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(b) §25.1411(d),(e),(f),(g): General Safety Equipment
(c) §25.1415: Ditching Equipment
(d) §25.1419: Ice Protection
g. Exemptions: Exemptions from the applicable regulations has been processed in accordance with the provisions of 14
CFR 11.25.
A43NM, Revision 4 Page 16 of 18 March 19, 2007
• Airbus petitioned for an exemption to §25.807(f)(4) with letter dated May 9, 2000 (the “60 foot rule” was
relocated to this section as of amdt 25-94). In reply issued on December 11, 2000, the FAA denied the petition
for exemption (ref. Exemption No. 7404).
• Exemption 7840, dated July 19, 2002, was issued to Airbus for non-compliance to §25.901(c) as it relates to
uncontrollable high thrust failure conditions.
The Direction Generale de 'Aviation Civile (DGAC) of France originally type certificated the Airbus Model A340-500 and A340-600
series airplanes under its type certificate number DGAC-F TC 183. The FAA validated this product under U.S. Type Certificate
Number A43NM. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of this product on
behalf of DGAC.
Production Basis:
A340 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.
Equipment:
• The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be
installed in the aircraft for certification.
• Cabin furnishings, equipment and arrangement shall conform to the following specification:
• 00F252K0010/C01for cabin seats.
• 00F252K0006/C01for galley.
• 00F252K0020/C01for cabin attendant seats
Hydraulic Fluids:
Type IV - Specification NSA 307110
Auxiliary Power Unit (APU)
Honeywell E. & S. 331-600[A] (Model Specification 31-15857-01A)
Maximum Allowable Speed (100%) 39,044 rpm
Maximum Gas Temperature:
Turbine Outlet Temperature
Starting
650 °C
1250 °C
Approved oils: See also Model Specification 31-15857-01A for approved oils.
Tires:
Refer to Airbus Service Bulletin
Environmental requirements for noise:
ICAO Annex 16 Volume 1 – Chapter 3, or Chapter 4 with Modification 55005.
VII. Data Pertinent to All Model A340-200, A340-300, A340-500 and A340-600 Series Airplanes:
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. A43NM as defined in TCDS A43NM and to be in condition for safe operation."
A43NM, Revision 4 Page 17 of 18 March 19, 2007
The regulatory basis U.S. airworthiness certification basis for aircraft type certificated under FAR Section 21.29 and
exported by the country of manufacture is FAR Sections 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 21.183(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.”
In order for the FAA to make the finding that an A340 aircraft is in a condition for safe operation, the FAA certificating
inspector or other authorized person must contact 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,
prior to issuance of the U.S. airworthiness certificate to obtain the FAA Required Modification List (RML) for the A340.
Prior to issuance of a Standard Airworthiness Certificate on any Airbus A340 model aircraft, all modifications shown in
the Model A340 RML must be accomplished in the interest of safety before the aircraft can be found to be in a condition
for safe operation.
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
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