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Model A340 Aircraft Airbus Document Refr. Revision No. Date
-311 AI/EV-O 34000 1 May 27, 1993
-312 AI/EV-O 34000 1 February 3, 1997
-313 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 :
A43NM, Revision 4 Page 4 of 18 March 19, 2007
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.
III. Data Pertinent to All Model A340-200 and A340-300 Series Airplanes:
Fuel:
Specification
Nomenclature United Sates France United Kingdom
Kerosene ASTM D 1655
(JET A) (JET A1)
AIR 3405C DERD
2494/2453
Wide Cut
ASTM D 1655
(JET B)
AIR 3407B DERD
2454/2486
MIL-T 5624 (JP4)
MIL-T 83133 (JP8)
AIR 3407B DERD
2454/2486
Additives: According to CFMI "Specific Operating Instructions", installation manual. The above-mentioned fuels are also
suitable for the APU.
Engine Limits:
Engine Limitations
CFMI CFM 56
-5C2 -5C2/4
-5C2/F -5C2/F4
-5C2/G -5C2/G4
CFMI CFM 56
-5C3/F -5C3/F4
-5C3/G -5C3/G4
CFMI CFM 56
-5C4
See FAA Data Sheet E37NE
Static Thrust at Sea Level
• Take-off (5 mn)1 (flat rated
30º C)
• Maximum continuous
(flat rated 25º C)
13878 daN (31,200 lbs)
12588 daN (28,300lbs)
14456 daN (32,500 lbs)
13077 daN (29,400 lbs)
15123 daN (34,000 lbs)
13371 daN (30,060 lbs)
Maximum Engine Speed
• N1 rpm (%)
• N2 rpm (%)
4800 (100.3%)
15,183 (105%)
4800 (100.3%)
15,183 (105%)
4985 (104.2%)
15,183 (105%)
Maximum Gas Temperature
• Take-off (5mn)1
• Maximum Continuous
• Starting2
950º C
915º C
725º C
965º C
930º C
725º C
975º C
940º C
725º C
Maximum Oil Temperature
(Supply Pump Outlet) ºC
• Take-off, Stabilized
• Transient (15 mn max.)
Minimum Pressure
140º C
155º C
89.6 KPa differential
140º C
155º C
89.6 KPa differential
140º C
155º C
89.6 KPa differential
Approved oils See CFMI Service Bulletin CFMI 79-001 or GE specification D50TF1, Type I and II
Table references:
(1) 10 minutes at take-off thrust allowed only in case of engine failure (at take-off or during go-around).
A43NM, Revision 4 Page 5 of 18 March 19, 2007
(2) 4 consecutive cycles of 2 minutes each
Airspeed Limits (Indicated Airspeed, IAS, unless otherwise stated):
• Maximum Operating Limit Speed/Mach, VMO/MMO 330 KIAS / .86 M
• 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
240
215
Intermediate Approach
Take-off
2 24/22 196 Take-off and Approach
3 24/26 186 Take-off, Approach, and Landing
FULL 24/32 180 Landing
• Minimum Control Speed, VMC Refer to AFM performance Section
(Performance Engineering Program/OCTOPUS)
Landing Gear Speeds:
• Maximum Speed with Landing Gear Operating (Extension and Retraction), VL0 250 KIAS/.55 M
• Maximum Speed with Landing Gear Locked Down, VLE 250 KIAS/.55M
•Tire Limit Speed (Ground Speed) 204 KTS
Center of Gravity Limits:
Refer to EASA-Approved AFM, US Version, Limitations Section for center of gravity envelope.
Note: 0% MAC is located 1275.51 in from the datum line.
Datum:
The aircraft reference zero datum point is located 251.37 in. forward of the fuselage nose, 275.8 in. 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
Number of Seats:
The maximum number of passengers approved for emergency evacuation is:
375 passengers with a 3 pair Type A and 1 pair Type 1 exits configuration, and
379 passengers with 4 pair Type A exits configuration.
A43NM, Revision 4 Page 6 of 18 March 19, 2007
　
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