 7528,6
Engine Starts: 8609, Ng
Cycl: 9052,70, Np Cycl:
9607,60
ENG*MO1 (Accessory
Gearbox)70BM015420 9845 - 15Y 5270,2 2010-11-29 1532,80 2025-11-25
ENG *MO2 (Axial Compressor) 70BM025020 3741 - 7200FH/15Y 5270,2 1531,70 2010-11-29 1532,805667,2 /
2025-11-25
Intermediate insp 3600FH
(Task 05-20-10-201-886)
2068,30FH remaining (Se
rad 184)
ENG **Axial Comp Wheel 2292152810 3777FB 14,000 Ng Cycl - 5270,2 9041,95C 9052,70C 4947,30C
ENG **FWD Ball Bearing 9609000166 18520 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG **AFT Ball Bearing 9609000166 18702 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG **Tail Gear Bearing 9606490202 23707 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG*MO3 (Gas Generator)
Ng70BMO35420 9936 - 3600FH/15Y 5270,2 1531,70 2010-11-29 1532,80
2067,2 /
2025-11-25
ENG **Centrifugal Impeller .0292252930 2329FT 14,000 Ng Cycl - 5270,2 9041,95C 9052,70C 4947,30C
ENG **Injection Wheel .0292254010 962AD 10,000 Ng Cycl - 5270,2 9041,95C 9052,70C 947,30C
ENG **1st Stage Disk .0292253240 ADH3973AD 10,000 Ng Cycl - 5270,2 9041,95C 9052,70C 947,30C
ENG **2nd Stage Disk .0292250400 J902AD 6,500 Ng Cycl - 5270,2 3563,15C 3573,90C 2926,10C AD 2010-0101R3
ENG**2nd Stage NGV FWD
Hub2292401800 10961PR 3,600FH - 5270,2 1531,70 1532,80 2067,20
ENG **2nd Stage NGV AFT Hub 2500019278 10744PR 3,600FH - 5270,2 1531,70 1532,80 2067,20
ENG **Bearing 9609000562 3273 3,600FH - 5270,2 1531,70 1532,80 2067,20
ENG**1st Stage Turbine
Blades229225A1L0 CC7/1 6000FH/12000 Ng Cycl - 5270,2
1531,70/
3563,15C
1532,80/
3573,90C
4467,20/
8426,10C
**2nd Stage Turbine 1531,70/ 1532,80/ 5667,20/ ENG
**2nd Stage Turbine
Blades.029225A2S0 XL5 7200FH/10000 Ng Cycl - 5270,2
1531,70/
3563,15C
1532,80/
3573,90C
5667,20/
6426,10C
ENG *MO4 (Free Turbine) Nf 70BMO45410 10274 - 7200FH/15Y 5270,2 1531,70 2010-11-29 1532,805667,2 /
2025-11-25
Intermediate insp 3600FH
(72.50.10) 2068,30FH
remaining.
ENG **Free Turbine Disk 2292802500 ADH4674AD 10,000 Np Cycl - 5270,2 9590,60C 9607,60C 392,40C
ENG **FWD Ball Bearing 9609000166 18661 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG **AFT Ball Bearing 9609000166 18652 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG **Roller Bearing 9606080705 5526 3,600FH - 5270,2 1531,70 1532,80 2067,20
ENG **Free Turbine Blades 029280A1N0 G22/1 7200FH/12000 Np Cycl - 5270,21531,70/
5328,90C
1532,80/
5345,90C
5667,20/
6654,10C
ENG*MO5 (Reduction
Gearbox)70BMO55420 9975 - 3600FH/15Y 5270,2 1531,70 2010-11-29 1532,80
2067,2 /
2025-11-25
ENG **FWD Drive Bearing 9609000397 149 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG **AFT Drive Bearing 9609000397 195 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG **FWD Int. Bearing 9609000247 8227 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG **AFT Int. Bearing 9609000247 8380 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG **Torquemeter Bearing 9609000631 2608 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG **Output Ball Bearing 9609000139 5184 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG **Output Roller Bearing 9609000266 5481 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG **Coupling Sleeve .0292708020 3764SET 3,600FH - 5270,2 1531,70 1532,80 2067,20
ENG **Left-Hand Nut .0292701370 83 3,600FH - 5270,2 1531,70 1532,80 2067,20
ENG *FCU Assy .0164540200 C500B - 3600FH/10Y 5270,2 1531,70 2010-12-01 1532,802067,20 /
2020-09-09Overhauled 2010-09-09
ENG **FCU Filter - - 3,000FH - 5270,2 1531,70 1532,80 1467,20
ENG *Free Wheel Shaft Assy .0292907680 3182B - 3600FH 5270,2 1531,70 1532,80 2067,20Overhauled 2010-09-21
ENG **Free Wheel 9560157860 6959 3,600FH - 5270,2 1531,70 1532,80 2067,20
ENG **Bearing 9608650901 7525SN 7,200FH - 5270,2 1531,70 1532,80 5667,20
ENG **Free Wheel Shaft .0292907740 426 12,000FH - 5270,2 1531,70 1532,80 10467,20
ENG *Starting Drain Valve .0174078030 1165M - 10Y 2010-09-16 2020-09-13
ENG *Drain Valve .0174126090 D032B - 10Y 2010-09-16 2020-09-13Overhauled 2009-03-16
77.10 *Tachometer 64550-007-1 (704A37611002) 21446 N/A N/A Moved from Eng 19047 to
new Eng 9835
77.20 *Oil Pressure Transmitter 64279-004-1 (704A37642060) 5194 N/A N/A Moved from Eng 19047 to
new Eng 9835
STC Subject Note!
FAA SR01452LA / EASA.IM.R.S.00292 Installation of an AKV, Inc. (formerly AKV Partners) Ng cycle counter, p/n 350NGTEC, in accordance with
Master Drawing List no NCC-001, Rev. B, dated January 10, 2004, or later FAA-approved revisions. The
present STC is the validation of the FAA STC SR01452LA whose FAA date of reissuance and amendment is
February 18, 2004.
Inst. but deaktivated.
Provision still installed
JCAB 97-109 / LFV 142/01 Sliding Window. JCAB 97-109 approved 1997-07-11. LFV approved 2001-11-29. LFV Flight Manual
Supplement Nr. S 46/01
Inst.
JCAB 97-107 / LFV 142/01 Floor Camera Hole. JCAB 97-107 approved 1997-07-11. LFV approved 2001-11-29. Inst.
TCCA SH91-20 / FAA SH856NE / LFV
139/01 / EASA.IM.R.S.01492
D350-561 Cargo Mirror Installation. TCCA approved 1991-04-10, FAA approved 2000-02-15, LFV approved
2001-11-18, EASA approved 2010-09-03. Installation of Dart Aero Accessories Inc. Cargo mirror in
accordance with Dart Aero Accessories Inc. Drawing D350-561, Revision B, dated March 29, 1991.
STC removed
TCCA SH92-18 / DGAC 44/96 / FAA
SH989NE / LFV 110/97 /
EASA.IM.R.S.01560
DGAC approved 1996-11-15, FAA approved 2009-06-30, EASA approved 2009-07-17. Installation of D350-
567 Vertical Reference (Floor) Window in accordance with Dart Aerospace Ltd. Installation Instructions
D350-567, Revision D, dated July 8, 2008 or later Transport Canada revision.
Inst.
Interval Action Reference Performed Due Notes
600FH Vertical Refefens Window Dart ICA-D350-567-R2 5270,2FH 5870,2FH STC
600FH Starter-Generator damper system Airbus SB 05.00.75 5270,2FH 5870,2FH
600FH Upper/Lower fin spar attachment Airbus SB 05.00.53 5270,2FH 5870,2FH
100FH/6M Hydraulic Pump Drive Shaft Splines Airbus ASB 29.00.045270,2FH /
2015-11-21
5370,2FH /
2016-05-21
6Y ELT Testing Kannad CMM 25-63-05 2015-11-06 2021-11-06
Batt exp date or
transmitting >1hELT Battery Kannad CMM 25-63-05 - 2017-09-01
6Y Corrosion lower bearing/splines M/R shaft Airbus SB 05.00.32 2015-11-21 2021-11-21
2Y Altimeter Indicator Check LFS 1980:5 (BCL-M 4.3) § 6 2015-10-13 2017-10-13
2Y Airspeed Indicator Check LFS 1980:5 (BCL-M 4.3) § 7 2015-10-13 2017-10-13
2Y Compass Deviation Check LFS 1980:5 (BCL-M 4.3) § 8 2012-08-08 2014-08-08
On the deferred
maintenance list
from PHAB
WO17220006.
165FH T/R Drive Shaft Bearings EASA AD 2015-0195 5270,2FH 5435,2FH
Repetitive (National) Requirements
4500FH/60000TC M/R Drive Cross Bar EASA AD 2015-00945270,2FH /
34216TC
9770,2FH /
94216TC
30FH T/R Pitch-Change Links EASA AD 2010-0006 5270,2FH 5300,2FH
660FH/2Y Coll. Pitch Lever Locking Stud EASA AD 2009-00195270,2FH /
2015-11-21
5930,2FH /
2017-11-21
2Y Mode S/C Transponders LVD 2-3368R1 2015-12-08 2017-12-08
550FH Rear Structure Junction Frame EASA AD F-2004-035 5270,2FH 5820,2FH
100FH Door ”Clear Vision” Window EASA AD F-1993-090-067R1 5270,2FH 5370,2FH
6500 Ng Cycl Second Stage Turbine Disc EASA AD 2010-0101R3 2010-09-212926,10 Ng Cycl
left
ALF/10FH Tail Rotor–Laminated Half-bearings – Inspection / Replacement EASA AD 2012-0257 5270,2FH 5280,2FH / ALF
165FH Tail Rotor Hub Pitch Horn – Inspection / Replacement EASA AD 2013-0133 5270,2FH 5435,2FH