SECTION 3
PIPER AIRCRAFT CORPORATION
EMERGENCY PROCEDURES
PA-28-236, DAKOTA
REPORT: VB-910
ISSUED: JUNE 1, 1978
3-8
REVISED: FEBRUARY 2, 1981
ENGINE ROUGHNESS
Carburetor heat ......................................................................................... ON
If roughness continues after one min:
Carburetor heat ........................................................................................OFF
Mixture ................................................................adjust for max. smoothness
Electric fuel pump .................................................................................... ON
Fuel selector ............................................................................... switch tanks
Engine gauges ........................................................................................check
Magneto switch................................................................L then R, then Both
If operation is satisfactory on either one, continue on that magneto at
reduced power and full “RICH” mixture to first airport.
Prepare for power off landing.
PROPELLER OVERSPEED
Throttle ................................................................................................. retard
Oil pressure............................................................................................check
Prop control ................................................................. full DECREASE rpm,
then set if any
control available
Airspeed .............................................................................................. reduce
Throttle ......................................................................... as required to remain
below 2400 rpm
Summary of Contents for PA-28-236 DAKOTA
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