FAA TYPE CERTIFICATE DATA SHEET NO. A46NM

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FAA TYPE CERTIFICATE DATA SHEET NO. A46NM
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Page no. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 Rev. no. 10 10 10 10 10 10 10 10 10 10 10 10 10 10 4 4 4 4 4 10 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A46NM Revision 10 Airbus A330-200 Series: Models: A330-201, A330-202, A330-203, A330-223, A330-243 A330-300 Series: Models: A330-301, A330-321, A330-322, A330-323, A330-341, A330-342, A330-343 March 19, 2007 FAA TYPE CERTIFICATE DATA SHEET NO. A46NM This data sheet which is part of Type Certificate No. A46NM prescribes conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of the US Federal Aviation Regulations. Type Certificate Holder: Airbus 1, Rond-Point Maurice Bellonte 31707 Blagnac France I. Type A330-200 Series Transport Category Airplanes: Airbus A330-201 - approved April 1, 2003 Airbus A330-202 - approved March 31, 1998 Airbus A330-203 –approved November 1, 2002 Airbus A330-223 - approved June 21, 1999 Airbus A330-243 - approved December 21, 2000 Model: Definition of Reference Airplane by Airbus Documents: A330-201 FAA A330-201 Type Design, ref. EAL 415.1338/02 Issue 1, dated November 6, 2002, for type definition A330-202 FAA A330-202 Type Design, ref. AI/EA-N 415.0531/98 Issue 3, dated May 25, 1998, for type definition and Type Certification Standard Equipment List, ref. 00G000A0102/C0S. A330-203 FAA A330-203 Type Design, ref. EAL 415.1988/02 Issue 2, dated August 5, 2002, for type definition A330-223 FAA A330-223 Type Design, ref. AI/EA-N 415.1223/98 Issue 2, dated August 20, 1998, for type definition and Type Certification Standard Equipment List, ref. 00G000A0123/C0S. A330-243 FAA A330-243 Type Design, ref. AI/EA-N 415.2406/98 Issue 1, dated December 11, 1998, for type definition and Type Certification Standard Equipment List, ref. 00G000A0143/C0S. Engines: Airplane Model Engine Model: Engine Type Certificate: A330-201 Two GE-CF6-80E1A2 turbojet engines FAA-Type Certificate E41NE A330-202 Two GE-CF6-80E1A4 turbojet engines FAA-Type Certificate E41NE A330-203 Two GE-CF6-80E1A3 turbojet engines FAA-Type Certificate E41NE A330-223 Two PW 4168A turbojet engines FAA-Type Certificate E36NE A330-243 Two RR 772B-60 turbojet engines FAA-Type Certificate E39NE A46NM Revision 10 2 March 19, 2007 Fuel: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Engine Limits: Engine Limitations A330-201 CF6-80E1A2 FAA Data Sheet E41NE A330-202 CF6-80E1A4 FAA Data Sheet E41NE A330-203 CF6-80E1A3 FAA Data Sheet E41NE A330-223 PW 4168A FAA Data Sheet E36NE A330-243 RR 772B-60 FAA Data Sheet E39NE Static Thrust at Sea Level • Take-off (5 mn)1 (flat rated 30º C) • maximum continuous (flat rated 25º C) 64,530 lbs 60,400 lbs 66,870 lbs 60,400 lbs 68, 530 lbs 60,400 lbs 68,600 lbs 59,357 lbs 71,100 lbs 63,560 lbs Maximum Engine Speed • N1 rpm (%) • N2 rpm (%) 3,835 (115.5%) 11,105 (113%) 3,835 (115.5%) 11,105 (113%) 3,835 (115.5%) 11,105 (113%) 3,600 10,450 3,861 (99%) 10,611 (100%) Maximum Gas Temperature • Take-off (5mn)1 • Maximum Continuous • Starting2 1,787º F (975º C) 1,724º F (940º C) 1,598º F (870º C) 1,787º F (975º C) 1,724º F (940º C) 1,598º F (870º C) 1,787º F (975º C) 1,724º F (940º C) 1,598º F (870º C) 1,157º F (625º C) 1,112º F (600º C) 1,148º F (620º C) 1,652º F (900º C) 1,562º F (850º C) 1,562º F (850º C) Maximum Oil Temperature (Supply Pump Outlet) ºC • Continuous Operation • Transient (15 mn max.) • Minimum Oil Pressure (PSI) 320º F (160º C) 347º F (175º C) 10.0 psid (69 Kpa) 320º F (160º C) 347º F (175º C) 10.0 psid (69 Kpa) 320º F (160º C) 347º F (175º C) 10.0 psid (69 KPa) 325º F (163º C) 350º F (177º C) 70.0 psid (482.6 KPa ) 374º F (190º C) 374º F (190º C) 24.0 psid Approved oils Brand Names: See GE Service Bulletin 79-001 Specification: See GE specification D50TF1, Class B Brand Names: See GE Service Bulletin 79-001 Specification: See GE specification D50TF1, Class B Brand Names: See GE Service Bulletin 79-001 Specification: See GE specification D50TF1, Class B Oils conforming to P&W Turbojet engine Service Bulletin 238, latest revision. -Aeroshell Turbine Oil (Royco) 500, 555, 560 -Mobil Jet Oil II 254, 291 -Exxon Turbo Oil 2197 Table references: (1) 10 minutes at take-off thrust allowed only in case of engine failure (at take-off or during go around). (2) 4 consecutive cycles of 2 minutes each. Airspeed Limits See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Center of Gravity Limits: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Datum: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Leveling Means: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. A46NM Revision 10 3 March 19, 2007 Maximum Weight: Model A330-200 Airplane A330-201/-202/-203/-223/-243 A330-223 Weight Variant 020 (Basic) kg / lb 050 (MOD 51802) kg / lb 052 (MOD 51804) kg / lb Maximum Take-off Weight, MTOW 230,000 / 507,150 230,000 / 507,150 233,000 / 513,765 Maximum Landing Weight, MLW 180,000 / 396,900 180,000 / 396,900 182,000 / 401,300 Maximum Zero Fuel Weight, MZFW 168,000 / 370,440 168,000 / 370,440 170,000 / 374,850 Minimum Crew: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Number of Seats: The maximum number of passengers approved for emergency evacuation is: 375 passengers with a 3 pairs of Type A and 1 pair Type 1 exits configuration, and 379 passengers with a 4 pairs of Type A exits configuration. Maximum Baggage: Cargo Compartment Maximum Load (kg / lb) Forward 18,869 / 41,606 Aft 15,241 / 33,606 Rear 3,468 / 7,646 For the positions and the loading conditions authorized in each position (references of containers, pallets and associated weight) see weight and Balance Manual: Airbus Document 00G080A0006/C2S for A330-200 airplanes. Fuel Capacity: 3 Tank Airplane Usable Fuel Unusable Fuel Tank liters gallons liters gallons Wing 91,300 24,121 348 70 Center 41,560 10,980 83 21.9 Trim Tank 6,230 1,646 6 1.6 Total 139,090 36,746 437 115.5 Maximum Operating Altitude: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Control Surface Movements: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Manufacturer’s Serial Numbers: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Import Requirements: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Certification Basis (A330-200): a. Part 25 of the FAR effective February 1, 1965, including the following: • Amendments 25-1 through 25-63, amendments 25-65, 25-66, 25-68, 25-69, 25-73, 25-75, 25-77, 25-78, 25-81, 25-82, 25-84 and 25-85 • § 25.851 as amended by amendment 25-74 • The following sections of Part 25 of the FAR as amended through amendment 25-72: A46NM Revision 10 4 March 19, 2007 FAR 25.21 FAR 25.29 FAR 25.111 FAR 25.147 FAR 25.177 FAR 25.181 FAR 25.205 FAR 25.307 FAR 25.331 FAR 25.341 FAR 25.343 FAR 25.345 FAR 25.351 FAR 25.361 FAR 25.373 FAR 25.395 FAR 25.397 FAR 25.415 FAR 25.459 FAR 25.571 (b) FAR 25.613 (Vertical stabilizer only) FAR 25.615 (Vertical stabilizer only) FAR 25.693 FAR 25.723 FAR 25.729 FAR 25.731 FAR 25.733 FAR 25.735 FAR 25.772 FAR 25.779 FAR 25.783 FAR 25.933 FAR25.979 FAR 25.1093 FAR 25.1381 FAR 25.1419 FAR 25.1522 FAR 25.1533 FAR 25.1543 FAR 25.1551 FAR 25.1581 FAR 25.1583 FAR 25.1587 b. Part 25 of the FAR amendment 25-64 with the following exceptions: • Cockpit seats will not meet FAR 25.562 amendment 25-64 but will meet FAR 25.561 • Compliance with 25.785(a), (b), and (c) at amendment 25-64 for front row seats in front of a bulkhead will be based on ensuring a 35 inch free head strike envelope. c. Special conditions in accordance with § 21.16 of the FAR. 1. Special conditions originally written for the A330-300 certification basis that are also included in the A330-200 certification basis: (published in the Federal Register April 15, 1993, Docket No. NM-75, Special Conditions No. 25-ANM-69) (1) Operation without Normal Electrical Power (2) Electronic Flight Control System (EFCS) failures and Mode Annunciation (3) Command Signal Integrity (4) Protection From Lightning and Unwanted Effects of High Intensity Radiated Fields (HIRF) (5) Interaction of Systems and Structures (6) Design Dive Speed (7) Design Maneuver Requirements (8) Limit Pilot Forces (9) Tail plane Tank Emergency Landing Loads (10) Limit Engine Torque (11) Flight Characteristics (12) Flight Envelope Protection (13) Side Stick Controllers (14) Computerized Airplane Flight Manual (AFM) Performance Information 2. Special condition for the optional installation of the Lower Deck Mobile Crew Rest Compartment: (published in the Federal Register on January 6, 2005, Docket No. NM287, Special Condition No. 25-281-SC) Lower Deck Mobile Crew Rest (LD-MCR) Compartment (optional installation) d. Part 34 of the FAR, effective September 10, 1990, including Amendment 34-1. e. Part 36 of the FAR, effective December 1, 1969, including Amendments 36-1 through 36-21. A46NM Revision 10 5 March 19, 2007 f. The technical requirements are complemented by the following guidance material: For precision approach and landing, 1. AC 120-29 2. AC 120-28C and for the automatic flight control system 1. AC 20-57A for automatic landing 2. AC 25.1329-1A for cruise g. Equivalent safety findings have been made in accordance with FAR 21.21(b)(1) for the following paragraphs of the FAR: (1) 25.335(d) for design airspeeds (2) 25.345 for high lift devices (3) 25.349 for control surface loads (4) 25.351(b) for unsymmetrical loads (5) 25.371 for gyroscopic loads (6) 25.373 for speed control devices (7) 25.101(I); 25.105(c)(1); 25.109(a)(b)(c)(d)(e)(f); 25.113(a)(b)(c); 25.115(a); 25.735(f)(g)(h)(b) for rejected takeoff and landing performance (8) 25.933(a)(1)(ii), 25.1309(b)(1) for flight critical thrust reverser (9) 25.1203(d) for turbine overheat detection (RR Trent 700 powered A330-243 only) (10) 25.1305(c)(6) Warning means for engine fuel filter contamination (RR Trent 700 powered A330-243 only) (11) 25.1305; 25.1501(b) for APU system flight deck instrumentation h. Optional requirements elected: • 25.801 for ditching. • 25.1419 for icing. Note 1: Compliance with the FAA Required Modification List for Airbus Model A330 Aircraft as included under the Import Requirements section of TCDS Revision 4, dated March 21, 2000 or later TCDS revision, is necessary for an A330 aircraft to be found in a condition for safe operation. • The FAA has accepted Model A330-223 aircraft in the Airbus as-delivered configuration for msn 609 and on as compliant with the applicable modifications of the A330 RML. FAA acceptance is based on the Airbus statement to the FAA (ref. Airbus letter EAL G03D0415493, dated July 9, 2004) that the RML modifications applicable to model A330-223 aircraft are either part of the FAA approved type design (ref. AI/EA-N 415.1223/98 Issue 2, dated August 20, 1998), required to be installed at aircraft delivery by DGAC/EASA AD, or required to be installed by Airbus on all A330-223 aircraft at time of delivery. The Direction Generale de 'Aviation Civile (DGAC) of France originally type certificated the Airbus Model A330-200 series airplanes under its type certificate number DGAC-F TC 184. The FAA validated this product under U.S. Type Certificate Number A46NM. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of DGAC. Production Basis: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Equipment: • The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. • The following Airbus Documents defines the set of modifications which comprise the FAA certificated type design. These documents contain certain modifications determined necessary for FAA certification, including installation of ozone converters, fuel system improvements and thrust reverser modifications. • EAL 415.1338/02 Issue 1, dated November 6, 2002 for the A330-201 • AI/EA-N 415.0531/98 Issue 3, dated May 25, 1998 for the A330-202 • AI/EAL 415.1988/01 Issue 2, dated August 5, 2001 for the A330-203 • AI/EA-N 415.1223/98 Issue 2, dated August 20, 1998 for the A330-223 • AI/EA-N 415.2406/98 Issue 1, dated December 11, 1998 for the A330-243 • Equipment approved for installation is listed in the Certification Standard Equipment List • 00G000A0102/C0S for the A330-202. • 00G000A0123/C0S for the A330-223. • 00G000A0143/C0S for the A330-243. • Cabin furnishings, equipment and arrangement shall conform to the following specification: • 00F252K0005/C01 for cabin seats, • 00F252K0006/C01 for galley, A46NM Revision 10 6 March 19, 2007 • 00F252K0020/C01 for cabin attendant seats. Hydraulic Fluids: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Auxiliary Power Unit (APU): See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Tires: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Service Information: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Airplane Flight Manual: Airplane operation must be in accordance with the EASA Approved Airplane Flight Manual (AFM), US version, listed below, or later EASA approved revision applicable to the specific airplane model, modification status and serial number. All placards required by either the AFM, the applicable operating rules, or the certification basis must be installed in the airplane. Model A330 Aircraft Airbus Document Reference Revision No. Date -201 STL 33000 1 March 10, 2003 -202 AI/ST-F 33000 2 January 6, 1999 -203 AI/ST-F 33000 1 October 24, 2002 -223 AI/ST-F 33000 2 January 6, 1999 -243 AI/ST-F 33000 2 March 15, 2000 Environmental requirements for noise: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. II. Airbus A330-300 Series Transport Category Airplanes: Airbus A330-301 - approved October 21, 1993 Airbus A330-321 - approved June 21, 1999 Airbus A330-322 - approved June 21, 1999 Airbus A330-323 - approved October 8, 1999: Airbus A330-341 – approved December 21, 2000 Airbus A330-342 - approved December 21, 2000 Airbus A330-343 - approved December 21, 2000 Model: Definition of Reference Airplane by Airbus Documents: A330-301 FAA A330-301 Type Design, ref. AI/EA-N 415.1181/96 Issue 3, dated July 16, 1997 for type definition and Type Certification Standard Equipment list, ref. 00G000A0101/C0S. A330-321 FAA A330-321 Type Design, ref. AI/EA-N 415.1184/96 Issue 3, dated June 25, 1998 for type definition and Type Certification Standard Equipment list, ref. 00G000A0121/C0S. A330-322 FAA A330-322 Type Design, ref. AI/EA-N 415.1183/99 Issue 3, dated June 25, 1998 for type definition and Type Certification Standard Equipment list, ref. 00G000A0121/C0S. A330-323 FAA A330-323 Type Design, ref. AI/EA-N 415.1630/99 Issue 1, dated July 20, 1999 for type definition and Type Certification Standard Equipment list, ref. 00G000A0123/C3S. A330-341 FAA A330-341 Type Design, ref. AI/EA-N 415.1187/96 Issue 2, dated December 11, 1998 for type definition and Type Certification Standard Equipment list, ref. 00G000A0141/C0S. A330-342 FAA A330-341 Type Design, ref. AI/EA-N 415.1182/96 Issue 2, dated December 11, 1998 for type definition and Type Certification Standard Equipment list, ref. 00G000A0141/C0S. A330-343 FAA A330-343 Type Design, ref. AI/EA-N 415.2027/99 Issue 1, dated October 22, 1999 for type definition and Type Certification Standard Equipment list, ref. 00G000A0143/C3S. A46NM Revision 10 7 March 19, 2007 Engines: Airplane Model: Engine Model: Engine Type Certificate: A330-301 Two GE-CF6-80E1A2 turbojet engines FAA-Type Certificate E41NE A330-321 Two PW 4164 turbojet engines FAA-Type Certificate E36NE A330-322 Two PW 4168 turbojet engines FAA-Type Certificate E36NE A330-323 Two PW 4168A turbojet engines FAA-Type Certificate E36NE A330-341 Two RR Trent 768-60 turbojet engines FAA-Type Certificate E39NE A330-342 Two RR Trent 772-60 turbojet engines FAA-Type Certificate E39NE A330-343 Two RR Trent 772B-60 turbojet engines FAA-Type Certificate E39NE Fuel: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Engine Limits: Engine Limitations A330-301 CF6-80E1A2 FAA Data Sheet E41NE Static Thrust at Sea Level • Take-off (5 mn)1 (flat rated 30º) • maximum continuous (flat rated 25º C) 64,530 lbs 60,400 lbs Maximum Engine Speed • N1 rpm (%) • N2 rpm (%) 3,835 (115.5%) 11,105 (113%) Maximum Gas Temperature • Take-off (5mn)1 • Maximum Continuous • Starting2 1,787º F (975º C) 1,724º F (940º C) 1,598º F (870º C) Maximum Oil Temperature (Supply Pump Outlet) ºC • Continuous Operation • Transient (15 mn max.) • Minimum Oil Pressure (PSI) 320º F (160º C) 347º F (175º C) 10.0 psid (69 KPa ) Approved oils See SB CFMI 79-001 or GE specification D50TF1 Class B Engine Limitations A330-321 PW 4164 FAA Data Sheet E36NE A330-322 PW 4168 FAA Data Sheet E36NE A330-323 PW 4168A FAA Data Sheet E36NE Static Thrust at Sea Level • Take-off (5 mn)1 (flat rated 30º ) • maximum continuous (flat rated 25º C) 64,500 lbs 55,800 lbs 68,600 lbs 59,357 lbs 68,600 lbs 59,357 lbs Maximum Engine Speed • N1 rpm (%) • N2 rpm (%) 3,600 (101%) 10,450 (103%) 3,600 (101%) 10,450 (103%) 3,600 (101%) 10,450 (103%) Maximum Gas Temperature • Take-off (5mn)1 • Maximum Continuous • Starting2 1,157º F (625º C) 1,112º F (600º C) 1,148º F (620º C) 1,157º F (625º C) 1,112º F (600º C) 1,148º F (620º C) 1,157º F (625º C) 1,112º F (600º C) 1,148º F (620º C) Maximum Oil Temperature (Supply Pump Outlet) ºC • Continuous Operation • Transient (15 mn max.) • Minimum Oil Pressure (PSI) 325º F (163º C) 350º F (177º C) 70.0 psid (482.6 KPa ) 325º F (163º C) 350º F (177º C) 70.0 psid (482.6 KPa ) 325º F (163º C) 350º F (177º C) 70.0 psid (482.6 KPa ) Approved oils See P&W Service Bulletin 238, latest revision. A46NM Revision 10 8 March 19, 2007 Engine Limitations A330-341 Trent 768-60 FAA Data Sheet E39NE A330-342 Trent 772-60 FAA Data Sheet E39NE A330-343 Trent 772B-60 FAA Data Sheet E39NE Static Thrust at Sea Level • Take-off (5 mn)1 (flat rated 30º ) • maximum continuous (flat rated 25º C) 67,500 lbs 60,410 lbs 71,100 lbs 63,560 lbs 71,100 lbs 63,560 lbs Maximum Engine Speed • N1 rpm (%) • N2 rpm (%) 3,861 (99%) 10,611 (100%) 3,861 (99%) 10,611 (100%) 3,861 (99%) 10,611 (100%) Maximum Gas Temperature • Take-off (5mn)1 • Maximum Continuous • Starting2 1,652º F (900º C) 1,562º F (850º C) 1,562º F (850º C) 1,652º F (900º C) 1,562º F (850º C) 1,562º F (850º C) 1,652º F (900º C) 1,562º F (850º C) 1,562º F (850º C) Maximum Oil Temperature (Supply Pump Outlet) ºC • Continuous Operation • Transient (15 mn max.) • Minimum Oil Pressure (PSI) 374º F (160º C) 374º F (175º C) 24.0 psid 374º F (160º C) 374º F (175º C) 24.0 psid 374º F (160º C) 374º F (175º C) 24.0 psid Approved oils -Aeroshell Turbine Oil (Royco) 500, 555, 560, Mobil Jet Oil II 254, 291,Exxon Turbo Oil 2197 Table references: (1) 10 minutes at take-off thrust allowed only in case of engine failure (at take-off or during go-around). (2) 4 consecutive cycles of 2 minutes each. Center of Gravity Limits: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Datum: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Leveling Means: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Maximum Weight: Model A330 Airplane A330-301/-321/-322/-341/-342 A330-301 Weight Variant 000 (Basic) kg / lb 002 (MOD 42600) kg / lb 001 (MOD 42200) kg / lb Maximum Take-off Weight, MTOW 212,000 / 467,460 212,000 / 467,460 184,000 / 405,720 Maximum Landing Weight, MLW 174,000 / 383,670 177,000 / 390,285 174,000 / 383,670 Maximum Zero Fuel Weight, MZFW 164,000 / 361,620 167,000 / 368,235 164,000 / 361,620 Model A330 Airplane A330-323/-343 A330-323 Weight Variant 020 (Basic) kg / lb 022 (MOD 47785) kg / lb 050 (MOD 51805) kg / lb 052 (MOD 51807) kg / lb Maximum Take-off Weight, MTOW 230,000 / 507,150 233,000 / 513,765 230,000 / 507,150 233,000 /513,765 Maximum Landing Weight, MLW 185,000 / 407,925 187,000 / 412,335 185,000 / 407,925 187,000 /412,335 Maximum Zero Fuel Weight, MZFW 173,000 / 381,465 175,000 / 385,875 173,000 / 381,465 175,000 /385,875 Minimum Crew: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Number of Seats: The maximum number of passengers approved for emergency evacuation is: 375 passengers with a 3 pair Type A and 1 pair Type 1 exit configuration, and 379 passengers with a 4 pair Type A exit configuration. A46NM Revision 10 9 March 19, 2007 Maximum Baggage: Cargo Compartment Maximum Load (kg / lb) Forward 22,861 / 50,408 Aft 18,507 / 40,808 Rear 3,468 / 7,647 For the positions and the loading conditions authorized in each position (references of containers, pallets and associated weight) see Weight and Balance Manual Ref. 00G080A0006/C3S for A330-300 airplanes. Fuel Capacity: Two Tank Airplane Usable Fuel Unusable fuel Model A330-301/-321/-322/-341/-342 A330-323/-343 All Models Tank Liters (kg) Gallons (lb) liters (kg) gallons (lb) liters (kg) gallons (lb) Wing 91,764 (73,411) 24,244 (161,871) 91,300 (73,040) 24,122 (161,053) 348 (279) 92 (615) Trim Tank 6,121 (4,897) 1,617 (10,798) 6,230 (4,984) 1,646 (10,990) 6 (5) 1.6 (11) Total 97,885 (78,308) 25,861 (172,669) 97,530 (78,024) 25,768 (172,043) 354 (284) 94 (626) Maximum Operating Altitude: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Control Surface Movements: (Total one-way travel in each direction of each movable control surface on the aircraft.) See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Manufacturer’s Serial Numbers: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Import Requirements: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Certification Basis (A330-300): a. Part 25 of the FAR effective February 1, 1965, including the following: • Amendments 25-1 through 25-63, amendments 25-65, 25-66, 25-77 b. Part 25 of the FAR amendment 25-64 with the following exceptions: • Cockpit seats will not meet FAR 25.562 amendment 25-64 but will meet FAR 25.561 • Compliance with 25.785(a), (b), and (c) at amendment 25-64 for front row seats in front of a bulkhead will be based on ensuring a 35 inch free head strike envelope. c. Special conditions in accordance with § 21.16 of the FAR. 1. Special conditions published in the Federal Register on April 15, 1993, (ref. Docket No. NM-75, Special Conditions No. 25-ANM-69): (1) Operation without Normal Electrical Power (2) Electronic Flight Control System (EFCS) failures and Mode Annunciation (3) Command Signal Integrity (4) Protection From Lightning and Unwanted Effects of High Intensity Radiated Fields (HIRF) (5) Interaction of Systems and Structures (6) Design Dive Speed (7) Design Maneuver Requirements (8) Limit Pilot Forces (9) Tail plane Tank Emergency Landing Loads A46NM Revision 10 10 March 19, 2007 (10) Limit Engine Torque (11) Flight Characteristics (12) Flight Envelope Protection (13) Side Stick Controllers (14) Computerized Airplane Flight Manual (AFM) Performance Information 2. Special condition for the optional installation of the Lower Deck Mobile Crew Rest Compartment: (published in the Federal Register on January 6, 2005, Docket No. NM287, Special Condition No. 25-281-SC) Lower Deck Mobile Crew Rest (LD-MCR) Compartment (optional installation) d. Special Federal Aviation regulation FAR Part 34, effective September 10, 1990. e. Part 36 of the FAR as amended by amendments 36-1 through 36-20. f. The technical requirements are complemented by the following guidance material: For precision approach and landing, 1. AC 120-29 2. AC 120-28C and for the automatic flight control system 1. AC 20-57A for automatic landing 2. AC 25.1329-1A for cruise g. Equivalent safety findings have been made in accordance with FAR 21.21(b)(1) for the following paragraphs of the FAR: (1) 25.335(d) for design airspeeds (2) 25.345 for high lift devices (3) 25.349 for control surface loads (4) 25.351(b) for unsymmetrical loads (5) 25.371 for gyroscopic loads (6) 25.373 for speed control devices (7) 25.101(I); 25.105(c)(1); 25.109(a)(b)(c)(d)(e)(f); 25.113(a)(b)(c); 25.115(a); 25.735(f)(g)(h)(b) for rejected takeoff and landing performance (8) 25.933(a)(1)(ii), 25.1309(b)(1) for flight critical thrust reverser (9) 25.1203(d) for turbine overheat detection (RR Trent 700 powered A330-341, -342, -343 only) (10) 25.1305(c)(6) Warning means for engine fuel filter contamination (RR Trent 700 powered A330-341, -342 and -343 only) (11) 25.1305: 25.1501(b) for APU system flight deck instrumentation h. Optional requirements elected: • 25.801 for ditching. • 25.1419 for icing. Note 1: Compliance with the FAA Required Modification List for Airbus Model A330 Aircraft as included under the Import Requirements section of TCDS Revision 4, dated March 21, 2000 or later TCDS revision, is necessary for an A330 aircraft to be found in a condition for safe operation. • The FAA has accepted Model A330-323 aircraft in the Airbus as-delivered configuration for msn 524 and on as compliant with the applicable modifications of the A330 RML. FAA acceptance is based on the Airbus statement to the FAA (ref. Airbus letter EAL G01M03003568 issue 2, dated June 24, 2003) that the RML modifications applicable to model A330-323 aircraft are either part of the FAA approved type design (ref. AI/EA-N 415.1630/99 Issue 1, dated July 20, 1999), required to be installed at aircraft delivery by DGAC AD, or required to be installed by Airbus on all Model A330-323 aircraft at time of delivery. The Direction Generale de 'Aviation Civile (DGAC) of France originally type certificated the Airbus Model A330-300 series airplanes under its type certificate number DGAC-F TC 184. The FAA validated this product under U.S. Type Certificate Number A46NM. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on behalf of DGAC. Production Basis: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. A46NM Revision 10 11 March 19, 2007 Equipment: • The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. • The following Airbus Documents defines the set of modifications which comprise the FAA certificated type design. This document contains certain modifications determined necessary for FAA certification, including installation of ozone converters, fuel system improvements and thrust reverser modifications. • AI/EA-N 415.1181/96 Issue 3, dated July 16, 1997 for the A330-301 • AI/EA-N 415.1184/96 Issue 3, dated June 25, 1998 for the A330-321 • AI/EA-N 415.1183/96 Issue 3, dated July 25, 1998 for the A330-322 • AI/EA-N 415.1630/99 Issue 1, dated July 20, 1999 for the A330-323 • AI/EA-N 415.1187/96 Issue 2, dated December 11, 1998 for the A330-341 • AI/EA-N 415.1182/99 Issue 2, dated December 11, 1998 for the A330-342 • AI/EA-N 415.2027/99 Issue 1, dated October 22, 1999 for the A330-343 • Equipment approved for installation is listed in the Certification Standard Equipment List • 00G000A0101/C0S for the A330-301. • 00G000A0121/C0S for the A330-321 and -322. • 00G000A0123/C3S for the A330-323. • 00G000A0141/C0S for the A330-341 and -342. • 00G000A0143/C3S for the A330-343. • Cabin furnishings, equipment and arrangement shall conform to the following specification: • 00F252K0005/C01 for cabin seats, • 00F252K0006/C01 for galley, • 00F252K0020/C01 for cabin attendant seats Hydraulic Fluid: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Auxiliary Power Unit (APU): See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Tires: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Service Information: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. Airplane Flight Manual: Airplane operation must be in accordance with the EASA-Approved Airplane Flight Manual (AFM), US version, listed below, or later EASA approved revision applicable to the specific airplane model, modification status and serial number. All placards required by either the AFM, the applicable operating rules, or the certification basis must be installed in the airplane. Aircraft Model A330 Airbus Document Reference. Revision No. Date -301 AI/EV-O 33000 3 January 6, 1999 -321, -322 AI/ST-F 33000 2 January 6, 1999 -323 AI/ST-F 33000 4 May 18, 2001 -341, -342 AI/ST-F 33000 3 March 15, 2000 -343 AI/ST-F 33000 2 March 15, 2000 Environmental requirements for noise: See Section III, Data pertinent to All Model A330-200 and A330-300 Series airplanes. _________________________________________________________________________________________________________ A46NM Revision 10 12 March 19, 2007 III. Data Pertinent to All Model A330-200 and A330-300 Series airplanes: Fuel: Specification Aircraft Nomenclature United States France United Kingdom A330-201 A330-202 A330-203 A330-301 Kerosene (conform to GE specification D50TF2 with current exception of JP4 and JET B) ASTM D 1655 (JET A) (JET A1) AIR 3405C DERD 2494/2453 A330-223 A330-321 A330-322 A330-323 Fuel and fuel additives conforming to the latest applicable issue of FAA approved Pratt & Whitney Turbojet Engine Service Bulletin 2016 may be used separately or mixed in any proportions without adversely affecting the engine operation or power output. A330-243 A330-341 A330-342 A330-343 Approved fuel and additives are identified in the relevant Operating instructions defined in the Rolls Royce Manual F-Trent – A330 (a) Additives: According to GE "Specific Operating Instructions", installation manual. The above mentioned fuels are also suitable for the APU. Airspeed Limits (Indicated Airspeed, IAS, unless otherwise stated): • Maximum Operating Limit Speed/Mach, VMO/MMO 330 KIAS / .86 • Design Diving Speed, VD 365 KIAS / .93 • Design Maneuvering Speed, VA Refer to AFM Performance Section • Maximum Flaps/Slats Extended Speed or Operating Speed, VFE Configuration Slats/Flaps/Ailerons º VFE (kt) 1 1 + F 16/0/0 16/8/0 16/8/5 240 215 205 Intermediate Approach Take-off Take-off 2 20/14/10 196 Take-off and Approach 3 23/22/10 186 Take-off, Approach, and Landing FULL 23/32 180 Landing • Minimum Control Speed, VMC Refer to AFM performance Section. (Performance Engineering Program/OCTOPUS) Landing Gear Speeds: • Maximum Speed with Landing Gear Operating (Extension and Retraction) VLO 250 KIAS / .55M • Maximum Speed with Landing Gear Locked Down, VLE 250 KIAS / .55M • Tire Limit Speed (Ground Speed) 203 KIAS (235mph) Center of Gravity Limits: Refer to EASA-Approved Airplane Flight Manual, US Version, Limitations Section for center of gravity envelope. Note: 0% MAC is located 1359.59 in. (34.532m) from the datum line Datum: The aircraft reference zero datum point is located 251.29 in. (6.3825 m) forward of the nose section, 275.6 in. (7m) under the fuselage centerline (datum line). Leveling Means: Inclinometer on cabin seat track rails (refer to WBM chapter 1.80). Minimum Crew: 2 - Pilots Maximum Operating Altitude Basic: 41,100 feet (12,527 m) slats and flaps retracted (clean) Option: 41,450 feet (12,634 m) slats and flaps retracted (clean) with modification 52536 20,000 feet (6,096 m) slats or slats/flaps extended. A46NM Revision 10 13 March 19, 2007 Control Surface Movements: (Total one-way travel in each direction of each movable control surface on the aircraft.) Control Surface Maximum Travel Aileron +25 /- 25º #1 Spoilers Speed Brake 23º Lift Dumper 35º #2,3 Spoilers Roll 35º Speed Brake 30º Lift Dumper 50º #4,5,6 Spoilers Roll 35º Speed Brake 30º Lift Dumper 50º Aileron Droop 10º Flaps 32º Slats 23º Stabilizers +2º/-14º Elevator +15º/-30º Rudder +30º/-30º Environmental requirements for noise: ICAO Annex 16 Volume 1 – Chapter 3, or Chapter 4 with Modification 55005. Manufacturer’s Serial Numbers/Production Basis: A330 aircraft, all series and models, are produced in France under production approval FR.21G.0035 (formerly FG 035) issued by the DGAC (on behalf of EASA) to Airbus. Import Requirements: The FAA can issue a U.S. airworthiness certificate based on an French Export Certificate of Airworthiness (Export C of A) signed by a representative of the Direction Generale de 'Aviation Civile (DGAC) of France on behalf of the European Community. The Export C of A should contain the following statement (in the English language): “The aircraft covered by this certificate has been examined, tested, and found to conform to the Type Design approved under FAA Type Certificate No. A46NM as defined in TCDS A46NM revision 4 (or later revision) and to be in condition for safe operation." The U.S. airworthiness certification basis for aircraft type certificated under FAR Section 21.29 and exported by the country of manufacture is FAR Section 21.183(c) or 21.185(c). The U.S. airworthiness certification basis for aircraft type certificated under FAR Section 21.29 exported from countries other than the country manufacture (e.g., third party country) is FAR Sections 21.183(d) or 21.185(b). These sections provide that U.S. airworthiness certificates are issued only if the Administrator finds “that the aircraft conforms to the type design and is in a condition for safe operation.” Notwithstanding that FAR sections 21.183(d) and 21.185(b) do not specifically address or require certification by the foreign civil airworthiness authority of the country of manufacture, such certification is the only practical way for an applicant to show, and the FAA to find conformity to the FAA-approved type design and condition for safe operation. Additional guidance is contained in FAA Advisory Circular (AC) 21-23, Airworthiness Certification of Civil Aircraft, Engines, Propellers, and Related Products Imported into the United States. FAA Required Modification List for Airbus Model A330 Aircraft: Prior to issuance of a Standard Airworthiness Certificate on any Airbus A330 model aircraft, all modifications shown on the (Model A330) Required Modification List (RML) with compliance times already past, must be accomplished before the aircraft can be found to be in a condition for safe operation. Note 1: RML modifications with compliance times already past means that relative to the date of issuance of an Airworthiness Certificate for an individual aircraft, the compliance time of the RML item in calendar time and/or flight hours and/or flight cycles has been exceeded. All future required modifications shown on the RML must be incorporated into the operator’s maintenance or inspection program prior to placement of the aircraft into operation . These future RML modifications must be incorporated prior to the compliance time specified in the RML and must remain with the airplane records. In the event of any transfer of the airplane to another operator these RML requirements must continue to be complied with and incorporated into the new operator’s maintenance program. Note 2: Future RML modifications means that relative to the date of issuance of an Airworthiness Certificate for an individual aircraft, the compliance time of the RML item in calendar time and/or flight hours and/or flight cycles has not yet been exceeded. A46NM Revision 10 14 March 19, 2007 Prior to issuance of a Standard Airworthiness Certificate on any Airbus A330 model aircraft, the following note must be placed on the Airworthiness Certificate: “CONTINUED AIRWORTHINESS: Type Certificate Data Sheet (TCDS) A46NM, Revision 4, dated March 21, 2000, contains the “FAA Required Modification List (RML)” that must be complied with for this aircraft to remain in a condition for safe operation. The RML is part of the permanent record for this aircraft; it must remain with the aircraft data and continue to be complied with in the event of transfer to another operator.” Note 3: The RML was finalized through its publication in TCDS Revision 4 and requirements will not be added by later TCDS revisions. Therefore, the RML in TCDS A46NM Revision 4 or any later TCDS revision are equivalent and acceptable for compliance. All future modifications that the FAA determines must be accomplished on U.S. registered aircraft will be addressed by issuance of an Airworthiness Directive (AD). Authority for these required modifications is given per the airworthiness certification provisions of 49 U.S.C. 44704 (c), which states "the Administrator may include in an airworthiness certificate terms required in the interest of safety". “Terms required in the interest of safety” include actions to correct unsafe conditions issued by the foreign authority of the state of design that also meet FAA criteria for corrective action. This law also gives the FAA the authority to adopt FAR § 21.183(c) and (d), which form the regulatory basis for the issue of standard U.S. airworthiness certificates on imported products. 14 CFR §21.183(c) and (d) provide that airworthiness certificates are issued only if the Administrator finds “that the aircraft conforms to the type design and is in a condition for safe operation.” The modifications identified in the list below are required in the interest of safety and are necessary for this airplane to be in a condition for safe operation. A Notice of Policy Statement announcing the FAA’s policy with respect to foreign mandatory continued airworthiness information, when no aircraft of the affected design are currently operating in the U.S. was published in the Federal Register on May 11, 1998 Alternative Methods of Compliance to an RML modification: For each RML modification, an alternative method of compliance (AMOC) or adjustment of the compliance time may be used if approved by the Manager, International Branch, ANM-116, FAA Transport Airplane Directorate; 1601 Lind Avenue Southwest; Renton, Washington 98055; telephone (425) 227-1263; fax (425) 227-1149. Operators shall submit their request through an appropriate FAA Principle Maintenance Inspector, who may add comments and then send it to the Manager, International Branch. FAA Compliance findings to the A330 RML: The FAA has accepted: (1) Model A330-323 aircraft in the Airbus as-delivered configuration for msn 524 and on as compliant with the applicable modifications of the A330 RML. FAA acceptance is based on the Airbus statement to the FAA (ref. Airbus letter EAL G01M03003568 issue 2, dated June 24, 2003) that the RML modifications applicable to model A330-323 aircraft are either part of the FAA approved type design (ref. AI/EA-N 415.1630/99 Issue 1, dated July 20, 1999), required to be installed at aircraft delivery by DGAC/EASA AD, or required to be installed by Airbus on all A330-323 aircraft at time of delivery. (2) Model A330-223 aircraft in the Airbus as-delivered configuration for msn 609 and on as compliant with the applicable modifications of the A330 RML. FAA acceptance is based on the Airbus statement to the FAA (ref. Airbus letter EAL G03D0415493, dated July 9, 2004) that the RML modifications applicable to model A330-223 aircraft are either part of the FAA approved type design (ref. AI/EA-N 415.1223/98 Issue 2, dated August 20, 1998), required to be installed at aircraft delivery by DGAC/EASA AD, or required to be installed by Airbus on all A330-223 aircraft at time of delivery. FAA Required Modification List(RML) for the Airbus Model A330 Aircraft: The RML for the A330 is composed of items 1A through 40B as listed on the following pages. A46NM Revision 4 15 March 21, 2000 A330 Required Modification List (RML) RML # DGAC CN # Mod # Mandatory Action Applicable To: S/B # S/B REV(s) Compliance Time 1A 1996-006- 024(B)R1 42409 FUSELAGE - REINFORCE JOINT AT FRAMES 48 - 53.2 Airplanes without mod 43475 or without SB A330- 21-3027 53-3015 1 or higher Frames 53/53.1/53.2: Prior to 5800 total flight cycles. For frames 48 to 52: Prior to 15600 total flight cycles. 1B 1996-006- 024(B)R1 42409 FUSELAGE - REINFORCE JOINT AT FRAMES 48 - 53.2 Airplanes with mod 43475 or with SB A330-21- 3027 53-3015 1 or higher Frames 53/53.1/53.2 prior to 5300 total flight cycles. For frames 48 to 52 prior to 14100 total flight cycles. 2 1997-265- 056(B)R1 N/A REVISE AMM AIRWORTHINESS LIMITS. ALL Model A330 Airplanes AMM CHAPTER 5 8 or higher Prior to C of A Issuance 3 1998-539- 088(B) N/A REPLACE FRANKENJURA EYE-END ON ELEVATOR SERVOCONTRLS ALL Model A330 Airplanes AOT 27-24 1 or higher Prior to 7/09/99 or C of A Issuance; whichever occurs later 4 1999-111- 093(B) 45870 AND 46231 AND 46891 INSTALL WIRING FOR E-BRAKE SHUTOFF VALVE ALL Model A330 Airplanes 29-3054 AND 32- 3083R2 3054: 0 or higher 3083: 2 or higher Prior to 7/31/01 or C of A Issuance; whichever occurs later 5 1999-123- 092(B) 43724, OR 44661, OR 44662 FLIGHT MANAGEMENT COMPUTER REPLACEMENT ALL Model A330 Airplanes 22-3011, OR 22- 3009, OR 22-3010 All SB’s revision 1 or higher Prior to 6/30/99 or C of A Issuance; whichever occurs later 6 1999-142- 097(B) 46170, OR 46596 FLIGHT CONTROL UNIT CHANGE Airplanes with Mod. 44887 OR with SB 22-3012 22-3021, OR 22-3020 1 or higher Prior to 6/30/99 or C of A Issuance; whichever occurs later 7 1999-144- 094(B)R1 45977 REPLACE RAT ACTUATOR Airplanes with Sundstrand RAT 29-3057 1 or higher Prior to 12/31/00 or C of A Issuance; whichever occurs later 8 1999-331- 098(B) 42447 REPLACE NLG HINGE FITTING BRACKETS ALL Model A330 Airplanes 52-3046 1 or higher Prior to 01/21/01 or C of A Issuance; whichever occurs later 9A 1999-350- 100(B)R1 46904, AND 46905 REPLACE PIVOT PINS & BELLCRANK ASSEMBLIES -202, -223,-243, - 323, -343 32-3095 1 or higher The Later of (a) and (b): (a) Prior to 4800 total flight cycles or within 5 years since new; which ever occurs first; and (b) Prior to 06/08/01 9B 1999-350- 100(B)R1 46902, AND 46903 REPLACE PIVOT PINS & BELLCRANK ASSEMBLIES ALL Model A330 Airplanes 32-3096 1 or higher Prior to 10 years since new or C of A Issuance; whichever occurs later 9C 1999-350- 100(B)R1 46904, AND 46905 REPLACE PIVOT PINS & BELLCRANK ASSEMBLIES -301, -321, -322, - 341, -342 32-3095 1 or higher The Later of (a) and (b): (a) Prior to 6500 total flight cycles or within 5 years since new; which ever occurs first; and (b) Prior to 06/08/01 10A 1999-406- 103(B) 45307 REPLACE HORIZONTAL HYDRAULIC BRACKET All Airplanes, except –202, with mod 43475 OR with SB 21-3027 53-3088 0 or higher Prior to 7880 total flight cycles or 30700 total flight hrs; whichever occurs first A46NM Revision 4 16 March 21, 2000 A330 Required Modification List (RML) RML # DGAC CN # Mod # Mandatory Action Applicable To: S/B # S/B REV(s) Compliance Time 10B 1999-406- 103(B) 45307 REPLACE HORIZONTAL HYDRAULIC BRACKET All Airplanes, except –202, without mod 43475 OR without SB 21-3027 53-3088 0 or higher Prior to 8620 total flight cycles or 33600 total flight hrs; whichever occurs first 10C 1999-406- 103(B) 45307 REPLACE HORIZONTAL HYDRAULIC BRACKET -202 53-3088 0 or higher Prior to 8540 total flight cycles or 33300 total flight hrs, whichever occurs first 11 1999-442- 104(B) 46820, OR 46865 PASSENGER/ CREW DOOR FRAME LININGS ALL Airplanes with mod 44461 OR 44462 OR 44463 OR 44464 OR 44465 25-3096 1 or higher Prior to 11/03/05 or C of A Issuance; whichever occurs later 12A 1999-449- 105(B) 45899 REINFORCE FRAME 40 -202, -223 53-3093 2 or higher Prior to 9700 Total flight cycles or 28800 total flight hours; whichever occurs first 12B 1999-449- 105(B) 45899 REINFORCE FRAME 40 -301, -321,-322, -341, -342 53-3093 1 or higher Prior to 7320 total flight cycles or 26130 total flight Hours; whichever occurs first 13 1999-508- 106(B) 41652, OR 43904 MODIFY LOWER SECTIONS OF FRAME 48 TO 53.2 ALL Model A330 Airplanes 53-3062 0 or higher Prior to 2300 Total flight cycles or C of A Issuance; whichever occurs later 14 95-053- 009(B)R3 44049 REPLACE HYDRAULIC SENSE LINES Airplanes equipped with PW model 4164 or 4168 engines 29-3019 1 or higher Prior to 10/31/97 or C of A Issuance; whichever occurs later 15 95-248-022(B) 42607 MOD - FUSELAGE STRINGER 39 ALL Model A330 Airplanes 53-3021 0 or higher Prior to 3800 total flight cycles 16 96-106-030(B) 41849 OR 43364 AFT CARGO COMPARTMENT DOOR ALL Model A330 Airplanes 52-3023 0 or higher Prior to 6000 total flight cycles 17 96-134- 031(B)R2 AND 97-266-057(B) ; OR LANDING GEAR FREE FALL EXTENSION ELECTRIC CIRCUIT ALL Model A330 Airplanes OR ; OR 41848 REINFORCE DOORFRAMES/ EMERGENCY EXITS Airplanes with Mod. 40161 53-3023 0 or higher Prior to 10000 total flight cycles A46NM Revision 4 18 March 21, 2000 A330 Required Modification List (RML) RML # DGAC CN # Mod # Mandatory Action Applicable To: S/B # S/B REV(s) Compliance Time 32 98-099-066(B) 42969 AND 45580 FUEL DENSITOMETERS - ATA 28 ALL Model A330 Airplanes 28-3044R1 OR 28-3053 and 28-3044R0 3044:1 or higher 3053: 0 or higher Prior to 6 Years since new 33 98-101-068(B) 43306 MODIFY DOOR STOP FITTING ON PASS DOORS ALL Model A330 Airplanes 53-3044 1 or higher Prior to 10000 total flight cycles 34 98-268- 073(B)R1 45534 REPLACE MLG DOOR All Airplanes with MLG door S/N AA1001 to AA1196; or SPAA001 to SPAA015 52-3049 0 or higher Prior to 2/18/00 or C of A Issuance; whichever occurs later 35 98-291-074(B) 44030, OR 43761 REINFORCE FRAME 65 REAR FUSELAGE ALL Model A330-300 Airplanes 53-3058 2 or higher Prior to 10000 total flight cycles 36 98-352-076(B) 46416 MOD MLG O/B PIN / BRAKE ROD TO MAIN STRUT ALL Model A330 Airplanes 32-3084 2 or higher Prior to 1/19/99 or C of A Issuance; whichever occurs later 37 98-454-082(B) ; OR ; OR LOWER KEELBEAM FITTING/FWD LOWER SHELL ALL Model A330 Airplanes 57-3032 3 or higher Prior to 6600 Total flight cycles or 21800 Total Flight Hrs, whichever occurs first 38A 98-484- 081(B)R1 46472 REPLACE PIVOT PINS OF SLIDE LOCKING MECHANISM All Airplanes with 44860 (Type 1 Emerg Exits) 52-3050 1 or higher Prior to 3/12/00 or C of A Issuance; whichever occurs later 38B 98-484- 081(B)R1 46471 REPLACE PIVOT PINS OF SLIDE LOCKING MECHANISM All Airplanes with 44330 (Mid & Aft Pax Doors) 52-3050 1 or higher Prior to 3/12/00 or C of A Issuance; whichever occurs later 38C 98-484- 081(B)R1 46473 REPLACE PIVOT PINS OF SLIDE LOCKING MECHANISM All Airplanes with 44332 (Type A Emerg Exits) 52-3050 1 or higher Prior to 3/12/00 or C of A Issuance; whichever occurs later 39 98-507-085(B) , OR , OR , OR , OR REPLACEDIAPHRAGM FOR EMERGENCY ACTUATOR ALL Model A330 Airplanes 52-3048 1 or higher Prior to 12/16/01 or C of A Issuance; whichever occurs later 40A 98-538- 087(B)R1 46353 MODIFY DOOR STAY MECHANISM EMERG EXITS All Airplanes with 44332 (Type A Emerg Exits) 52-3051 1 or higher Prior to 3/31/00 or C of A Issuance; whichever occurs later 40B 98-538- 087(B)R1 46352 MODIFY DOOR STAY MECHANISM MID/AFT EXITS All Airplanes with 44330 (Mid & Aft Pax Doors) 52-3051 1 or higher Prior to 3/31/00 or C of A Issuance; whichever occurs later A46NM Revision 10 19 March 19, 2007 Hydraulic Fluids: Type IV - Specification NSA 30.7110 Auxiliary Power Unit (APU): Garrett Airesearch GTCP 331-350C (Specification 31-7677A) Maximum Allowable Speed (107%) 41,730 RPM Maximum Gas Temperature: Turbine Outlet Temperature Starting 650 °C 1250 °C Approved oils: See Garrett report GT-7800 or Garrett Maintenance Manual. Tires: Refer to Airbus Service Bulletin (SB) A330-32-3004. SERVICE INFORMATION: Each of the documents listed below that contain a statement that it is approved by the European Aviation Safety Agency (EASA) - or for approvals made before September 28, 2003 - by the DGAC France, are accepted by the FAA and are considered FAA approved. Additionally, approvals issued by Airbus under the authority of EASA approved Design Organization EASA.21J.031 - or for approvals made before September 28, 2003 - under the authority of by DGAC Design Organization Approval No. C01 or JAA Design Organization Approval No. F.JA.02 are considered FAA approved. These approvals pertain to the type design only. • Airbus Service Bulletins, except as noted below, • Structural repair manuals, • Vendor manuals referenced in Airbus service bulletins • US version of Aircraft flight manuals, • Repair Instructions. Note: Design changes that are contained in Airbus Service Bulletins and that are classified as Level 1 Major in accordance with the US/France Bilateral Aviation Safety Agreement Implementation Procedures for Airworthiness must be approved by the FAA. GENERAL NOTES: (All Models of A330 Series Airplanes) Note 1: A current Weight and Balance report including list of the equipment included in the certificated empty weight, and loading instructions, when necessary, must be provided for each aircraft at the time of original airworthiness certification and at all times thereafter. Refer to Airbus Documents 00G080A0006/C2S for A330-200 series aircraft and 00G080A0006/C3S for A330-300 series aircraft. Note 2: Instructions For Continued Airworthiness required under § 21.50 for service life limits on components, required inspections and inspection intervals, and certification maintenance requirements: 􀂃 A330 Maintenance Review Board Report 00G050A0002/C01 approved by the FAA; • Safe Life Airworthiness Limitation Items are provided in the A330 Airworthiness Limitation Section (ALS) sub-parts 1-2 and 1-3 and approved by EASA (Ref. Document 00G050AM091/C01); • Certification Maintenance Requirements (CMR’s) are provided in the A330 Airworthiness Limitations Section (ALS) Part 3 approved by EASA (Document 00G050A0003/C01); • Damage Tolerant Airworthiness Limitation Items are provided in the A330 Airworthiness Limitations Section (ALS) Part 2 approved by EASA (Document 00G050A3301/C01) • Fuel Airworthiness Limitations are provided in the A330 Airworthiness Limitations Section (ALS) Part 5 approved by EASA (Document 95A.1932/05) Note 3: Compliance with the FAA Required Modification List for Airbus Model A330 Aircraft as included under the Import Requirements section of TCDS Revision 4, dated March 21, 2000 or later TCDS revision, is necessary for an A330 aircraft to be found in a condition for safe operation. The FAA has accepted: 􀂃 Model A330-323 aircraft in the Airbus as-delivered configuration for msn 524 and on as compliant with the applicable modifications of the A330 RML. 􀂃 Model A330-223 aircraft in the Airbus as-delivered configuration for msn 609 and on as compliant with the applicable modifications of the A330 RML. Note 4: A330-301: If modification 42792, “Autoflight-FMGEC-Introduce L5 Standard on A330 Aircraft,” is embodied the aircraft is qualified for CAT III precision approach and autoland. This does not constitute operational approval. A46NM Revision 10 20 March 19, 2007 Note 5: A330-321 and A330-322: If modification 43397, “Autoflight-FMGEC-Certify CAT III Autoland for A330 with P&W engines,” is embodied, the aircraft is qualified for CAT III precision approach and autoland. This does not constitute an operational approval. Note 6: A330-201, A330-202, A330-203,-223, -243, -323, -341, -342 and -343: The aircraft Type Design is qualified for CAT III precision approach and autoland. This does not constitute an operational approval. Note 7: ETOPS: The Type Design reliability and performance of the airframe-engine combinations listed below have been evaluated in accordance with AC 120-42A and found suitable for (180 minute maximum diversion time) extended range operations when configured, maintained and operated in accordance with the approved airplane configuration CMP document. This finding does not constitute an FAA approval to conduct extended range operations. Operational approval must be obtained from the FAA by the operator. • Model A330-323. The approved CMP is Airbus document AI/EA 5001, Revision 1, dated October 21, 1999. • Model A330-223. The approved CMP is Airbus document AI/EA 5001, Revision 2, dated July 12, 2004. Note 7: “Enhanced” refers to those model A330 aircraft identified by Weight Variant (WV) 050 or WV 052. Aircraft with either of these WV’s have the modifications defined by Level 1 major change project: “Fly By Wire (FBW) and Structural Enhanced Changes installed in production. ...END...

dexmonk 发表于 2012-4-20 00:19:28

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FAA TYPE CERTIFICATE DATA SHEET NO. A46NM