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Douglas C-133A Cargo Master

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The C-133 was developed to fulfill USAF requirements for a large capacity, strategic cargo a/c. The a/c went directly into production (no prototypes) with first flight 23/APR/1953.  A total of 45 -As and -Bs were built and operated until 1971.

General:

Type: Transport

Crew: 4

Seating: 4

First Flight: 23/Apr/1956

Specifications

 

Propulsion

 

Performance

 

Length:

Height:

Wingspan:

Empty Weight:

Gross Weight:

157' 6"

48' 8"

179' 8"

lbs.

282000 lbs.

No. Engines:

Horsepower:

Powerplant:

4

7000 hp per engine

Pratt & Whitney T34

Range:

Speed (max):

Speed (cruise):

Climb:

Ceiling:

1925 miles

350 mph

310 mph

- ft/sec

18950 ft

Armament:

None

       

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