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AN2

From SKYbrary Wiki
Aircraft
Name An-2
Manufacturer PZL-MIELEC
Body Narrow
Wing Fixed Wing
Position Biplane
Tail Regular tail, high set
WTC Light
Type code L1P
Engine Piston
Engine count Single
Position Nose mounted
Landing gear Tailwheel fixed
Mass group 2


Manufacturered as:

AICSA An-2
ANTONOV An-2
NANCHANG Y-5
PZL-MIELEC An-2 Antek
PZL-MIELEC Antek
SHIJIAZHUANG Y-5


PZL-MIELEC An-2

PZL-MIELEC An-2 PZL-MIELEC An-2 3D

Description

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 18.2 m59.711 ft
Length 12.7 m41.667 ft
Height 4 m13.123 ft
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

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS 180 kts IAS 180 kts IAS kts MACH TAS 120 kts MACH IAS 180 kts IAS 180 kts Vapp (IAS) kts
Distance 300 m ROC 1000 ft/min ROC 700 ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD 1000 ft/min MCS kts Distance 320 m
MTOW 55005,500 kg
5.5 tonnes
kg
Ceiling FL120 ROD 1000 ft/min APC
WTC L Range 480480 nm
888,960 m
888.96 km
2,916,535.435 ft
NM

Accidents & Serious Incidents involving AN2

None on SKYbrary