The first Skymaster, Model 336 Skymaster, had fixed landing gear and initially flew on February 28, 1961.[4][5] It went into production in May 1963[1] with 195 being produced through mid-1964.[2]
In February 1965, Cessna introduced the Model 337 Super Skymaster.[6] The model was larger, and had more powerful engines, retractable landing gear, and a dorsal air scoop for the rear engine. (The "Super" prefix was subsequently dropped from the name.)[2] In 1966, the turbocharged T337 was introduced, and in 1973, the pressurized P337G entered production.[2]
Cessna built 2993 Skymasters of all variants, including 513 military O-2 versions.[1] Production in America ended in 1982, but was continued by Reims in France, with the FTB337 STOL and the military FTMA Milirole.[5]
Fuselage close-up with door openFlight deck
The Skymaster handles differently from a conventional twin-engine aircraft, primarily in that if an engine fails, the plane will not yaw toward that engine. Without the issue of differential thrust inherent to conventional (engine-on-wing) twins, engine failure on takeoff will not produce yaw from the runway heading. 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; however, performance in speed and, particularly, rate of climb are affected. Flying a Skymaster requires a pilot to hold a multiengine rating, although many countries issue a special "centerline thrust rating" for the Skymaster and other similarly configured aircraft.[2]
Ground handling requires certain attention and procedures. The rear engine tends to overheat and can quit while taxiing on very hot days.[7] Accidents have occurred when the runway is shorter than the single-engine take-off roll and pilots, unaware of a rear engine shutdown, have attempted take-off on the nose engine alone.[8]Federal Aviation AdministrationAirworthiness Directive 77-08-05 prohibits single-engine take-offs and requires the installation of a placard marked "DO NOT INITIATE SINGLE ENGINE TAKEOFF".[9]
The Skymaster's unique sound is made by its rear pusher propeller slicing through turbulent air from the front propeller and over the airframe while its front tractor propeller addresses undisturbed air.[2]
During the Rhodesian Bush War, the Reims-Cessna FTB 337G 'Lynx' was the main light attack aircraft used by Rhodesian Security Forces during Fire Force counterinsurgencyair assault missions, which began in 1974. The Lynxes were armed with twin Browning .303 machine guns mounted above the wing and 37mm SNEB rockets, locally made Mini "Alpha" Bombs (cluster bombs), Mini "Golf" Bombs (450lb (200kg) blast and shrapnel bomb) and Frantan (a napalm variant carried in frangible drop tanks) bombs.[11]
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, which 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 over international waters. Both aircraft were downed by a MiG-29, while a second jet fighter, a MiG-23, orbited nearby.[12]
Cessna has historically used model years similar to U.S. auto manufacturers, with sales of new models typically starting a few months prior to the actual calendar year.
336 Skymaster
Original variant first flown in 1961 and introduced for the 1963 and 1964 model years. The 336 had a six-seat cabin and was powered by two 195hp (145kW)Continental IO-360-A engines. Production aircraft differed from the prototypes in that they had a roomier cabin and a redesigned rear engine cowling to improve engine cooling and reduce cabin noise. Gross weight was 3,900lb (1,800kg).[13][14] A total of 197 built; 2 prototypes and 195 production aircraft (102 in 1963 and 93 in 1964).[15][16]
337 Super Skymaster
The 1965 model year brought major changes to the Skymaster, which led to a new model number, 337, being assigned. The most significant change was the addition of retractable undercarriage similar to that of the Cessna 210 Centurion, which sat four inches lower than the 336 for ease of entry/exit. Other changes included a redesigned nose cowling and new rear engine intake, greater wing angle of incidence, shortened ventral tail fins, increased elevator chord, and an increased gross weight of 4,200lb (1,900kg). The 337 was powered by two 210hp (160kW) Continental IO-360-C or IO-360-D engines.[13][14] 239 total built; 1 prototype and 238 production aircraft.[16][17]
337A Super Skymaster
1966 model year with canted engine instruments and rotary-type door latches.[13][14] 284 built.[16][17] 31 were later modified to MC337A standard with loudspeakers and leaflet dispensers for use by the United States Air Force as the O-2B Skymaster.[5][13]
1967 model year with improved brakes, 38A alternators, a redesigned cabin heating system, a split-bus electrical system, and an increased gross weight of 4,300lb (2,000kg). A version powered by turbocharged 210hp (160kW) Continental TSIO-360-A engines was also offered as the T337B.[13][14] 231 built, plus 479 M337B military variants as the O-2A Skymaster.[5][16][17]
337C/T337C Super Skymaster
1968 model year with a new instrument panel, improved seat belts, and an increased gross weight of 4,400lb (2,000kg) (4,500lb (2,000kg) for the T337C).[13][14] 223 built.[16][17]
337D/T337D Super Skymaster
1969 model year with reduced elevator chord and increased elevator up travel, electroluminescent instrument panel lighting, and new cowl flap controls. Also offered as the turbocharged T337D.[13][14] 215 built.[16][17]
337E/T337E Super Skymaster
1970 model year with conical cambered wingtips, a new fuel quantity system, and an increased gross weight of 4,440lb (2,010kg) (4,630lb (2,100kg) for the T337E).[13][14] 123 built, plus 24 in France by Reims Aviation for the European market as the F337E.[16][17][18]
FTA337E
One aircraft converted from the 20th production F337E.[16]
337F/T337F Super Skymaster
Introduced for the 1971 model year with an increased gross weight of 4,630lb (2,100kg) (same as the T337F) a refined instrument panel, a padded glareshield, a front engine access panel, and other minor changes. The 1972 model year introduced nose-mounted landing/taxi lights and minor interior changes. The turbocharged T337F was only offered for the 1971 model year.[13][14] 147 total built; 83 (1971) and 64 (1972). Reims also built a total of 31 as the F337F; 21 (1971) and 10 (1972).[16][17][18]
337G Super Skymaster
Introduced for the 1973 model year with a recontoured nose cap, flush wingtip lights, low-drag front exhaust stack and wing strut fairings, a flush-mounted pitot port on the left wing strut, a split airstair door replacing the cabin and baggage doors, aileron gap seals, and a hydraulic powerpack replacing the engine-driven pump. Power was provided by two 210hp (160kW) Continental IO-360-G engines. The 1974 model year introduced recessed parking brake control, a hydraulic gear accumulator, and improved subpanel rocker switches. 1975 introduced an optional 148USgal (560L) auxiliary fuel system and the Skymaster II with a preferred options package. 1976 introduced a "Camber-Lift" wing, a redesigned instrument panel, and a reworked fuel system with tail boom fuel sump tanks removed. 1977 introduced a new front propeller airfoil and an auxiliary master power switch. A turbocharged version of the unpressurized 337G was not offered.[13][14] 354 total built; 88 (1973), 56 (1974), 65 (1975), 77 (1976), and 68 (1977). Reims also built a total of 29 as the F337G; 8 (1973), 8 (1974), 5 (1975), 3 (1976), and 5 (1977).[16][17][18]
Reims FT337GP Pressurized Skymaster
P337G Pressurized Skymaster
Also known as the T337G,[note 1] introduced for the 1973 model year as a turbocharged, pressurized version of the 337G. The P337G was powered by two 225hp (168kW) TSIO-360-C engines. Like the 337G, the Skymaster II option was also available for the P337G.[13][14] 292 total built; 1 (1971 prototype), 148 (1973), 45 (1974), 31 (1975), 32 (1976), and 35 (1977). Reims also built a total of 22 as the FT337GP; 8 (1973), 5 (1974), 2 (1975), 2 (1976), and 5 (1977).[16][17][18]
FTB337G
Military variant of the F337G with Sierra Industries Robertson STOL modifications and underwing hardpoints. Known as the Lynx in Rhodesian Air Force service. 61 built.[5][11][16]
337H/T337H Super Skymaster
Introduced for the 1978 model year with redesigned control wheels and minor interior refinements. The turbocharged version was also offered after a six year absence as the T337H, which was powered by two 210hp (160kW) Continental TSIO-360-H engines. The T337H-SP was introduced for the 1980 model year and was powered by TSIO-360-JB engines. The 1980 model year replaced the engines of the 337H and T337H with the TSIO-360-GB and TSIO-360-HB, respectively.[13][14][17] 140 total built; 58 (1978), 47 (1979 337H/T337H), 1 (1979 T337H-SP prototype), 24 (1980 337H/T337H), and 10 (1980 T337H-SP). Reims also built 2 aircraft in 1978 as the F337H.[16][17][18]
P337H Pressurized Skymaster
Introduced for the 1978 model year as a turbocharged, pressurized version of the 337H powered by two 225hp (168kW) TSIO-360-C engines, which were replaced by the TSIO-360-C for the 1980 model year.[13][14] 64 total built; 26 (1978), 24 (1979), and 15 (1980). Reims also built 1 aircraft in 1978 as the FT337HP.[16][17][18]
348
Based on the M337B but with two 317shp (236kW)Allison 250-B15 turboprop engines, a longer span wing, and improved high lift devices. Designated O-2T, only a single prototype was built.[19][14]
351
Also known as the O-2TT, a proposed variant of the O-2T with a tandem two-seat cockpit for the pilot and observer. Only a mockup was built.[5][19][14][16]
377/327 Baby Skymaster
Reduced-scale four-seat version of the 337 first proposed in 1965 as the Model 377 with cantilever wings replacing the 336/337 strut-braced configuration. The 377 was later redesignated as the Model 327 in 1967 and was first flown in December of that year. One prototype was built before the project was canceled 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.[20][13]
Hybrid electric aircraft with the forward piston engine replaced by an electric motor powered by a battery, in a parallel hybrid configuration. The demonstrator first flew on 6 June 2019, before Hawaiian regional carrier Mokulele Airlines experiment connecting Maui airports with the aircraft.
An extensive single-turboprop engine STOL cargo plane conversion of the Skymaster. Front engine was replaced with a Garrett AiResearch TPE-331turboprop; rear engine was removed, and its space filled with an extended cargo pod.
Groen RevCon 6-X
Test conversion of a Cessna 337 Skymaster airplane. This aircraft conversion tested the theory of using fixed-wing airplanes as the basic airframes for gyroplanes to reduce cost and shorten development time.
Built by Spectrum Aircraft Corporation of Van Nuys, California, it was an extensive single-turboprop engine conversion of a Reims FTB337G constructed in the mid 1980s. They removed the nose engine, lengthened the nose, and replaced the rear engine with a turboprop.[22]
Summit Sentry O2-337
Summit Aviation of Middletown, Delaware re-manufactured existing used 337 airframes into the militarized O2-337 which includes four wing-mounted NATO standard pylons capable of carrying 350lb (159kg) each for 7.62mm and 12.7mm gun pods, rocket launchers, bombs, markers and flares. The aircraft was marketed for the target identification and marking, reconnaissance, helicopter escort and aerial photography roles. Examples were sold to the Haitian Air Force, Honduras, Nicaragua, Senegal and the Thai Navy. The variant was still in production in 1987.[4]
VoltAero hybrid electric conversion
VoltAero is a startup company formed in September 2017 by the CTO and test pilot of the 2014 Airbus E-Fan 1.0. The company has been established in Royan, with support from the French Nouvelle-Aquitaine region. It is developing a hybrid electric aircraft testbed based on the Skymaster, which is intended to fly in late February 2019. It will be followed up by the VoltAero Cassio prototype in 2020, a clean-sheet, all-composite design.[23]
Força Aérea de Moçambique (3 x FTB-337G) - ex-Portuguese Air Force FTB-337G refurbished and offered by the Government of Portugal to Mozambique in 2011 and 2012.[27]
Portuguese Air Force[4] (32 × 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.
Simpson, Roderick W. (1991). Airlife's general aviation: a guide to post-war general aviation manufacturers and their aircraft. Shrewsbury: Airlife Publ. [u.a.] ISBN978-1-85310-194-6.
Fontanellaz, Adrien; Cooper, Tom; Matos, Jose Augusto (2020). War of Intervention in Angola, Volume 3: Angolan and Cuban Air Forces, 1975-1985. Warwick, UK: Helion & Company Publishing. ISBN978-1-913118-61-7.
Taylor, John W. R. Jane's All The World's Aircraft 1969–70. London: Sampson Low, Marston & Company, 1969. ISBN0-354-00051-9.
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Angola
Burkina Faso
Colombia
Mozambique
Namibia
Nicaragua
Togo
Zimbabwe
Argentina
Bangladesh
Chile
Chad
Ecuador
El Salvador
Equatorial Guinea
Guinea-Bissau
Haiti
Jamaica
Niger
Mexico
Portugal
Rhodesia
Senegal
Sri Lanka
