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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 Model
A340 RML 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. Additional guidance is contained in FAA advisory Circular 21-23, Airworthiness Certification
of Civil Aircraft, Engines, Propellers, and Related Products Imported into the United States.
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 A340 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:
• 00F080A0002/C2S for A340-211 and -212;
• 00F080A0001/C3S for A340-311 and -312;
A43NM, Revision 4 Page 18 of 18 March 19, 2007
• 00F080A0004/C0S for A340-213 and -313;
• 00F080A0601/C6S for A340-642;
• 00G080A0006/C3S for A340-541.
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:
• Safe Life Airworthiness Limitation Items are provided in the A340 Airworthiness Limitations Section (ALS) sub
parts 1-2 and 1-3 approved by EASA (Document 00F050AM091/C01);
• Damage-Tolerant Airworthiness Limitation Items are provided in the A340 Airworthiness Limitations Section
(ALS) part 2 approved by EASA (Document 00F050A3401/C01);
• Certification Maintenance Requirements (CMR’s) are provided in the A340 Airworthiness Limitations Section
(ALS) Part 3 approved by EASA (Document 00F050A0003/C01);
• A340 Maintenance Review Board Report 00F050A0002/C01 aproved by FAA.
• Fuel Airworthiness Limitations are provided in the A340 Airworthiness Limitations Section (ALS) Part 5
approved by EASA (Document 95A.1933/05)
Note 3: Compliance with the FAA Required Modification List (RML) is necessary for an A340-200, A340-300, A340-
500 or A340-600 aircraft to be found in a condition for safe operation. (See Import Requirements in TCDS
section VII Data Pertinent to All Model A340-200, A340-300, A340-500 and A340-600 Series Airplanes).
Note 4: For Airbus model A340-541: Airbus modifications 51344 and 51452 that extend the Kevlar liner in the RCT and
improve the RCT fuel jettison rate are required as a condition for type certification and must be installed prior to
issuance of a standard U.S airworthiness certificate.
….END….
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
　
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