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Piper PA-28-161 User Manual

Piper PA-28-161
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SECTION
4
NORMAL
PROCEDURES
GROUND
CHECK
PIPER
AIRCRAFT
CORPORATION
PA-28-161, WARRIOR II
Throttle
..............................................
2000 RPM
Magnetos
..........•.........................
max. drop
175
RPM
-max. diff.
50
RPM
Vacuum
...........•...............................
4.8" - 5.1" HG
Oil temp
.....................................•.............
check
Oil pressure
................................................
check
Air conditioner
.............................................
check
Annunciator panel
....................................
press-to-test
Carburetor heat
.............................................
check
Engine
is
warm for takeoff when throttle can be opened without engine
faltering.
Electric fuel pump
..........................................
OFF
..
Fuel pressure
.............
,
..................................
check
Throttle . .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . retard
BEFORE
TAKEOFF
Master switch
...............................................
ON
Flight instruments
...........................................
check
Fuel selector
.........................................
proper tank
Electric fuel pump
...........................................
ON
Engine gauges
........................
...................•
check
Carburetor heat
.............................................
OFF
Seat backs
..............................•..................
erect
Mixture
..•.......•.....................•....................
set
Primer
.............•....•••...•.........•......•........••..
lock
Belts/ harness
.......................................
fastened/ check
Empty seats
..........................................
: . . seat belts
snugly fastened
Flaps
•.......................................................
set
Trim tab
..•..................................................
set
Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . free
Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . latch
Air conditioner
.............................................
OFF
REPORT:
VB-1180
4-8
ISSUED: AUGUST 13, 1982

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Piper PA-28-161 Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelPA-28-161 Warrior II
EngineLycoming O-320-D3G
Horsepower160 hp
Seating Capacity4
Wingspan35 ft (10.7 m)
Length24 ft 0 in
Maximum Speed127 knots
Cruise Speed122 knots
Maximum Takeoff Weight2, 325 lb (1, 055 kg)
Fuel Capacity48 US gallons (182 L)

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