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• An-12
• Aircraft description
• Technical characteristics

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• An-12

Technical characteristics

 FLIGHT PERFORMANCE:

 

OVERALL DIMENSIONS:

wing span, m.	38,015
aircraft length, m.	33,109
height, m.	11,44
wing area, m2	121,70
lg base, m.	7,85
cargo cabin:
- width, m.	2,89
- height, m.	2,40
- length, m.	13,50
- volume, m3	90,00
door dimensions, m.:
- width	0,80
- length	1,48

 

 

 

 

 

 

POWERPLANT:

 

Engine power conditions:
Takeoff power:
- engine rotational speed, rpm/%	12300+90 /95,5-96,2
- max. hourly fuel consumption, kg./h.	1030
Maximum Continuous Power:
- engine rotational speed, rpm/%	12300+90 /95,5-96,2
- max. hourly fuel consumption, kg./h.	927
Maximum Cruise Power:
- engine rotational speed, rpm/%	12300+90 /95,5-96,2
- max. hourly fuel consumption, kg./h.	855
Overall Dimensions, mm.
- length	3096 ± 5
- width	842 ± 5
- height	1180 ± 5
Dry weight, kg.	1040+2%

 

 

CARGO CABIN

The An-12 aircraft fuselage with elevated tail and big cargo door provides for convenient conditions of large-size cargo handling and paradropping. The 2.5t capacity airborne cargo handling device and quick-release transporter facilitate and accelerate the landing, mooring and unloading operations. The loading of large-size equipment is made through cargo door with ramp in the rear part of fuselage. The cargo cabin is not pressurized but equipped with individual oxygen supply system.