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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
(a) McCauley 1C160/DTM 7553
Static rpm at maximum permissible throttle setting: Not over 2420, not under 2300
No additional tolerance permitted
Diameter: not over 75 in., not under 74 in.
(b) Spinner: Dwg. 0550320
2. Propeller (floatplane only)
(a) McCauley 1A175/ETM 8043
Static rpm at maximum permissible throttle setting:
Not over 2570, not under 2470
No additional tolerance permitted
Diameter: not over 80 in., not under 78.5 in.
(b) Spinner: Dwg. 0550320

*Airspeed limits
(CAS)

Maneuvering

99 knots (landplane)
96 knots (floatplane)

(See Note 4 on use of CAS)

Maximum structural cruising

127 knots

Never exceed
Flaps extended

158 knots
85 knots

C.G. range

Landplane:
Normal category

(+39.5) to (+47.3) at 2400 lbs.
(+35.0) to (+47.3) at 1950 lbs. or less

 

Utility category

(+36.5) to (+40.5) at 2100 lbs.
(+35.0) to (+40.5) at 1950 lbs. or less

Seaplane: (Edo 89-2000 or 89A2000 floats)
Normal category

(+39.8) to (+45.5) at 2220 lbs.
(+36.4) to (+45.5) at 1825 lbs. or less

 

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)
See Note 1 for data on unusable fuel.

 

Oil capacity

2 gal. (-13.1), 3.5 gal. usable

 

Control surface movements

Wing flaps

Takeoff 0° - 10°
Landing
0° - 30° +0°, -2°

 

Ailerons

Up 20° ±1°
Down 15° ±1°

Elevator tab

Up 28° +1°, -0°
Down 13° +1°, -0° (floatplane)
Up 22° +1°, -0°
Down 19° +1°, -0° (landplane)

 

Elevator
(Neutral position is with bottom of balance area flush with bottom of stabilizer.)

Up 28° +1°, -0°
Down 23° +1°, -0°

 

Rudder
(landplane)
(seaplane)
(Measured parallel to W.L.)

Right 16° ±1°
Left 16° ±1° (landplane)
Right 19° ±1°
Left 15° ±1° (seaplane)

Serial numbers eligible

17274010 through 17275034 (1981 model)
17275035 through 17275759 (1982 model)
17275760 through 17276079 (1983 model)
17276080 through 17276259 (1984 model)
17276260 through 17276516 (1985 model)
17276517 through 17276654 (1986 model)

 

X. Model 172Q, Cutlass, 4 PCLM (Normal Category), approved October 15, 1982

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