- Aircraft History, Specification and Information -
Cessna 337 Super Skymaster
Cessna 337A Super Skymaster - N502CS - Pushpull Aircraft
1966 Cessna 337A Super Skymaster
N502CS (sn 337-0280)
Photo taken Jul. 27, 2010 @ Oshkosh (EAA AirVenture Fly-in), WI - USA (OSH / KOSH)
Photo © Marcel Siegenthaler

The Cessna Skymaster is a United States twin-engine civil utility aircraft built in a push-pull configuration. Its engines are mounted in the nose and rear of its pod-style fuselage. Twin booms extend aft of the wings to the vertical stabilizers, with the rear engine between them. The horizontal stabilizer is aft of the pusher propeller, mounted between and connecting the two booms. The combined tractor and pusher engines produce 'centerline' thrust and a unique sound.


The first Skymaster, model 336, had fixed landing gear and first flew on February 28, 1961. It went into production in May 1963, and 195 were produced through mid 1964.

In February 1965 Cessna introduced the model 337 Super Skymaster. The model was larger, and had more powerful engines, retractable landing gear, and a dorsal air scoop for the rear engine ("Super" was subsequently dropped from the name). In 1966 the turbocharged T337 was introduced, and in 1973 the pressurized P337G entered production.

Cessna built 2993 Skymasters of all variants, including 513 military O-2 versions. Production in America ended in 1982 but continued with Reims in France with the FTB337 STOL and the military FTMA Milirole. Production totalled 94 units.


The Skymaster handles differently from a conventional twin-engine aircraft, primarily in that it will not yaw into the dead engine if one engine fails. Without the issue of differential thrust inherent to conventional (engine-on-wing) twins, engine failure on takeoff will not produce yaw from the runway direction. With no one-engine-out minimum controllable speed(Vmc), in-flight control at any flying speed with an engine inoperative is not as critical as it is with engines on the wing with the associated leverage. Nevertheless, the Skymaster requires a multi-engine-rating, although many countries issue a special "centerline thrust rating" for Skymaster and other like-configurated aircraft.

Ground handling requires certain attention and procedures. The rear engine tends to overheat and can quit while taxiing on very hot days. There have been accidents when pilots, unaware of the shutdown, have attempted take-off on the nose engine alone, even though the single-engine take-off roll exceeded the particular runway length. FAA Airworthiness Directive 77-08-05 prohibits single engine take-offs and requires the installation of a placard with words that say "DO NOT INITIATE SINGLE ENGINE TAKEOFF".

The Skymaster produces a unique sound: a combination sound of its rear propeller slicing through turbulent air from the front prop and over the airframe, while its nose propeller addresses undisturbed air.

Operational history

From 1976 until the middle 1990s, the California Department of Forestry and Fire Protection used O-2 variants of the 337 Skymaster as tactical aircraft during firefighting operations. These were replaced with North American OV-10 Broncos, starting in 1993.

Brothers to the Rescue
From 1991 until 2001 the Cuban exile group Hermanos al Rescate (Brothers to the Rescue) used Skymasters, among other aircraft, to fly search and rescue missions over the Florida Straits looking for rafters attempting to cross the Straits to defect from Cuba and, when they found them, dropped life-saving supplies to them. Rescues were coordinated with the US Coast Guard, who worked closely with the group. They chose Skymasters because their high wing offered better visibility of the waters below, they were reliable and easy to fly for long-duration missions (averaging 7 hours), and they added a margin of safety with twin engine centerline thrust. In 1996, two of the Brothers to the Rescue Skymasters were shot down by the Cuban Air Force (FAC) over international waters. Both aircraft were downed by a MiG-29, while a second jet fighter, a MiG-23 orbited nearby.


  • Cessna 327 Baby Skymaster - reduced scale four-seat version of the 337, with cantilever wings replacing the 336/337strut-braced configuration. It first flew in December 1967. One prototype was built before the project was cancelled in 1968 due to lack of commercial interest in the design. The prototype was delivered to NASA to serve as a full-scale model for wind tunnel testing. It was used in a joint Langley Research Center and Cessna project on noise reduction and the use of ducted versus free propellers.
  • Cessna 336 Skymaster - production version powered by two 195 hp (145 kW) Continental IO-360-A engines, 195 built.
  • Cessna 337 Super Skymaster - 336; retractable undercarriage, redesigned nose cowling and new rear engine intake, and greater wing angle of incidence, powered by two 210 hp (160 kW) Continental IO-360-C engines, 239 built.
  • Cessna 337A Super Skymaster - 337; minor detail changes, 255 built.
  • Cessna 337B Super Skymaster - 337A; increased take-off gross weight, optional belly cargo pack, 230 built.
  • Cessna T337B (1967) Turbo Super Skymaster - 337B; two Continental turbocharged fuel injected 210 hp (160 kW) engines which boosted service ceiling to 33,000 feet (10,000 m), cruise speed to 233 mph (375 km/h), and range to 1,640 miles (2,640 km)
  • Cessna 337C Super Skymaster - 337B; new instrument panel and increased take-off gross-weight, 223 built.
  • Cessna 337D Super Skymaster - 337C; minor detail changes, 215 built.
  • Cessna 337E Super Skymaster - 337D; cambered wingtips and minor changes, 100 built.
  • Cessna 337F Super Skymaster - 337E; increased take-off gross weight, 114 built.
  • Cessna 337G Super Skymaster - 337F; split airstair entry door, smaller rear side windows, improved flaps, larger front propeller, powered by Continental IO-360-G engines, 352 built.
  • Cessna P337G Super Skymaster - 337G; pressurized cabin and turbocharged engines, 292 built.
  • Cessna 337H Skymaster - 337G; minor changes and optional turbocharged engines, 136 built.
  • Cessna P337H Pressurized Skymaster - T337G; minor changes, 64 built.
  • Cessna 337M - US military version designated O-2 Skymaster in service, 513 built.
  • Cessna O-2A - US military designation of the 337M Forward air control, observation aircraft for the US Air Force. 501 delivered to the USAF and 12 to the Imperial Iranian Air Force
  • Cessna O-2B - Psychological warfare version for the US Air Force (31 former civil aircraft were converted to O-2B).
  • Cessna O-2TT - Twin turboprop-powered version of the O-2.
  • Cessna Summit Sentry O2-337 - Military version.
  • Cessna Lynx - Armed military version for the Rhodesian Air Force.
  • Cessna T337H-SP

Reims Cessna

  • Reims Cessna F337E Super Skymaster, 24 built.
  • Reims Cessna F337F Super Skymaster, 31 built.
  • Reims Cessna F337G Super Skymaster, 29 built.
  • Reims Cessna FT337G Super Skymaster, 22 built.
  • Reims Cessna F337H Super Skymaster, 1 built.
  • Reims Cessna FP337H Pressurized Skymaster, 1 built.
  • Reims Cessna FTB337G Milirole; military F337G with Sierra Industries Robertson STOL modifications and underwing hardpoints, 61 built.
  • Reims Cessna Lynx - Rhodesian designation for 21 FTB337Gs delivered to the Rhodesian Air Force.


  • Conroy Stolifter is an extensive single-turboprop engine STOL cargo plane conversion of the Skymaster. Front engine was replaced with a Garrett AiResearch TPE-331 turboprop; rear engine was deleted, and its space filled with an extended cargo pod.
  • The AVE Mizar flying car, created by Advanced Vehicle Engineers, was an attachment of Skymaster wings, tail, and rear engine to a Ford Pinto outfitted with aircraft controls and instruments.
  • Summit Sentry - Summit Aviation built a militarized Skymaster as the O2-337 in 1980, and sold a few examples to the Haitian Air Force and the Thai Navy
  • Spectrum Aircraft Corporation of Van Nuys, California made an extensive single-turboprop engine conversion of a Reims FTB337G in the mid 1980s: the Spectrum SA-550. They removed the nose engine, lengthened the nose, and replaced the rear engine with a turboprop.

Military operators

  • Bangladesh
    Bangladesh Army
  • Burkina Faso
  • Chad
  • Chile
    Chilean Air Force
  • Colombia
  • Costa Rica
  • Ecuador
  • El Salvador
  • Equatorial Guinea
  • Guinea-Bissau
  • Haiti
    Haitian Air Force
  • Iran
    Imperial Iranian Air Force
  • Jamaica
  • Mexico
  • Nicaragua
    8 x 0-2A
    1 x 0-2B
  • Niger
    Military of Niger
  • Paraguay
    Paraguayan Air Force: 1 x 337RG
  • Peru
  • Portugal
    Portuguese Air Force (32 x FTB-337G) - Purchased in 1973 to replace the force's aging Dornier Do 27 fleet, which had been used intensively in the Portuguese Colonial War. The first 337 deliveries did not arrive until December 1974 - after the end of the war. The last Skymaster in service with the Portuguese Air Force was retired on July 25, 2007.
  • Rhodesia
    Rhodesian Air Force
  • South Africa
    South African Air Force
  • South Korea
    Republic of Korea Air Force
  • Sri Lanka
    Sri Lanka Air Force
  • Swaziland
    Military of Swaziland
  • Thailand
    Royal Thai Navy
  • Togo
    Togo Air Force
  • Trinidad and Tobago
  • United States
    United States Air Force
  • Zimbabwe
    Air Force of Zimbabwe

Specifications (337D)

General characteristics
Crew: 1
Capacity: 5 passengers
Length: 29 ft 9 in (9.07 m)
Wingspan: 38 ft 0 in (11.58 m)
Height: 9 ft 4 in (2.84 m)
Wing area: 201 ft² (18.7 m²)
Empty weight: 2,655 lb (1,204 kg)
Max takeoff weight: 4,400 lb (2,000 kg)
Powerplant: 2× Continental IO-360-C piston engine, 210 hp (157 kW) each

Maximum speed: 200 mph (174 kn, 320 km/h)
Range: 764 mi (664 nmi, 1,220 km)
Service ceiling: 19,500 ft (5,944 m)
Rate of climb: 1,200 ft/min (6.1 m/s)

Last updated September 27, 2010
This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Cessna Skymaster".
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