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CESSNA
MODELT210M
SECTION 2
LIMITATIONS
WEIGHT LIMITS
Maximum Takeoff Weight: 3800 lbs.
Maximum Landing Weight: 3800 lbs.
Maximum Weight in Baggage Compartment:
Baggage - Forward of wheel well on folded down aft seat (Station 89 to
110): 120 lbs.
Baggage
-
On and aft of wheel well (Station 110 to 152): 120 lbs.
CENTER OF GRAVITY LIMITS
Center of Gravity Range with Landing Gear Extended:
Forward: 37.0 inches aft of datum at 3000 lbs. or less, with straight line
variation to 42.5 inches aft of datum at 3800 lbs.
Aft: 53.0 inches aft of datum at all weights.
Moment Change Due To Retracting Landing Gear: +3207 lb. -ins.
Reference Datum: Lower portion of front face of firewaH.
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 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
2-7
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