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The exterior lights master switch on the outboard throttle
must be on for any exterior light to l?mction (except
for approach lighta). The pilot light control panel is
shown in Figure 2-129. A two-channel flasher unit is
used for flashing lights. One channel flashes the anticollision
and position lights and has circuit protection f?om
the ANTICOLUXJPP POSiPOS LTS circuit breaker
(211). The second flasher channel flashes the AOA indexer
and approach lights and has circuit protection
from the ANGLE OF ATTK IND AC circuit breaker
(3F3).
Note
The anticollision, position, and supplementary
position, formation, and taxi lights are
inoperative when operating on emergency
generator.
2.39.1.1 Position Lights. The position lights consist
of a red light on the left wingtip, a green light on the
right wingtip, and a white position light in the left fin
cap assembly. Supplemental position lights include. upper
and lower red lights on the leg wing glove and upper
and lower green lights on the right wing glove. When
the wind-sweep angle is forward of 25”, the wingtip
position lights are operational; when the wings are swept
all of 25”, the wingtip position lights are disabled and
the glove position lights are operational. When operating
in steady mode with the nosegear down and locked
and the wings forward of 25’, both the wingtip position
lights and the glove position lights are operational. The
position lights are powered tiom the right main ac bus
through the exterior lights master relay.
Note
When the anticollision lights are on, the
flasher for the position lights is disabled and
the lights revert to steady.
2.39.1.2 Anticollislon Lights. There are three red,
flashing anticollision lights. One anticollision light is
installed in the bottom of the inframd pod on the lower
forward fuselage. Another anticollision light is installed
in the top forward part of the left vertical stabilizer. The
third anticollision light is on the top aft part of the right
vertical stabilizer and directs its anticollision beacon up
and down.
The lower fuselage forward anticollision light remainsoffduringtakeoffandlandingwiththenosewheel
door open. With the nosewheel door closed, the lower
tirselagef orward anticollision light will operatew ith the
ANTI COLLISION light switch set to ON. The anticolliiionlights
are powered throughthe right mainbus with
circuit protection on the RIO ac right main circuit
breaker panel TAXI/FORM LT (3A2).
2.39.1.3 Formation Lights. The formation lights
consist of wingtip lights on each wing, fuselage lights,
and vertical fin tip lights on both sides of the aircraft.
All formation lights are green. Intensity of the lights
is controlled by the FORMATION thumbwheel on the
MASTER LIGHT panel. Electrical power is supplied
through the right main bus with circuit protection on the
RIO ac right main circuit breaker panel TAXI/FORM
LT (3A2).
2.39.1.4 Taxi Light. The taxi light installed on the
nosewheeils a fixed-position light. A limit switch ont he
nosegear door will turn the light off when the gear is
retracted. A two-position, ON and OFF, switch is on the
MASTER LIGHT panel. Electrical power is supplied
through the right main bus with circuit protection on the
RIO circuit breaker panel TAXI/FORM LT (3A2).
2.39.2 Interior Lights. The interior lighting of the
cockpit consists of red instrument panel and console
panel lights, red and white floodlights for additional
console and instrument panel lighting, and utility/map
lights for each flightcrew station. At the pilot station, the
interior lights are controlled from the MASTER LIGHT
panel on the right outboard console. The RIO can control
the interior lighting tirn the interior light panel on the
RIO right outboard console.
2.39.2.1 Instrument and Console Panel
Lights. All flight instrnme.ntsin the pilot and RIO instrument
panel and console panel lights are lighti by
white lighting. Individual thumbwheel controls are
2-251 ORIGINAL
NAVAIR 0%FlUADFigure
2-129. Cockpit Light Chtrols (Sheet 1 of 3)
2.252
NAVAIR OI-F14AA~-~
NOMENCLATURE FUNCTION
@ b.~;iOLLlSION light ON and OFF - Energizes or deenergizes the anticollision lights. When
anticollision lights are on, the flasher unit for the position
lights is disabled.
@ F’z’;fON lights flasher FLASH - Causes the wing or supplementary tail and position lights
to operate in a flashing mode with landing gear up. With
gear down supplementary lights operate steady only.
STEADY - With the wing and tail (or either) position lights on, lights
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F-14D 飞行手册 Flight Manual 1(181)
