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intermix between 5C3/F and 5C3/G on the same aircraft is allowed.
FAA-Type Certificate E37NE
A340-213 Four CFMI-CFM56-5C4 FAA-Type Certificate E37NE
A43NM, Revision 4 Page 2 of 18 March 19, 2007
Maximum Weight:
Variant 000
(Basic)
kg / lb
001
(MOD 41302)
kg / lb
Maximum Ramp Weight 254,400 / 560,952 257,900 / 568,670
Maximum Take-off Weight, MTOW 253,500 / 558,968 257,000 / 566,685
Maximum Landing Weight, MLW 181,000 / 399,105 181,000 / 399,105
Maximum Zero Fuel Weight, MZFW 169,000 / 372,645 169,000 / 372,645
Maximum Baggage:
Cargo Compartment Maximum Load
(kg / lb)
Forward 18,507 / 40,809
Aft 15,241 / 33,606
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: Airbus Document 00F080A0002/C2S for A340-211 and A340-212 and
00F080A0004/C0S for A340-213.
Aircraft 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 A340 Aircraft Airbus Document Refr. Revision No. Date
-211 AI/EV-O 34000 1 May 27, 1993
-212 AI/EV-O 34000 1 February 3, 1997
-213 AI/EV-O 34000 1 February 3, 1997
For information on Fuel, Engine Limits, Airspeed Limits, Center of Gravity Limits, Datum, Leveling Means,
Minimum Crew, Number Seats, Fuel Capacity, Maximum Operating Altitude, Control Surface Movements,
Certification Basis, Production Basis, Equipment, Hydraulic Fluids, Auxiliary Power Unit (APU), Tires and
Environmental requirements for noise :
See Section III, Data Pertinent to All Model A340-200 and A340-300 Series Airplanes.
For information on Import Requirements, Service Information and General Notes: See section VII, Data Pertinent to
All Model A340-200, A340-300, A340-500 and A340-600 Series Airplanes.
II. Type A340-300 Series Transport Category Airplanes:
Airbus A340-311 - approved May 27, 1993:
Airbus A340-312 - approved July 7, 1994:
Airbus A340-313 - approved October 2, 1997:
The A340-300 series differs from the A340-200 series aircraft by the addition of 8 fuselage frames.
Model: Definition of Reference Airplane by Airbus Documents:
A43NM, Revision 4 Page 3 of 18 March 19, 2007
A340-311 FAA A340-311 Type Design, ref. AI/EA-N 415.02695/96 Issue 4, dated June 11, 1997, for type
definition and Type Certification Standard Equipment List, ref. 00F000A0101/C0S.
A340-312 FAA A340-312 Type Design, ref. AI/EA-N 415.0270/96 Issue 4, dated June 11, 1997, for type
definition and Type Certification Standard Equipment List, ref. 00F000A0102/C0S.
A340-313 FAA A340-313 Type Design, ref. AI/EA-N 415.0272/96 Issue 4, dated June 11, 1997, for type
definition and Type Certification Standard Equipment List, ref. 00F000A0103/C0S.
Engines
Airplane Model Engine Model: Engine Type Certificate:
A340-311 Four CFMI-CFM 56-5C2 or four CFM 56-5C2/F or four CFM 56-
5C2/G. Engine intermix between 5C2 and 5C2/F and 5C2/G on
the same aircraft is allowed.
FAA-Type Certificate E37NE
A340-312 Four CFMI-CFM 56-5C3/F or four CFM 56-5C3/G. Engine
intermix between 5C3/F and 5C3/G on the same aircraft is allowed.
FAA-Type Certificate E37NE
A340-313 Four CFMI-CFM56-5C4 FAA-Type Certificate E37NE
Maximum Weight:
Variant 000
(Basic)
kg / lb
001
(MOD 41302)
kg / lb
Maximum Ramp Weight 254,400 / 560,952 257,900 / 568,670
Maximum Take-off Weight, MTOW 253,500 / 558,968 257,000 / 566,685
Maximum Landing Weight, MLW 186,000 / 410,130 186,000 / 410,130
Maximum Zero Fuel Weight, MZFW 174,000 / 383,670 174,000 / 383,670
Maximum Baggage:
Cargo Compartment Maximum Load
(kg / lb)
Forward 22,861 / 50,409
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. Airbus Document 00F080A0002/C3S for A340-311 and A340-312
Ref. Airbus Document 00F080A0004/C0S for A340-313
Aircraft 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
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