PZL-MIELEC An-2

Aircraft
Name: 
An-2
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
Biplane
Tail: 
Regular tail, high set
WTC
L
Type Code: 
L1P
Engine: 
Piston
Engine Count: 
Single
Position: 
Nose mounted
Landing gear: 
Tailwheel fixed
Manufacturered as
ANTONOV An-2
NANCHANG Y-5
PZL-MIELEC An-2 Antek
PZL-MIELEC Antek
AICSA An-2
SHIJIAZHUANG Y-5

AN2

Biplane utility transport aircraft. In service since 1948. Production was transferred to Poland's 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).

Technical Data
Wing span: 
18.20 m
Length: 
12.70 m
Height: 
4.00 m
Powerplant: 

1 x 1.000 HP PZL Kalisz Asz-62IR 9 cylinder radial engine with 4 blade propeller. Y-5: 1 x 1.000 HP PZL Kalisz Asz-62IR-16 or 1 x 986 HP Zhuzhou HS5 9 cylinder radial engine with 4 blade propeller.

Engine Model: 
Shvetsov ASh-62
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
300 m
MTOW: 
5500 kg
Initial Climb (to 5000 ft)
IAS: 
180 kts
ROC: 
1000 ft/min
Initial Climb (to FL150)
IAS: 
180 kts
ROC: 
700
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
120 kts
MACH: 
n/a
Ceiling: 
120
Range: 
480 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
180 kts
ROD: 
1000 ft/min
Descent (FL100 & below)
IAS: 
180 kts
MCS: 
n/a
ROD: 
1000 ft/min
Approach
Vapp (IAS): 
n/a
Distance: 
320 m

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