The Cessna Skymaster

DEVELOPMENT

The first model of the Skymaster was the 336. It had fixed landing gear and first flew in February 1961. It went into production in 1963 and 195 were produced to mid 1964.

In 1965 Cessna introduced the model 337 Super Skymaster. This aircraft was larger, had more powerful engines, retractable landing gear and a dorsal air scoop for the rear engine (the "Super" was subsequently dropped from the name). In 1967 the turbocharged T377 was introduced and in 1972 the pressurized T377G entered production. Cessna built 1,859 standard and turbocharged Skymasters and 332 T337Gs. In addition, they built 513 military O-2 versions.

Cessna production ended in 1980 but Skymaster production continued with Reims in France with the FTB337 STOL and the military FTMA Milirole. Reims produced a total of 94 Skymasters.

After a 20-year hiatus the centerline thrust, pod and twin-boom concept has been revived in the Adam A500.

OPERATIONAL HISTORY

The US Army used the O-2 variant as a Forward Air Controller platform during the Vietnam War.

The California Division of Forestry uses the O-2 variant as spotter planes during firefighting operations.

In 1994 the Cuban exile group Hermanos al Rescate (Brothers to the Rescue) used Skymasters to drop life-saving supplies to rafters attempting to cross the Florida Straits to defect from Cuba. They chose Skymasters because they were eaiser to control at slow speeds than conventional twin-engine aircraft. One plane contacted the water (it is difficult to judge altitude over relatively calm water), damaging the landing gear doors and the nose propeller. Since the rear engine is mounted higher, it wasn't damaged and the aircraft was able to return to Florida to make a belly landing.

VARIANTS

CESSNA 336

336

CESSNA 337

337A
337B
337M - US military version, designated O-2 Skymaster in service
     O-2A
     O-2B
     O-2T - turboprop-powered O-2

337C
337D
337E
337F
337G
337H
T337B - turbocharged engines
T337C
T337D
T337E
T337F
T337G
T337H
P337H
T337H-SP

REIMS F337
F337
F337P - pressurized
FTB337G - STOL version

SUMMIT SENTRY
Summit Aviation built a militarized Skymaster as the O2-337 in 1980, and sold a few examples to the Haiti Air Corps and the Thai Air Force

SPECTRUM SA-550
Spectrum Aircraft Corporation of Van Nuys, California made an extensive 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. This aircraft (serial number 61) is currently registered to Basler Turbo Conversions of Oshkosh, Wisconsin.

SPECIAL CHARACTERISTICS

The Skymaster has different handling characteristics than a conventional twin-engine aircraft. Foremost is that it will not yaw into the dead engine if one engine quits. Consequently, it has no tendency to depart the runway if an engine fails on the takeoff roll. The adage, "dead foot, dead engine" -- used to remind a pilot which propeller to feather when an engine quits -- is useless with the Skymaster. When a Skymaster loses power, the pilot must use the instruments to determine which engine has failed. The Skymaster is also controllable at lower airspeeds than a comparable conventional twin. There is no minimum controllable speed advisory (Vmc) on the airspeed indicator.

The Skymaster requires a multi-engine-rated pilot. The pilot must be trained to manage both engines, and must also be trained to handle the special characteristics of a multiengine aircraft with centerline thrust.

The Skymaster produces a unique unmistakable sound. All rear-engined aircraft produce a characteristic sound as the propeller slices through turbulant air coming off the airframe. Since the Skymaster also has a nose engine, with a propeller that operates in undisturbed air, its sound is different from a pure pusher.