Piper PA 28-181 Manual page 23

PIPER AIRCRAFT CORPORATION SECTION 3
PA.2I-1t1, ARCHER II EMERGENCY PNOCEDURES
ELECTRICAL OVERLOAD (Altern tor ov.r 20 rmps rbovc krown
elecdc.l lo.d)
FOR AIRPLANES WITH SEPARATE BAT AND ALT SWITCH
OPERATION
A L T s w i t c h . . . . . . . . . . . . . . . . . . . . . . . . . . . O N
B A T s w i t c h . . . . . . . . . . . . . . . . . . . . . . . . . . O F F
If alt€rnator loads are reduccd:
Electrical load... , ,.. ,. . Reducc to Minimum
Iind as soon as practical,
NOTE
Du€ to increased system voltag€ and radio
frequcncy noise, operation with ALT switch
ON and BATswitch OFF shouldb€ madc only
wh€n required by an electrical system failure.
lf alternator loads are not reduced:
A L T s w i t c h . . . . . . . . . . .
. . . . . . . . . . . . . . . O F F
B A T s w i t c h . , . , , . . , . . ,
. . . . . . . . . A s r e q u i r e d
knd as soon as possible. Anticipare complete electrical failurc.
SPIN RECOVERY
T h r o t t l e . . . . . . . . . . . . . .
, . . . . . . . . . . . . . . . i d l e
A i l e r o n s . . . . . . . . , . . , , .
. . . . . . . . . . . . . n c u t r a l
Rudder . . . . . . . . . . . . . . .
...... full opposite to
direction of rotation
C o n t r o l w h e e l . . , . . . , . .
, . . . . . . . . f u u f o r u , a r d
R u d d e r . . . . . . . . . . . . . . .
. . , . . . . . n c u t r a l ( w h e n
rotation stopo
Control wheel . . , . . , . . , . . . . . . . . . . . . . . . . . , , . . as required to smoothly
regain level flight altitude
ISSUEDT JULY 2, 1979
REVISED: JÄNUARY 14, l9El
Rf,PORTT vFll20