43-22650: Difference between revisions
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The two fuselages under the spine are 399 ([[43-22650]]) (left) and 400 ([[43-22651]]) (right) at the [[Douglas Tulsa]] factory. <br> | The two fuselages under the spine are 399 ([[43-22650]]) (left) and 400 ([[43-22651]]) (right) at the [[Douglas Tulsa]] factory. <br> | ||
[[File:022 WM.jpg|600px]] | [[File:022 WM.jpg|600px]] | ||
Tail assemblies at the [[Douglas Tulsa]] factory. The center tail here reads 400 ([[43-22651]]) and the bottom most one in pencil reads 401 ([[43-22652]]). We can infer that the topmost tail assembly is 399 ([[43-22650]]). <br> | |||
[[File:029 WM.jpg|600px]] | |||
==Sources== | ==Sources== |
Latest revision as of 16:53, 3 August 2020
A-26C-25 Invader | |||
---|---|---|---|
Builders: Douglas Aircraft Company | |||
Operators: United States Air Force | |||
Number Built: | |||
First Built: | |||
GENERAL CHARACTERISTICS | |||
Type: Light Attack Bomber | |||
Wet Weight: 31,000 lbs | |||
Length: 51' 3" (15.24 m) | |||
Height: 18' 6" (5.64 m) | |||
Wingspan: 70' (21.34 m) | |||
Wing Area: 540 Sq. Feet (50.17 m²) | |||
Speed: 212 mph | |||
Max Speed: 370 mph | |||
Ceiling: 31,300 feet | |||
Powerplant: 2x Pratt & Whitney R-2800-27 | |||
Horsepower: 2,000 each | |||
Fuel Capacity: 1,600 US Gallons | |||
Range: | |||
Crew: 3 | |||
Passengers: 1 | |||
ARMAMENT | |||
Nose Guns: None | |||
Dorsal Turret: 2x .50 Machine Guns | |||
Ventral Turret: 2x .50 Machine Guns | |||
Payload: 4,000 lbs internal 2,000 lbs wing points | |||
Donate | |||
Even a small donation of a couple of dollars goes a long way in helping |
See also: List of Invaders by Serial Number, Serial Numbers starting with 43
Operational History
unknown
Accidents
Unknown
Crew
Unknown
Disposition
Unknown.
Images
The two fuselages under the spine are 398 (43-22649) (left) and 399 (43-22650) (right) at the Douglas Tulsa factory.
The two fuselages under the spine are 399 (43-22650) (left) and 400 (43-22651) (right) at the Douglas Tulsa factory.
Tail assemblies at the Douglas Tulsa factory. The center tail here reads 400 (43-22651) and the bottom most one in pencil reads 401 (43-22652). We can infer that the topmost tail assembly is 399 (43-22650).
Sources
Databases searched:
- AAIR -
- MACR -
- KORWALD -
- Baugher