CESSNA SECTION 4 - NORMAL PROCEDURES
MODEL 182T FAA APPROVED
ELEVATOR TRIM
A neutral index mark is added to the pedestal cover which cor-
responds to the zero degree trim tab position. As loadings vary to-
wards the forward C.G. limit, elevator trim settings towards the nose
up and nose down ends of this takeoff range, respectively, will pro-
vide comfortable control wheel forces during takeoff and initial climb
out.
LANDING LIGHTS
If landing lights are to be used to enhance the visibility of the
airplane in the traffic pattern or enroute, it is recommended that only
the taxi light be used. This will extend the service life of the landing
light appreciably.
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
runup 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, it
is very important that the throttle be advanced slowly. This allows
the airplane to start rolling before high RPM is developed, and the
gravel will be blown back of the propeller rather than pulled into it.
Prior to takeoff from fields which require maximum performance,
the mixture should be leaned to the fuel flow values provided on the
Maximum Power Fuel Flow placard in a full throttle, static runup.
After full throttle is applied, adjust the throttle friction lock
clockwise to prevent the throttle from creeping back from a
maximum power position. Similar friction lock adjustments should
be made as required in other flight conditions to maintain a fixed
throttle setting.
Feb 23/01 4-23
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