Spin Recovery; Open Door; Carburetor Icing - Piper Dakota PA-28-236 Pilot Operating Handbook

PIPER AIRCRAFT CORPORATION SECTION 3
PA-28-236, DAKOTA EMERGENCY PROCEDURES
If alternator loads are not reduced
ALT switch ..............................................................................................OFF
BAT switch ................................................................................... as required
Land as soon as possible. Anticipate complete electrical failure.

SPIN RECOVERY

Rudder ....................................................................................full opposite to
direction of rotation
Control wheel .................................................................... full forward while
neutralizing ailerons
Throttle ...................................................................................................close
Rudder .............................................................. neutral (when rotation stops)
Control wheel ............................................................as required to smoothly
regain level flight attitude

OPEN DOOR

If both upper and side latches are open, the door will trail slightly open and
airspeeds will be reduced slightly.
To close the door in flight:
Slow airplane to 83 KIAS.
Cabin vents .............................................................................................close
Storm window......................................................................................... open
If upper latch is open .............................................................................. latch
If side latch is open ...................................................... pull on arm rest while
moving latch handle to
latched position.
If both latches are open ........................................................... latch side latch
then top latch

CARBURETOR ICING

Carburetor heat ......................................................................................... ON
Mixture ................................................................adjust for max. smoothness
ISSUED: JUNE 1, 1978 REPORT: VB-910
REVISED: FEBRUARY 2, 1981 3-7