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Page 11 of 25 |
3A12 - Revision 63 - CESSNA AIRCRAFT COMPANY
Engine |
Lycoming O-320-D2J |
|
*Fuel |
100LL/100 minimum grade aviation gasoline |
|
*Engine limits |
For all operations, 2700 rpm (160 hp) |
|
Propeller and propeller limits |
1. Propeller |
|
*Airspeed limits |
Maneuvering |
99 knots (landplane) |
(See Note 4 on use of CAS) |
Maximum structural cruising |
127 knots |
Never exceed |
158 knots |
|
C.G. range |
Landplane: |
(+39.5) to (+47.3) at 2400 lbs. |
|
Utility category |
(+36.5) to (+40.5) at 2100 lbs. |
Seaplane: (Edo 89-2000 or 89A2000 floats) |
(+39.8) to (+45.5) at 2220 lbs. |
|
|
Straight line variation between points given. |
|
Empty weight C.G. Range |
None |
|
*Maximum weight |
Normal category: |
2400 lb. (landplane); 2220 lb. (seaplane) |
Utility category: |
2100 lb. (landplane) |
|
Number of seats |
4 (2 at +34 to +46, 2 at +73) (Occupant on child's optional jump seat at +96) |
|
Maximum baggage |
120 lb. at +95 |
|
Fuel capacity |
42 gal. total, 40 gal. usable (two 21.5 gal. tanks in wings at +48) |
|
Oil capacity |
2 gal. (-13.1), 3.5 gal. usable |
|
Control surface movements |
Wing flaps |
Takeoff 0° - 10° |
|
Ailerons |
Up 20° ±1° |
Elevator tab |
Up 28° +1°, -0° |
|
|
Elevator |
Up 28° +1°, -0° |
|
Rudder |
Right 16° ±1° |
Serial numbers eligible |
17274010 through 17275034 (1981 model) |
|
X. Model 172Q, Cutlass, 4 PCLM (Normal Category), approved October 15, 1982
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