TYPE CERTIFICATE DATA SHEET EA-2014T04 EA-2014T04-07 Type Certificate … · 2016-12-20 · TYPE...

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 /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


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


Continuous Steady - 96.8 98.0


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]



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)


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


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.

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


Limit

N1

(%) N2 (%)

Takeoff

power

OEI Steady - 96.8 98.5


AEO & WAI

OFF or ON

Steady - 96.8 98.5


Continuous Steady - 96.8 98.0


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


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


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


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


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


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


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 –


SM-02 - EFCS: Flight Control Surface Position Awareness –


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



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


PR-26 - Engine Fuel Shutoff Valve Indication 25.1141(f)(2) –


PR-30 - APU Fuel Shutoff Valve Indication 25.1141(f)(2) –


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) –


SM-14 - Flight Control System Failure Criteria 25.671(c)(2) &


2014

SM-18 - Combined Aircraft Pressurization Outflow and Positive

Pressure Differential Relief Valves 25.841(b(1) & 25.843(b)(1) –


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 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


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


ES-21 - Dive Speed Definition with Speed Protection System –


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


SE-15 - Systems and Data Networks Security-Isolation or

Protection From Unauthorized Passenger Domain Systems Access



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 –


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


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 –


SM-02 - EFCS: Flight Control Surface Position Awareness –


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) –


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


EI-31 - Step down for cabin Emergency Exit RBAC 25.807(a)(3) –


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


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


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) –


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


PR-26 - Engine Fuel Shutoff Valve Indication 25.1141(f)(2) –


PR-30 - APU Fuel Shutoff Valve Indication 25.1141(f)(2) –


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


2014

SM-05 - Ventilation (Humidity Requirement) 25.831(g) –


SM-14 - Flight Control System Failure Criteria 25.671(c)(2) &


2014

SM-18 - Combined Aircraft Pressurization Outflow and Positive

Pressure Differential Relief Valves 25.841(b(1) & 25.843(b)(1) –


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

TYPE CERTIFICATE DATA SHEET EA-2014T04 EA-2014T04-07 Type Certificate … · 2016-12-20 · TYPE...

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