Arrow PA-28R-201 Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 168

Sn 2837001 and up
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SECTION 7
DESCR/OPERATION
7.17 ELECTRICAL SYSTEM
PIPER AIRCRAFT CORPORATION
PA-28R-20I, ARROW
All switches are grouped in a switch panel above the power quadrant.
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The circuit breaker panel is located on the lower right side of the instrument
panel. Each breaker is clearly marked to show which circuit it protects. Also,
circuit provisions are made to handle the addition of communications and
navigational equipment.
Standard electrical accessories include alternator, starter, electric fuel
pump, stall warning horn, ammeter, and annunciator panel.
The annunciator panel includes alternator, low oil pressure, and low
vacuum indicator lights. The annunciator panel lights are provided only as a
warning to the pilot that a system may not be operating properly, and that he
should check and monitor the applicable system gauge to determine when or
if action is required.
Optional electrical accessories include navigation, ground recognition.
anti-collision, landing. instrument panel, and cabin dome lights. The
navigation lights are controlled by a rocker switch on the main switch panel.
Radio, panel, and switch lights are controlled by rheostat switches located
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below and to the right of the pilot's control wheel adjacent to the engine
instruments.
An optional light, mounted in the overhead panel, provides instrument
and cockpit lighting for night flying. The light is controlled by a rheostat
switch located adjacent to the light. A map light window in the lens is
actuated by an adjacent switch.
The optional wing tip recognition light consists of two lights, one in each
wing tip, and is operated by a rocker type switch in the main switch panel.
WARNING
The navigation lights (NAY L1GHn switch
must be off to obtain full intensity gear lights
during daytime flying. When the airplane is
operated at night and the NAY LIGHT switch
is turned on, the gear lights will automatically
dim.
The anti-collision and landing lights are controlled by rocker switches
on the main switch panel.
REPORT: VB-1365
7-14
ISSUED: SEPTEMBER 15, 1988
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