AN2
PZL-MIELEC An-2
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
Manufactured as
SHIJIAZHUANG Y-5
PZL-MIELEC An-2 Antek
PZL-MIELEC Antek
NANCHANG Y-5
ANTONOV An-2
AICSA An-2
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 (metric)
18.20 m
Length (metric)
12.70 m
Height (metric)
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(s)
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
