曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

either crewmember to use the light as a signal lamp. The
utility and map lights are supplied electrical power from
the ac essentiaNl o. 2 bus anda rep rotectedb y the UTILITY
LTS circuit breaker (3A6).
2.39.3 Warning and Indicator Lights. Warning,
caution, and advisory lights (Figures 2-130 and 2-
13 1) are provided in both cockpits to alert the pilot
and RIO of aircraft equipment malfunctions, unsafe
operating conditions, or that a particular system is in
operation.
Warning lights illuminate red with black letters to
warn of hazardous conditions that require immediate
corrective action. Caution lights show yellow letters
on an opaque background to indicate an impending
dangerous condition. The lower halfofthe CAUTION
ADVISORY panel consists of advisory lights that
show green letters on opaque background. Advisory
lights indicate degraded operations that may require
corrective action.
ORIGINAL 2.254
NAVAIR Ol-F14AAD-I
Figure Z-130. Pilot Indicator Lights (Sheet 1 of 5)
2-255 ORIGINAL
NAVAIR 0%F14AAD-1
NOMENCIATURE I FUNCTION
0 SAM Steady illumination when a surface-to-air missile tracking radar is
(warning) detected. Flashing when a missile has been launched.
AM Steady illumination when an anti-aircraft tracking radar is detected.
(warning) Flashing when an AAA radar firing signal is detected.
cw Indicates continuous wave emitter detected.
(warning)
Al Steady illumination indicates an airborne interceptor tracking is detected.
(warning)
0
WHEELS Flashes with flaps down more than IO”, either throftle below approximately
(warning) 55%, and any landing gear not down and locked.
BRAKES Indicates antiskid failure or failure of priority valve in the brake power
(warning) module to switch to combined hydraulic system (operating in AUX brake
mode). Illuminates when parking brake is pulled.
ACLSIAP
(caution)
NWS ENGA
(caution)
AUTO THROT
(caution)
@ KiOry)
@ EEi)
0
HOT TRIG
(warning)
@ El;; CAU-mN
@ zning)
@
EMERG STORES
JEI-DACK
(warning)
Auto pilot and automatic carrier landing system mode disengaged.
Indicates nosewheel steering is engaged and will respond as a function of
rudder pedal displacement. Automatically centers with hook down.
Indicates APC has been disengaged by means other than the THROTTLE
MODE switch.
Indicates radar locked on target.
Indicates target meets specified fAR requirements.
Indicates that firing logic conditions are available. Pilot’s trigger or bomb
button and RIO’s launch butfon will fire or release ordnance when
actuated.
Flashes when any light on the pilot’s CAUTION ADVISORY panel
illuminates.
Fire/overheat condition in engine nacelle.
Indicates EMERG STORES JETT pushbutton is activated.
Note
The following lights on the CAUTION ADVISORY
panel are in alphabetical order
Figure 2-130. Pilot Indicator Lights (Sheet 2 of 5)
ORIGINAL 2-256
NAVAIR OW14AAD-1
NOMENCLATURE FUNCTION
@
AUTO PILOT Indicates failure of one or more pilot relief modes.
(caution)
AUX FIRE
Eisory)
Indicates low pressure (approximately 90 psi below the nominal 600 psi) in
the auxiliary fire extinguishing agent container.
BINGO
(caution)
Indicates total fuel quantity indicator is less than BINGO preset value.
BLEED DUCT
(caution)
Indicates bleed air leak sensing elements detect temperatures greater than
575°F between engine and primary heat exchanger. Also indicates hot air
leak detection (excess of 255” F) between primary heat exchanger and
ECB turbine compressor.
B/U OXY LOW
(caution)
Indicates backup oxygen system pressure is 200 psi or less.
CADC
(caution)
Indicates failure associated with air data computer.
ENG FIRE
Ex-r
(advisory)
Indicates low pressure (approximately 90 psi below the nominal 600 psi) in
the fire extinguishing agent container.
L ENG SEC
R ENG SEC
(caution)
FLAP
(caution)
Indicates augmenter fan temperature controller @FTC) is in secondary
mode. Afterburner is inoperative and thrust levels can vary from as rile as
65% to as much as 116% of primary mode MIL thrust.
Indicates: Disagreement between main and/or auxiliary flap position, or
asymmetry lockout. CADC failure. WG SWP DR NO. 2/MANUV FLAP (LEI)
circuit breaker pulled. Landing flaps down and airspeed greater than 225
knots.
L FUEL LOW
R FUEL LOW
(caution)
L FUEL PRESS
R FUEL PRESS
(caution)
Indicates fuel thermistors uncovered in aft and left or forward and right fuel
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：F-14D 飛行手冊 Flight Manual 1(183)