Piper PA 28-181 User Manual

PIPER AIRCRAFT CORPORATION
PA-2&181, ARCHER ll
sEcTtoN 3
EMERGENCY PROCEDURDS
3.3 EMERGENCY PROCEDURES CHECK LIST
ENGINE FIRE DURING STÄRT
Starter
,.. .. ,.... .. .. . ... .. .. ,
crank engine
Mixtur€ ,.. ... .. .. ,. . . .. ........ idle cut-off
Throttl€ ... ..,.. .. ,. . . .. .... ...... ... open
Electric fuel
pump
... ... ....... ..... ...
OFF
Fuel
selector ... ,.. ,... .. .. .. ... ... ...
OFF
Abandon if fir€ continucs.
ENGINE POWER LOSS DURING TAKEOFF
If sufficicnt runway rcmains for a normal landing,
land straight ahcad.
If insufficient
runway remains:
Maintgin safe airspecd.
Make only shallow turn to
avoid
obstructions.
Flaps as situation r€quires.
If sufficient
altitude has been
gained
ro attempt
a
restart:
Maintain safe airspe€d.
Fu€l s€lector
swtch to tank
containing fuel
Electric fuel
pump
. ... .. . .. ...
.. ,, ch€ck ON
Mixture ... .. ... .. .. ..
. . .. ..
..,check RICH
Carburetor h€at
.. ....
.. .. ,. , ... .......
ON
Primer .. .. .. ... .. .. ..
. . .... . ..
,,.. .
locked
If
power
is not regained,
proceed
with
power
off landing.
ISSUED:
JULY 2, 1979
REVISEDT
MAY 29. l9t0
REPORT: VB-1120
3.3

Piper PA 28-181 Specifications

General

Manufacturer	Piper Aircraft
Engine	Lycoming O-360-A4M
Horsepower	180 hp
Wingspan	35 ft 6 in (10.82 m)
Height	7 ft 3 in (2.21 m)
Maximum Takeoff Weight	2, 550 lb (1, 157 kg)
Seating	4
Service Ceiling	14, 100 ft
Fuel Capacity	50 US gal (190 L)
Propeller	Fixed Pitch