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automatically sent to the GPS to aid the acquisition of satellites. After
satellite acquisition, the GPS backloads satellite time to the SDC thus
synchronizing the SDC with precise GPS time. This GPS time
backload is only performed once per flight after the initial MC1
power-up.
· Manually changing ZTOD, LTOD, or the DATE with WonW resets
SDC time and/or date and reinitializes the GPS (even if GPS had a
good satellite acquisition). GPS reinitialization will delay the availability
of AINS position keeping. GPS time synchronization will not be
available until a subsequent MC1 power-up (cold start). ARC-210
radios will need to be re-synched to enable HAVE QUICK operations.
25. Weapons/sensors - ON/BIT CHECK (as required)
26. BIT page - NOTE DEGD/FAIL INDICATIONS
26A. HMD - ALIGN
NOTE
Canopy must be down and locked to align HMD.
27. Standby attitude data - CHECK
a. ATT switch - STBY
b. Verify INS attitude data is replaced by standby attitude data on the HUD and check
agreement of standby and INS data.
c. ATT switch - AUTO
28. OBOGS system - CHECK
a. OBOGS control switch - ON
b. OXY FLOW knob - ON/MASK ON (both cockpits)
c. OBOGS electronic BIT button - PRESS AND RELEASE
d. Verify OBOGS DEGD caution set and removed (typically within 15 seconds)
e. OXY FLOW knob - OFF/MASK OFF (both cockpits)
A1-F18EA-NFM-000
III-7-26 CHANGE 1
7.4 TAXI CHECKS
1. Canopy - EITHER FULL UP OR FULL DOWN FOR TAXI
Taxiing with the canopy at an intermediate position can result in canopy
attach point damage and failure.
2. Normal brakes - CHECK
3. Nosewheel steering - CHECK IN HIGH MODE L/R
NOTE
When using brakes, apply firm, steady brake pedal pressure. Use
nosewheel steering whenever possible, minimizing differential braking.
Avoid dragging brakes or light brake applications except as necessary
for drying wet brakes. Wet brakes can degrade brake effectiveness by
as much as 50%. Hard momentary braking with wet brakes during taxi
can reduce drying time. At heavy gross weight, make all turns at
minimum speed and maximum practical radius.
Figure 7-2. Checklist Display
A1-F18EA-NFM-000
III-7-27 ORIGINAL
7.5 TAKEOFF
7.5.1 Before Takeoff Checks.
For MAX power catapult launches only -
1. ABLIM option - BOX
2. ABLIM advisory - VERIFY DISPLAYED
For all takeoffs -
3. Checklist page (figure 7-2)
a. FUEL TYPE - VERIFY
b. T.O. checklist - COMPLETE (challenge and response)
Aircrew takeoff checks -
WSO PILOT
CONTROLS
WINGS
TRIM
FLAPS
HOOK / HARNESS
WARNING LIGHTS
NWS
SEAT(s) ARM
ARMED, AFT INITIATE, HANDLES
STOWED
FREE and CLEAR (visually check)
SPREAD and LOCKED, BEER CANS DOWN,
CAUTION OUT, SWITCH LEVER-LOCKED
15, 30, 30, 40, and 4 UP (or as set for catapult
launch)
HALF (FULL), INDICATING HALF (FULL)
UP, LIGHT OUT, ATTACHED 8 POINTS
OUT, CAUTIONS OUT, ADVISORIES
CHECKED, RALT ON, SET AT XXX FEET
LO
FRONT
−
A1-F18EA-NFM-000
III-7-28 ORIGINAL
c. Navigation brief - WSO VERBALIZE AS REQUIRED
Ensure the WINGFOLD switch is lever-locked in the SPREAD position.
If the wings are commanded to unlock or fold during a catapult shot, the
wings will unlock, the ailerons will fair, the wings may fold partially, and
the aircraft will settle.
WSO must make sure the EJECTION MODE handle is in AFT INITIATE
(NORM) and the EMERG LDG GEAR and EMERG BRK handles
are fully stowed.
NOTE
· EJECT SEL is displayed in the F/A-18F only.
· Rear cockpit command eject is enabled when the EJECTION MODE
handle is in the AFT INITIATE position. When a passenger unfamiliar
with the F/A-18F occupies the aft cockpit, the NORM position may
be utilized.
4. Canopy - CHECK CLEAR/CLOSED
Prior to operating the canopy switch, confirm aircrew are clear to reduce
the potential for injury.
A1-F18EA-NFM-000
III-7-29 ORIGINAL
5. OXY FLOW knob - ON/MASK ON (both cockpits)
Continued operation and use of the OBOGS system with an OBOGS
DEGD caution may result in hypoxia.
It is possible to place the OXY FLOW knob in an intermediate position
between the ON and OFF detents, which may result in a reduced flow of
oxygen. The OXY FLOW knob should always be fully rotated to the ON
or OFF detent position.
NOTE
Rotating the OBOGS monitor pneumatic BIT plunger, while pushing it
up, can result in the locking of the button in the maintenance position
and intermittent OBOGS DEGD cautions. Rotation of the BIT plunger
disengages the locking slot allowing the plunger to extend and move
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NATOPS Flight Manual 飞行手册 1(136)
