Cessna 402C - Page 26

(.~~402C
MANEUVER LIMITS
This is a normal category airplane.
spins, are prohibited.
SECTION 2
LIMITATIONS
Aerobatic maneuvers, including
Fuel Quantity:
FLIGHT LOAD FACTOR LIMITS
The design load factors are 150% of the following. and in all cases the
structure exceeds design loads.
At Design Takeoff Weight of 6850 Pounds:
a. Landing gear up, wing flaps 0
0
+3.6G to -1.44G
b. Landing gear down, wing flaps 450 D.OG to +2.0G
FLIGHT CREW LIMITS
Minimum Flight Crew for FAR 91 operations is one pilot.
OPERATION LIMITS
The standard airplane is approved for day and night operation under VFR
conditions. With the proper optional equipment installed. the airplane is
approved for day and night IFR operations and flight into icing conditions
as defined by the FAA.
FUEL LIMITATIONS
Fuel Pressure:
a. Minimum: 3.0 PSI (0 Pounds Per Hour)
b. Maximum: 18.5 PSI (214.0 Pounds Per Hour)
'1~ :; ..... (~~
a. Minimum fuel for takeoff is 20 gallons in each main tank.
Maneuvering Fuel:
a.
Due to possible fuel starvation, maximum side slip duration time is 30
seconds. The airplane is considered in a side slip anytime the turn and
bank II ball II is more than one half ball out of the center (coordinated
flight) position.
Fuel (Approved Fuel Grades And Colors):
PRIMARY - 100 (Formerly 100/130) Grade Aviation Fuel (Green).
ALTERNATE - 100LL Grade Aviation Fuel (Blue).
FAA Approved
1 November 1979
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