曝光台 注意防骗
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emergency oxygen.
6. CABIN PRESS switch - RAM/DUMP
7. OXY FLOW knob - OFF
8. OBOGS control switch - OFF
If AV AIR HOT caution appears -
9. Non-essential avionics equipment - OFF (e.g.,
RADAR, UFCD controlled avionics, ECM,
sensors, MC2)
10. Land as soon as possible.
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 1 of 55)
V-12-3 ORIGINAL
Warning Lights
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
SINGLE
L BLEED
or
R BLEED
Warning Light
(which does not go out)
²Bleed Air Left (Right),
Bleed Air Left (Right)²
· Bleed air leak detected on designated side AND
the overheat condition still exists (e.g., automatic
BALD shutdown did not secure the leak).
If the L or R BLEED warning light is out, the
overheat condition no longer exists.
Bleed air leak MSP codes: 953, 954, 955, 956, 957,
958, 959, 960, or 961 (code determines leak location).
If displayed, the L or R BLD OFF caution indicates
that the corresponding primary bleed air shutoff
valve is commanded closed and is NOT an indication
of actual valve position.
If the aft avionics cooling fan has been disabled, the
OFF/RAM position of the ECS MODE switch will
not energize the aft avionics cooling fan. In this
case, only limited avionics cooling is available using
ram air. With the AV COOL switch set to EMERG,
only the following essential avionics receive adequate
cooling: FCC A, one AHRS, and the right
transformer rectifier. All other avionics systems are
susceptible to failure or shutdown due to heat. Ambient
temperature significantly influences the rate
at which avionics systems fail.
*1. BLEED AIR knob affected engine - OFF (DO
NOT CYCLE)
If light still on, do the following in order
until the light goes out -
*2. Throttle affected engine - IDLE
*3. Throttle affected engine - OFF
*4. BLEED AIR knob - OFF (DO NOT CYCLE)
If both bleeds secured -
*5. Emergency oxygen green ring - PULL
If light still on -
6. Land as soon as possible.
If light goes out -
6. Land as soon as practical.
If both bleeds secured -
1. Maintain altitude below 10,000 feet.
2. Maintain airspeed below 325 KCAS (300 to 325
KCAS optimum).
3. ECS MODE switch - OFF/RAM
4. AV COOL switch - EMERG
Once below 10,000 feet -
5. Consider removing mask and resetting
emergency oxygen.
6. CABIN PRESS switch - RAM/DUMP
7. OXY FLOW knob - OFF
8. OBOGS control switch - OFF
If AV AIR HOT caution appears OR aft
avionics cooling fan disabled -
9. Non-essential avionics equipment - OFF (e.g.,
RADAR, UFCD controlled avionics, ECM,
sensors, MC2)
10. Land as soon as possible.
A1-F18EA-NFM-000
Figure 12-1. Warning/Caution/Advisory Displays (Sheet 2 of 55)
V-12-4 ORIGINAL
Warning Lights
INDICATOR · CAUSE / REMARKS CORRECTIVE ACTION
FIRE
Warning Light
²Engine Fire Left
(Right),
Engine Fire Left
(Right)²
· Fire condition detected in corresponding engine/
AMAD bay.
If dual FIRE light indications and unable to determine
which light came on first, check engine instruments
for indications of a fire. High fuel flow,
high EGT, rough running, or smoke and fumes may
indicate the affected side, even if present prior to
the FIRE light coming on. Do not hesitate to push
the FIRE EXTGH READY light and lower the
HOOK handle once FIRE procedures have been
initiated. Fire testing indicates that early use of the
fire bottle is the best opportunity to put out a fire
and, most importantly, keep it out. If the hook release
cable is damaged by an engine bay fire, it may
be impossible to lower the hook.
An engine bay fire may damage the engine bay
door, which is critical to structural integrity. Following
an engine bay fire, limit maneuvering to 5g,
limit descent rate at touchdown to less than 1,000
fpm, and minimize roll and yaw at landing. An off
center arrestment following an engine fire can lead
to catastrophic structural failure.
GROUND
*1. Throttles - OFF
*2. FIRE light affected engine - PUSH
*3. FIRE EXTGH READY light - PUSH
*4. BATT switch - OFF
*5. Egress
ON TAKEOFF
*1. ABORT or execute Emergency Takeoff Procedure.
INFLIGHT
Dual FIRE lights -
*1. Throttles - Minimum practical for flight
Single FIRE light or Dual when side confirmed
-
*2. Throttle affected engine - OFF
*3. FIRE light affected engine - PUSH
*4. FIRE EXTGH READY light - PUSH
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本文链接地址：
NATOPS Flight Manual 飞行手册 2(16)
