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
Manufacturered 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: 
45.10 m
Length: 
42.40 m
Height: 
14.70 m
Powerplant: 

4 × Europrop TP400-D6 turboprop (8,250 kW).

Engine Model: 
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

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