Piper Dakota Maintenance Manual page 346

GENERAL
This chapter provides instructions for maintenance of the lighting equipment on this aircraft.
DESCRIPTION AND OPERATION
Electrical switches are located on the right center instrument panel, and the circuit breakers are located
on the lower right instrument panel. A rheostat switch on the left side of the switch panel controls the
navigational lights and radio lights. A similar switch on the right side controls and dims the panel lights.
The annunciator panel includes alternator and low oil pressure indicator lights. When the optional gyro
system is installed, the annunciator panel also includes a low vacuum indicator light.
A rotating beacon is locate on the vertical fin and anti-collision lights (strobe) are mounted on each wing tip.
TROUBLESHOOTING
When checking the lighting system, the master switch must be ON in order for the lights to operate.
Ensure the circuit breaker protecting the light being checked is pushed in.
PIPER AIRCRAFT
PA-28-236
MAINTENANCE MANUAL
2C22
33 - 02 - 00
Page 33 - 01
Reissued: August 1, 1986