type certificate data sheet nº ea-9806 ea-9806-12 type

TYPE CERTIFICATE DATA SHEET Nº EA-9806

Type Certificate Holder:

AIRBUS S.A.S. 2 rond-point Emile Dewoitine 31700 Blagnac FRANCE

EA-9806-12 Sheet 01

AIRBUS

A330-200 Series:

A330-201 / 202 / 203 223 / 243

A330-300 Series:

A330-301 / 302 / 303 / 321 322 / 323 / 341 / 342 / 343

A330-200 Freighter Series:

A330-223F / 243F

A330-900 Series: A330-941

11 December 2019

This data sheet, which is part of Type Certificate No. 9806, 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 - A330-200 Series:

Model A330-201 (Transport Category) approved 27 November 2018;

Model A330-202, (Transport Category) and A330-223, (Transport Category), approved 26 October 1998;

Model A330-203 (Transport Category), approved 27 May 2002; and

Model A330-243, (Transport Category), approved 21 May 2001.

ENGINE A330-201: Two GE-CF6-80E1A2 turbofan engines.

A330-202: Two GE-CF6-80E1A4 turbofan engines. See Note 8.

A330-203: Two GE-CF6-80E1A3 turbofan engines.

A330-243: Two RR RB-211 Trent 772B-60 turbofan engines.

A330-223

Two PW 4170 turbofan engines. Two PW 4168A turbofan engines Two PW 4168A-1D turbofan engines

ENGINE RATINGS A330-201

GE CF6-0E1A2 A330-202

GE CF6-80E1A4 A330-203

GE CF6-0E1A3 A330-223 PW 4168A/

PW4168A-1D PW 4170

A330-243 RR Trent 772B-60

Static Thrust at Sea Level:

• Take-off (5 mn)1 (flat rated 30º C)

• Maximum continuous

(flat rated 25º C)

68 530 lb

60 400 lb

66 870 lb

60 400 lb

68 530 lb

60 400 lb

68 600 lb 70 000 lb

59 357 lb 59357 lb

71 100 lb

63 650 lb

(1) 10 minutes at take-off thrust allowed only in case of engine failure (at take-off or during go-around).

AIRBUS 11 December 2019 EA-9806-12 Sheet 2/19

II - A330-300 Series

Model A330-301, (Transport Category), A330-321, (Transport Category) and A330-322, (Transport Category), approved 26 October 1998.

Model A330-302 (Transport Category), A330-303 (Transport Category), A330-323 (Transport Category), A330-341 (Transport Category), A330-342 (Transport Category), and A330-343, (Transport Category), approved 27 November 2018.

ENGINE A330-301: Two GE-CF6-80E1A2 turbofan engines. A330-302: Two GE-CF6-80E1A2 turbofan engines or

Two GE-CF6-80E1A4 turbofan engines. See Note 8. A330-303: Two GE-CF6-80E1A3 turbofan engines

A330-321: Two PW 4164 turbofan engines or Two PW 4164-1D turbofan engines.

A330-322: Two PW 4168 turbofan engines or Two PW4168-1D turbofan engines.

A330-323: Two PW 4164-1D turbofan engines or Two PW 4168A turbofan engines or Two PW4168A-1D turbofan engines or Two PW 4170 turbofan engines.

A330-341: Two (2) Rolls Royce Trent 768-60 turbofan engines

A330-342: Two (2) Rolls Royce Trent 772-60 turbofan engines

MAXIMUM WEIGHT

A330-201 A330-202 A330-203 A330-223 A330-243

Min W/V

Min W/V

Min W/V

Min W/V

Min W/V

Max W/V

Min W/V

Max W/V

Min W/V

Max W/V

(W/V Weight per Variant –

Takeoff (MTOW):

192 238 192 242 192 242 192 242 192 242

metric tons.) Landing (MLW):

180 182 180 182 180 182 180 182 180 182

Zero Fuel (MZFW): 168 170 166 170 166 170 166 170 166 170

MAXIMUM PASSENGERS

The maximum number of passengers approved for emergency evacuation is: - 375 basic (when 3 type A and 1 type 1 doors installed); and - 406 when 4 type A doors installed (Mod. 40161). See interior layout drawing for the maximum passenger capacities approved for each aircraft when delivered.

MAXIMUM BAGGAGE Cargo compartment Maximum load (kg)

Forward 18 869

Aft 15 241

Rear (bulk) 3 468

For the positions and the loading conditions authorized in each position (references of containers, pallets and associated weights), see Weight and Balance Manual Ref. 00G080A0006/C2S.

FUEL CAPACITY (0.8 kg/l)

Tank Usable fuel liters (kg) Unusable fuel liters (kg) Unusable fuel liters (kg) Mod 205749

- Wing 91 300 (73 040) 348 (279) 190 (152)

- Center 41 560 (33 248) 83 (67) 83 (67)

- Trim tank 6 230 (4 984) 6 (5) 6 (5)

Total 139 090 (111 272) 437 (350) 279 (223)


A330-343: Two (2) Rolls Royce Trent 768-60 turbofan engines or Two (2) Rolls Royce Trent 772B-60 turbofan engines

ENGINE RATINGS Static Thrust at Sea Level

Take-off (5 mn)1 (flat rated 30º C)

Maximum continuous (flat rated 25º C)

A330-301 GE CF6-80E1A2

64.530 lbs

60.400 lbs

A330-302 GE-CF6-80E1A2 GE-CF6-80E1A4

64.530 lbs 66.870 lbs

60.400 lbs 60.400 lbs

A330-303 GE-CF6-80E1A3

68.530 lbs

60.400 lbs

A330-321 PW 4164

PW 4164-1D

64.500 lbs

55.800 lbs

A330-322 PW4168/ PW4168-1D

68.600 lbs

59.357 lbs

A330-323 PW 4164-1D

PW 4168A/PW4168A-1D PW 4170

64.500 lbs 68.600 lbs 70.000 lbs

55.800 lbs 59.357 lbs 59.357 lbs

A330-341 Trent 768-60

67.500 lbs

60.410 lbs

A330-342 Trent 772-60

71.100 lbs

63.650 lbs

A330-343 Trent 768-60

Trent 772B-60

67.500 lbs 71.100 lbs

60.410 lbs 63.650 lbs


MAXIMUM WEIGHT

Takeoff (MTOW): Landing (MLW): Zero Fuel (MZFW): (W/V Weight per Variant metric tons)

A330-301 Min W/V 184 174 164 Max W/V 217 187 175

A330-302 Min W/V 190 185 171 Max W/V 242 187 175

A330-303 Min W/V 205 185 171 Max W/V 242 187 175

A330-321 Min W/V 212 174 164 Max W/V 218 182 172

A330-322 Min W/V 212 174 164 Max W/V 218 182 172

A330-323 Min W/V 184 174 164 Max W/V 242 187 175

A330-341 Min W/V 205 174 164 Max W/V 218 182 172

A330-342 Min W/V 184 174 164 Max W/V 242 187 175

A330-343 Min W/V 184 174 164 Max W/V 242 187 175


MAXIMUM PASSENGERS

The maximum number of passengers approved for emergency evacuation is: - 375 basic (when 3 type A and 1 type 1 doors installed); and - 440 when 4 type A doors installed (Mod. 40161). See interior layout drawing for the maximum passenger capacities approved for each aircraft when delivered.

MAXIMUM BAGGAGE Cargo compartment Maximum load (kg) Forward 22 861 Aft 18 507 Rear (bulk) 3 468 For the positions and the loading conditions authorized in each position (references of

containers, pallets and associated weights), see Weight and Balance Manual Ref. 00G080A0006/C3S.


2 TANK AEROPLANE:

Usable fuel liters (kg)

Unusable fuel liters (kg)

A/C Model

GE A330-301

A330-302 A330-303

All models

PW A330-321 A330-322

A330-323

RR A330-341

A330-342 (except WV22 & 52) A330-342 (WV22 & 52)

A330-343

Basic MOD 205749

Wing 91 764 (73 411) 91 300 (73 040) 348 (279) 190 (152)

Trim tank 6 121 (4 897) 6 230 (4 984) 6 (5) 6 (5)

Total 97 885 (78 308) 97 530 (78 024) 354 (284) 196 (157)

3 TANK AEROPLANE:

Usable fuel liters (kg)

Unusable fuel liters (kg)

A/C Model

GE A330-302 WV 030s, 050s, 060s, 080s A330-303 WV 050s, 060s, 080s

All models

PW A330-323 WV 030s, 050s, 060s, 080s

RR A330-342 WV 050s, 060s, 080s A330-343 WV 030s, 050s, 060s, 080s

Basic MOD 205749

Wing 91 300 (73 040) 348 (279) 190 (152)

Center 41 560 (33 248) 83 (67) 83 (67)

Trim tank 6 230 (4 984) 6 (5) 6 (5)

Total 139 090 (111 272) 437 (350) 279 (223)


III - A330-200 Series Freighter Series

Model A330-223F and A330-243F, (Transport Category) approved 04 December 2013;

ENGINE A330-223F:

Two PW 4170 turbofan engines. Two PW 4168A-1D turbofan engines One Pratt&Whitney 4168A turbofan engine.

A330-243F: Two RR RB-211 Trent 772B-60 turbofan engines. ENGINE RATINGS A330-223F

PW 4170 A330-223F A330-223F

PW4168A-1D PW4168A A330-243F

R Trent 772B-60 Static Thrust at Sea Level:

• Take-off (5 min)1 (flat rated 30º C)

• Maximum continuous (flat rated 25º C)

70 000 lb

59 357 lb

68 600 lb 68 600 lb

59 357 lb 59 357 lb

71 100 lb

63 560 lb


(2) Only one of the PW4168A engine should be installed on the freighter.

MAXIMUM WEIGHT A330-200F Min W/V Max W/V

Takeoff (MTOW): 227 000 kg 233 000 kg

Landing (MLW): 187 000 kg 187 000 kg

Zero Fuel (MZFW): 173 000 kg 178 000 kg

MAXIMUM OCCUPANTS The maximum 12 supernumeraries may occupy the courier area aft the

flight deck. Total occupancy of the airplane is limited to 16 persons including flight crew.


Forward 18 869

Aft 15 241

Rear (bulk) 3 468

Main Deck 65 000 Range Mode

For the positions and the loading conditions authorized in each position (references of containers, pallets and associated weights), see Weight and Balance Manual Ref. 00G080A0006/C2S.

FUEL CAPACITY (0.8 kg/l) With mod. 58623/200281 and without mod. 58623

Tank Usable fuel liters (kg) Unusable fuel liters (kg) Unusable fuel liters (kg) Mod 205749

Wing 91 300 (73 040) 348 (279) 190 (152)

Center 41 560 (33 248) 83 (67) 83 (67)

Trim tank 6 230 (4 984) 6 (5) 6 (5)

Total 139 090 (111 272) 437 (350) 279 (223)

With mod. 58623 and without mod. 200281 Wing 91 300 (73 040) 348 (279) 190 (152)

Trim tank 6 230 (4 984) 6 (5) 6 (5)

Total 97 530 (78 024) 354 (284) 196 (157)


IV - A330-900 Series – see Note 9

Model A330-941 (Transport Category) approved 04 December 2018;

ENGINE A330-941:

Two Rolls Royce Trent 7000-72 turbofan engines.

ENGINE RATINGS A330-941

Trent 7000-72 Static Thrust at Sea Level:

• Take-off (5 min)1 (flat rated 30º C)

• Maximum continuous (flat rated 25º C)

72,834 lb

65 005 lb


MAXIMUM WEIGHT A330-941

(W/V Weight per Min W/V Max W/V

Variant metric tons.) Takeoff (MTOW): 230 242

Landing (MLW): 191 191

Zero Fuel (MZFW): 177 181

(*) Linear variation beween those weights

MAXIMUM PASSENGERS The maximum number of passengers approved for emergency evacuation is: - 375 basic (when 3 type A and 1 type 1 doors installed); and - 440 when 4 type A doors installed (Mod. 40161). See interior layout drawing for the maximum passenger capacities and cabin crew approved for each aircraft when delivered.


Forward 22 861

Aft 18 507

Rear (bulk) 3 468

For the positions and the loading conditions authorized in each position (references of containers, pallets and associated weights), see Weight and Balance Manual Ref. 00G080A3WBM/C9S


Tank Usable fuel liters (kg) Unusable fuel (kg)

Wing 91 300 (73 040) 190 (152)

Center 41 560 (33 248) 83 (67)

Trim tank 6 230 (4 984) 6 (5)

Total 139 090 (111 272) 279 (223)


DATA PERTINENT TO ALL MODELS:

ENVIRONMENTAL REQUIREMENTS

Environmental requirements for noise and vented fuel: ICAO Annex 16 Volume I – Part II, Chapter 4 for Noise. Compliance with Chapter 4 had originally been demonstrated through MOD 55005. Compliance with Chapter 4 is now achieved without MOD 55005 (see EASA TCDSN A.004 for details) ICAO Annex 16 Volume II (Vented Fuel) – Part II, Chapter 2. For A-330-900 series environmental requirements see certification basis.

FUEL A330-201, A330-202, A330-203, A330-301, A330-302: - Kerosene: JET A, JET A1, JP5, JP8, N°3 JET fuel, TS-1, RT - Additives: According to GE “Specific Operating Instructions”

installation manual.

A330-223, A330-321, A330-322, A330-323, A330-223F:

Kerosene: JETA, JETA1, JP5, JP8, N°3 JET fuel, TS-1, RT

- Fuel additives conforming to the latest applicable issue of FAA-approved Pratt & Whitney Turbofan Engine Service Bulletin No. 2016 may be used separately or mixed in any proportions without adversely affecting the engine operation or power output.

A330-243, A330-243F, A330-341, A330-342, A330-343, A330-941:

Kerosene:JET A, JET A1, JP5, JP8, N°3 JET fuel, TS-1, RT, JP4, JET B

- Approved fuel and fuel additives are identified in the relevant Operating Instructions defined in Rolls Royce manual F-Trent – A330.

The above-mentioned fuels are also suitable for the APU.

AIRSPEED LIMITS (IAS) Maximum operating (VMO/MMO): 330 kias/0.86

Design diving (VD) 365 kias/0.93

Design maneuvering (VA) Refer to AFM performance section.

Flaps extended (VFE)

Config. Slats/Flaps/ Ailerons(°)

VFE (kt)

Intermediate approach Take-off

1 16/0/0 16/8/0

240 215

Take-off 1 + F 16/8/5 205

Take-off and approach 2 20/14/10 196

Take-off, approach, landing 3 23/22/10 186

Landing Full 23/32 180

Minimum control speed (VMC) Refer to AFM performance section.

L. G. extended (VLE) 250 kias/0.55

L. G. operation (VLO) 250 kias/0.55

Tire limit (ground speed) 203 kias (235 mph)

CG RANGE Refer to EASA-Approved Brazilian Airplane Flight Manual Limitations

Section for center of gravity envelope. DATUM The aircraft reference zero datum point is located 6.382,5 m forward of the

nose section, 7 m under the fuselage centerline (datum line). LEVELING MEANS Inclinometer on cabin seat track rails (refer to WBM chapter 1.80).


MEAN AERODYNAMIC CHORD The MAC is 7.279 m MAC is located 11.122 m from the center line. MINIMUM CREW 2 (pilot and copilot) MAX. OPERATING ALTITUDE See applicable approved AFM. TEMPERATURE OPERATING See applicable approved AFM. LIMITS CONTROL SURFACE MOVEMENTS

Total one-way travel in each direction of each movable control surface on the aircraft.

Control surface: Maximum travel: Flaps: 32 Aileron 25 Aileron droop 10 Elevator +15/-30 Rudder 30 # 1 Spoilers speed brake 25, lift dumper 34,5 # 2,3,4,5,6 Spoilers roll 35, speed brake 30, lift dumper 50 Slats 23 Stabilizers +2/-14 HYDRAULIC FLUIDS Type IV - Specification NSA 307-110. AUXILIARY POWER UNIT

Garret Airesearch GTCP 331-350C (Specification 31-7677A). Approved oils: See Garret report GT-7800.

TIRES Refer to Airbus Service Bulletin (SB) A330-32-3004. AIRPLANE FLIGHT MANUAL Refer to:

AI/ST-F 33000 (A330-202, A330-203, A330-223, A330-243, A330-323, A330-341, A330-342, A330-343); AI/EV-O 33000 (A330-301, A330-321, A330-322); STL 33000 (A330-200F series, A330-201, A330-302, A330-303, A330-941).

S/N’S ELIGIBLE A Certificate of Airworthiness for Export endorsed as noted under "Import

Requirements" must be submitted for each individual aircraft for which application for a Brazilian Certificate of Airworthiness is made.

IMPORT ELEGIBILITY A Brazilian Certificate of Airworthiness may be issued on the basis of on a

EASA Export Certificate on Airworthiness (or a third country Export Certificate on Airworthiness, in case of used aircraft imported from such country), including the following statement:

“The aircraft covered by this certificate has been inspected, tested and found to be in conformity with the Brazilian approved type design as defined by the Brazilian Type Certificate no. 9806 and in condition of safe operation”.

Note 4 contains the Brazilian requirements for the acceptance of these airplanes.


CERTIFICATION BASIS RBHA 25 corresponding to FAR 25 including amendments 1 through 63, effective on the reference date 15 Jun. 88;

RBHA 34 corresponding to ICAO Annex 16 Vol. II, 2nd. Ed.,

RBHA 36 corresponding to ICAO Annex 16 Vol. I, 2nd. Ed., plus the following items:

a. A330-200 Series additional basic requirements (derivative assessment): - RBHA 25 Amendments 69, 82 and 84 corresponding to the respective

FAR 25 amendments 69, 82 and 84, effective on the reference date 23 Jan. 96;

- RBHA 25.21, 25.29, 25.111, 25.147, 25.177, 25.181, 25.205, 25.307, 25.331, 25.341, 25.343, 25.351, 25.373, 25.395, 25.459, 25.571(b), 25.613 (vertical stabilizer only) , 25.615 (vertical stabilizer only), 25.979, 25.1419, 25.1533 and 25.1583 amendment 72 corresponding to the respective FAR 25 amendment 72, effective on the reference date 23 Jan. 96; and

- RBHA 25.851 amendment 74 corresponding to the respective FAR 25 amendment 74, effective on the reference date 23 Jan. 96.

b. Airbus elect-to-comply requirements: - RBHA 25 amendments 64, 65, 66 and 77 corresponding to FAR 25

amendments 64, 65, 66 and 77, effective on 16 Jun. 88, 11 Oct. 88, 26 Sep. 88, and 29 Jul. 92, respectively, with the exception that cockpit seats and front row seats in front of a bulkhead do not meet section 25.562; compliance with 25.785 (b), (c) and (d) for front row seats in front of a bulkhead were based on ensuring a 35 inch free head strike envelope.

- RBHA 25 amendments 68, 73, 75, 78, 81 and 85 corresponding to the respective FAR 25 amendments 68, 73, 75, 78, 81 and 85, effective on the reference date 23 Jan. 96 (A330-200 Series only).

- RBHA 25.345, 25.361, 25.397, 25.415, 25.693, 25.723, 25.729, 25.731, 25.733, 25.735, 25.772, 25.933, 25.1093, 25.1381, 25.1522, 25.1543, 25.1551, 25.1581 and 25.1587 Amendment 72 corresponding to the respective FAR 25 amendment 72, effective on the reference date 23 Jan. 96] (A330-200 Series only).

c. JAA/EASA requirements and procedures, endorsed by Brazilian Certification Authority or accepted as providing equivalent level of safety in relation to the applicable RBHA 25 requirements:

1. JAR 25 requirements effective on the reference date 15 Jun. 88: - JAR 25 Ch. 13: - JAR 25.107(e)(1)(iv) - VLOF margins - JAR 25.571(e)(1) - Bird Impact (A330-300 Series only) - JAR 25 Ch. 14 (A330-200 Series only): - JAR 25.305 - Strength and Deformation - JAR 25.321 - Flight Loads - General - JAR 25.331 - Symmetric Manoeuvering Conditions - JAR 25.333 - Flight Envelope - JAR 25.335 - Design Airspeeds - JAR 25.341 - Gust and Turbulence Loads - JAR 25.343 - Design Fuel and Oil Loads - JAR 25.345 - High Lift Devices - JAR 25.349 - Rolling Conditions - JAR 25.351 - Yaw Manoeuvering Conditions - JAR 25.371 - Gyroscopic loads - JAR 25.373 - Speed Control Devices - JAR 25.391 - Control Surface Loads - General - JAR 25.427 - Unsymmetrical Loads


CERTIFICATION BASIS (cont.) - JAR 25.571 - Damage Tolerance 2. JAA/EASA Special Conditions (SC) [A330-200/300]: - SC A-1 Discrete Gust Requirements - NPA 25C-205/ OP 91/1 (A330-300 only) - SC A-2 Interaction of Systems and Structure - NPA 25C-199 - SC A-3 Design Manoeuver Requirement - SC A-4 Design Dive Speed - SC A-5 Limit Pilot Forces and Torques - SC A-7 Stalling Speeds for Structural Design - SC A-11 Aeroelastic stability requirements (NPA 25B, C, D-236) - SC E-2 Underfloor Crew Rest Compartment - SC E-11 Bulk crew rest compartment (applicable from January 2002) - SC E-19 F/C sliding screens (applicable from September 2003) - SC E-5.1 Lower deck Lavatory (applicable from August 2000) - SC E-8.1 Lower deck stowage area (applicable from August 2000) - SC E-128 Improved flammability standards for thermal/acoustic insulation (applicable from February 2009) - SC E-130 Application of heat release and smoke density requirements to seat materials (applicable from February 2010) - SC E-1014 HIC compliance for front row seating (inflatable restraints) (applicable from July 2007)

- SC F-1 Stalling and Scheduled Operating Speeds (A330-300 only) - SC F-101 Stalling and Scheduled Operating Speeds (A330-200 only) - SC F-2 Motion and Effect of Cockpit Controls - SC F-3 Static Longitudinal Stability - SC F-4 Static Directional and Lateral Stability - SC F-5 Flight Envelope Protection - SC F-6 Normal Load Factor Limiting System - SC G-5 Resistance to fire terminology (NPA 25D-181) (A330-200 only) - SC G-7 Function and Reliability Testing - SC G-105 Resistance to fire (A330-200 only) - SC H-01 Enhanced Airworthiness Programme for Aeroplane Systems ICA on EWIS (applicable from May 2010) - SC P-1 FADEC - SC P-2 Centre of gravity control system - SC P-27 Flammability Reduction System - SC S-3 Landing Gear Warning - NPA 25D-162 (A330-300 only) - SC S-6 Lightning Protection Indirect Effects - SC S-10 Effects of External Radiations upon Aircraft Systems - SC S-10.1 Effects of external radiations upon aircraft systems (A330-200 only) - SC S-10.2 Effects of external radiations upon aircraft systems (A330-200 only) - SC S-13 Autothrust System - SC S-16 Control Signal Integrity - SC S-18 Electronic Flight Control - SC S-20 Emergency Electrical Power - NPA 25D, F-179 - SC S-23 Electrical Wiring and Miscellaneous Electrical Requirements - NPA 25F-191 - SC S-24 Doors - NPA 25D, F-251 (A330-300 only) - SC S-38 Towbarless towing


CERTIFICATION BASIS (cont.) 3. Equivalent Safety Demonstrations (all Models):

- CRI A-128 Rigid barrier wall emergency conditions - CRI F-8 Accelerate Stop Distances - RBHA 25.101; 25.105;

25.109; 25.113; 25.115; 25.735 (A330-300 only) - CRI F-8.1 Accelerate Stop Distances - RBHA 25.101; 25.105;

25.109; 25.113; 25.115; 25.735 (A330-200 only) - CRI S-21 Brakes Wear Limits - RBHA 25.735 - CRI S-45 Oil Temperature Indication - RBHA 25.1549 - CRI P-4 In Flight Thrust Reverse Deployment - RBHA 25.933;

25.1309 - CRI P-9 provides an equivalent level of safety to JAR

25.1203(d) for Rolls-Royce Trent 700 engines. - ESF E-18 provides an equivalent level of safety to JAR 25.819(f)

(applicable from November 2003) (A330-200/300) - ESF E-15 provides an equivalent level of safety to JAR 25.772

(applicable from July 2002) (A330-200/300) - ESF E-21 provides an equivalent level of safety to JAR 25.811(f)

[A330-200F only] - ESF E-1022 provides an equivalent level of safety to JAR 25.853(b)

(applicable from August 2005) (A330-200/300) - ESF F-128 Improved flammability standards for thermal/acoustic

insulation (applicable from February 2009) - ESF S-48 provides an equivalent level of safety to JAR AWO 313

4. Extended Range Twin Engine Airplane Operations Technical Conditions:

- AMJ 120-42/IL 20 - CRI G-6 – ETOPS (A330-300 only) - CRI G-106 – ETOPS (A330-200/300 only (except WV080)) - CRI G-106F – ETOPS (A330-200F only (except WV080)) - EASA CRI – ETOPS G-8 (A330-200/300 only)

5. Precision Approach and Landing:

- JAR AWO Change 1 - NPA JAR AWO 3 - NPA JAR AWO 8 - CRI S-148 (A330-200 only) - OP AWO 91/1 (A330-200 only)

d. Additional Technical Conditions: - FAA Special Condition No. 10 - Limit Engine Torque, as published in the USA Federal Register 1 November 1993, Docket No. NM-86, Special Conditions Number 25-ANM-77.

A330-200 Freighter Series a. additional basic requirements (derivative assessment):

- RBHA 25 Amendments corresponding to the respective FAR 25 amendments 25-1 through 25-63. And amendments 25-65, 25-66, 25-68, 25-69, 25-73, 25-75, 25-77, 25-78, 25-81, 25-82, 25-84, 25-85, 25-99 and 25-105 effective on the reference date 23 Jan. 96;

- Sections 25.21, 25.29, 25.111, 25.147, 25.177, 25.181, 25.205, 25.307, 25.361, 25.373, 25.395, 25.397 25.415, 25.459, 25.571(b), 25.613 (vertical stabilizer only) , 25.615 (vertical stabilizer only), 25.625 (Courier area), 25.693, 25.723, 25.729, 25.731, 25.733, 25.735, 25.772, 25.779, 25.783, 25.791 Courier area, 25.803 Courier area, 25.810 Courier area, 25.933, 25.979, 25.1093, 25.1381, 25.1419, 25.1522, 25.1533, 25.1543, 25.1551, 25.1581, 25.1583 and 25.1587 amendment 72 corresponding to the respective FAR 25


CERTIFICATION BASIS (cont.)

amendment 72, effective on the reference date 23 Jan. 96; and - RBHA 25.851 amendment 74 corresponding to the respective FAR 25

amendment 74, effective on the reference date 23 Jan. 96. - RBHA 25.1316 amendment 80 corresponding to the respective FAR

25 amendment 80, effective on the reference date 23 Jan. 96. - RBHA 25.305, 25.321, 25.331, 25.333, 25.335, 25.341, 25.343,

25.345, 25.349, 25.351, 25.371, 25.373, 25.391, 25.427 Amendment 25-86, effective 11 Mar. 96.

- ESF P4 In Flight Thrust Reverse deployment - RBHA 25.933, 25.1309 ANAC Decision nº 035/2013 The ANAC has granted exemption to RBAC 25 amendment 129 paragraphs 25.785(j), 25.813(b), 25.851(a)(3), 25.1439(a) and 25.1447(c)(1) for Airbus models A330-223F and A330-243F.

ANAC endorses EASA Special Conditions for the A30-200F:

E-124 Courier compartment E-125 Class E cargo compartment fire protection of essential systems E-127 Flammability standard for thermal / acoustic insulation materials The following original Special Condition and Equivalent Safety Level CRIs

applicable to the A330-200 defined in CRI G-101 issue 4 remain effective for the A330-200F:

SC A-2 Interaction of systems and structure SC A-3 Design manoeuvre requirements SC A-4 Design dive speed VD SC A-5 Limit pilot forces and torque SC A-7 Stalling speeds for structural design SC A-11 Aero-elastic stability requirements SC A-128 Rigid barrier wall emergency conditions SC F-101 Stalling and scheduled operating speeds SC F-2 Motion and effects of cockpit controls SC F-3 Static longitudinal stability SC F-4 Static directional and lateral stability SC F-5 Flight envelope protections SC F-6 Normal load factor limiting system SC G-105 Resistance to fire SC P-1 FADEC SC P-2 Trim Tank SC S-6 Lightning protection indirect effects SC S-10.2 Effects of external radiations upon aircraft systems SC S-13 Auto-thrust system SC S-16 Control signal integrity SC S-18 Electronic flight control SC S-20 Emergency electrical power SC S-23 Electrical wiring and miscellaneous electrical requirements SC S-38 Towbarless towing SC H-01 Enhanced Airworthiness Program for Aeroplane Systems - ICA on

EWIS (applicable from May 2010) ESF F 8.1 & ESF S-21 equivalent safety level to JAR 25 accelerate-stop and brakes qualification requirements (NPA 25 B, D, G 244).


CERTIFICATION BASIS (cont.)

A330-900 Series

Brazilian Type Certificate No. 9806 was amended based on RBAC 21.29, including the following requirements valid on the date of application 1st July 2017:

RBAC 25 “Requisitos De Aeronavegabilidade: Aviões Categoria Transporte”, amendments 25-1 through 25-136, which endorses the 14 CFR Part 25, effective Jan. 11, 2012, as amended by 25-1 through 25-136, RBAC 34 amendment 34-4, corresponding to 14 CFR Part 34 amendment 4, effective on 28 Apr. 2009, RBAC 36 amendment 36-28, corresponding to 14 CFR Part 36 amendment 28, effective on 04 Jan 2006 and RBAC 26 amendment 1. The compliance was verified through equivalency finding to JAA JAR 25 Change 13 – 14 and EASA Certification Specification 25, Amendment 25-2 through 25-17 – Large Aeroplanes including JAA/EASA issued Special Conditions, Equivalent Level of Safety accepted by ANAC and additional ANAC issued Equivalent Level of Safety and Exemptions, ICAO Annex 16 – Environmental Protection, Volume 1, Edition 7, Amendment 11-B and ICAO Annex 16 – Fuel Venting, Volume 2, as noted: Airworthiness Requirements Original Airworthiness Requirements (at time of TC): JAR 25 Change 13 effective on October 5, 1989 except as follows: - JAR 25.561 is applied at change 12 for wing tanks outside the fuselage contour; - For showing compliance with JAR 25.785(a)(b)(c), the front row seats located behind a bulkhead are not tested according to JAR 25.562(c)(5)(6). Instead, a minimum 35 inches distance between the seats and the bulkhead is considered as an acceptable alternative. With the following JAR 25 paragraphs applicable at change 14: 25.307, 25.335(f), 25.345(c), 25.361, 25.371, 25.395, 25.397, 25.459, 25.571, 25.603 (applicable to vertical stabilizer only), 25.613 (applicable to vertical stabilizer only), 25.615 (applicable to vertical stabilizer only), 25.679, 25.723(a)(c), 25.729, 25.731, 25.733, 25.735, 25.772, 25.777, 25.779(a), 25.783, 25.851, 25.855, 25.863, 25.867, 25X899 (applicable to vertical stabilizer only), 25.963(g) (applicable to fuel centre tank only), 25.979, 25.1303, 25.1381, 25.1415, 25.1543 Plus the following CS 25 paragraphs applicable at Amdt 2 25.021, 25.103(b), 25.105(a), 25.111(c), 25.119, 25.121 (except (a)), 25.123(b), 25.125, 25.207, 25.237, 25.253, 25.1419 Plus the following CS 25 paragraphs applicable at Amdt 13 25.963(e) (Fuel Tank Access Covers) Plus the following CS 25 paragraphs applicable at Amdt 15 (applicable at the reference date) 25.023, 25.025, 25.027, 25.029, 25.031, 25.101, 25.103 (except (b)), 25.105 (except (a)), 25.107 (except (h)), 25.109, 25.111 (except (c)), 25.113, 25.115, 25.117, 25.121(a), 25.123 (except (b)), 25.143 (except (c)(i)(j)(l)), 25.145, 25.147, 25.149, 25.161, 25.171, 25.173, 25.175, 25.177, 25.181, 25.201, 25.203, 25.231, 25.233, 25.235, 25.251, 25.253 (except (c)), 25.255, 25.301, 25.302, 25.303, 25.305, 25.307(a), 25.321, 25.331,


25.333, 25.335 (except (f)), 25.337, 25.341, 25.343, 25.345 (except (c)), 25.349, 25.351, 25.365 (except (e),(f),(g)), 25.367, 25.373, 25.415, 25.427, 25.457, 25.471(b), 25.473, 25.479, 25.481(except (b)), 25.483, 25.485, 25.489, 25.491, 25.493, 25.495, 25.499, 25.503, 25.507, 25.509, 25.511, 25.519, 25.561(c) (applicable to large items of masses only), 25.571, 25.619, 25.625, 25.629, 25.631, 25.683(b), 25.773(b), 25.777(i), 25.809(g) (applicable to Door 3 panelization area only), 25.843(a), 25.901(c), 25.963(a), 25.963(d1) (applicable to fuel centre tank only), 25.1001(a)(b)(c) , 25.1323(c)(d), 25.1325(e), 25.1337, 25.1355, 25.1383, 25.1501, 25.1503, 25.1505, 25.1507, 25.1511, 25.1513, 25.1515, 25.1516, 25.1517, 25.1519, 25.1531, 25.1533, 25.1535, 25.1581, 25.1583, 25.1585, 25.1587, 25.1591 Plus the following CS 25 paragraphs applicable at Amdt 15 related to engine installation: (New Engine, Pylon, pre-cooler, air inlet and nacelle, Structural adaptation of the wing at the wing/pylon interface, Electro Pneumatic Bleed Air System) 25.301, 25.303, 25.307, 25.361(a), 25.362, 25.363, 25.365(e1),25.371, 25.561(c), 25.571, 25.581, 25.603, 25.605, 25.607, 25.609, 25.611, 25.613, 25.619, 25.621, 25.625, 25.631, 25.721 (except (a)), 25.723(b), 25.771(e), 25.779(b), 25.851 (except (a)), 25.856(a), 25.863, 25.865, 25.867, 25.869(a), 25.899, 25.901, 25.903, 25.933, 25.934, 25.939, 25.943, 25.951, 25.952, 25.954, 25.955(a), 25.959, 25.961, 25.963(d5), 25.981(a), 25.993 (except (f)), 25.994, 25.995, 25.997, 25.999, 25.1001(a)(b), 25.1011, 25.1013, 25.1015, 25.1017, 25.1019, 25.1021, 25.1023, 25.1025, 25.1041, 25.1043, 25.1045, 25.1091, 25.1093, 25.1103, 25.1121, 25.1123, 25.1141, 25.1143, 25.1145, 25.1155, 25.1163, 25.1165, 25.1167, 25.1181, 25.1182, 25.1183, 25.1185, 25.1187, 25.1189 (except (c),(f),(g),(h)), 25.1191, 25.1193, 25.1195, 25.1197, 25.1199, 25.1201, 25.1203, 25.1207, 25.1301, 25.1305, 25.1309, 25.1315, 25.1321(d), 25.1351 (except (a),(c)), 25.1353 (except (c)), 25.1357, 25.1360(a), 25.1431, 25.1435(a), 25.1438, 25.1461, 25.1521, 25.1527, 25.1549, 25.1551, 25.1557(b), 25.1593, 25.1701, 25.1703 (except (c)), 25.1705, 25.1707, 25.1709, 25.1711, 25.1713, 25.1715, 25.1717, 25.1719, 25.1721 (except (c)), 25.1723, 25.1725, 25.1727, 25.1731 Plus the following CS 25 paragraphs applicable at Amdt 15 related to aerodynamic changes: (New winglet with wing span increase, Wing Aerodynamic clean up, Wing twist change, Wing engine interference, new navigation and strobe lights) 25.301, 25.303, 25.307, 25.373, 25.391, 25.393, 25.445, 25.571 (except (e4)), 25.581, 25.603, 25.605, 25.607, 25.609, 25.611, 25.613, 25.619, 25.625, 25.631, 25.683(b), 25.723(b), 25.863 (except (c)), 25.869(a), 25.899, 25.954, 25.959, 25.1001(a)(b), 25.1301(a), 25.1305, 25.1309, 25.1353 (except (c)), 25.1357, 25.1360(a), 25.1385, 25.1387, 25.1389, 25.1391, 25.1393, 25.1395, 25.1397, 25.1401, 25.1403, 25.1431, 25.1438, 25.1525 Plus the following CS 25 paragraphs applicable at Amdt 17: 25.1316, 25.1317 Additional Airworthiness Requirements (added Post TC): The following requirements are additionally applicable when an A/C configuration include the subject optional design change(s): - The following requirements may be considered to certify the following


optional designs: - CS 25.791 Original issue for symbolic no smoking signs in

lavatories - CS 25.811 and CS 25.812 Amdt. 3 for multi lingual “EXIT” signs. - CS 25.851(a)(c) Amdt 17 for Halon Free Hand Held Fire

Extinguishers - Compliance with Commission regulation (EU) N° 744/2010 of 18 August 2010 amending regulation (EC) n° 1005/2009 of the European Parliament and of the Council on substances that deplete the ozone layer, with regard to the critical uses of halon).

All weather operations

JAR AWO change 1 plus: - Orange paper AWO 91/1, - NPA JAR AWO 3, - NPA JAR AWO 8 (CRI S-148 - Longitudinal touchdown

performance + MABH deletion).

Airborne Communication, Navigation, Surveillance

CS-ACNS Initial Issue - Subpart B, Section 2 – for optional modifications (Post TC)

installing FANS aiming at answering to SES mandate as defined in (EU) N° 29/2009 and amended by (EU) N° 310/2015 of 26 Febuary 2015.

- Subpart D – for optional modifications installing transponders aiming at answering to SES mandate as defined in (EU) No 1207/2011 and amended by (EU) No 1028/2014 of 26 September 2014.

- Subpart E, Section 2 – for RVSM

Special Conditions Original Special Conditions part of Certification Basis (at time of TC):

- JAA Numbering: SC A-5 Limit pilot forces and torque SC E-128 Improved flammability standards for thermal/acoustic insulation SC F-126 Flight Recorders including Data Link Recording SC G-105 Resistance to Fire Terminology SC P-02 Centre of Gravity Control System SC P-27 Flammability Reduction System SC P-32 Fuel Tank Safety SC S-6 Lightning protection indirect effects SC S-10 Effects of external radiations upon aircraft systems (including S-10.1 and S-10.2) SC S-13 Autothrust system SC S-16 Control signal integrity SC S-18 Electronic flight controls SC S-20 Emergency electrical power (NPA 25D, F-179) SC S-21 Brake Wear Limits SC S-23 Electrical wiring and miscellaneous electrical requirements SC S-38 Towbarless towing -EASA Numbering: SC B-01 Stalling and scheduled operating speeds


SC B-02 Electronic Flight Control System (EFCS) Control Surface Awareness SC B-04 Static Directional, Lateral and Longitudinal Stability and Low Energy Awareness SC B-05 Flight Envelope Protection SC B-06 Load Factor Limiting System SC D-03 Brake Kinetic Energy Capacity SC E-03 Engine Cowl retention SC H-01 Enhanced Airworthiness Programme for Aeroplane Systems - ICA on EWIS Additional Special Conditions part of the Certification Basis (added post TC): The following Special Conditions are additionally applicable when an A/C configuration include the subject optional design change(s): - JAA Numbering: SC E-2 Underfloor Crew rest compartment (superseded by SC D-04 for new design) SC E-130 Application of heat release and smoke density requirements to seat materials SC E-1014 HIC compliance for front row seating (inflatable restraints) - EASA Numbering: SC B-09 Soft go around SC D-04 Crew Rest Compartment SC F-131 Flight Instrument External Probes – Qualification in Icing Conditions SC F-134 Head Up Display Installation SC F-137 Security Protection of Aircraft Systems and Networks SC F-GEN-01 Non-rechargeable lithium battery installations, applicable by the date of the TCDS EASA.A.004 at issue 52 Exemptions ANAC Exemptions

PR-02 – Uncontrollable High Thrust in high crosswinds or contaminated runway - RBAC 25.779(b)(1) according to Decision nº 143 of 4 October 2018

SM-01 - RBAC 25.841(a)(2)(i) and (ii), and (a)(3) according to Decision nº 133 of 5 September 2018 Equivalent Safety Findings Original Equivalent Safety Findings part of Certification Basis (at time of TC): - JAA Numbering: ESF E-21 Emergency exit marking reflectance ESF E-29 Fuselage burn through – aft pressure bulkhead ESF E-30 Fuselage burn through – belly fairing ESF E-31 Fuselage burn through – bilge area ESF E-1022 Improved flammability standards for thermal / acoustic insulation materials ESF S-45 Oil temperature indication - EASA Numbering: ESF D-05 Packs off operations ESF E-02 Warning Means for RR Engine Fuel Filters ESF E-05 Thrust Reverser Testing


ESF E-10 Fire Extinguishing Agent Concentration ESF E-12 RR T7000 – Turbine Overheat Detection ESF E-14 RR T7000 engine zone (seals & caps) fire withstanding capability ESF E-15 Nacelles areas behind Firewalls ESF F-04 Landing light switch Additional Equivalent Safety Findings part of the Certification Basis (added post TC): The following Equivalent Safety Findings are additionally applicable when an A/C configuration include the subject optional design change(s): - JAA Numbering: ESF E-15 Reinforced security cockpit door ESF S-1066 Cat III Operations - Excess deviation alert - EASA Numbering: ESF B-100 Vibration / buffeting compliance criteria for large external antenna installation ESF D-101 Green arrow and “Open” Placard of Emergency Exit marking ESF F-128 Minimum Mass Flow of Supplemental Oxygen ESF F-129 Crew Determination of Quantity of Oxygen in Passenger Oxygen System ANAC ELOS:

PR-01 - Digital Only Display of Turbine Engine Intermediate (N2) and High(N3) Rotor Speeds - RBAC 25.1549 according to Ordinance nº 2772 of 4 September 2018 PR-02 - Motion and Effect of Cockpit Control - RBAC 25.779(b)(1) according to Ordinance nº 2770 of 4 September 2018 Environmental requirements for noise, fuel venting and emissions: - Noise: ICAO Annex 16 – Environmental Protection, Volume 1, Edition

7, Amendment 11-B (See EASA TCDSN A.004 for details) - Fuel venting and emissions: ICAO Annex 16 – Fuel Venting, Volume 2,

and corresponding CS-34 requirement.

SIGNIFICANT CHANGES 204809 & 204025 - Project G3ActCT: fuel - main transfer system Special Conditions

Models A330-302, A330-303, A330-323, A330-342, A330-343 can be modified as per Mods 204809 & 204025. The Certification Basis is updated with the following requirements at JAR 25 Change 14 for: - JAR 25.733 (c)(1)

- JAR 25.963 (g) for fuel centre tank

- JAR 25.979 And EASA CRI SC (JAA Numbering): SC P-27 Flammability Reduction System (June 2010) SC P-32 Fuel Tank Safety (November 2013)

203897, 203898, 203899, 203900 & 204809 – G3W08x Weight Variants 080 to 083

Models A330-302, A330-303, A330-323, A330-342, A330-343 can be modified as per Mods 204809 & 204025. The Certification Basis is updated according to in EASA CRI G-9.


All models are produced under approval Part 21 G N° FR.21G.0035 issued by DGAC to AIRBUS S.A.S. Since July 21st, 2008 all models are produced under approval Part 21 G N° EASA.21G.001 issued by EASA to AIRBUS S.A.S.

REQUIRED EQUIPMENT The basic required equipment, as prescribed in the applicable

airworthiness regulations (see Certification Basis) must be installed in the airplane, including the additional Brazilian requirements (Note 4). Cabin furnishings, equipment and arrangement shall conform to the following specification: - 00F252K0005/C01 for cabin seats; - 00F252K0006/C01 for galley; and - 00F252K0020/C01 for cabin attendant seats.

NOTES: NOTE 1 Weight and Balance: a current weight balance report, including list of equipment included in

the certificated empty weight and loading instructions when necessary, must be provided for each aircraft at the time of original certification.

NOTE 2 Markings and Placards: all markings and placards for passenger information, external

markings for emergency, and load limits in cargo/baggage compartments must be presented in Portuguese or bilingual. A list of these placards and the respective translations acceptable to Brazilian Certification Authority is provided in the Airbus booklets: D13029506 for Passenger and Crew and D15008523 for Exterior.

NOTE 3 Continuing Airworthiness: service bulletins, structural repair manuals, aircraft flight manuals, and overhaul and maintenance manuals, which contain a statement that the document is DGAC/EASA approved, are accepted by the Brazilian Certification Authority and are considered Brazilian Certification Authority approved. These approvals pertain to the type design only. Limitation applicable to Safe Life Airworthiness Limitation Items are provided in the A330 Airworthiness Limitations Sections (ALS) sub-parts 1-2 and 1-3 approved by EASA. Limitations applicable to Damage Tolerant Airworthiness Limitations Items are provided in the A330 Airworthiness Limitations Section (ALS) Part 2 approved by EASA.

NOTE 3 Certification Maintenance Requirements are provided in the A330 Airworthiness Limitation Section (ALS) Part 3 approved by EASA. Limitations applicable to Ageing System Maintenance are provided in the A330 Airworthiness Limitation Section (ALS) Part 4 approved by EASA; Fuel Airworthiness Limitations are provided in the A330 Airworthiness Limitations Section (ALS) Part 5 approved by EASA; and Maintenance Review Board Report.

NOTE 4

The Brazilian Certification Authority approved Type Design corresponds to the EASA approved Type Design plus the following specific requirements: - EASA-approved Brazilian AFM; - Markings and placards in Portuguese language or bilingual; - Ozone filter (Mod. 40219 must be incorporated in the A330-300 and A330-900 series aircraft); - Approved cabin configurations for Brazilian aircraft: Mod. 44607 (A330-300 Series); Mod’s 55774 and 46051 (A330-200 Series); Mod 207244 and Mod 206185 (A330-900 series). - Modifications 207304, 207153 and 207400 must be incorporated in the A330-900 series aircraft.

type certificate data sheet nº ea-9806 ea-9806-12 type

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