Exterior; Removal And Installation Of Landing Light - Piper Dakota Maintenance Manual

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The OIL warning light is controlled by an oil pressure sensor switch incorporated in the oil line and is
located at the firewall. The sensor switch activates when oil pressure is below 35 psi.
The ALT warning light is illuminated by current flowing from the bus bar to the alternator circuit. This
condition exists when the alternator is not operating properly and output is zero. During normal operation, the
alternator warning circuit isalso supplied with power from the top diode terminal. This current flows through a
5amp fuse to the resistor and diode creating a condition which does not allow the warning light to light.
The test button is used to check operation of the lights when the engine is running. The lights will work
when the engine is not running, if the master switch is turned on.
Oil pressure sensor and vacuum sensor switches are similar in
looks and size. Ensure correct unit is installed per parts catalog
part number and description

EXTERIOR

GENERAL
The landing and taxi light is contained in one light bulb. It is a 100 watt unit located in the nose cowl. The
light is controlled by a switch and protected by a 10 amp circuit breaker. The three navigation lights are
controlled by a single switch and protected by a 10 amp circuit breaker. Optional anti-collision strobe lights are
mounted on each wing tip in the same assembly as the navigation lights. These units are rated to flash at
approximately 50 times per minute.
LANDING LIGHT

REMOVAL AND INSTALLATION OF LANDING LIGHT

l.
Remove screw securing clamp to bottom of lamp.
Take note of wire placement on lamp to facilitate reinstallation .
2. Pull lamp out and remove two electrical leads connected to it.
3. To install lamp, reconnect electrical leads and insert lamp into position. Position clamp at bottom and
secure with screw.
PIPER AIRCRAFT
PA-28-236
MAINTENANCE MANUAL
—NOTE—
Refer to chapter 71 if carburetor ice detector is installed.
—CAUTION—
—NOTE—
2D2
33 - 42 - 00
Page 33 - 05
Reissued: August 1, 1986

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