Center Of Gravity Limits; Maneuver Limits; Flight Load Factor Limits; Kinds Of Operation Limits - Cessna 182Q 1979 Pilot Operating Handbook

CESSNA
MODEL 182Q
NOTE
SECTION 2
LIMITATIONS
The maximum combined weight capacity for baggage
areas A and B, including the hatshelf, is 200 lbs. The
maximum hatshelf load is 25 lbs.
CENTER OF GRAVITY LIMITS
Center of Gravity Range:
Forward: 33.0 inches aft of datum at 2250 lbs. or less, with straight line
variation to 39.5 inches aft of datum at 2950 lbs.
Aft: 48.5 inches aft of datum at all weights.
Reference Datum: Front face of firewall.
MANEUVER LIMITS
This airplane is certificated in the normal category. The normal
category is applicable to aircraft intended for non-aerobatic operations.
These include any maneuvers incidental to normal flying, stalls (except
whip stalls), lazy eights, chandelles, and steep turns in which the angle of
bank is not more than 60°.
Aerobatic maneuvers, including spins, are not approved.
FLIGHT LOAD FACTOR LIMITS
Flight Load Factors:
*Flaps Up: +3.8g, -1.52g
*Flaps Down: +2.0g
*The design load factors are 150% of the above, and in all cases, the
structure meets or exceeds design loads.
KINDS OF OPERATION LIMITS
The airplane is equipped for day VFR and may be equipped for night
VFR and/ or IFR operations. FAR Part 91 establishes the minimum
required instrumentation and equipment for these operations. The refer-
ence to types of flight operations on the operating limitations placard
reflects equipment installed at the time of Airworthiness Certificate
issuance.
Flight into known icing conditions is prohibited.
1 October 1978 2-7