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CG-4A

cg4a

Description

Indicated stall speed in flight configuration: 65..86 km/h
Dive speed limit: 241 km/h
Maximum load factor: 3.5 G
Stall angle of attack in flight configuration: 16 °

Takeoff speed: 86..113 km/h
Glideslope speed: 98..128 km/h
Landing speed: 81..106 km/h
Landing angle: 8 °

Optimal descent speed on glideslope: 2 m/s

Note 1: the data provided is for international standard atmosphere (ISA).
Note 2: flight performance ranges are given for possible aircraft mass ranges.

Empty weight: 1769 kg
Minimum weight: 2383 kg
Standard weight: 3402 kg
Maximum takeoff weight: 4082 kg
Useful load: 2313 kg

Length: 14.73 m
Wingspan: 25.2 m
Wing surface: 79.25 m²

Combat debut: July 1943

Operation features:

Modifications

Braking Parachute
Installation of braking parachute for reducing the landing run distance
Additional mass: 32 kg
Estimated speed loss: 2 km/h

13 airborne troopers
13 airborne troopers with ammunition
Additional mass: 1415 kg

Willys MB
Willys MB 1⁄4 ton 4x4 utility truck
Additional mass: 1630 kg

Cargo, 1000 kg
1000 kg of military cargo
Additional mass: 1000 kg