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

Flashing when an AAA radar firing signal is detected.
Indicates a continuous wave emitter is detected.
Steady illumination indicates an airborne interceptor tracking is detected.
Flashes when any caution light on the RID’s CAUTION ADVISORY panel
illuminates.
@ g%y
CABIN PRESS
(caution)
FUEL LOW
(caution)
Indicates DD and/or TID controls and displays are overheating.
Indicates aircraft cabin pressure has dropped below &psi pressure
differential or cockpit altitude is above 27,000 feet.
Indicates fuel thermistors uncovered in aft and left or forward and right fuel
feed group (approximately 1,000 pounds) remaining in individual fuel feed
group.
B/U OXY LOW
(caution)
Indicates backup oxygen system pressure is 200 psi or less.
CANOPY
(caution)
Indicates that canopy is not in down and locked position.
Figure 2-131. RIO Indicator Lights (Sheet 2 of 3)
2-261 ORIGINAL
m Il.” I I”..
Indicates either seat is in the SAFE position.
RDR ENABLED
(caution)
READ MFD
(caution)
Indicates that radar operation on the ground is possible or failure of right
main landing gear safety switch or wiring.
Indicates any or all of the following warning, caution, or advisory legends
that appear on the upper left corner of the MFD.
SDU ALARM IMU
ASPJ HOT CIU HOT
JTID HOT DPl HOT
RWR DP2 HOT
FWD ASPJ SMS HOT
AFT ASPJ AFT CG
MCI HUD HOT
MC2 RWR HOT
MC1 HOT DSS HOT
MC2 HOT DEKI HOT
CIU IRST HOT
INS
BINGO
(caution)
Indicates total fuel quantity indicator is less than BINGO preset value.
SENSOR COND
(advisory)
Indicates coolant temperature exiting heat exchanger is 104”F, radar
coolant pump output pressure is below 60 psi, or the overtemperature
switch has shutdown the coolant pump.
COOLING AIR
(advisory)
Indicates an overtemperature condition exists in the electronic forced air
cooling system. With degraded cabin pressure or flow, indicates possible
bleed duct failure forward of primary heat exchanger and 400” modulating
valve.
OBOGS
(caution)
Indicates a switchover to backup oxygen or OBOGS switch OFF
SAHRS
(advisory)
Indicates attitude or heading information from SAHRS is unreliable.
Figure 2-13 1. RIO Indicator Lights (Sheet 3 of 3)
ORIGINAL 2-262
NAVAIR 01.F14AAD-1
Radiation hazard exists on deck when the
RDR ENABLED caution light is illmninated.
The light indicates that the RADAR
TEST ENABLE switch (maintenance
switch) is in the “A” (radiate and scan) position.
This condition permits the weight-onwheels
interlock to be bypasseda, llowing the
tmnsmitter to radiate out the antenna when
RADAR XMIT is selected on the hand control
unit. Illumination of the light does not
indicate a weight-on-wheels failure.
2.39.3.1 MASTER CAUTION Light. The pilot
MASTER CAUTION light is centrally located on the
master caution/master arm control panel, and, in the aft
cockpit, the RIO MASTER CAUTION light is on the
left instrument panel. When the lights are illuminated,
yellow letters show on an opaque background. Individual
MASTER CAUTION lights flash whenever a caution
light on the respective caution and advisory panel
illuminates. A MASTER CAUTION light may be
turned off by depressing its lens. This will activate a
reset switch that rearms the master circuit for a subsequent
caution light. A caution light lit on the caution
and advisory panel willnotbetumed offbyresettingthe
MASTER CAUTION light.
2.39.3.2 Indicator Lights Test. Acheckofallindicator
lights can be performed while airborne or during
on-deck operations. The pilot caution and advisory
lights, the MASTER CAUTION light, and all associated
circuitry are tested through the MASTER TEST panel.
The test is initiated by selecting LTS and pressing the
master test knob. Electrical power is routed through the
circuitry to provide simulated failure signals to the caution
and advisory lights. Illumination of each warning,
caution, and advisory light verifies proper continuity of
the indicator lights. A malfunction is indicated by failure
of a light to illuminate.
Illumination of any caution light causes the MASTER
CAUTION light to flash. If the MASTER CAUTION
light illuminates steadily during the LTS test, it
indicates a failure of the MASTER CAUTION light,
primary power failure, failure of the flasher module, or
that failure has been detected by the BIT circuits.
The following indicator lights are also illuminated by
　
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(185)