Piper PA 28-181 Manual page 20

Archer iii
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SECTION 3
PTPER AIRCRAFT CORPORATTON
EMERGENCY PROCEDURES
PA-2t.IEI, ARCHER II
ENGINE POWER LOSS IN FLIGHT
Fuel sclcctor
switch to tank
Erectric
rüer pump
. .. .. .. ::::i':l::3il
M i x t u r e , , , . . . . . . . . . . .
. . . . . . . . . . . , . . . R I C H
C a r b u r e t o r
h e a t
. . . . . . . . . . . . . . . . , , . . . . . O N
Engine gaugcs. .... .,..
.. . check for indication
primer...........,..
.:i::::::i:"'üi1T
Ifno fuel pressure is indicated, check tank selector positionto be sur€ i( is on
a tank containiDg fuel.
When pow.r i5 restored:
C a r b u r e t o r
h c a t
, . , . . . . . . . , , . . . . . . , , . . O F F
E l c c t r i c f u e l p u m p
. , . . . . . . . . . . . . . . . . . . O F F
If power is nor restored prepare for power ott landinS.
Trim for 76 KIAS
POWER OFF LANDING
Locatc suitable ficld.
Establish spiral patrern.
i000 ft. abo!c fieldat_do*nwind posirion for normal landing approach.
whcn ficld can casily be reached dow to 66 K|AS for shonel ünding.
Touchdowns should normally b€ made at lowest possible airspeed wirh full
flaps.
Whcn commitred ro landing:
l g n i t i o n . . . . . , . . . . . . . .
. . . . . . . . . . , . . . . O F F
M a s t e r s w i t c h
. . . . . . . . . . . . . . . . . . . . . . . . o F F
F u e l s c l c c t o r
. . . . . . . . . . , . . . . . . . , , . . . . . O F F
M i x t u r € . . , . . . . . . . . . . .
. . . . . . . . . . i d l e c u t - o f f
S € a t b € l t a n d h a r n e s s . , .
. . . . . . . . . . . . . , , . l i g h t
REPORTT Vllr20
T4
IssUEDr JULY 4 1979

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