FAA TYPE CERTIFICATE DATA SHEET NO. A46NM

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FAA TYPE CERTIFICATE DATA SHEET NO. A46NM

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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 [just as for future airworthiness limitations listed in the Airworthiness Limitation Section
(ALS)]. 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)
[45271];
OR [44143
AND SBA330-
32-
3070R0]
LANDING GEAR
FREE FALL
EXTENSION
ELECTRIC CIRCUIT
ALL Model A330
Airplanes
[32-
3048R3]
OR
[32-
3048R0, R1
or R2 AND
32-3070R0)
-3048:3 or
higher, OR
3048:
0,1, or 2
AND 3070:
0 or higher
Prior to 3/23/99 or C of A
Issuance; whichever occurs
later
18 96-136-
032(B)R1
43689 AND
44603
ELECTRICAL
POWER-APU FUEL
PUMPS ELEC
SUPPLY
ALL Model A330
Airplanes
28-3041 3 or higher Prior to 3/1/98 or C of A
Issuance; whichever occurs
later
19 96-159-
033(B)R2
44173,
OR
44237
MLG- SHORTENING
MECHANISM
BELLCRANK
ALL Model A330
Airplanes
without Mod
43029 installed
32-3047 2 or higher Prior to 1/07/99 or C of A
Issuance; whichever occurs
later
A46NM Revision 4 17 March 21, 2000
A330 Required Modification List (RML)
RML
#
DGAC CN # Mod # Mandatory Action Applicable To: S/B # S/B REV(s) Compliance Time
20 96-184-
036(B)R2
46558 ICE PROTECTIONWING
ANTI ICE
VALVES
ALL Model A330
Airplanes
S/B 30-
3020
-3020:
0 or higher
Prior to C of A Issuance
21 97-004-041(B) 43697,
OR
43761
REAR FUSELAGE
CARGO DOOR
FRAME
ALL Model A330
Airplanes
53-3048 0 or higher Prior to 7000 total flight
cycles
22 97-154-
049(B)R1
44457 AND
45022
RADIO ANTENNA
ALTIMETER
"THOMSON"
ALL Model A330
Airplanes fitted
with Radio
Altimeter P/N
9599-607-19501
34-3044
AND
21-3053
AND
92-3017
All S/Bs:
0 or higher
Prior to 10/31/98 or C of A
Issuance; whichever occurs
later
23 97-178-051(B) 44918 A/C RAM AIR
OUTLET DUCT
ALL Model A330
Airplanes
21-3059 0 or higher Prior to 6/30/98 or C of A
Issuance; whichever occurs
later
24 97-179-052(B) 45088, OR
45087
FWD FLAP TRACKS ALL Model A330
Airplanes
57-3048 1 or higher Prior to 3500 total flight
hours
25 97-204-053(B) 41856,
OR
45224
FWD FUSELAGEREINFORCE
DBLR/OUTFLOW
VALVE
ALL Model A330
Airplanes
53-3084 0 or higher Prior to 7500 total flight
cycles
26 97-361-
058(B)R2
44511 AND
41671
MLG-SHORTENING
MECHANISM
BELLCRANK BOLTS
ALL Model A330
Airplanes without
Mod
43029 installed
32-3056 1 or higher Prior to12000 total flight
cycles on the MLG
27 97-386-060(B) 45077
OR
45564
HOT TRANSFORECTIFIERS
OPERATION
ALL Model A330
Airplanes
24-3019 1 or higher Prior to 12/31/98 or C of A
Issuance; whichever occurs
later
28 98-022-
062(B)R1
46115 PNEUMATIC LEAK
DETECTION
SYSTEM WIRING
ALL Model A330
Airplanes
AOT 36-04
OR
SB 36-3012
AOT: 0 or
higher
-3012:
0 or higher
Prior to 12/16/98 or C of A
Issuance; whichever occurs
later
29 98-023-063(B) 43441,
OR
41848
CENTER FUSELAGE
REINFORCE FR
53.3/53.5
ALL Model A330
Airplanes with
Mod. 40161
53-3039 1 or higher Prior to 10000 total flight
cycles
30 98-024-064(B) 44360,
OR
44440
REINFORCE KEEL
ANGLE OF FRONT
SPAR FR40
All Airplanes with
Mod. 41652
57-3046 0 or higher Prior to 4000 total flight
cycles
31 98-098-065(B) [42351AND
42353 AND
43438]; 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) [43577];
OR [41652
AND
44440]; OR
[41652
AND
44360]
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) [45090], OR
[45155], OR
[45197], OR
[45904], OR
[45904 and
45905]
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...

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