*****AIRCRAFT “Antonov
- 38”*****
REFERENCE
INFORMATION (by Aircraft performance database)
*****Aircraft Features*****
Wing
position: High wing (wing struts)
Engine
position: (Front) Wing leading mounted
Tail
configuration: Double fin, mid set
Landing gear:
Tricycle fixed
Wing
Span:
Length:
Height:
Power
plant: 2 x 1.118 KW AlliendSignal
TPE331-14GR-801E turboprops
with 5 blade propellers.
Accommodation:
Flightcrew of two and up to 27 passengers.
Notes: Commuter airliner
and utility transport. In limited service since 1997 in Russia (mainly
Siberia). A Russian stretched developement of the
AN-28.
Alternative names:
ANTONOV An-38.
*****Total Flight Simulator aircraft weight
with full fuel*****
VMO -
Maximum Operating Speed 360 KIAS
MMO -
Maximum Operating Speed Mach 0.55 Mach
Turbulent
Air Penetration Speed 000 KIAS/.00 Mach
VLO -
Maximum Gear Operating Speed 000 KIAS
VLE -
Maximum Landing Gear Extension Speed
000 KIAS/.00 Mach
*****Maximum Flap Placard Speeds*****
Flaps
degrees KIAS
1 000
2 000
5 000
10 000
15 000
25 000
30 000
40 000
*****Take-off*****
WTC: M
Distance: 500 mt
V2
(IAS): 100 kts
*****Climbing*****
-(to
IAS: 130 kt
ROC: 1000 ft/min
-(to
FL150)
IAS: 160 kt
ROC: 1000 ft/min
-(to
FL240)
IAS: na kt
ROC: na ft/min
-(mach)
mach: na
ROC: na ft/min
*****Cruise*****
TAS: n200 kt
MACh: nd
Ceiling: FL140
Range: 800 NM
*****Descent *****
- (to
FL240)
mach: na
ROD: na ft/min
- (to
FL100)
IAS: 290 kt
ROD: 800 ft/min
*****Approach*****
IAS: 200 kt
MCS: nd kt
ROD: 800 ft/min
*****Landing*****
Vht
(IAS): 120 kt
APC: B
Distance: 900 mt