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Piper PA-28-161 Maintenance Manual

Piper PA-28-161
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PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 1
Nov 30/06
2K9
28-40-00
INDICATING
1. Standard Installation
A. Description
The Warrior III fuel quantity gauge is a dual instrument (two indicators in one case), calibrated in
fractional divisions of 0, 5, 10, 15, 20 (gallons), and F (FULL). A transmitter unit (i.e. - sender),
comprising a resistance strip and a movable control arm, is installed in each fuel tank. The arm
position is controlled by a float in the fuel tank. The float position is transmitted electrically to the
indicator needles, which move to show the amount of fuel in each tank.
Gauge removal and installation instructions are found in 39-10-00.
B. Troubleshooting.
Troubles unique to the fuel indicating system are listed in Chart 1 along with their probable causes
and likely remedies.
C. Fuel Quantity Transmitter Unit (i. e. - Sender)
(1) Removal
(a) Remove fuel tank. (See Fuel Tank - Removal, 28-10-00.)
(b) Disconnect transmitter wire from the connection post.
(c) Cut the safety wire securing the five attaching screws.
(d) Remove the five attaching screws. Remove the transmitter unit.
(2) Installation
(a) Position transmitter and gasket to the fuel tank. Secure with five machine screws and
washers.
(b) Safety the machine screws with MS20995-C32 wire.
(c) Connect transmitter wire to the connection post.
(d) Install the fuel tank. (See Fuel Tank - Installation, 28-10-00.)

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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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