CESSNA
SECTION 4
MODEL T182T NAV III
NORMAL PROCEDURES
GFC 700 AFCS
U.S.
BEFORE TAKEOFF
(Continued)
ELEVATOR TRIM
The elevator trim tab is in the takeoff position when the trim pointer is
aligned with the index mark on the pedestal cover. Adjust the trim
wheel during flight as necessary to make control wheel forces more
neutral.
LANDING LIGHTS
It is recommended that only the taxi light be used to enhance the
visibility of the airplane in the traffic pattern or enroute. This will extend
the service life of the landing light.
TAKEOFF
POWER CHECK
It is important to check full throttle engine operation early in the takeoff
roll. Any sign of rough engine operation or sluggish engine acceleration
is good cause for discontinuing the takeoff. If this occurs, you are
justified in making a thorough full throttle static run-up before another
takeoff is attempted. The engine should run smoothly and turn
approximately 2350 - 2400 RPM.
Full throttle run-ups over loose gravel are especially harmful to
propeller tips. When takeoffs must be made over a gravel surface,
advance the throttle slowly. This allows the airplane to start rolling
before high RPM is developed, and the gravel will be blown behind the
propeller rather than pulled into it.
On the first flight of the day when the throttle is advanced for takeoff,
manifold pressure will normally exceed 32 in.hg. and fuel flows will
exceed 24 GPH if the throttle is opened fully. On any takeoff, the
manifold pressure should be monitored and the throttle set to provide
32 in.hg.; then, for maximum engine power, the mixture should be
adjusted as required, during the initial takeoff roll to 24 GPH fuel flow.
(Continued Next Page)
T182TPHBUS-00
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