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(JET A) (JET A1)
AIR 3405C DERD
2494/2453
Wide Cut
ASTM D 1655
(JET B)
91056
(72845)
DERD
2454/2486
MIL-T-5624 (JP 4)
MIL-T-83133 (JP 8)
AIR 3407B DERD
2454/2486
Additives: According to RR "Specific Operating Instructions", OI-Trent-A340. The above-mentioned fuels are also
suitable for the APU.
Engine Limits:
Rolls-Royce
RB 211 Trent 556-61
Rolls-Royce
RB 211 Trent 553-61
Engine Limitations
See FAA Data Sheet E00066NE See FAA Data Sheet E00066NE
Static Thrust at Sea Level
• Take-off (5 mn)1 (flat rated 30º
C)
• maximum continuous
(flat rated 25º C)
58,462 lbs (26,004 daN)
44,359 lbs (19,731 daN)
55,780 lbs (24,811 daN)
44,359 lbs (19,731 daN)
Maximum Engine Speed
• N1 rpm (%)
• N2 rpm (%)
3,900 (100%)
9,100 (100%)
3,900 (100%)
9,100 (100%)
Maximum Gas Temperature
• Take-off (10mn)1
• Maximum Continuous
• Starting
- Ground
- Inflight
900º C
850º C
700º C
850° C
900º C
850º C
700º C
850° C
Maximum Oil Temperature
(Combined scavenge temperature)
ºC
Minimum Pressure
196º C
25 psi (172 kPa)
196° C
25 psi (172 kPa)
Approved oils - Aeroshell Turbine Oil (Royco
Turbine Oil) 555
- Mobil Jet Oil II, 254, 291
- Aeroshell Turbine Oil (Royco
Turbine Oil) 555
- Mobil Jet Oil II, 254, 291
Table references:
(1) 10 minutes at take-off thrust allowed only in case of engine failure (at take-off or during go-around).
Airspeed Limits (Indicated Airspeed, IAS, unless otherwise stated):
• Maximum Operating Limit Speed/Mach, VMO/MMO 330 KIAS / .86 M
A43NM, Revision 4 Page 13 of 18 March 19, 2007
• Design Diving Speed, VD 365 KIAS/ .93 M
• Design Maneuvering Speed, VA Refer to AFM performance Section
• Maximum Flaps/Slats Extended Speed or Operating Speed, VFE
Configuration Slats/Flaps º VFE (kt)
1 20/0
20/17
280
233
Intermediate Approach
Take-off
2 23/22 216 Take-off and Approach
3 23/29 206 Take-off and Approach
FULL 23/34 200 Landing
• Minimum Control Speed, VMC Refer to AFM performance Section
(Performance Engineering Program/OCTOPUS)
Landing Gear Speeds:
• Maximum Speed with Landing Gear 250 KIAS/.55 M
Operating (Extension and Retraction), VL0
• Maximum Speed with Landing Gear 250 KIAS/.55 M
Locked Down, VLE
Tire Limit Speed (Ground Speed) 204 KIAS
Center of Gravity Limits:
Refer to EASA-Approved AFM, US Version, Limitations Section for center of gravity envelope.
Note: For A340-600, the 0% MAC is located 1,617 inch (41.034 m) from the datum line.
For A340-500, the 0% MAC is located 1,408 inch (35.734 m) from the datum line.
Datum:
The aircraft reference zero datum point is located 251.37 inch (6.38 m) forward of the fuselage nose, 275.8 inch (7 m)
under the fuselage centerline (datum line).
Leveling Means:
Inclinometer on cabin seat track rails (refer to AMM chapter 08.20.00).
Minimum Crew:
2 – Pilot and copilot
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
Inner Aileron +20°/-30°
Outer Aileron +25°/-25°
Ailerons Maneuver Load Alleviation 11°
#1 Spoiler Speed Brake 25°
Lift Dumper 35°
#2,3 Spoilers Roll 35°
Speed Brake 35°
Lift Dumper 50°
#4,5,6 Spoilers Roll 40°
Speed Brake 40°
Lift Dumper 50°
A43NM, Revision 4 Page 14 of 18 March 19, 2007
Manoeuvre Load Alleviation 9°
Aileron Droop 10°
Flaps 33.7°
Slats 1 21°
Slats 2 to 7 24°
Stabilizers +2°/-14°
Elevator +17°/-30°
Rudder +35°/-35°
Certification Basis (A340-600 and A340-500)
The reference date for the determination of the certification basis was December 31, 1997.
a. 14 CFR Part 25, dated February 1, 1965 as amended by Amendments 25-1 through Amendment 25-95 inclusive plus
Amendments 25-97, 25-98 and 25-104 with the following exceptions:
Excepted FAR Allowed Amendment Level Comments
　
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