ISSUED: JUNE 1, 1978
REPORT: VB-910
4-7
PIPER AIRCRAFT CORPORATION
SECTION 4
PA-28-236, DAKOTA
NORMAL PROCEDURES
REVISED: JULY 13, 1984
Proceed with normal start
Throttle ......................................................................... lowest possible RPM
External power plug ................................................ disconnect from fuselage
Master switch................................................................. ON - check ammeter
Oil pressure............................................................................................check
WARM-UP
Throttle .............................................................................1000 to 1200 RPM
TAXIING
Chocks .............................................................................................. removed
Taxi area ................................................................................................. clear
Parking brake ......................................................................................release
Throttle .......................................................................................apply slowly
Prop ................................................................................................high RPM
Brakes ....................................................................................................check
Steering..................................................................................................check
GROUND CHECK
Parking brake ............................................................................................. set
Propeller ............................................................................... full INCREASE
Throttle ..........................................................................................2000 RPM
Magnetos ..................................................... max. drop 175 RPM - max. diff.
50 RPM
Vacuum ......................................................................................5.0” Hg. + .
1
Oil temp .................................................................................................check
Oil pressure............................................................................................check
Annunciator panel ....................................................................... press-to-test
Air conditioner.......................................................................................check
Carburetor heat ......................................................................................check
Propeller .......................................................exercise ~ then full INCREASE
Electric fuel pump ...................................................................................OFF
Fuel pressure ..........................................................................................check
Throttle ................................................................................................. retard
Summary of Contents for PA-28-236 DAKOTA
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