Transmitter/Fuel Gauge Tolerances - Piper CHEROKEE WARRIOR PA-28-151 1995 Maintenance Manual

Airplane
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PIPER CHEROKEE WARRIOR SERVICE MANUAL
5. Connect external power supply unit. Connect the red (positive) lead to the starter solenoid
heavy terminal which is not connected to the starter.
6
Adjust power supply unit to provide 13.5 to 14.5 Vdc. Allow gauges to warm-up for a
m i n imum of three minutes.
Connect a wire to the sender side of each gauge. To read gauge
ground wire momentarily to airframe through a 200
tor at the 0 and 5 gallon positions; through a 35
the 10 through 20 gallon positions; no resistor at the full (25
gallon) position.
Place one U. S. gallon of fuel in each tank. Momentarily ground wire through a 200 Ω resistor
7
to airframe.
8. After needle on each gauge descends to a stable reading (:15 seconds minimum), observe fuel
quantity gauge. It should read empty. (Refer to chart 2802 for tolerances permitted between fuel gauge reading
and actual fuel in tank.)
9 . Add fuel to tank in five U.S. gallon increments until tank is full. Ground wire through
a p p r opriate resistor to airframe. Check gauge readings.
To obtain specified tolerances, adjust float assembly per
instructions given in Paragraph 9-15, .
TABLE IX-I. TRANSMITTER/FUEL GAUGE TOLERANCES
Actual Fuel in
Tank (U.S. Gal)
Full
20
15
10
b . To check PA-28-151 and P28-161, Warrior II with Stewart Warner or Rochester fuel quantity
t r a n smitter unit and gauges:
Rochester sending units are not compatible with A. C .
Sparkplug or Stewart Warner gauges. Rochester gauges must
be used with Rochester sending units
1. Pre-installation check:
Added: February 28, 1995
— NOTE —
NOTE
MAIN TANK
5
0
CAUTION
2A18
Island Enterprises
resis -
resistor at
Gauge Reading
(U.S. Gal)
22 to Full*
17 to 24
12 to 17
7 to 12
2 to 6
0 to -2
*Plus one needle width
FUEL SYSTEM

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