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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
　
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