dehavillano bombardier dashb · bombardier inc. highly recommend that modsum 80900267 be...

•

deHAVILLANO BOMBARDIER DASHB

SERVICE BULLETIN ____ Customer _____________________ _

Support

ATA SYSTEM: 5251 NUMBER: 8-52-61

.. -· .. ,_

BOMBARDIER AEROSPACE REGIONAL AIRCRAFT CONSIDER THIS SERVICE BULLETIN TO BE PARTICULARLY SIGNIFICANT AND

URGES OPERATORS TO PROMPTLY EVALUATE THE CONTENTS ,_ .. , .,

SUBJECT: Doors - Cockpit Door - Latch Block Replacement and Rework of Strike Plate - ModSum 80902145

1. PLANNING INFORMATION

A. Effectivity

Aircraft Affected:

1,

In-Service: DHC-8 Aircraft Models 102, 103, 106, 201, 202, 301, 311, 314 and 315 Serial Numbers 452, 464, 490, 506, 508 thru 557 with Pre-Requisite ModSum 80900267 / Service Bulletin 8-52-58 incorporated.

Production: ModSum 80902145 is not applicable to production aircraft.

NOTE: The instructions in this Service Bulletin are only applicable to the systems and parts installed at the time of delivery on the aircraft or as changed by Bombardier Aerospace Service Bulletin(s). Before you do this bulletin, examine all STC or equivalent action changes to make sure this bulletin can be completed.

20 Oct 2006 S.S. 8-52-61 of 10

SERVICE BULLETIN 8-52-61

Spares Affected:

None

B. Reason Problem: An operator has reported an inability to perform the door emergency

removal test after incorporation of ModSum 80900267 (Service Bulletin 8-52-58).

Cause: Completion of the door emergency removal test was prevented by fouling of the door latch on the strike plate and latch block.

Solution: This ModSum / Service Bulletin provides a new latch block and elongation of the slot in the striker plate.

C. Description

The procedures in this service bulletin give the instructions to do the tasks that follow:

- The flight compartment door is removed

- The strike plate and latch block are removed from the door right hand post

- A new latch block is bonded to the door right hand post with a kept retaining plate and screws

- The slot in the strike plate is elongated and the plate is re-installed with existing fasteners

- The flight compartment door is installed and tested

- Log entries are made

D. Compliance

Bombardier Inc. highly recommend that ModSum 80900267 be incorporated at the earliest opportunity unless otherwise directed by the operator's airworthiness authority.

NOTE: Operators of aircraft under the authority of Transport Canada should refer to Airworthiness Directive CF-2005-34R1 (pending)

E. Approval

The technical content of this Service Bulletin has been approved under the authority of the Transport Canada Civil Aviation (TCCA) Design Approval Organization No: DAO #93-0-02.

20 Oct 2006 S.S. 8-52-61 of 10


F. Manpower

It will take an estimated 3.00 man-hours to complete this Service Bulletin. The breakdown of the man-hours is shown in the table that follows:

TASK MAN-HOURS

Job Set-Up 0.00

Procedure 3.00

Test I RTS 0.00

Close-Out 0.00

All costs to incorporate this modification are the responsibility of the Operator

G. Material - Price and Availability

Latch Block 821590-065 is available through the Customer Accounts Service Team at Bombardier Aerospace Regional Aircraft division. Operators should submit a purchase order specifying aircraft serial number(s) to:

Bombardier Aerospace Customer Accounts Services Team (Mail Stop N11-32} 123 Garratt Blvd. Downsview Ontario Canada M3K-1 Y5

Facsimile: (416) 375-3060 Telephone : (416) 375-3920

Part Number

821590-065

Description

Latch Block Assy

H. Tooling - Price and Availability

None

20 Oct 2006

Price (US$)

Quoted at time of order

Delivery

Will be given at time of order

S.S. 8-52-61 of 10


I. Weight and Balance

None

J. Electrical Load Data

Not affected

K. Publications Affected

Dash 8 Illustrated Parts Catalogue . . .... . ....... .. .... PSM 1 -8-4 and

PSM 1-82-4 and

PSM 1-83-4

Modifications Manual .... . ......... . .......... . ..... PSM 1-813-12

L. References

The initial issue of this service bulletin was prepared to the engineering drawings and related data that follows:

DRAWING SHEET REV

8MK4092 1 -H 826337 1 -B

ModSum 8Q902145 Rev-A

ModSum 8Q900267 Rev-C. (Service Bulletin 8-52-58 Rev 'A')

Transport Canada Airworthiness Directive CF-2005-34R1 (pending)

2. MATERIAL INFORMATION

A. Parts Required per Aircraft

Part Number Qty per Description Remarks Aircraft

821590-065 1 Latch Block Assy

In addition to the above parts, the following materials are required for the completion of this service bulletin and may be manufactured by the operator, procured as single items from Bombardier Aerospace Regional Aircraft or purchased directly from industry sources. Addresses of manufacturers and suppliers not shown below are listed in either Maintenance Manual Chapter 20 or in Structural Repair Manual Chapter 51.

20 Oct 2006 S.B. 8-52-61 of 10


Part Number Qty per Description Remarks Aircraft

EC 1357N 3 oz. Adhesive OHMS A6.II Type II Class I

RTV 1 02 or 732 3 oz. Sealant DSC 233-2 (white silicone)

9185 (414.12) 1 oz. Primer (base) .. .. 402 1 oz . Hardener .. ... 62 1 oz . Thinner

Mankiewicz Gerber & Co.

DA 2.8 (404.12) 1 oz. Paint (Grey Cloud) ... .400 1 oz . Hardener ..... 62 Thinner

Primer 9185 (414.12) and paint DA 2.8 (404.12) is available from:

Mankiewicz Gerber & Co. Georg-Wilhelm Strasse 189, 021107 Hamburg, Germany

Telephone: +49 (0) 40 75 1 O 30 Facsimile: +49 (0) 40 75 1 o 34 15 E-mail [email protected]

NOTE: This service bulletin is self-contained (illustrated). No drawings will be supplied.

B. Parts Required to Modify Spares

None

C. Special Tools and Equipment Required

None

20 Oct 2006 S.B. 8-52-61 of 10


D. Existing Parts Accountability

The following parts may be affected by this service bulletin. Indented parts are components of the next higher assembly. The quantity (Qty.) column lists the quantity that may be affected per aircraft for non-indented parts and the quantity per next higher assembly for indented parts.

Existing New Part Part Number Description Qty. IC DC Number PNC

5411 Latch Block 1 A DIS 821590-065 s 9701109-1 Strike plate 1 A RWK 826337-101 s

IC Interchangeability Code

A Not interchangeable. B Removed Part. No direct replacement. C Conditionally Interchangeable. Installation of superseded part negates the

intent of this service bulletin.-

DC Disposition

DIS Discard Part. MUI Multiple Usage Item: Return to stock if serviceable. RWK Rework existing part in accordance with this service bulletin. RWI Rework existing part per ..... SAL Salvage. Return to operator's stores for salvage consideration.

PNC Part Number Code

N No equivalent Bombardier Inc. part number for reworked part. Indicate on part that this service bulletin has been accomplished. ·

R Part number after rework. · S Superseding or equivalent part number. X Reworked part and superseding part are functionally and physically

equivalent but not identical.

20 Oct 2006 S.B. 8-52-61 of 10


3. ACCOMPLISHMENT INSTRUCTIONS

A. Procedure

(1) In aircraft with ModSum 8Q900267 (Service Bulletin 8-52-58) already incorporated, open the flight compartment door.

(2) Remove strike plate 9701109-1 from the right hand door post and keep with fasteners.

(3) Elongate the slot in the strike plate as shown in Figure 1. Touch up bared metal. Re-identify the strike plate as 826337 -101.

(4) Carefully remove existing latch block (bonded and on pins) from the right hand door post. Do not damage the surrounding decorative finish. Keep the plate and fasteners and discard the latch block.

(5) Clean door post and bond new latch block 821590-065 to existing location (pins) with adhesive EC 1357N or equivalent (refer to Maintenance Manual (AMM) Chapter 20-25-55 or Task 20-25-55-390-801).

(6) Paint bared spot on door edge. Use equivalent to primer 9185 (base 414.12 with hardener 402 and thinner 62). Finish with Grey Cloud DA 2.8 (base 404.12 with hardener 400 and thinner 62).

(7) Apply a fillet of sealant RTV 102 or RTV 732 or equivalent around all edges of the latch block (refer to AMM Chapter 20-25-50 or Task 20-25-50-300-801 ).

(8) Install reworked strike plate 826337-101 with kept screws NAS514P1032-8.

~ Do the following Door Removal Function Test:

(a) / With the door in its closed and latched position, pull the upper two hinge J pins down and place the red pegs in their detentes.

C9J/ Push the door aft until the hinges are clear of the door and allow the door ,n to drop off the bottom hinge. This may be assisted by pushing down on

~· , J the red strap located about the mid-point of the door.

20 Oct 2006

Rotate the door to starboard, releasing it from the latch, taking care not to damage the surrounding decor panels.

Re-install flight compartment door.

S.B. 8-52-61 of 10

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ORIGINAL BLOCK

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TOUCH-UP STRIKE PLATE

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ELONGATE LATC~7 SLOT AS REQ'D

STRIKE PLATE 826337-101 "'

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S.S. 8-52-61 of 10


yclos,Out · (u/ ~ove all tools and equipment from the work area.

©An incorporation of this ModSum, make an entry that conforms to local regulatory requirements in the applicable logbook(s}. Enter component serial numbers if applicable. Enter this ModSum number only after complete and functional incorporation of all work defined in this service bulletin.

20 Oct 2006 S.B. 8-52-61 of 10


This Page Intentionally Blank

20 Oct 2006 S.B. 8-52-61 of 10

BOMBARDIER

SERVICE BULLETIN (SB) - RECORD OF INCORPORATION - Q SERIES DASH 8 AIRCRAFT

To: Partner Data Co-Ordinator (Toronto)

Bombardier Aerospace Regional Aircraft

Phone: (1) 416 375 3534

From: ----------------Company:---------------

Phone: Extn: --------- -----Facsimile: (1) 416 375 4538 Facsimile: Date: -------- -----E-mail: [email protected] E-mail: ___________ _

The data that you provide below will help us record the incorporation of this modsum and the aircraft effectivity in the maintenance manual.

Operator: Service Bulletin: Revision:

Aircraft Serial Number: Model Number: Date Bulletin Completed :


Aircraft Serial Number: Model Number: Date Bulletin Completed:










Fax this sheet to (1) 416 375 4538 or PDF to:

[email protected] -~-

BOMBARDIER

SERVICE BULLETIN (SB) COMMENT SHEET - Q SERIES DASH 8 AIRCRAFT

To: SB Focal (Toronto) "Bob Barriault"

Bombardier Aerospace Regional Aircraft

Phone: (1) 416 375 4078

Facsimile: (1) 416 375 4538

From: ______________ _

Company: ____________ _

Phone: Extn: -------- -----Facsimile: Date: ------- -----

E-mail: [email protected] E-mail: _____________ _

Select appropriate box(es) and add comments or suggestions you would like us to know that may enhance the quality of our service bulletins.

Service Bulletin: Revision: ModSum: ------- --- --------1. PLANNING INFORMATION

D Effectivity

D Approval

D Electrical Load

D Reason

D Manpower

D Tooling

2. MATERIAL INFORMATION

D Description

D Material

D References

o Compliance

D Weight and Balance

D Publications Affected

D Kit Content D Special Tools/Equipment D Parts to Modify Spares

D Consumables D Disposition of Existing Parts D Other ----------

3. ACCOMPLISHMENT INSTRUCTIONS

D Procedure o Close-Out o Test D Job Set-Up

D lllustration(s) D Other ___________________ _

4. COMMENTS, REMARKS, SUGGESTIONS

Fax this sheet to (1) 416 375 4538 or PDF to:

bob.barriau lt@aero. bombardier.com Nov200f

'

AIRWORTIDNESS DIRECTIVE

www.faa.gov/aircraft/safety/alerts/ www.gpoaccess.gov/fr/advanced.html

U.S. Department of Transportation

Federal Aviation Administration

2006-12-16 Bombardier, Inc. (Formerly de Havilland, Inc.): Amendment 39-14642. Docket No. FAA-2006-2441 l; Directorate Identifier 2006-NM-033-AD.

Effective Date

(a) This AD becomes effective July 18, 2006.

Affected ADs

(b) None.

Applicability

(c) This AD applies to Bombardier Model DHC-8-102, -103 , -106, -201, -202, -301, -311 , -314,

and -315 airplanes, certificated in any category; serial numbers 003 through 557 inclusive; equipped

with cockpit door installation part numbers (P/Ns) identified in Table 1 of this AD.

Unsafe Condition

TABLE 1.-COCKPIT DOOR INSTALLATIONS AFFECTED BY TIDS AD

PIN Dash No.(s) 82510074 All. 82510294 All. 82510310 -001 824597 -001 H85250010 All. 82510700 All. 82510704 All except -502 and - 503.

(d) This AD results from a report that, during structural testing of the cockpit door, the lower hinge block rotated and caused the mating hinge pin to disengage, and caused excessive door deflection . We are issuing this AD to prevent failure of a door attachment, which could result in uncontrolled release of the cockpit door under certain fuselage decompression conditions, and possible damage to the aircraft structure.

Compliance

(e) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.

4

Modification

(f) Within 24 months after the effective date of this AD, modify the cockpit door from a singlepoint attachment to a two-point attachment in accordance with the Accomplishment Instructions of the applicable service bulletin in Table 2 of this AD.

TABLE 2.-BOMBARDIER SERVICE BULLETINS Use this Bombardier service bulletin-

8-52-54, Revision A, dated November 5, 2004

8-52-58, dated May 12, 2004

For airplane serial numbers-003 through 451 inclusive, 453 through 463 inclusive, 465 through 489 inclusive, 491 through 505 inclusive, and 507. 452, 464, 490, 506, and 508 through 557 inclusive.

Note 1: Bombardier Service Bulletin 8-52-54 refers to Bombardier Series 100/300 Modification Summary (Mods um) 8Q 100859 as an additional source of service information for installing a hinge pin with a two-point attachment. Bombardier Service Bulletin 8-52-58 refers to Bombardier Series 100/300 Mods um 8Q900267 as an additional source of service information for reworking and installing the cockpit door, and reworking the lower hinge attachment to provide a downward-facing pin with a two-point attachment.

Prior/Concurrent Requirements

(g) Prior to or concurrently with the modification in paragraph (f) of this AD, do the applicable actions specified in Table 3 of this AD according to a method approved by either the Manager, New York Aircraft Certification (ACO), FAA; or Transport Canada Civil Aviation (TCCA) (or its delegated agent). One approved method is the applicable modification or Modsum listed in the "One approved method for doing these actions" column of Table 3 of this AD.

TABLE 3.-BOMBARDIER SERVICE BULLETINS For airplanes affected

by Bombardier Service Bulletin-

8-52- 54, Revision A, dated November 5, 2004.

8- 52-58, dated May 12, 2004

That have these serial numbers-

003 through 407 inclusive, 409 through 412 inclusive, and 414 through 433 inclusive.

452, 464, 490,506, and 508 through 557 inclusive.

Do these actions-

Rework the cockpit door emergency release. Install a new label regarding alternate release of the door. Install the cockpit door Install the cockpit door Install the cockpit door with a blow-out door panel.

5

One approved method for doing these actions-

De Havilland Aircraft of Canada, Limited, Modification 8/2337. De Havilland Aircraft of Canada, Limited, Modification 8/3339. Bombardier Series I 00/300 Mods um 8Q200015. Bombardier Series 100/300 Modsum 8Q420101. Bombardier Series 100/300 Modsum 8Q420143.

Actions Done In Accordance With Previous Revision of Service Bulletin

(h) Actions done before the effective date of this AD in accordance with Bombardier Service

Bulletin 8-52-54, dated May 12, 2004, are acceptable for compliance with the corresponding requirements in paragraph (f) of this AD.

Alternative Methods of Compliance (AMOCs)

(i)( I) The Manager, New York Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39 .19.

(2) Before using any AMOC approved in accordance with§ 39.19 on any airplane to which the

AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office.

Related Information

(j) Canadian airworthiness directive CF-2005-34, dated August 29, 2005, also addresses the

subject of this AD.

Material Incorporated by Reference

(k) You must use the Bombardier serv ice information identified in Table 4 of this AD to perform

the actions that are required by this AD, as applicable, unless the AD specifies otherwise. The Director of the Federal Register approved the incorporation by reference of these documents in

accordance w ith 5 U.S.C. 552(a) and I CFR part 51. Contact Bombardier, Inc. , Bombardier Regional

Aircraft Division, 123 Garratt Boulevard, Downsview, Ontario M3K 1 Y5, Canada, for a copy of this

service information. You may review copies at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street, SW., Room PL-401, Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov; or at the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal _register/code_ of Jederal _regulationsl ibr _locations. html.

TABLE 4.-MA TERIAL IN CORPORA TED BY REFERENCE

Bombardier Service Bulletin Revision level Date 8-52-54 A Nov. 5, 2004. 8- 52-58 Original May 12, 2004.

Issued in Renton, Washington, on June 5, 2006. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 06-5286 Filed 6-12-06; 8:45 am] BILLING CODE 4910-13-P

6

RECORD OF AIRFRAME 4

AIRWORTHINESS DIRECTIVES (A/Dl, SERVICE BULLETINS (S/Bl, SPECIAL INSPECTIONS (S/1) AND MODIFICATIONS (MODS)

2

2 7, JHLI 10G§

2 8, SEP. 2005

I 7. Feb. ~nn5

MESSMlllD - IS

l 3. JUNI 2006

0 OS: EASA PART-145 AT.1 45.001 , FAR-AUXY103F Austrian Airlines AG '2.DD/.::,- / Z-/C..,

~ VO: EASA PART-145 AT.145.030 Tyrolean Airways -Tiroler Luftfahrt GmbH W.O. Rev. 2

LTP Maintenance Workorder ©® ,,. ,,. ,,., 111 I

""'"""'

Air~idft/ Cual".: 0 A32 0 A33 [ YA34 D 873 D 876

D 877 0 CRJ 0 DH8 0 F70 0 F100

0 MD8 0 3RD 0 COMP

Date Issued by ATA D Pirep t-2_0_._S_e-=-p_2_0_0_7-+-ID ____ VM_E_N-l..-___ 5_2_-_6--10 O Maint No.2138036 Flt No. From "'To/ ~ Sched (Side 1 of 2) AS

Stn INN Statistics I 0 Base P/N

S/N D Canni Project 0 Struct. Damage

0 Tech. lrreg. 0 Insurance 0 Warranty

MEL Ref: MEL Interval 0 HIL 0 Flt Deck Info O Cabin Info O SDC

Classification ~ rn) [g [QJ O F.B. req . 0 AOG Risk ETOPS Restr.: CAT Restr.: L..=:__ _ ___: ___ _i__::=.._ _____ _L ____ --=== =c.l,_------=====-1

OPS Reporting Text:

List any available Fault Codes, MessaQes, Observations either in Description- or Action Text ,,. PERFORM SBB-52 - 061 (SERVICE BULLETIN) REV. 00

DOOR - COCKPIT DOOR - L ATCH BLOCK REPLACEMENT AND REWORK OF STRIKE

C PLATE 0 'E. --~ ! ! !ATTENTION AD CF -2005-34 R.1 ! ! ! Wr-- --------- ---------------------------------------------0

r,~rcraft l og \_ _Fntry req. If T askcard Finding renort Task No.:

ID ETOPS/ Critical Path

I /SBB 52 061 REV.00 PERFORMED

PERFORM F / C OF DOOR REMOVAL

l zone I TO STEP 8 ON

I Area I PAGE 7 OF 10.

(STEP 9)

Date ID / SiaW~ 2'"' 03 . 01 VSTI IL P.);

rlJ - ~ 14

C 0

DOOR REMOVAL F / C PERFORMED ACC SBB-5 2-061 REV.00

STEP 9 .

/I I 04. 01 VLIN

'tJ f--- -------------- --------------------------11--- -+- - - - -I-----~ <(

- 0 .1---------- ---t-----t----t------t

Reference D SBB-52 - 061 / SB Type I No.: W,F, C D, I, M

Valid Ext. Codes: Combination of GT/ Groundlime, MP/ Manoower TOI Tool HA/ Hanaar, PW/ P~=rwork, PR/ Partraauest and CH/ Chance IC/ lncomalete IS/ lnsutticienl NA/ Not avail WR/ Wrona

Transfer Due Date TAH TAC Prio Ext. Codes ID Sign

0 PIC for MEL Dispatch

06 .Sep . 2008 2 VMEN

tJ Administrat ion·/ Service Task Workorder, no Maintenance Release required ~ Workorder Completion: IOI CRS to be issued in TAL /VO onlv\ or Base Maintenance CRS /OS onlv\

D This aircraft or airframe identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and is approved for return to service.

The undersigned for the Austrian Airlines FAR 145 Approved Repair Station, Certificate Number. AUXY 103F at Austrian Airlines Technical Base A-1300 Vienna Airport , Austria, Europe.

VO Certifies that the work specified except as otherwise specified was carried out in accordance with PART-145 and in respect lo that work the aircrafVaircraft component is considered ready for release to

service.

Approval No.:

V . Closing Station

0 OS EASA PART-145 AT.145.001 0 VO EASA PART-145 AT.145.030 0 Other ,, _ ...,,.,._ ~-----------/Closing Date

INN O 4 . Jan . 2 0 0 8

'Time UTC tast Flt No. Hrs: 15 ' 2 9 4 ~~Jcv Cyc: 16 '7 3 ../-. V""°' VMUI 09 :43 OS903 'Y

D_bl lnsp.lD (if re~ IJ,, Sign ~ ~

ORIGINAL printed by WARTUNG on Friday, the 4.January 2008 at 09:51 out of database prod_vo hosted on amosp.vie.aua.com / produced by AMOS

LJ OS: EASA PART-145 AT.145.001 , FAR-AUXY103F Austrian Ai rl ines AG Jg! VO: EASA PART-1 45 AT.1 45.030 Tyrolean Airways - Tiroler Luftfahrt GmbH W.O. Rev. 2

Request

0 Taxi D Jacking D Double lnsp.

D Test / Verification Flight D Dock D Weight & Balance

D Idle Run D External Hydraulic D Defuel No.2138036 D Pwr Run D Hangar D Troubleshooting (Side 2 of 2)

Partnumber Description Qty IPC Reference Pickslip /for unknown P/Nl

8Z1590-065 LATCH BLOCK ASSY 1 2 PS oartlv booked

EC1357 ADHESIVE 1 2 PS partly booked

RTV102 ADHESIVE 1 2 PS partlv booked

Planning: Shop/Qua!. Work Time

Shop or CA Est. Hrs Shop or CA Est. Hrs ID Start Date Start Time Work Time

A 02:30 / : : : Bl 00 : 30 : : :

: : : :

Est. Gnd : : : Time (Hrs): : : :

Work Time .~ ' 1· : : ., ID Start Date Start Time Work Time : :

VSTI 03.Jan . 2008 00 : 00 1(02 : 00 : :

VLIN 04.Jan . 2008 00 : 00 00 : 30 : :

: : : : : : : :

: : : :

: : : :

: : : :

: : : : Additional Cost Items (E.g. Hangar, Aircraft Towing, Accomodation , Transport, Tax, Travel Order, Local Purchase, ... )

Hangar: Hrs I Towing: Hrs I Others: Indemnity Clause: Austrian Airlines I Tyrolean Ai rways shall not be liable for any damage or claim arising from or connected with the perlonnance of services or the supply of goods by Austrian Airlines/ Tyrolean Airways, unless such damage or claim is due to the wilful misconduct of Austrian Airlines / Tyrolean AjrwalJS, which has to be proven by the customer. The customer shall indemnify Austrian Airlines/ Tyrolean Airways, its agents and employees against any legal liability for claims or suits, including costs and expenses incidental thereto, arising from or connected with the perlonmance of the services or the supply of goods by Austrian Airlines I Tyrolean Airways, unless such liability is due to the wilful misconduct of Austrian Airlines I Tyrolean Airways, which has to be proven by the customer. The customer shall be liable towards Austrian Airlines / Tyrolean Airways for damages caused by negligence or wilful misconduct of the customer or its employees. Any dispute arising under this contract shall be subject to the non exclusive jurisdiction of the competent court in Vienna. The applicable law of this contract shall be the law of Austria.

Client authorized signature Date

D Austrian Airli nes Technik Tel. : +43 (0) 1 7007 62566 ~ Tyrolean Airway•· Tlroler Luftfahrt GmbH Tel.: +43 (0) 512 22221811 Austrian Airlines Technical Base Fax.: +43 (0) 1 7007 63766 Technical Department Fax.: +43 (0) 512 2801 02 1300 Vienna Airport E-Mail: [email protected] Fuerstenweg 190 E-Mail: mcc @tyrolean.at Austria Sita: VIEMCOS I 6020 Innsbruck Sita: INNTPVO

, Austria

VO Only I D A-Log I D E-Log I D Kardex I g;!..M9>d-Ldg I D TO-Stat. I D RD-Stat. I D SOO-Statj D TPP Entered in I D APU I D P-Log I D Due-List J,15-,t-;i'od4tat. I D EO-Stat. I D CR-Stat. I D AMS j W&B Tech. Lori:

~1}11:~. ORIGINAL printed by WARTUNG on Friday, the 4.January 2008 at 09:51 out of database _vo hosted on amosp.vie.aua.com produced by AMO S www.swiss-as.com

dehavillano bombardier dashb · bombardier inc. highly recommend that modsum 80900267 be...

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