AN38
ANTONOV An-38
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
Manufactured 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 (metric)
22.10 m
Length (metric)
15.50 m
Height (metric)
4.30 m
Powerplant
2 x 1.118 KW Allied Signal TPE331-14GR-801E turboprops with 5 blade propellers.
Engine Model(s)
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
