ANTONOV An-70

Aircraft
Name: 
An-70
Manufacturer: 
ANTONOV
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
High wing
Tail: 
Regular tail, low set
WTC: 
M
APC: 
C
Type Code: 
L4T
Engine: 
Turboprop
Engine Count: 
Multi
Position: 
(Front) Wing leading mounted
Landing gear: 
Tricycle retractable
Manufacturered as
ANTONOV An-70

AN70

Heavy freighter. On order for Russian and Ukrainian Air Force. Developed as replacement for AN-12. Short take-off freighter version An-70T. Presently existing as prototype only. Planned in many military and civil versions.

Technical Data
Wing span: 
44.10 m
Length: 
40.70 m
Height: 
16.10 m
Powerplant: 

4 x 13.800 SHP Progress D-27 turbofans with 14 blade propellers.

Engine Model: 
Progress D-27
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
1800 m
MTOW: 
130000 kg
Initial Climb (to 5000 ft)
IAS: 
220 kts
ROC: 
1000 ft/min
Initial Climb (to FL150)
IAS: 
400 kts
ROC: 
1000
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
430 kts
MACH: 
n/a
Ceiling: 
400
Range: 
730 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: 
2200 m

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