SECTION 2
OPERATING LIMITATIONS
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.
2-14
U.S.
CESSNA
MODEL 208B (867 SHP)
GARMIN G1000
FAA APPROVED
208BPHCUS-01