| Modification | Cessna 150M |
| Wing span, m | 10.2 |
| Aircraft length, m | 7.04 |
| Airplane height, m | 2.6 |
| Wing surface area, m2 | 14.80 |
| Aircraft empty weight, kg | 447 |
| Max gross takeoff weight, kg | 681 |
| Engine type | 1 Teledyne Continental O-200-A |
| Power, hp | 100 |
| Max speed, km/h | 200 |
| Cruise speed, km/h | 166 |
| Economic speed, km/h | 148 |
| Перегоночная дальность, км | 1361 |
| Operational range, km | 563 |
| Max climb capability, m/min | 195 |
| Service ceiling, m | 4663 |
| Crew | 1 pilot |
| Useful load: | 1 pax + 60 kg cargo |
| Fuel used: | 98 (MOGAS) and 100LL (AVGAS) |
| Max amount of fuel: | 22.5 U.S Gallons (85 litres) |
| Average flight duration: | 3.3 hour |
| Oil used:: | Aeroshell 50215 |
Speed/ Сonsumption
| Pressure Alt | RPM | 20° BELOW ISA KTAS/GPH |
ISA TEMP KTAS/GPH |
20° ABOVE ISA KTAS/GPH |
| 2000 | 2400 2300 2200 |
92/4.7 87/4.1 83/3.7 |
91/4.3 87/3.9 82/3.5 |
91/4.1 86/3.7 81/3.3 |
| 4000 | 2400 2300 2200 |
91/4.4 87/3.9 82/3.5 |
91/4.1 86/3.7 81/3.3 |
90/3.9 85/3.5 80/3.2 |
| 6000 | 2500 2400 2300 |
95/4.4 91/4.2 86/3.7 |
95/4.3 90/3.9 85/3.5 |
94/4.1 89/3.7 84/3.4 |
| 8000 | 2500 2400 2300 |
95/4.4 90/4.0 85/3.6 |
94/4.1 89/3.7 84/3.4 |
93/3.9 88/3.5 82/3.2 |
1 KTAS = 1.852 km/h
1 GPH = 3.79 litres
Speed table
Takeoff:
Normal Climb Out - 60-70 KIAS (110-129 km/h)
Climb:
Normal - 65-75 KIAS (120 - 139 km/h)
Best Rate of Climb, Sea Level - 68 KIAS (126 km/h)
Best Angle of Climb - 56 KIAS (103 km/h)
Landing:
Normal Approach, Flaps Up - 60-70 KIAS (110-129 km/h)
Normal Approach, Flaps 40° - 50-60 KIAS (92-110 km/h)
Short Field Approach, Flaps 40° - 52 KIAS (96 km/h)
Maximum Crosswind:
Takeoff - 13 knots (6.7 m/s)
Landing - 13 knots (6.7 m/s)
Normal Climb Out - 60-70 KIAS (110-129 km/h)
Climb:
Normal - 65-75 KIAS (120 - 139 km/h)
Best Rate of Climb, Sea Level - 68 KIAS (126 km/h)
Best Angle of Climb - 56 KIAS (103 km/h)
Landing:
Normal Approach, Flaps Up - 60-70 KIAS (110-129 km/h)
Normal Approach, Flaps 40° - 50-60 KIAS (92-110 km/h)
Short Field Approach, Flaps 40° - 52 KIAS (96 km/h)
Maximum Crosswind:
Takeoff - 13 knots (6.7 m/s)
Landing - 13 knots (6.7 m/s)
| SPEED | KIAS | KM/H | REMARKS | |
| Vne | Never Exceed Speed | 141 | 261 | Do not exceed this speed in any operation |
| Vno | Maximum Structural Cruising Speed |
107 | 200 | Do not exceed this speed expect in smooth air |
| Va | Maneuvering Speed: 1600 Pounds 1450 Pounds 1300 Pounds |
97 93 88 |
180 172 163 |
Do not make full or abrupt contorl movements above this speed |
| Vfe | Maximum Flap Extended Speed: | 85 | 157 | Do not exceed this speed with flaps down |
White Arc: 42 - 85 (78 - 157 km/h) Full Flap Operating Range. Lower limit is maximum weight Vso in landing configuration. Upper limit is maximum speed permissible with flaps extended.
Green Arc: 47 - 107 (87 - 200 km/h) Normal Operating Range. Lower limit is maximum weight Vg at most forward C.G. with flaps retracted. Upper limit is maximum structural cruising speed.
Yellow Arc: 107 - 141 (200 - 260 km/h) Operations must be conducted with caution and only in smooth air
Red Line: 141 (260 km/h) Maximum speed for all operations
