Two-seat training, touring and light commuting aircraft.
Aircraft was also available as a patroller version with larger side windows, a message chute and larger fuel tanks. ICAO type designation is ‘C150’.

last update: 8 September 2006

Original Model 150 was introduced on the market in October 1958. Basically a Cessna 140 equipped with a nosewheel. The Model 150F superseded the 150E and had a swept vertical tail compared to the ‘E’. Model 150F entered the market in 1962. A total of 2933 150F's were produced when production ended in 1966.

wing: High-wing braced monoplane, wing section NACA 2412. All-metal single spar with all-metal skin. Frise-type all-metal ailerons and single-slotted manually-operated all-metal flaps.
fuselage: All-metal semi-monocoque structure.
tail: Cantilever monoplane, all-metal structure, trim-tab in port elevator
landing gear: Fixed tricycle type, Cessna 'Land-o-matic' spring-steel main legs, Cleveland single-disc hydraulic, toe-operated brakes on main wheels. Steerable nosewheel on shock-absorbing strut.

- Aircraft can be equipped with a glider-towing hook.

- One Continental O-200-A horizontally-opposed, air-cooled 4-cylinder engine delivering 100 hp (74 kW).
- Engine drives a 2-blade fixed pitch propeller.
- Total fuel capacity 98 l (26 USG); 2 all-metal fuel tanks in wing; Patroller version total capacity 132 l (35 USG).

- Electrical system: 14V DC standard.
- Vacuum system: standard in trainer and commuter version, optional in other versions.

Wide choice of radio's including VHF-transceiver, VOR/LOC nav receiver and ADF from Cessna, King or Narco. Cessna Nav-O-Matic 200 single-axis autopilot optional.

Two persons side-by-side in completely enclosed cabin, luggage compartment behind seats, capacity 54 kg (120 lbs). Aircraft can be fitted with 'family seat' in luggage compartment, for 1 or 2 children not exceeding 54 kg (120 lbs) total weight. Heating and ventilation standard.

N/A

External:# wing span; 10.22 m / 33.50 ft# overall length; 6.58 m / 21.58 ft# overall height; 2.11 m / 6.92 ft# wing area; 14.9 sq m / 160 sq ft# aspect ratio; 7.0

max. t-o weight; 726 kg / 1600 lbs# empty weight; 440 kg / 970 lbs# empty weight, Patroller version; 442 kg / 975 lbs# wing loading; 49 kg/sq m / 10.0 lbs/sq ft# power loading; 7.3 kg/hp / 16.0 lbs/hp

max. speed at S/L; 113 kts / 210 km/h# max. cruising speed, 75% power, 7500 ft; 106 kts / 196 km/h# economical cruising speed, 10000 ft; 86 kts / 159 km/h# range at max. cruise speed, no res.; 427 nm / 790 km# range at economical cruise speed, no res.; 491 nm / 910 km# range, Patroller version, economical cruise speed; 769 nm / 1425 km# service ceiling; 12650 ft / 3850 m# max. rate of climb; 670 ft/min / 3.4 m/s# stall speed, 40 deg flaps; 43 kts / 80 km/h# t-o run; 224 m / 735 ft# t-o distance to 15 m; 422 m / 1385 ft# landing distance from 15 m; 328 m / 1075 ft# landing run; 136 m / 445 ft