Descent; Approach And Landing; Stopping Engine - Piper Dakota PA-28-236 Pilot Operating Handbook

SECTION 4
NORMAL PROCEDURES

DESCENT

NORMAL
Throttle .................................................................. as required for 1000 FPM
Propeller ........................................................................................2400 RPM
Airspeed .........................................................................................137 KIAS
Mixture .....................................................................................................rich
Carburetor heat ......................................................................... on if required
POWER OFF
Carburetor heat ......................................................................... on if required
Throttle .................................................................................................closed
Airspeed ....................................................................................... as required
Mixture ......................................................................................... as required
Power ...................................................................... verify with throttle every

APPROACH AND LANDING

Fuel selector .................................................................................proper tank
Seat backs ............................................................................................... erect
Belts / harness ...........................................................................fasten / adjust
Electric fuel pump .................................................................................... ON
Air conditioner.........................................................................................OFF
Mixture ...................................................................................................... set
Propeller .................................................................................................... set
Flaps .......................................................................... down - 102 KIAS max.
Trim to 72 KIAS.

STOPPING ENGINE

Flaps .................................................................................................... retract
Electric fuel pump ...................................................................................OFF
Air conditioner.........................................................................................OFF
Radios ......................................................................................................OFF
Propeller ............................................................................... full INCREASE
Throttle ................................................................................................ full aft
Mixture ......................................................................................... idle cut-off
Magnetos .................................................................................................OFF
Master switch...........................................................................................OFF
REPORT: VB-910
4-10
PIPER AIRCRAFT CORPORATION
ISSUED: JUNE 1, 1978
REVISED: NOVEMBER 20, 1981
PA-28-236, DAKOTA
descent
30 seconds