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V. Type A340-500 Series Transport Category Airplanes:
Airbus Model A340-541 - approved January 27, 2003
Model: Definition of Reference Airplane by Airbus Documents:
A340-541 FAA A340-541 Type Design, ref. EAL 415.1445/02 Issue 01, dated November 28, 2002, for type
definition.
The A340-500 series is shorther than the A340-600 by 14 frames. It is intended for long range operations having
additional fuel capacity over that of the –600 with the installation of a rear center tank (RCT).
The following table provides a list of required design improvement modifications for the 5-frame RCT (defined by Airbus
modification no. 47020) on Model A340-500 series aircraft. The modifications extend the Kevlar liner in the RCT and
improve the RCT fuel jettison rate. Airbus modifications 51344 and 51452 are required as a condition for type
certification and must be installed prior to issuance of a standard U.S airworthiness certificate.
.
Airbus Modification No. Airbus Modification Title
51344 Install Liners between RCT Forward and Rear Pressure
Bulkheads (5 inter-frames)
51452 Relocate RCT Transfer/Refuel Restrictors to increase Jettison
rate
Engines
Airplane Model Engine Model: Engine Type Certificate:
A340-541 Four Rolls-Royce– Trent 553-61 turbojet engines FAA-Type Certificate
E00066NE
Maximum Weight:
Variant 000
(Mod 51000)
kg / lb
001
(Mod 51080)
kg / lb
Maximum Ramp Weight 369,200 / 814,086 373,200 / 822,906
Maximum Take-off Weight, MTOW 368,000 / 811,440 372,000 / 820,260
Maximum Landing Weight, MLW 240,000 / 529,200 243,000 / 535,815
Maximum Zero Fuel Weight, MZFW 225,000 / 496,125 230,000 / 507,150
Number of Seats:
The maximum number of passengers approved for emergency evacuation is 375 passengers with a 3 pair of Type A and 1
pair of Type I exits configuration.
Maximum Baggage:
Cargo Compartment Maximum Load
(kg / lb)
Forward 24,494 / 54,009
Aft 16,330 / 36,008
Rear 3,458 / 7,625
For the positions and the loading conditions authorized in each position (references of containers, pallets and associated
weight) see weight and Balance Manual:
A43NM, Revision 4 Page 11 of 18 March 19, 2007
Ref. Airbus Document 00F080A0501/C5S for A340-541
Fuel Capacity:
Tank Capacity
Usable Fuel Unusable Fuel
Tank liters
(kg)
gallons
(lb)
Liters
(kg)
gallons
(lb)
Tank 1 / 4 49,002
(39,202)
12,945
(86,421)
68
(54)
18
(120)
Tank 2 / 3 69,514
(55,611)
18,364
(122,598)
230
(184)
61
(406)
Outer 12,290
(9,832)
3,247
(21,677)
34
(27)
9
(60)
Wing
Total 130,806
(104,645)
34,556
(230,696)
332
(265)
88
(586)
Center
(with jet pumps : modification 50812)
55,133
(44,106)
14,566
(97,254)
240
(192)
63
(423)
Rear Center 5 frame
(with liner: modification 51344)
19,741
(15,793)
5,216
(34,824)
100
(80)
26
(176)
Trim Tank 7,886
(6,309)
2,083
(13,911)
25
(20)
7
(44)
Total 213,566
(170,853)
56,421
(376,685)
697
(557)
184
(1,229)
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 A340 Aircraft Airbus Document Refr. Revision No. Date
-541 STL 34000 1 January 16, 2003
For information on Fuel, Engine Limits, Airspeed Limits, Center of Gravity Limits, Datum, Leveling Means,
Minimum Crew, 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 VI, Data Pertinent to All Model A340-500 and A340-600 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.
A43NM, Revision 4 Page 12 of 18 March 19, 2007
VI. Data Pertinent to All Model A340-500 and A340-600 Series Airplanes:
Fuel:
Specification
Nomenclature United Sates France United Kingdom
Kerosene ASTM D 1655
　
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