Piper CHEROKEE CRUISER PA-28-140 Information Manual page 131

CHEROKEE CRUISER
8-2
8. The shape of the wing fuel tanks is such that in certain maneuvers the fuel may move
away from the tank outlet. If the outlet is uncovered, the fuel flow will be
interrupted and a temporary loss of power may result. Pilots can prevent inadvertent
uncovering of the outlet by avoiding maneuvers which could result in uncovering the
outlet.
Extreme running turning takeoffs should be avoided as fuel flow interruption
may occur.
Prolonged slips or skids which result in excess of 2000 feet of altitude loss, or
other radical or extreme maneuvers which could cause uncovering of the fuel outlet
must be avoided as fuel flow interruption may occur when tank being used is not full.
9. Anti-collision lights should not be operating when flying through overcast and clouds,
since reflected light can produce spacial disorientation. Do not operate strobe lights
when taxiing in the vicinity of other aircraft.
10. The rudder pedals are suspended from a torque tube which extends across the
fuselage. The pilot should become familiar with the proper positioning of his feet on
the rudder pedals so as to avoid interference with the torque tube when moving the
rudder pedals or operating the toe brakes.
11. In an effort to avoid accidents, pilots should obtain and study the safety related
information made available in FAA publications such as regulations, advisory
circulars, Aviation News, AIM and safety aids.
12. During letdown and low power flight operations, it may be necessary to lean because
of excessively rich mixture. Always go to full rich prior to landing sequence.
13. When leaning, careful observation of the temperature instruments should be practiced.
14. When alternate fuels are used, the engine should be run up to 1200 RPM for one
minute prior to shutdown to clean out any unburned fuel.
OPERATING TIPS
REVISED: APRIL 19, 1976