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TYPE CERTIFICATE DATA SHEET EA-2014T04
Type Certificate Holder:
EMBRAER S.A. Av. Brigadeiro Faria Lima, 2.170 12227-901 – S.J dos Campos –SP Brazil
EA-2014T04-07
Sheet 01
EMBRAER
EMB-550, EMB-545
13 December 2016
This data sheet, which is part of Type Certificate No. 2014T04, prescribes conditions and limitations under which the
product, for which the Type Certificate was issued, meets the airworthiness requirements of the Brazilian Aeronautical
Regulations
I – Model EMB-550 (Transport Category), approved on August 12th, 2014.
ENGINE Two turbofans Honeywell AS907-3-1E
FUEL ASTM D1655, JET A and A1
Brazilian standard CNP08 or later, QAV – 1
Chinese standard GB6537-94 or later, Jet fuel No. 3
Standard MIL-DTL-83133, JP-8
Standard DEF STAN 91-91 AVTUR
GOST 10227–86 (Russian RT, TS-1 Premium and TS-1 Regular)
ENGINE LIMITS
ITT limits
Operation Conditions Operating
Limits
Thrust Setting State Time
limit Max. ITT (°C)
Ground Start - 5 s 650
Inflight
s
t
a
r
t
ITT < 250°C
and N2 <
18% [1]
- - 400
All other
start
conditions
- - 800
Takeoff
power
OEI Steady 10 min 955
Transient 2 min 970
AEO & WAI
OFF
Steady 5 min 955
Transient 2 min 970
AEO & WAI
ON [2]
Steady 5 min 955
Transient 2 min 970
Maximum Continuous Steady - 950 1- ITT limit remains 400°C until N2 goes above 18% during the start.
EMBRAER 13 December 2016 EA-2014T04-07 Page 2/16
2- Below 80 KIAS, the maximum ITT is 923°C for steady state. For transient state,
the maximum ITT is 938°C.
N1 AND N2 LIMITS
OPERATING CONDITIONS OPERATING
LIMITS
Thrust Setting State Time
Limit
N1
(%) N2 (%)
Takeoff
power
OEI Steady - 96.8 98.5
Transient 7 s 98.0 99.9
AEO & WAI
OFF or ON
Steady - 96.8 98.5
Transient 7 s 98.0 99.9
Continuous Steady - 96.8 98.0
Transient 7 s 98.0 99.9
AIRSPEED LIMITS
Maximum operating Speeds (VMO/MMO):
Altitude Speed
0 to 10 000 ft (0 a 3 048 m) 300 IAS (154 m/s)
10 000 a 30 000 ft (3 048 a 9 144 m) 320 IAS (165 m/s)
30 000 a 45 000 ft (9 144 a 13 716 m) 0.83 Mach
Maneuvering (VA): 205 IAS (105 m/s)
Flaps extended (VFE):
Flap position Speed
Flap 1 210 IAS (108 m/s)
Flap 2 185 IAS (95 m/s)
Flap 3 185 IAS (95 m/s)
Flap full 170 IAS (88 m/s)
Landing gear maximum operation/extended speed (VLO/LE):
VLO –Landing gear operation 250 IAS (129 m/s)
VLE – Landing gear extended 250 IAS (129 m/s)
APU Honeywell 36-150[EMB]
APU LIMITS
Parameter Minimum Maximum
Start
Altitude
Ground [1] [1]
In-flight - 31 000 ft
(9 449 m)
Temperature Ground [2] [2]
In-flight - 37°C [2]
EMBRAER 13 December 2016 EA-2014T04-07 Page 3/16
Parameter Minimum Maximum
Operation Altitude
Electrical
Power
Limit
- 31 000 ft
(9 449 m)
In-flight
Assisted
Engine
Start
- 23 000 ft
(7 010 m)
ECS - 20 000 ft
(6 096 m)
Temperature [2] [2]
Rotor Speed - 106%
EGT Start - 985°C
Continuous - 757°C
1- APU altitude for ground start matches the Airplane Operational
Envelope.
2- APU temperature matches the Airplane Operational Envelope
temperature.
CG RANGE See the Approved Airplane Flight Manual - AFM 3921-100
DATUM The airplane datum is a plane, perpendicular to the fuselage centerline,
located at 429.92 in (10.93 m) ahead of the wing jack points.
LEVELING MEANS Check aircraft AMM – chapter 8
MEAN AERODYNAMIC CHORD MAC lenght = 100.79 in (2.56 m)
MAXIMUM WEIGHT
Without BS 550-042-0004
lb (kg)
With BS 550-042-0004
lb (kg)
Ramp 38 096 (17 280) 38 536 (17 480)
Takeoff 37 920 (17 200) 38 360 (17 400)
Land 34 128 (15 480) 34 524 (15 660)
Zero Fuel 26 500 (12 020) 26 500 (12 020)
MINIMUM CREW 2 Pilots
MAXIMUM OCCUPANTS 12 Passengers
MAXIMUM BAGGAGE Wardrobe 88 lb. (153.15 in. aft of datum)
Internal Stowage Compartment 330 lb. (452.76 in. aft of datum)
External Cargo Compartment 881 lb. (543.30 in. aft of datum)
FUEL CAPACITY Total fuel capacity of 13 146.3 lb (5 963.1 kg.), two wing tanks 6 573.2
lb (2 981.5 kg) each, @ 367.72 in (9.34 m) aft of datum
OIL CAPACITY Tank mounted on each engine: 7.6 U.S. quarts (7.19 liter) total on each
engine
HYDRAULIC FLUID CAPACITY 109.6 lb. at 496.34 in. aft of datum
MAXIMUM OPERATING ALTITUDE
45 000 ft (13 716 m)
EMBRAER 13 December 2016 EA-2014T04-07 Page 4/16
TEMPERATURE OPERATING LIMITS
See the Approved Airplane Flight Manual - AFM 3921-100
CONTROL SURFACE MOVEMENTS
Elevator Up 25° ±1°
Down 15° ±1°
Rudder Right 30° ±1°
Left 30° ±1°
Aileron Up 25° ±0.8°
Down 15° ±0.8°
Wing Flap TO 7° ±1°
TO/Land 37° ±1.5°
Spoiler
Inboard Middle Outboard
Inflight 30° ±1.3° 30° ±1.4° 30° ±1.9°
Ground 40.5° ±1.3° 43° ±1.4° 40.5°±1.9°
Horiz. Stabilizer Up 12° ±0.5°
Down 3° ±0.5°
SERIAL NUMBER 55000001 up to 55009999, except 55000009 and 55000020
II– Model EMB-545 (Transport Category), approved on August 11th, 2015.
ENGINE Two turbofans Honeywell AS907-3-1E
FUEL ASTM D1655, JET A and A1
Brazilian standard CNP08 or later, QAV – 1
Chinese standard GB6537-94 or later, Jet fuel No. 3
Standard MIL-DTL-83133, JP-8
Standard DEF STAN 91-91 AVTUR
GOST 10227–86 (Russian RT, TS-1 Premium and TS-1 Regular)
ENGINE LIMITS
ITT limits
Operation Conditions Operating
Limits
Thrust Setting State Time
limit Max. ITT (°C)
Ground Start - 5 s 650
EMBRAER 13 December 2016 EA-2014T04-07 Page 5/16
Inflight
s
t
a
r
t
ITT < 250°C
and N2 <
18% [1]
- - 400
All other
start
conditions
- - 800
Takeoff
power
OEI Steady 10 min 955
Transient 2 min 970
AEO & WAI
OFF
Steady 5 min 955
Transient 2 min 970
AEO & WAI
ON [2]
Steady 5 min 955
Transient 2 min 970
Maximum Continuous Steady - 950 1- ITT limit remains 400°C until N2 goes above 18% during the start.
2- Below 80 KIAS, the maximum ITT is 923°C for steady state. For transient state,
the maximum ITT is 938°C.
N1 AND N2 LIMITS
OPERATING CONDITIONS OPERATING
LIMITS
Thrust Setting State Time
Limit
N1
(%) N2 (%)
Takeoff
power
OEI Steady - 96.8 98.5
Transient 7 s 98.0 99.9
AEO & WAI
OFF or ON
Steady - 96.8 98.5
Transient 7 s 98.0 99.9
Continuous Steady - 96.8 98.0
Transient 7 s 98.0 99.9
AIRSPEED LIMITS
Maximum operating Speeds (VMO/MMO):
Altitude Speed
0 to 10 000 ft (0 a 3 048 m) 300 IAS (154 m/s)
10 000 a 30 000 ft (3 048 a 9 144 m) 320 IAS (165 m/s)
30 000 a 45 000 ft (9 144 a 13 716 m) 0.83 Mach
Maneuvering (VA): 205 IAS (105 m/s)
Flaps extended (VFE):
Flap position Speed
Flap 1 210 IAS (108 m/s)
Flap 2 185 IAS (95 m/s)
Flap 3 185 IAS (95 m/s)
Flap full 170 IAS (88 m/s)
Landing gear maximum operation/extended speed (VLO/LE):
EMBRAER 13 December 2016 EA-2014T04-07 Page 6/16
VLO –Landing gear operation 250 IAS (129 m/s)
VLE – Landing gear extended 250 IAS (129 m/s)
APU Honeywell 36-150[EMB]
APU LIMITS
Parameter Minimum Maximum
Start
Altitude
Ground [1] [1]
In-flight - 31 000 ft
(9 449 m)
Temperature Ground [2] [2]
In-flight - 37°C [2]
Operation Altitude
Electrical
Power
Limit
- 31 000 ft
(9 449 m)
In-flight
Assisted
Engine
Start
- 23 000 ft
(7 010 m)
ECS - 20 000 ft
(6 096 m)
Temperature [2] [2]
Rotor Speed - 106%
EGT Start - 985°C
Continuous - 757°C
1- APU altitude for ground start matches the Airplane Operational
Envelope.
2- APU temperature matches the Airplane Operational Envelope
temperature.
CG RANGE See the Approved Airplane Flight Manual - AFM 3921-400
DATUM The airplane datum is a plane, perpendicular to the fuselage centerline,
located at 404.33 in (10.27 m) ahead of the wing jack points.
LEVELING MEANS Check aircraft AMM – chapter 8
MEAN AERODYNAMIC CHORD MAC lenght = 100.79 in (2.56 m)
MAXIMUM WEIGHT
Without BS 550-042-0004
lb (kg)
With BS 550-042-0004
lb (kg)
Ramp 35 406 (16 060) 35 891 (16 280)
Takeoff 35 274 (16 000) 35 758 (16 220)
Land 32 518 (14 750) 32 518 (14 750)
Zero Fuel 25 904 (11 750) 25 904 (11 750)
MINIMUM CREW 2 Pilots
MAXIMUM OCCUPANTS 10 Passengers
EMBRAER 13 December 2016 EA-2014T04-07 Page 7/16
MAXIMUM BAGGAGE Wardrobe 88 lb. (153.15 in. aft of datum)
Internal Stowage Compartment 330 lb. (409.45 in. aft of datum)
External Cargo Compartment 881 lb. (500.00 in. aft of datum)
FUEL CAPACITY Total fuel capacity of 10 939 lb (4962 kg.), two wing tanks 5 470 lb
(2481 kg) each, @ 342.1 in (8.69 m) aft of datum for aircraft pre-mod
SB 550-28-0002 or equivalent factory-icorporated modification.
Total fuel capacity of 12 940 lb (5870 kg.), two wing tanks 6 470 lb
(2935 kg) each, @ 339.5 in (8.62 m) aft of datum for aircraft post-mod
SB 550-28-0002 or equivalent factory-icorporated modification.
OIL CAPACITY Tank mounted on each engine: 7.6 U.S. quarts (7.19 liter) total on each
engine
HYDRAULIC FLUID CAPACITY 105.2 lb (47.7 kg) @ 467.2 in (11.9m) aft of datum
MAXIMUM OPERATING ALTITUDE
45 000 ft (13 716 m)
TEMPERATURE OPERATING LIMITS
See the Approved Airplane Flight Manual - AFM 3921-400
CONTROL SURFACE MOVEMENTS
Elevator Up 25° ±1°
Down 15° ±1°
Rudder Right 30° ±1°
Left 30° ±1°
Aileron Up 25° ±0.8°
Down 15° ±0.8°
Wing Flap TO 7° ±1°
TO/Land 37° ±1.5°
Spoiler
Inboard Middle Outboard
Inflight 30° ±1.3° 30° ±1.4° 30° ±1.9°
Ground 40.5° ±1.3° 43° ±1.4° 40.5°±1.9°
Horiz. Stabilizer Up 12° ±0.5°
Down 3° ±0.5°
SERIAL NUMBER 55000009, 55000020, 55010003 and subsequent
CERTIFICATION BASIS EMB-550
EMBRAER 13 December 2016 EA-2014T04-07 Page 8/16
1. RBAC 25 (Brazilian Airworthiness Standard: Transport Category
Aircraft), corresponding to US 14 CFR part 25, including
amendments 25-1 through 25-128 effective on 29 May 2009.
Special Conditions:
ES-01 - Sudden Engine Stoppage – according to ANAC resolution
No. 271, dated April 9th, 2013
ES-04 - Design Roll Maneuver for Electronic Flight Controls –
according to ANAC resolution No 214, dated January 25th, 2012
ES-11 - Limit Pilot Force for Side Stick Controls – according to
ANAC resolution No. 290, dated October 8th, 2013
ES-16 - Interaction of Systems and Structures – according to
ANAC resolution No. 294, dated November 26th, 2013
ES-21 - Dive Speed Definition with Speed Protection System –
according to ANAC resolution No. 282, dated September 17th,
2013
ES-23 - Landing Pitchover Condition – according to ANAC
resolution No. 298, dated December 18th of 2013
EI-07 - Single and multiple place side facing seats, and airbag
systems in the shoulder belt Electrical/Electronic Systems –
according to ANAC resolution No. 383, dated June 28th, 2016
SE-03 - Operation Without Normal Electrical Power – according to
ANAC resolution No. 295, dated November 26th, 2013
SE-15 - Systems and Data Networks Security-Isolation or
Protection From Unauthorized Passenger Domain Systems Access
– according to ANAC resolution No. 321, dated May 27th, 2014
SE-16 - Systems and Data Networks Security-Protection of
Airplane Systems and Data Networks from Unauthorized External
Access – according to ANAC resolution No. 322, dated May 29th,
2014
EV-03 - Flight Envelope Protection: Pitch and Roll and High Speed
Limiting Functions – according to ANAC resolution No. 315, dated
May 6th, 2014
EV-07 - Flight Envelope Protection: Normal Load Factor (g)
Limiting – according to ANAC resolution No. 314, dated May 6th,
2014
EV-08 - EFCS: Lateral-Directional and Longitudinal Stability and
Low Energy Awareness – according to ANAC resolution No. 289,
dated October 8th, 2013
EV-17 - Performance Credit for ATTCS during Go-Around –
according to ANAC resolution No. 287, dated September 27th, 2013
EV-25 - Flight Envelope Protection: High Incidence Protection and
situational awareness – according to ANAC resolution No. 312,
dated May 6th, 2014
EV-27 – Steep Approach Mode Functionality (SAM) - according
to ANAC resolution No. 300, dated January 7th, 2014
EMBRAER 13 December 2016 EA-2014T04-07 Page 9/16
EV-37 - Flight Envelope Protection – General – according to
ANAC resolution No. 313, dated May 6th, 2014
EV-38 - Hydrophobic Coating – according to ANAC resolution No.
283, dated September 17th, 2013
EV-46 - Credit for Robust Envelope Protection in Icing Conditions
– according to ANAC resolution No. 311, dated May 6th, 2014
EV-47 – Synthetic Vision System (SVS) and Enhanced Flight
Vision Systems (EFVS) on Head Up Display (HUD) – according
to ANAC resolution 384, dated June 28th, 2016
SM-01 - Flight control system multiple modes of operation –
according to ANAC resolution No. 286, dated September 27th, 2013
SM-02 - EFCS: Flight Control Surface Position Awareness –
according to ANAC resolution No. 285, dated September 27th, 2013
SM-06 - Side Stick Controllers – according to ANAC resolution
No. 292, dated October 31st, 2013
SM-09 - Electrical/Electronic Equipment Bay Fire Detection and
Smoke Penetration – according to ANAC resolution No. 301, dated
January 14th, 2014
SM-17 - Stowage Compartment Fire Protection – according to
ANAC resolution No. 333, dated July 1st, 2014
Equivalent Level of Safety:
ES-05 - Fuel Tank Crashworthiness RBAC 25.721 & 25.963 (d) –
according to ANAC ordinance 1529/SAR, dated July 9th de 2014
ES-07 - Failure Criteria Under Aeroelastic Stability RBAC 25.629;
25.671 & 25.1309 – according to ANAC ordinance 1656/SAR,
dated July 22nd, 2014
ES-13 - Checked Maneuver Loads RBAC 25.331(c)(2) – according
to ANAC ordinance1520/SAR, dated July 7th, 2014
ES-17 - Minor Crash Criteria RBAC 25.721 & 25.963(d) –
according to ANAC ordinance1657/SAR, dated July 22nd, 2014
ES-22 - Gust and Turbulence Loads RBAC 25.341 & others –
according to ANAC ordinance 1659/SAR, dated July 22nd, 2014
EI-08 - Graphical Exit Symbol RBAC 25.811 – according to
ANAC ordinance 3220/SAR, dated December 5th, 2013
EI-17 - Step down - Lavatory Emergency Exit RBAC 25.807(a)(3)
– according to ANAC ordinance 1523/SAR, dated July 8th, 2014
EI-29 - Emergency exit marking – according to ANAC ordinance
1799/SAR, dated August 1st, 2014
EI-36 - Belted Toilet Side-facing Seat ATD Placement – according
to ANAC ordinance 2070/SAR, dated August 15th, 2016
SE-04 - Position Lights and Anti-collision Lights System –
according to ANAC ordinance 1798/SAR, dated August 1st, 2014
SE-14 - Landing Lights Single Switch 25.1383(b) – according to
ANAC ordinance 3360/SAR, dated December 19th, 2013
EMBRAER 13 December 2016 EA-2014T04-07 Page 10/16
SE-17 - High Intensity Radiated Fields (HIRF) Equipment
Protection Test Levels. 25.1317 – according to ANAC ordinance
3359/SAR, dated December 19th, 2013
SM-08 - High Altitude Takeoffand Landing Operation up to 14000
ft RBAC 25.841(a) & 25.841(b)(6) - according to ANAC ordinance
2061/SAR, dated July 30th, 2015
PR-03 - Thrust Reverser Equivalent Level of Safety
25.933(a)(1)(ii) – according to ANAC ordinance 3276/SAR, dated
December 12th, 2013
PR-06 - Engine fire detectors in tailpipe 25.1203(a) – according to
ANAC ordinance 1521/SAR, dated July 7th, 2014
PR-14 - Digital only Display of turbine engine High / Intermediate
pressure rotor speed (N2) 25.1305(c)(3) – according to ANAC
ordinance 1522/SAR, dated July 8th, 2014
PR-16 - Adoption of APU Harmonized Requirements 25.901(c) –
according to ANAC ordinance 1701/SAR, dated July 24th, 2014
PR-18 - Lack of On/Off Switch for ATTCS System 25.904 &
25.1309 – according to ANAC decision No. 88 dated August 3rd,
2011
PR-24 - Thrust Reverser System Tests 25.934 – according to
ANAC ordinance 1524/SAR, dated July 8th, 2014
PR-26 - Engine Fuel Shutoff Valve Indication 25.1141(f)(2) –
according to ANAC ordinance 1528/SAR, dated July 9th de 2014
PR-30 - APU Fuel Shutoff Valve Indication 25.1141(f)(2) –
according to ANAC ordinance 1528/SAR, dated July 9th de 2014
PR-31 - Fire Protection of Adjacent Components of the Engine
Nacelle 25.867 – according to ANAC ordinance 1658/SAR, dated
July 22nd, 2014
EV-29 - Design assurance and safety assessment 25.1309 and
25.1301 – according to ANAC ordinance 0216/SAR, dated January
24th, 2014
EV-35 - Electronic Flight Control System: Mistrim Maneuvering
25.255 – according to ANAC ordinance 1702/SAR, dated July 24th,
2014
SM-05 - Ventilation (Humidity Requirement) 25.831(g) –
according to ANAC ordinance 1519/SAR, dated July 7th, 2014
SM-14 - Flight Control System Failure Criteria 25.671(c)(2) &
25.1309 – according to ANAC ordinance 1527/SAR, dated July 9th,
2014
SM-18 - Combined Aircraft Pressurization Outflow and Positive
Pressure Differential Relief Valves 25.841(b(1) & 25.843(b)(1) –
according to ANAC ordinance 1525/SAR, dated July 8th, 2014
Exemptions
EI-10 - Passenger Cabin Interior Doors RBAC 25.813(e) – Granted
according to ANAC Decision No. 134, dated November 26th, 2013
EMBRAER 13 December 2016 EA-2014T04-07 Page 11/16
EI-25 - Passenger Information Signs RBAC 25.791(a) – Granted
according to ANAC Decision No. 151, dated December 16th, 2013
EI-27 - Overwing Outside View Means RBAC 25.809(a) – Granted
according to ANAC Decision No. 25, dated March 25th, 2014
EI-38 - Temporary non-compliance with Leg flail requirement
RBAC 25.562(a), 25.785(b) e itens (b)(5) e (b)(7) da SC No. 25-
033 – Granted according to ANAC Decision No. 175 dated
December 5th, 2016
SE-01 - Lightning Protection of Fuel Tank Structure 25.981(a)(3)
– Granted according to ANAC Decision No. 119, dated November
5th, 2013
2. RBAC 34 - Requisitos para drenagem de combustível e emissões
de escapamento de aviões com motores a turbine (Fuel Venting and
Exhaust Emission Requirements for Turbine Engine Powered),
corresponding to the 14 CFR Part 34, as amended on the Type
Certificate issuance date
3. RBAC 36 - Requisitos de ruído para aeronave. (Noise Standard for
aircrafts) corresponding to the 14 CFR Part 36, including
amendments 36-1 through 36-28 effective on February 3rd, 2006.
4. Optional Icing requirements 25.1403 e 25.1419 compliant.
5. Not approved for ditching, 25.1411 e 25.1415 compliant.
6. The aircraft is RVSM capable from S/N 55000001 and on. Each
operator must obtain RVSM operating approval according to local
operational regulations.
NOTES: EMB-550
NOTE 1 Weight and balance.
Current weight and balance report, including the list of equipment that
are part of the certificated basic empty weight and loading instructions,
must be provided for each aircraft at the time of original certification.
The certificated empty weight and corresponding center of gravity
location must include:
Unusable fuel 88.6 lb (40.2 kg) at 356.50 in. (9.06 m) aft of
datum
Full engine oil 48.5 lb (22 kg) at 559.37 in. (14.21 m) aft of
datum
APU oil 4.4 lb (2 kg) at 673.50 in. (17.11 m) aft of
datum
Hydraulic Fluid 109.6 lb (49.7 kg) at 496.34 in (12.60 m) aft
of datum
NOTE 2 Markings and placards.
All marking and placards required by the applicable certification
requirements (see certification basics) and by the operational
requirements must be installed in the appropriated locations. Required
EMBRAER 13 December 2016 EA-2014T04-07 Page 12/16
placards and marking are listed in chapter Eleven (11) of the Aircraft
Illustrated Parts Catalog (AIPC).
NOTE 3 Continuing Airworthiness.
See Maintenance Manual, Chapter Four (4), "Airworthiness
Limitations" for Systems Airworthiness Limitations, Structure
Airworthiness Limitations (ALI) and Life-Limited Items (LLI).
The life limit for rotating parts on the AS907-3-1E engine is in engine
Light Maintenance Manual, Airworthiness Limitations Section
NOTE 4 Airplanes must be operated according to the ANAC Approved Airplane
Flight Manual (AFM), part number AFM-3921-100 dated August 12th,
2014 or later approved revisions.
NOTE 5 The EMB-550 is often referred to in Embraer marketing literature as
the “Legacy 500”. This is strictly a marketing designation and is not
part of the official model designation
CERTIFICATION BASIS EMB-545
1. RBAC 25 (Brazilian Airworthiness Standard: Transport Category
Aircraft), corresponding to US 14 CFR part 25, including
amendments 25-1 through 25-129 effective on 2 September 2009.
Special Conditions:
ES-01 - Sudden Engine Stoppage – according to ANAC resolution
No. 271, dated April 9th, 2013
ES-04 - Design Roll Maneuver for Electronic Flight Controls –
according to ANAC resolution No. 214, dated January 25th, 2012
ES-11 - Limit Pilot Force for Side Stick Controls – according to
ANAC resolution No. 290, dated October 8th, 2013
ES-16 - Interaction of Systems and Structures – according to
ANAC resolution No. 294, dated November 26th, 2013
ES-21 - Dive Speed Definition with Speed Protection System –
according to ANAC resolution No. 282, dated September 17th, 2013
ES-23 - Landing Pitchover Condition – according to ANAC
resolution No. 298, dated December 18th of 2013
EI-07 - Single and multiple place side facing seats, and airbag
systems in the shoulder belt Electrical/Electronic Systems –
according to ANAC resolution No. 383, dated June 28th, 2016
EI-30 - Seats with inflatable lap belts – according to ANAC
resolution No. 368, dated December 1st, 2015
EI-32- Structural armrest between seats – according to ANAC
resolution No. 369, dated December 1st, 2015
SE-03 - Operation Without Normal Electrical Power – according to
ANAC resolution No. 295, dated November 26th, 2013
SE-15 - Systems and Data Networks Security-Isolation or
Protection From Unauthorized Passenger Domain Systems Access
– according to ANAC resolution No. 321, dated May 27th, 2014
EMBRAER 13 December 2016 EA-2014T04-07 Page 13/16
SE-16 - Systems and Data Networks Security-Protection of
Airplane Systems and Data Networks from Unauthorized External
Access – according to ANAC resolution No. 322, dated May 29th,
2014
EV-03 - Flight Envelope Protection: Pitch and Roll and High Speed
Limiting Functions – according to ANAC resolution No. 315, dated
May 6th, 2014
EV-07 - Flight Envelope Protection: Normal Load Factor (g)
Limiting – according to ANAC resolution No. 314, dated May 6th,
2014
EV-08 - EFCS: Lateral-Directional and Longitudinal Stability and
Low Energy Awareness – according to ANAC resolution No. 289,
dated October 8th, 2013
EV-17 - Performance Credit for ATTCS during Go-Around –
according to ANAC resolution No. 287, dated September 27th, 2013
EV-25 - Flight Envelope Protection: High Incidence Protection and
situational awareness – according to ANAC resolution No. 312,
dated May 6th, 2014
EV-27 – Steep Approach Mode Functionality (SAM) - according
to ANAC resolution No. 300, dated January 7th, 2014
EV-37 - Flight Envelope Protection – General – according to
ANAC resolution No. 313, dated May 6th, 2014
EV-38 - Hydrophobic Coating – according to ANAC resolution No.
283, dated September 17th, 2013
EV-46 - Credit for Robust Envelope Protection in Icing Conditions
– according to ANAC resolution No. 311, dated May 6th, 2014
EV-47 – Synthetic Vision System (SVS) and Enhanced Flight
Vision Systems (EFVS) on Head Up Display (HUD) – according
to ANAC resolution 384, dated June 28th, 2016
SM-01 - Flight control system multiple modes of operation –
according to ANAC resolution No. 286, dated September 27th, 2013
SM-02 - EFCS: Flight Control Surface Position Awareness –
according to ANAC resolution No. 285, dated September 27th, 2013
SM-06 - Side Stick Controllers – according to ANAC resolution
No. 292, dated October 31st, 2013
SM-09 - Electrical/Electronic Equipment Bay Fire Detection and
Smoke Penetration – according to ANAC resolution No. 301, dated
January 14th, 2014
SM-17 - Stowage Compartment Fire Protection – according to
ANAC resolution No. 333, dated July 1st, 2014
Equivalent Level of Safety:
ES-05 - Fuel Tank Crashworthiness RBAC 25.721 & 25.963 (d) –
according to ANAC ordinance 1529/SAR, dated July 9th de 2014
ES-07 - Failure Criteria Under Aeroelastic Stability RBAC 25.629;
25.671 & 25.1309 – according to ANAC ordinance 1656/SAR,
dated July 22nd, 2014
EMBRAER 13 December 2016 EA-2014T04-07 Page 14/16
ES-13 - Checked Maneuver Loads RBAC 25.331(c)(2) – according
to ANAC ordinance1520/SAR, dated July 7th, 2014
ES-17 - Minor Crash Criteria RBAC 25.721 & 25.963(d) –
according to ANAC ordinance1657/SAR, dated July 22nd, 2014
ES-22 - Gust and Turbulence Loads RBAC 25.341 & others –
according to ANAC ordinance 1659/SAR, dated July 22nd, 2014
EI-08 - Graphical Exit Symbol RBAC 25.811 – according to
ANAC ordinance 3220/SAR, dated December 5th, 2013
EI-31 - Step down for cabin Emergency Exit RBAC 25.807(a)(3) –
according to ANAC ordinance 3220/SAR, dated July 27th, 2015
EI-29 - Emergency exit marking – according to ANAC ordinance
1799/SAR, dated August 1st, 2014
EI-36 - Belted Toilet Side-facing Seat ATD Placement – according
to ANAC ordinance 2070/SAR, dated August 15th, 2016
SE-04 - Position Lights and Anti-collision Lights System –
according to ANAC ordinance 1798/SAR, dated August 1st, 2014
SE-14 - Landing Lights Single Switch 25.1383(b) – according to
ANAC ordinance 3360/SAR, dated December 19th, 2013
SE-17 - High Intensity Radiated Fields (HIRF) Equipment
Protection Test Levels. 25.1317 – according to ANAC ordinance
3359/SAR, dated December 19th, 2013
SM-08 - High Altitude Takeoffand Landing Operation up to 14000
ft RBAC 25.841(a) & 25.841(b)(6) - according to ANAC ordinance
2061/SAR, dated July 30th, 2015
PR-03 - Thrust Reverser Equivalent Level of Safety
25.933(a)(1)(ii) – according to ANAC ordinance 3276/SAR, dated
December 12th, 2013
PR-06 - Engine fire detectors in tailpipe 25.1203(a) – according to
ANAC ordinance 1521/SAR, dated July 7th, 2014
PR-14 - Digital only Display of turbine engine High / Intermediate
pressure rotor speed (N2) 25.1305(c)(3) – according to ANAC
ordinance 1522/SAR, dated July 8th, 2014
PR-16 - Adoption of APU Harmonized Requirements 25.901(c) –
according to ANAC ordinance 1701/SAR, dated July 24th, 2014
PR-18 - Lack of On/Off Switch for ATTCS System 25.904 &
25.1309 – according to ANAC decision No. 88 dated August 3rd,
2011
PR-24 - Thrust Reverser System Tests 25.934 – according to
ANAC ordinance 1524/SAR, dated July 8th, 2014
PR-26 - Engine Fuel Shutoff Valve Indication 25.1141(f)(2) –
according to ANAC ordinance 1528/SAR, dated July 9th de 2014
PR-30 - APU Fuel Shutoff Valve Indication 25.1141(f)(2) –
according to ANAC ordinance 1528/SAR, dated July 9th de 2014
PR-31 - Fire Protection of Adjacent Components of the Engine
Nacelle 25.867 – according to ANAC ordinance 1658/SAR, dated
July 22nd, 2014
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EV-29 - Design assurance and safety assessment 25.1309 and
25.1301 – according to ANAC ordinance 0216/SAR, dated January
24th, 2014
EV-35 - Electronic Flight Control System: Mistrim Maneuvering
25.255 – according to ANAC ordinance 1702/SAR, dated July 24th,
2014
SM-05 - Ventilation (Humidity Requirement) 25.831(g) –
according to ANAC ordinance 1519/SAR, dated July 7th, 2014
SM-14 - Flight Control System Failure Criteria 25.671(c)(2) &
25.1309 – according to ANAC ordinance 1527/SAR, dated July 9th,
2014
SM-18 - Combined Aircraft Pressurization Outflow and Positive
Pressure Differential Relief Valves 25.841(b(1) & 25.843(b)(1) –
according to ANAC ordinance 1525/SAR, dated July 8th, 2014
Exemptions
EI-10 - Passenger Cabin Interior Doors RBAC 25.813(e) – Granted
according to ANAC Decision No. 134, dated November 26th, 2013
EI-25 - Passenger Information Signs RBAC 25.791(a) – Granted
according to ANAC Decision No. 151, dated December 16th, 2013
EI-27 - Overwing Outside View Means RBAC 25.809(a) – Granted
according to ANAC Decision No. 25, dated March 25th, 2014
EI-38 - Temporary non-compliance with Leg flail requirement
RBAC 25.562(a), 25.785(b) e itens (b)(5) e (b)(7) da SC No. 25-
033 – Granted according to ANAC Decision No. 175 dated
December 5th, 2016
SE-01 - Lightning Protection of Fuel Tank Structure 25.981(a)(3)
– Granted according to ANAC Decision No. 119, dated November
5th, 2013
2. RBAC 34 - Requisitos para drenagem de combustível e emissões
de escapamento de aviões com motores a turbine (Fuel Venting and
Exhaust Emission Requirements for Turbine Engine Powered),
corresponding to the 14 CFR Part 34, as amended on the Type
Certificate issuance date
3. RBAC 36 - Requisitos de ruído para aeronave. (Noise Standard for
aircrafts) corresponding to the 14 CFR Part 36, including
amendments 36-1 through 36-28 effective on February 3rd, 2006.
4. Optional Icing requirements 25.1403 e 25.1419 compliant.
5. Not approved for ditching, 25.1411 e 25.1415 compliant.
6. The aircraft is RVSM capable from S/N 55000009 and on. Each
operator must obtain RVSM operating approval according to local
operational regulations.
NOTES: EMB-545
NOTE 1 Weight and balance.
Current weight and balance report, including the list of equipment that
are part of the certificated basic empty weight and loading instructions,
must be provided for each aircraft at the time of original certification.
EMBRAER 13 Decembef 2016 EA-2014T04-07 Pago 16/16
The certificated empty weight and corresponding conter of gravitylocation musa include:
NOTE 2 Markines and placards
Al] marking and placards required by the applicable certificationrequirements (see. certification basics) and by the operationalrequirements musa be installed in the apprópriated locations. Requiredplacards and marking are listed in chapter Elevcn (11) of the Aircraftlllustrated Paras Catalog(AIPC).
NOTE 3 Continuing Airworthiness
See Maintenance - Manual, Chapter Four (4), "AirworthinessLimitations" for Systems Airworthiness Limitations, StructureAirworthiness Limitations (ALI) and Lide-Limited ltems (LLI).
The bife limit for rotating parts on the AS907-3-IE engine is in engineLight Maintenance Manual, Airworthiness Limitations Section
NOTE 4 Airplanesmust be operated according to the ANAC Approved AirplaneFlight Manual (AFM), pari óumber AFM-3921-400 dated August 11'h,2015 or laser appl.oved révisions
NOTE 5 The EMB-545 is often referred to in Embraer marketing literatura asthe "Legacy 450". This is strictly a marketing designation and is notpart of the official modem designation
Original in the Portuguese language signed by:
MACIO IGAWAGerente-Geral de Cehificação de Produto Aeronáutico
(Manager, AeronLJtical Product Certification)
/ ê
Unusable fuGI 88.6 lb (40.2 kg) at 330:70 in. (8.04 m) aft ofdatum
Full engine oil 48.5 lb (22 kg) at 519.70 in. (13.20 m) aft ofdatum
APU oil 4.4 lb (2 kg) at 631.20 in.'(16.00 m) aft ofdatum
Hydraulic Fluid 105.2 lb (47.7 kg) at 467.20 in (11.90 m) aftof datum