Piper PA 28-181 User Manual

PIPER ATRCRAFT
CORPORATION
PA-28.I8I,
ARCHER II
SECTION
4
NORMAL
PROCEDURES
WALK.AROUND
Figure 4-l
4.5 NORMAL PROCEDURES CHECK LIST
PRf,FLIGHT CHECK
Control wheel release
belts
Avronics . . .
.
. ,
. . . . .
,
.
.....,..........
OFF
Masrer switch .. . . .. .. .. . . ..
.... ..
.
.. ON
Fuel
quantity gauges
. . . . . . . . . . . . .
, . .
.
.
check
Masler
switch .
.. . . .. .. .. . . .. .... .. . .
OFF
Ignition .
. . . . . . . . . . . . .
................
OFF
Exterior
".
, ,.. ., . ,.. . .. ..
,
check
for damage
Control
surfaces . . .. . .. check
for int€rfercnce
-
free
of ic€, snow, frost
Hinges.. ,.
.. .. .. .. .
.
.
.. check for interf.rence
wings ... . . . . . . . . . . ..
. frce ofic€,
snow,
frost
Stall
warniog ... .. .. ..
.. ... . .. .,
.. .. , ,check
Fuel tanks . .. .. .. .. ..
.. .. .. .. . chcck supply
visually
-
secür€ caps
REPORT: VB-1120
+3
ISSUED: JULY T, 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