Airplane | N5440H | Comments |
Model | Cessna 172M, Skyhawk II | |
Engine | Lycoming O-320-E2D, 150 HP | |
Fuel | 80/87 minimum grade aviation gasoline | Please re-fill all Twin Oaks Aircraft with AvGas 100LL. only |
Engine limits | For all operations, 2700 rpm | |
Airspeed Limits(CAS) | Maneuvering 112 mph ( 97 knots)Maximum structural cruising 145 mph (126 knots)Never exceed 182 mph (158 knots)Flaps extended 100 mph ( 87 knots) | |
C.G. range | +38.5 to +47.3 at 2300 lbs. +35.0 to +47.3 at 1950 lbs. or less | |
Maximum Takeoff Weight | 2300 lbs. | |
| Standard Empty Weight | 1335 lbs. | |
| Maximum Useful Load: | 965 lbs. | |
| Maximum Useful Load with full fuel: | 713 lbs. | |
Number of seats | 4 | Two at +34 to +46, two at +73 . Occupant on child's optional jump seat at +96. |
Maximum baggage | 120 lbs. | At +95. |
Fuel capacity | 42 gal. total, 38 gal. usable (two 21 gal. tanks in wings at +48) | See Note 1 for data on unusable fuel |
Oil capacity | 2 gal. (-14.0), 1-1/2 gal. usable | See Note 1 for data on un-drainable oil |
Wing flaps | Takeoff 0° to 10° Landing 0° to 40° | |
NOTES: | 1) The certified empty weight and corresponding center of gravity location must include unusable fuel of 24 pounds at (+46) and full oil of 11.3 pounds at (-14). | |
