Cessna C-106 Loadmaster

C-106 Loadmaster

The P260 demonstrator
Role	Military transport monoplane
National origin	United States
Manufacturer	Cessna Aircraft
First flight	1943
Number built	2

The Cessna C-106 Loadmaster (or Cessna P260) was a 1940s American twin-engined transport monoplane.^[1] Built of plywood it did not enter production due to a wartime shortage of material.^[1]

Development

The C-106 Loadmaster was a twin-engined high-wing cantilever monoplane with a retractable tailwheel landing gear.^[2] It was powered by two 600 hp Pratt & Whitney R-1340 engines.^[1] Two company owned P260 demonstrators were built and given the military designation C-106 Loadmaster.^[1] An order for 500 was cancelled due to a shortage of plywood.^[1]

Variants

C-106: Military designation for company owned P260 prototype with two R-1340-S3H1 engines.
C-106A: Military designation for company owned P260 prototype with two R-1340-AN-2 engines.

Specifications

Data from ^[2]

General characteristics

Crew: 4
Length: 51 ft 1 in (15.57 m)
Wingspan: 64 ft 8 in (19.71 m)
Powerplant: 2 × Pratt & Whitney R-1340^[1]^[3] air-cooled radial piston engine, 600 hp (450 kW) each

Performance

Maximum speed: 195 mph (314 km/h; 169 kn)

References

Wikimedia Commons has media related to Cessna C-106 Loadmaster.

Notes

1 2 3 4 5 6 Andrade 1979, p. 84
1 2 "American airplanes - Cessna". www.aerofiles.com. 4 April 2009. Retrieved 2009-12-29.
↑ Note: Aerofile has two Pratt & Whitney R-1830 being used.

Bibliography

Andrade, John (1979). U.S.Military Aircraft Designations and Serials since 1909. Midland Counties Publications. ISBN 0-904597-22-9.

Cessna aircraft

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Cessna Citation
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Military

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United States military transport aircraft designations, Army/Air Force and Tri-Service systems

Army/Air Force sequence (1925-1962)	C-1 C-2 C-3 C-4 C-5 C-6 C-7 C-8 C-9 C-10 C-11 C-12 C-13¹ C-14 C-15 C-16 C-17 C-18 C-19 C-20 C-21 C-22 C-23 C-24 C-25 C-26 C-27 C-28 C-29 C-30 C-31 C-32 C-33 C-34 C-35 C-36 C-37 C-38 C-39 C-40 C-41/A C-42 C-43 C-44 C-45 C-46 C-47/T C-48 C-49 C-50 C-51 C-52 C-53 C-54 C-55 C-56 C-57 C-58 C-59 C-60 C-61 C-62 C-63 C-64 C-65 C-66 C-67 C-68 C-69 C-70/A/B/C/D C-71 C-72 C-73 C-74 C-75 C-76 C-77/B-D C-78 C-79 C-80 C-81 C-82 C-83 C-84 C-85 C-86 C-87 C-88 C-89 C-90 C-91 C-92 C-93 C-94 C-95 C-96 C-97/KC-97 C-98 C-99 C-100 C-101 C-102 C-103 C-104 C-105 C-106 C-107 C-108 C-109 C-110 C-111 C-112 C-113 C-114 C-115 C-116 C-117 C-118 C-119 C-120 C-121/F C-122 C-123/A C-124 C-125 C-126 C-127 (I) C-127 (II) C-128 C-129 C-130/J C-131 C-132 C-133 C-134 C-135/KC-135 C-136 C-137 C-138¹ C-139¹ C-140 C-141 C-142

Tri-service sequence (1962-present)	C-1 C-2 C-3 C-4 C-5 C-6 C-7/B C-8 C-9 C-10 C-11 C-12 C-13¹ C-14 C-15 C-16¹ C-17 C-18 C-19 C-20A-D/F-H C-21 C-22 C-23 C-24 C-25 C-26 C-27/J C-28 C-29 C-30¹ C-31 C-32 C-33 C-34¹ C-35 C-36 C-37A/B C-38 C-39¹ C-40 C-41 C-42¹ C-43¹ C-44¹ C-45 C-46

Revived original sequence (2005-present)	C-143 C-144 C-145 C-146

Non-sequential designations	C-767 C-880

¹ Not assigned See also: AC-47 • AC-119 • AC-130 • DC-130 • EC-130 • HC-130 • KC-130 • LC-130 • MC-130 • WC-130 • CT-39 • CT-43

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Cessna C-106 Loadmaster

Development

Variants

Specifications

See also

References