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SELECTIVE JETTISON
Requirements:
a. Wing stations: (1) WoffW, (2) LDG GEAR handle UP, (3) MASTER ARM switch - ARM, (4) racks/launchers unlocked.
b. Fuselage stations: Also (5) landing gear up and locked.
1. Find a clear area (if possible).
2. LT TEST switch - TEST Verify all jettison pushtiles are illuminated.
3. Jettison pushtiles - SELECT DESIRED STATIONS (CTR, LI, RI, LM, RM, LO, RO)
4. SELECT JETT knob - ROTATE (as required)
a. L FUS MSL - Left fuselage missile
b. R FUS MSL - Right fuselage missile
c. RACK/LCHR - Rack/launcher (jettisons whatever is attached to the selected parent racks)
d. STORES - (1) Jettisons ordnance loaded on selected parent racks, CVERs, or IMERs;
(2) Jettisons missiles attached to launchers on selected stations except HARM;
(3) HARM anti-compromise launch.
5. SIM mode - UNBOXED
6. MASTER ARM switch - ARM
7. SELECT JETT button - PUSH Jettison sequential by selected stations: RM, LM, RI, LI, CL, RO, LO (350 ms)
After jettison -
8. MASTER ARM switch - SAFE
9. SELECT JETT knob - SAFE
NOTE
¥ Outboard station ADU-773 missile rails cannot be jettisoned, since they are installed in place of a BRU-32 rack.
¥ If multiple stations selected for STORE jettison include AGM-88s, the first HARM in the default sequence is launched first, then
the sequence continues from that station, releasing the remaining selected non-HARM stores. Regardless of the number
selected, only one HARM is launched each time the SELECT JETT button is pushed.
¥ With the SELECT JETT knob rotated out of the SAFE position, the SMS unlocks all racks/launchers. When SAFE is reselected,
racks/launchers are not locked again until commanded by either lowering the landing gear or selecting SIM mode.
AUX RELEASE
Requirements: (1) station must be HALKD or HAULK following a failed normal release or SELECT JETT attempt, (2) WoffW, (3)
LDG GEAR handle UP, (4) MASTER ARM switch - ARM, (5) racks/launchers unlocked. (6) and only if an auxiliary cartridge is
installed in the HUNG parent rack.
WARNING
During an AUX REL, the Mk 19 auxiliary cartridge is fired, opening the selected parent rackÕs hooks and allowing the attached
store or rack/launcher to free fall from the aircraft. Lacking a forced ejection, this release mode is prohibited except in an
emergency and then only in 1.0g level flight.
NOTE
A Mk 19 auxiliary cartridge is not installed in a parent rack when a wing station is loaded with an IMER, a HARM, a Maverick, a
Harpoon, or a SLAM.
1. Find a clear area (if possible).
2. LT TEST switch - TEST Verify all jettison pushtiles are illuminated.
3. AUX REL switch - ENABLE
4. Jettison pushtiles - SELECT HUNG STATION(S)
5. SELECT JETT knob - ROTATE TO EITHER RACK/LCHR or STORES
6. SIM mode - UNBOXED
7. MASTER ARM switch - ARM
8. SELECT JETT button - PUSH
Fires the aux cartridge(s) for gravity release of all stores/racks/launchers from the selected parent rack(s).
After AUX REL -
9. MASTER ARM switch - SAFE
10. SELECT JETT knob - SAFE
11. AUX REL switch - NORM
Figure 15-8. External Stores Jettison Chart
A1-F18EA-NFM-000
V-15-21 ORIGINAL
15.13 FCS FAILURE INDICATIONS AND EFFECTS
FCS failures are indicated by various cautions and by FCS format Xs and BLIN codes. Following
display or annunciation of an FCS caution, the FCS format should be used to identify the exact
malfunction/failure.
With the failure of FCC channels 1 and 3, the FCS format displays the word INVALID in place of
the G-LIM advisory. Subsequent FCS failures or resets will not be displayed.
The following figures depict typical FCS failure indications and their effects for the majority of FCS
related malfunctions/failures.
EFFECTS:
Loss of speedbrake function.
Figure 15-9. FCS Failure Indications and
Effects
A1-F18EA-NFM-000
V-15-22 ORIGINAL
EFFECTS:
ATC inoperative.
Normal NWS inoperative.
Loss of HUD barometric altitude (radar altitude
available below 5,000 feet).
Standby altimeter available.
Loss of IFF altitude reporting.
Loss of speedbrake function.
Loss of AOA/yaw rate warning tone.
Autopilot pitch mode defaults to FPAH if BALT
or RALT were previously selected.
MAD sensor data lost.
EFFECTS:
Loss of speedbrake function.
Figure 15-10. FCS Failure Indications and
Effects
Figure 15-11. FCS Failure Indications and
Effects
A1-F18EA-NFM-000
V-15-23 CHANGE 1
EFFECTS:
ATC inoperative.
Normal NWS inoperative.
Loss of AOA approach/indexer lights.
Loss of speedbrake function.
Loss of AHRS over temperature detection.
EFFECTS:
ATC inoperative.
　
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本文鏈接地址：NATOPS Flight Manual 飛行手冊 2(57)