*****AIRCRAFT “Antonov
- 2T”*****
REFERENCE
INFORMATION (by Aircraft performance database)
*****Aircraft Features*****
Wing
position: Biplane
Engine
position: Nose mounted
Tail
configuration: Regular tail, high set
Landing
gear: Tailwheel fixed
Wing Span:
Length:
Height:
Power
plant: An-2: 1 x 1.000 HP PZL Kalisz Asz-61R 9 cylinder radial
engine
with 4 blade propeller.
Accommodation:
One or two pilots and
12 passengers.
Notes: Biplane utility transport aircraft.
In service since 1948. Production was transferred to Polands
PZL Mielec in the 1960s (first flight 23. Oct. 1960).
More than 15.000 aircraft have been built in Russia, Poland and China (Y-5).
Alternative names:
An-2, Antek, ANTONOV An-2, NANCHANG Y-5,
PZL-MIELEC An-2 Antek
SHIJIAZHUANG Y-5, Y-5.
*****Total
Flight Simulator aircraft weight with full fuel*****
VMO -
Maximum Operating Speed 100 KIAS
MMO -
Maximum Operating Speed Mach nd 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: L
Distance: 150 mt
V2
(IAS): 45 kts
*****Climbing*****
-(to
IAS: 75 kt
ROC: 650 ft/min
-(to
FL150)
IAS: 75 kt
ROC: 550 ft/min
-(to
FL240)
IAS: na kt
ROC: na ft/min
-(mach)
mach: na
ROC: na ft/min
*****Cruise*****
TAS: 100 kt
MACh: nd
Ceiling: FL150
Range: 500 NM
*****Descent *****
- (to
FL240)
mach: nd
ROD: nd ft/min
- (to
FL100)
IAS: 100 kt
ROD: 500 ft/min
*****Approach*****
IAS: 100 kt
MCS: nd kt
ROD: 50 ft/min
*****Landing*****
Vht
(IAS): 55 kt
APC: A
Distance: 170 mt