A400
AIRBUS A400M Atlas
AIRBUS A400M Atlas
Aircraft
Name
A400M Atlas
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
High swept wing
Tail
T-tail
WTC
H
APC
C
Type Code
L4T
RFF Category
8
Engine
Turboprop
Engine Count
Multi
Position
Underwing mounted
Landing gear
Tricycle retractable
Manufactured as
AIRBUS A-400M
A400
The Airbus A400M Atlas is a multi-national four-engine turboprop military transport aircraft. It was designed by Airbus Military as a tactical airlifter with strategic capabilities. The aircraft's maiden flight took place on 11 December 2009.
Technical Data
Wing span (metric)
45.10 m
Length (metric)
42.40 m
Height (metric)
14.70 m
Powerplant
4 × Europrop TP400-D6 turboprop (8,250 kW).
Engine Model(s)
Europrop International TP400
Indicative Performance Data
Take-Off
V2
n/a
Distance
940 m
MTOW
141000 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
421 kts
MACH
0.72
Ceiling
290
Range
1781 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
625 m
