Piper ARCHER II - Spin Recovery

PIPER
AIRCRAFT
CORPORATION
SECTION
3
PA-28-181,
ARCHER
II
EMERGENCY
PROCEDURES
ELECTRICAL
OVERLOAD
(Alternator
over
20
amps
above
known
electrical
load)
FOR
AIRPLANES
WITH
SEPARATE
BAT
AND
ALT
SWITCH
OPERATION
ALT switch ...... cece cece cece cece eeuscuccceteresens Laaeee ON
BAT switch .......... cc cece cc cee cancceccccecurctcuncveececs OFF
If alternator loads are reduced:
Electrical load ...... 0.0 cc cc cece ccc ect neeteaees Reduce to Minimum
Land as soon as practical.
NOTE
Due to increased system voltage and radio
frequency noise, operation with ALT switch
ON and BAT switch OFF should be made only
when required by an electrical system failure.
If alternator loads are not reduced:
ALT switch 0... 0. ccc ccc cece cece cnc neceecceectucccuneasceens OFF
BAT Switch ...... 2c cece cece eset cece cenecnurecnaces As required
Land as soon as possible. Anticipate complete electrical failure.
SPIN RECOVERY
Throttle 2... ccc cece cece eee cece cee cure enreeuesecenenas idle
Ailerons 2.2... 00. cece eee e ence cece cece enveneuccuucueeene neutral
Rudder... .. ccc ccc ccc cece ee ee ree ecenseeees full opposite to
direction of rotation
Control wheel ........ cece cee cece cece cece ee ec cesses full forward
Rudder... ccc ccc cece cece cece cet ee ees eeeeeunnees neutral (when
rotation stops)
Control wheel .. 2.0... ce cece ee eee tee eens as required to smoothly
regain level flight altitude
ISSUED: JULY 2, 1979 REPORT: VB-1120
REVISED: JANUARY 14, 1981 3-7