ANTONOV An-38

Aircraft
Name: 
An-38
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
High wing
Tail: 
Double fin, mid set
WTC
M
APC
B
Engine: 
Turboprop
Engine Count: 
Multi
Position: 
(Front) Wing leading mounted
Landing gear: 
Tailwheel retractable
Manufacturered as
ANTONOV An-38

AN38

Commuter airliner and utility transport. In limited service since 1997 in Russia (mainly Siberia). A Russian stretched development of the AN-28.

Technical Data
Wing span: 
22.10 m
Length: 
15.50 m
Height: 
4.30 m
Powerplant: 

2 x 1.118 KW Allied Signal TPE331-14GR-801E turboprops with 5 blade propellers.

Engine Model: 
AlliedSignal TPE-331
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
800 m
MTOW: 
9900 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: 
180 kts
MACH: 
n/a
Ceiling: 
270
Range: 
430 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: 
500 m

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