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North American Aircraft Logo (Circa 1943)



OA-10A | ERB-17G/H | L-5 | R-6A | C-47 | P-38

Wingspan: 67 Ft. 7 In.
Length: 51 Ft. 0 In.
Height: 15 Ft. 9 In.
Weight: 33,500 Lbs loaded
Armament: Fourteen .50-cal. machine guns and one 75mm T13E1 cannon plus 3,200 lbs. of bomb
Engines: Two Wright R-2600-13 turbo-supercharged radials of 1,700 hp. each (take-off power)
Max speed: 275 mph at 13,000 Ft.
Cruising speed: 230 mph
Range:  1,350 miles
Service Ceiling: 24,800 Ft.

The North American B-25D was identical to the B-25C; the only difference was the manufacturing plant.
The -D was built at North American Aviation's (NAA) Kansas City, Missouri plant and the -C was built at the Inglewood, California plant. B-25D production was done in eight blocks of two NAA models (NA-87 and NA-100). The aircraft remained in production until the spring of 1944 when the last of 2,290 B-25Ds built was delivered.

The B-25Ds first flight was on 3 January 1942 and the first aircraft was accepted by the Army Air Force about a month later. Improvements to the basic B-25C/D design were incorporated into the production line as well as at depots and in the field.

Often, the only way to positively identify an aircraft model was by its serial number.
For example, early B-25Ds were built without ventral turrets and many aircraft didn't have the engine exhaust stacks common on late model aircraft. The navigator's sighting dome was omitted on some -C and -D models also.

Source:  US Air Force Museum

The B-25 that the 2nd Emergency Rescue Squadron had assigned was used for passenger transport and various other missions. It was not used as a bomber or for any other offensive reason and seemed to be excess on property on the TO & E.
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