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Fuel Capacity:
3 Tank Airplane
Usable Fuel Unusable Fuel
Tank liters
(kg)
gallons
(lb)
liters
(kg)
gallons
(lb)
Wing 91,056
(72,845)
24,054
(164,052)
245
(196)
70
(41)
Center 41,468
(33,174)
10,955
(74,173)
83
(66)
22
(150)
Trim Tank 6,114
(4,891)
1,615
(11,014)
6
(5)
1.6
(11)
Total 138,638
(110,910)
36,627
(249,796)
334
(267)
88
(600)
Maximum Operating Altitude:
• Basic: 41,100 feet (12,527m) slats and flaps retracted (clean)
• Option: 41,450 feet (12,634m) slats and flaps retracted (clean) with modification 52536
• 20,000 feet (6,096 m) slats or slats/flaps extended
Control Surface Movements (Total one-way travel in each direction of each movable control surface on the aircraft.)
Control Surface Maximum Travel
Aileron +25°/-25°
#1 Spoiler Speed Brake 25°
Lift Dumper 35°
#2,3 Spoilers Roll 35°
Speed Brake 30°
Lift Dumper 50°
#4,5 Spoilers Roll 35°
Speed Brake 30°
Lift Dumper 50°
Aileron Droop 10°
Flaps 32°
Slats 1 21°
Slats 2 to 7 24°
Stabilizers +2°/-14°
Elevator +15°/-30°
Rudder +31.6°/-31.6°
Certification Basis (A340-200 and A340-300):
a. Part 25 of the FAR effective February 1, 1965, including amendments 25-1 through 25-63 and amendments 25-
65, 25-66 and 25-77.
b. Part 25 of the FAR amendment 25-64 with the following exceptions:
• Cockpit seats will not meet FAR 25.562 amendment 25-64 but will meet FAR 25.561
• Compliance with 25.785(a), (b), and (d) at amendment 25-64 for front row seats in front of a bulkhead will be
based on ensuring a 35 inch free head strike envelope.
c. Special Federal Aviation regulation FAR Part 34 as amended by Amendments 27-1, through 27-7.
d. Part 36 of the FAR as amended by amendments 36-1 through 36-20.
A43NM, Revision 4 Page 7 of 18 March 19, 2007
e. FAA Special conditions issued for the A340 in accordance with Section 21.16 of the FAR and published in the
Federal Register April 15, 1993, (Docket No. NM-75, Special Conditions No. 25-ANM-69), as follows:
(1) Electronic Flight Control System (EFCS) failures and Mode Annunciation
(2) Command Signal Integrity
(3) Protection From Lightning and Unwanted Effects of High Intensity Radiated Fields (HIRF)
(4) Interaction of Systems and Structures
(5) Design Dive Speed
(6) Design Maneuver Requirements
(7) Limit Pilot Forces
(8) Tail plane Tank Emergency Landing Loads
(9) Limit Engine Torque
(10) Ground Load Conditions for Center Landing Gear
(11) Flight Characteristics
(12) Flight Envelope Protection
(13) Side Stick Controllers
(14) Computerized Airplane Flight Manual (AFM) Performance Information
f. For precision approach and landing, the applicable technical requirements are complemented by
AC 120-29 and AC 120-28C.
g. For the automatic flight control system, the applicable technical requirements are complemented by
AC 20-57A for automatic landing and by AC 25.1329-1A for cruise.
h. Equivalent safety findings have been made in accordance with FAR 21.21(b)(1) for the following paragraphs of
the FAR:
(1) 25.335(d) for design airspeeds
(2) 25.345 for high lift devices
(3) 25.349 for control surface loads
(4) 25.351(b) for unsymmetrical loads
(5) 25.371 for gyroscopic loads
(6) 25.373 for speed control devices
(7) 25.101(I); 25.105(c)(1); 25.109(a)(b)(c)(d)(e)(f); 25.113(a)(b)(c); 25.115(a); 25.735(f)(g)(h)(b) for
rejected takeoff and landing performance
i. Optional requirements elected:
• 25.801 for ditching.
• 25.1419 for icing.
The Direction Generale de 'Aviation Civile (DGAC) of France originally type certificated the Airbus Model A340-200
and A340-300 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.
• Equipment approved for installation is listed in the Type Certification Standard Equipment Lists; 00F000A0101/C0S for
　
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