Piper PA 28-181 User Manual

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
Mixture
, , , . . . . . . . . . . .
...........,...
RICH
Carburetor
heat
.. ......
.. ......
, ,.. ...
ON
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:
Carburetor hcat
,. ,. .. .. ..
, ,.. ....
,,..
OFF
Elcctric fuel
pump
. ,. .. .. ...
.... ....
.. OFF
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:
lgnition
.. ...
, ....... .
.. ...
.... .,..
..
OFF
Master switch
. .
.. . .... .. .
.. ..... ...
.. oFF
Fuel sclcctor
..........,.......,,.....
OFF
Mixtur€
.. ,.. . ....
....
.. ... .
.... idle
cut-off
S€at b€lt
and harness.
,.
. .. ....
.... ..,
, .light
REPORTT
Vllr20
T4
IssUEDr
JULY
4
1979

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