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Posted 6/24/2009 Printable Fact Sheet
Beech C-45H
Beech C-45H side view (S/N 52-10825) assigned to the Airways and Air Communications Service (AACS). (U.S. Air Force photo)
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In 1952 432 Beech C-45, AT-7 and AT-11s were completely rebuilt and upgraded with new components. Because of the extensive rework and modifications bringing the aircraft to "zero-time" status, the planes were re-designated C-45H and given 1952 serial numbers.

The C-45H, like the G model, was fitted with a strengthened center wing section, new landing gear, larger engine nacelles, constant speed, feathering propellers and instrument upgrades. The one of the significant differences between the G and H model was the lack of an autopilot on the -H model.

More than 400 C-45Hs entered service in 1952 and remained throughout the 1950s into the early 1960s. The planes were used primarily for staff transport, light cargo, liaison and administrative missions.

Type Number built/
C-45 11 Beech Model B18S
C-45A 20 8 seat improvement
C-45B 223 Improved C-45A
UC-45C 2 Impressed B18S
UC-45D 2 Modified AT-7
UC-45E 6 Modified AT-7B
UC-45F 1522 Seven place version
C-45G 372 Rebuilt C-45, AT-7 & AT-11
TC-45G 96 Navigator Training Aircraft
C-45H 432 Rebuilt C-45

Engines: Two Pratt & Whitney R-985-AN-14B Wasp Junior radials of 450 hp each
Maximum speed: 219 mph
Cruising speed: 150 mph
Range: 1,140 miles
Service ceiling: 18,200 ft.
Span: 47 ft. 8 in.
Length: 34 ft. 8 in.
Height: 9 ft. 2 in.
Weight: 9,300 lbs. loaded weight
Crew: One or two (pilot and co-pilot)
Passenger capacity: Five or six
Serial numbers: 52-10539 to 52-10970

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