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From Wikipedia, the free encyclopedia

Model 150
Role Light utility aircraft, basic trainer
Manufacturer Cessna
First flight September 12, 1957
Produced 1958–1977
Number built 23,949[citation needed]
Unit cost
US$12,000-25,000 (2007)
Variants Cessna 152
Cessna 150s produced before 1964, such as this 1962 Cessna 150B, had a straight tail and no rear window
Cessna 150s produced before 1964, such as this 1962 Cessna 150B, had a straight tail and no rear window
A 1964 Cessna 150D. The 1964 model 150D and the 150E had an Omni-Vision rear window, but retained the straight tail of the earlier 150
A 1964 Cessna 150D. The 1964 model 150D and the 150E had an Omni-Vision rear window, but retained the straight tail of the earlier 150
1967 Reims-Cessna F150G showing the short dorsal strake and swept tail that was introduced with the 1966 model 150F
1967 Reims-Cessna F150G showing the short dorsal strake and swept tail that was introduced with the 1966 model 150F
1968 Reims-Cessna F150H
1968 Reims-Cessna F150H
1973 Cessna C150L showing its longer dorsal strake than earlier models
1973 Cessna C150L showing its longer dorsal strake than earlier models
1976 model Cessna 150M showing its 15% larger tail and rudder area
1976 model Cessna 150M showing its 15% larger tail and rudder area
1967 model Cessna 150G instrument panel
1967 model Cessna 150G instrument panel
A significant number of Cessna 150s have been converted to taildragger configuration using STC kits. This example is a Cessna 150F.
A significant number of Cessna 150s have been converted to taildragger configuration using STC kits. This example is a Cessna 150F.
Cessna 150G on floats
Cessna 150G on floats

The Cessna 150 is a two-seat tricycle gear general aviation airplane that was designed for flight training, touring and personal use.[1] In 1977 it was succeeded in production by the Cessna 152, a minor modification to the original design.

The Cessna 150 is the fifth most produced civilian plane ever, with 23,839 aircraft produced.[2] The Cessna 150 was offered for sale in the 150 basic model, Commuter, Commuter II, Patroller and the aerobatic Aerobat models.

In 2007 Cessna announced a successor to the Model 150 and 152, the Model 162 Skycatcher.


Development of the Model 150 began in the mid-1950s with the decision by Cessna Aircraft to produce a successor to the popular Cessna 140 which finished production in 1951. The main changes in the 150 design were the use of tricycle landing gear, which is easier to learn to use than the tailwheel landing gear of the Cessna 140, and replacing the rounded wingtips and horizontal and vertical stabilizers with more modern, squared-off profiles. In addition, the narrow, hinged wing flaps of the 140 were replaced by larger, far more effective Fowler flaps.[3]

The Cessna 150 prototype first flew on September 12, 1957, with production commencing in September 1958 at Cessna's Wichita, Kansas plant.[4] 1,764 aircraft were also produced by Reims Aviation under license in France. These French manufactured 150s were designated Reims F-150, the "F" indicating they were built in France.

American-made 150s were all produced with the Continental O-200-A 100 hp (75 kW) engine, but the Reims-built aircraft are powered by a Rolls Royce-built Continental O-200-As. Some versions have Continental O-240-A engines.

All models from 1966 onwards have larger doors and increased baggage space. With the 1967 Model 150G the doors were bowed outwards 1.5 inches (38 mm) on each side to provide more cabin elbow room.

The 150 was succeeded in the summer of 1977 by the closely related Cessna 152. The 152 is more economical to operate due to the increased TBO (time between overhaul) of the Lycoming O-235 engine. The 152 had its flap travel limited to 30 degrees, from the 150's 40 degree flap deflection, for better climb with full flaps and the maximum certified gross weight was increased from 1,600 lb (726 kg) on the 150 to 1670 lb (757 kg) on the 152. Production of the 152 ended in 1985 when manufacturing of all Cessna piston singles was suspended.[1]


A total of 22,138 Cessna 150s were built in the United States, including 21,404 Commuters and 734 Aerobats. Reims Aviation completed 1,764 F-150s, of which 1,428 were Commuters and 336 were Aerobats. A Reims affiliate in Argentina also assembled 47 F-150s, including 38 Commuters and 9 Aerobats.[citation needed]

Of all the Cessna 150-152 models, the 1966 model year was the most plentiful with 3,067 1966 Cessna 150s produced. This was the first year the aircraft featured a swept tail fin, increased baggage area and electrically operated flaps.



The first model year of the Cessna 150 carried no suffix letter. It was available as the "150" or the upgraded "Commuter". The engine was a 100 horsepower (75 kW) Continental O-200, the gross weight was 1,500 lb (680 kg) and flaps were actuated manually with a lever between the seats. Production commenced late in 1958 as the 1959 model year.

The cost was US$6,995 for the Standard Model 150, $7,940 for the Trainer and $8,545 for the Commuter.[4]

The 1960 model introduced a 35-ampere generator on the Commuter. The "patroller" was also introduced in 1960. This was a standard 150 with acrylic glass windows on the lower doors, 35 US gallon long-range fuel tanks and a message chute for dropping packages to the ground.

Production was 122 in 1958, 648 in 1959 and 354 in 1960.[5]


The 1961 model incorporated enough changes to justify a suffix letter and thus was designated the “150A”.

The "A" had its main landing gear moved aft by two inches to eliminate the problem of the aircraft ending up on its tail while loading people and baggage and also to improve nosewheel steering authority.

The "A" also had 15% larger rear side windows and new adjustable seats. 344 were constructed.[5]


The 150B was the 1962 model. It had a new propeller that increased cruise speed by 2 knots (3.7 km/h) and the option of a two-passenger child seat for the baggage compartment. 331 "B" models were built.[5] The Commuter version cost US$8,995.[6]


The 1963 model was the "C", which introduced the option of larger 6.00×6 inch tires to replace the standard 5.00×5 tires and fuel quick drains. 472 were completed.[5]


The 1964 "D" model brought the first dramatic change to the 150 – the introduction of a rear window under the marketing name Omni-Vision. The rear window changed the look of the 150 and cost 3 mph (4.8 km/h) in cruise speed. It also resulted in a larger baggage compartment and a greater structural weight allowance for baggage from 80 to 120 lb (54 kg). The unswept tailfin from previous years was retained for another two years. Elevator and rudder mass balances were increased to reduce flutter potential caused by the less aerodynamic rear fuselage. The gross weight of the aircraft was also increased in 1964 to 1,600 lb (730 kg), where it would stay until the advent of the Cessna 152. 804 150Ds were built.[5]

Many people find the new cabin more "airy" and pleasant, due to the increased light.[7]


The 1965 Cessna 150E saw only the addition of new seats, although the standard empty weight went up 40 lb (18 kg) that year to 1,010 lb (460 kg). The "E" model saw production increase to 1637 aircraft.[5]


The 1966 model saw great changes to the 150 design. The tailfin was swept back 35 degrees to match the styling of the Cessna 172 and other models. The cabin doors were made 23% wider, new brakes were brought in and the 6.00×6 tires were made standard. The previously manual flaps were now electrically actuated through a panel-mounted flap switch. The old electric stall warning system was replaced with a pneumatic-type. The baggage compartment was enlarged by 50%. A total of 3087 of the newly styled "F" models were produced.[5]

1966 was also the first production of French Reims-built F-150s, with 67 built as the F150F.[8]


In the 1967 model, the instrument panel was redesigned. The doors were "bowed" out to give three more inches of shoulder and hip room which was needed in the small cabin. The "G" model also saw a new short-stroke nose oleo introduced to reduce the drag created by the nosewheel assembly. The previously fitted generator was replaced by a 60-ampere alternator, reflecting the increasing avionics that the planes were being fitted with.

The "G" model was also the first Cessna 150 variant certified for floats. A total of 2114 "G" models were built, plus 152 built by Reims as F150G.[5]


The 1968 model 150 was designated the "H". It introduced a new-style center console, designed to improve legroom. A new electric flap switch was also fitted that allowed "hands-off" retraction of the flaps, but not extension. 2007 150Hs were built in Wichita, with 170 built by Reims as the F150H.[5]


There was no 150 "India" model as Cessna didn't want it to look like a Cessna 1,501. This did not prevent Cessna from designating an "India" model Cessna 172 however.[5]


The 150J, in 1969, brought a new key-operated starter that replaced the old "pull-style" starter. The new starter was more "car-like" but not as reliable as the old one and also more expensive to repair.

An auxiliary power plug was also made available as an option in 1969, along with "rocker" style electrical switches. 1714 "J" models were built,[5] plus 140 built by Reims as the F150J.


1970 was the year that Cessna introduced the A150K Aerobat, a Cessna 150K with limited aerobatic capabilities. It retained the 100 horsepower (75 kW) Continental O-200 all 150s used, but differed from the baseline 150K in having more structural strength, being rated +6/−3 g. Other "aerobatic" features included four-point harnesses for both occupants, dual overhead skylights for upward visibility (which, while standard on the Cessna 140, had not been part of the 150 design) jettisonable doors, a more sporty checkerboard paint scheme and removable seat cushions so that parachutes could be worn. In 1970, an Aerobat cost $12,000 as opposed to the $11,450 price for a 150K Commuter model.[9]

Both the new Aerobat and the non-aerobatic 150K also sported new conical cambered wingtips in 1970. A total of 832 "K" models were built, including A150Ks.[5] Reims built 129 as the F150K and 81 as the FA150K.


The 150L had the longest production run of any 150 sub-model, being produced 1971–74.

New in 1971 were tubular landing gear legs with a 16% greater width (6 feet 6 inches (1.98 m) to 7 feet 7 inches (2.31 m) for better ground handling. These replaced the previous flat steel leaf spring gear. Also in 1971, the landing and taxi lights were moved from the wing leading edge to the nose bowl to better illuminate the ground. They were an improvement, but bulb life was reduced due to the heat and vibration of that location. They were moved back to the wing on the 1984 model Cessna 152.

The "L" also introduced a longer dorsal strake that reached to the rear window. This was done more for styling than for aerodynamics and the empty weight accordingly went up 10 lb (4.5 kg) over the "K". 879 were built in 1971.

In 1972 the "L" received new fuel filler caps to reduce moisture seepage, and better seats and seat tracks. 1100 were built in 1972.

The 1973 "L" model brought in lower seats to provide more headroom for taller pilots. 1460 of the 1973 models were built.

The final "L" model was produced in 1974. The only change this model year was the propeller on the A150L Aerobat, to a new Clark Y airfoil that increased cruise by 4 mph (6.4 km/h). 1080 150s were produced in 1974.[5]

Total "L" production was 4519, plus the 485 built by Reims as the F150L and 39 FA150L Aerobats. An additional 39 were built in Argentina by DINFIA as the A-150L.[10]

FRA150L Aerobat

Reims produced a variant of the FA150L Aerobat with a Rolls-Royce Continental O-240-A engine, 141 built.[10]


The final Cessna 150 model was the 150M. It introduced the "Commuter II" upgrade package that included many optional avionics and trim items as standard. The "M" also brought an increased fin height, by 6 inches (150 mm). This increased the rudder and fin area by 15% to improve crosswind handling. The "M" was produced for three years: 1975–77.

Inertia-reel restraints became available as an option with the 1975 model year. 1269 1975 model 150Ms were built.

In 1976 the "M" gained a suite of electrical circuit breakers to replace the previous fuses used. It was also fitted with a fully articulated pilot seat as standard equipment (this seat had been optional on some earlier models). 1399 were built.

The 1977 model year was the last for the Cessna 150. It added only "pre-select" flaps, allowing the pilot to set the flaps to any position without the pilot having to hold the switch during flap travel, enabling the pilot to concentrate on other flying duties. Only 427 1977 model 150Ms were built as production shifted to the improved Cessna 152 in the early part of 1977.

The many refinements incorporated into the 150 over the years had cost the aircraft a lot of useful load. The very first 150 weighed 962 lb (436 kg) empty, whereas the last "M Commuter II" had an empty weight of 1,129 lb (512 kg). This increase in empty weight of 167 lb (76 kg) was offset only by a gross weight increase of 100 lb (45 kg) in 1964.[3] The 152 would bring a much-needed 70 lb (32 kg) increase in gross weight to 1,670 lb (760 kg).[5]

A total of 3097 "M" models were built during its three-year run.[5] An additional 285 were built by Reims as the F150M and 141 FA150M Aerobats. Reims also built 75 A150Ls with F150M modifications.


Reims produced a variant of the Rolls-Royce Continental O-240-A powered FRA150L Aerobat with the same improvements as the F150M, 75 built.[10]

Modifications available

There are hundreds of modifications available for the Cessna 150. Some of the most frequently installed include:

  • Vortex generators and STOL kits that reduce the stall speed of the plane.[11]
  • Flap gap seals to reduce drag and increase rate of climb.[11]
  • Different wing tips, some of which claim various cruise speed increases and stall speed reductions.[11]
  • Auto fuel STCs, which permit the use of automobile fuel instead of the more expensive aviation fuel.
  • Larger engines, up to 180 horsepower (130 kW).[11]
  • Taildragger landing gear.[11]
  • Auxiliary fuel tanks for larger capacity.[11]
  • Door catches to replace the factory ones that often fail in service.[11]
  • Belly fuel drain valves to drain fuel from the lowest point in the fuel system.[11]

Noteworthy flights

Cessna 150M Instrument Panel
Cessna 150M Instrument Panel
  • On September 12, 1994, Frank Eugene Corder intentionally crashed a Cessna 150L onto the South Lawn of the White House against the south wall of the Executive Mansion, in an apparent suicide. Corder was killed, but no one else was injured and damage to property on the ground was minimal.
  • In 1996 a Cessna 150 was flown from the United States to South Africa in several stages, crossing the Atlantic along the way. An extra 60 gallon fuel tank was installed (beyond the standard 22.5 gallons) and the plane took off 500 lb (230 kg) over gross weight.[12]



Cessna 150L
Cessna 150L

The aircraft is popular with flying schools as well as private individuals.


T-51A of the U.S. Air Force
T-51A of the U.S. Air Force
 Democratic Republic of the Congo
 Ivory Coast
 Sri Lanka
 United States


Specifications (1976 Commuter II)

1959 model Cessna 150
1959 model Cessna 150

Data from Jane's All The World's Aircraft[28]

General characteristics

  • Crew: one
  • Capacity: one passenger (plus two children not exceeding 120 lb (54 kg) on optional bench seat in baggage space)
  • Length: 23 ft 11 in (7.29 m)
  • Wingspan: 33 ft 2 in (10.11 m)
  • Height: 8 ft 6 in (2.59 m)
  • Wing area: 160 sq ft (15 m2)
  • Aspect ratio: 6.7:1
  • Airfoil: NACA 2412
  • Empty weight: 1,122 lb (509 kg)
  • Max takeoff weight: 1,600 lb (726 kg)
  • Fuel capacity: 22.5 US gal (18.7 imp gal; 85 L) usable internal fuel
  • Powerplant: 1 × Continental O-200-A air-cooled horizontally-opposed engine, 100 hp (75 kW)
  • Propellers: 2-bladed McCauley metal fixed-pitch propeller, 5 ft 9 in (1.75 m) diameter


  • Maximum speed: 109 kn (125 mph, 202 km/h) at sea level
  • Cruise speed: 82 kn (94 mph, 152 km/h) at 10,000 ft (3,050 m) (econ cruise)
  • Stall speed: 42 kn (48 mph, 78 km/h) (flaps down, power off)
  • Never exceed speed: 140 kn (160 mph, 260 km/h)
  • Range: 420 nmi (480 mi, 780 km) (econ cruise, standard fuel)
  • Service ceiling: 14,000 ft (4,300 m)
  • Rate of climb: 670 ft/min (3.4 m/s)
  • Take-off run to 50 ft (15 m): 1,385 ft (422 m)
  • Landing run from 50 ft (15 m): 1,075 ft (328 m)

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists



  1. ^ a b Plane and Pilot: 1978 Aircraft Directory, pages 22-23. Werner & Werner Corp, Santa Monica CA, 1977. ISBN 0-918312-00-0
  2. ^ Thompson, William (1991). Cessna Wings for the World. Bend, Or.: Maverick Publications. p. 16. ISBN 0-89288-221-2.
  3. ^ a b National Flightshops: All Those Cessna 150s. National Flightshops, St Petersburg FL, 1978.
  4. ^ a b Thompson, William (1991). Cessna Wings for the World. Bend, Or.: Maverick Publications. p. 9. ISBN 0-89288-221-2.
  5. ^ a b c d e f g h i j k l m n o Clarke, Bill: Cessna 150 and 152 first edition, pages 26-95. TAB Books, 1987. ISBN 0-8306-9022-0
  6. ^ Thompson, William (1991). Cessna Wings for the World. Bend, Or.: Maverick Publications. ISBN 0-89288-221-2.
  7. ^ Thompson, William (1991). Cessna Wings for the World. Bend, Or.: Maverick Publications. p. 11. ISBN 0-89288-221-2.
  8. ^ Thompson, William (1991). Cessna Wings for the World. Bend, Or.: Maverick Publications. p. 12. ISBN 0-89288-221-2.
  9. ^ Thompson, William (1991). Cessna Wings for the World. Bend, Or.: Maverick Publications. p. 14. ISBN 0-89288-221-2.
  10. ^ a b c Simpson 1996, pp. 96–97.
  11. ^ a b c d e f g h Clarke, Bill: Cessna 150 and 152 first edition, pages 197-212. TAB Books, 1987. ISBN 0-8306-9022-0
  12. ^ Kleynhans, Joan. "Transatlantic Cessna 150". Archived from the original on October 3, 2017. Retrieved July 24, 2017.
  13. ^ Andrade 1982, p. 36.
  14. ^ Andrade 1982, p. 342.
  15. ^ Andrade 1982, p. 57.
  16. ^ Andrade 1982, p. 126.
  17. ^ Andrade 1982, p. 147.
  18. ^ Andrade 1982, p. 157.
  19. ^ Andrade 1982, p. 176.
  20. ^ Andrade 1982, p. 194.
  21. ^ Andrade 1982, p. 209.
  22. ^ "DOD 4120.15-L - Addendum". Archived from the original on 7 July 2013. Retrieved 8 July 2015.
  23. ^ "Aircraft Accident Report Golden West Airlines, Inc., De Havilland DHC-6 N6383, and CessnAir Aviation, Inc., Cessna 150, N11421" (PDF). National Transportation Safety Board. August 7, 1975. Archived (PDF) from the original on March 3, 2016. Retrieved July 24, 2017.
  24. ^ "National Transportation Safety Board Aviation Accident Final Report Accident Number: ERA15MA259A". National Transportation Safety Board. November 15, 2016. Retrieved July 24, 2017.
  25. ^ "National Transportation Safety Board Aviation Accident Final Report Accident Number: ERA15MA259B". National Transportation Safety Board. November 15, 2016. Retrieved July 24, 2017.[permanent dead link]
  26. ^ "Two dead after F-16, Cessna collide over South Carolina". Fox News. Archived from the original on 8 July 2015. Retrieved 8 July 2015.
  27. ^ "Two Dead In F-16-Cessna Collision". AVweb. Archived from the original on 9 July 2015. Retrieved 8 July 2015.
  28. ^ Taylor 1976, p. 254.


External links

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