SECTION 2 CESSNA
OPERATING LIMITATIONS MODEL 208B (867 SHP)
GARMIN G1000
U.S.
FAA APPROVED
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
Maximum Takeoff Weight . . . . . . . . . . . . . . . . . 8807 Pounds (3994 kg)
*Flaps UP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . +3.8g, -1.52g
*Flaps LAND (All Settings). . . . . . . . . . . . . . . . . . . . . . . . . . . . +2.4g
*The design load factors are 150% of the above, and in all cases,
the structure meets or exceeds design loads.
FLIGHT CREW LIMITS
One pilot required in left seat.
208BPHCUS-01
2-14
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