Piper PA-28-236 DAKOTA, Pilot Operating Handbook

Page: 58 / 367

ISSUED: JUNE 1, 1978 REPORT: VB-910
3-7
PIPER AIRCRAFT CORPORATION SECTION 3
PA-28-236, DAKOTA EMERGENCY PROCEDURES
REVISED: FEBRUARY 2, 1981
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