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13. L(R) DDI, HUD, and MPCD knobs - OFF
NOTE
Power to the UFCD is controlled by the MPCD knob, so the UFCD
knob does not need to be OFF.
14. COMM 1 and 2 knobs - OFF
15. CVRS mode switch - OFF
16. ALT switch - BARO or RDR
17. ATT switch - AUTO
18. Standby attitude reference indicator - CAGED
19. IR COOL switch - OFF
20. SPIN switch - NORM/GUARD DOWN
21. HOOK handle - UP
22. WINGFOLD switch - SAME AS WING POSITION
23. AV COOL switch - NORM
Pedestal Panel (aircraft 165660 and up) -
1. ECM JETT button - NOT PUSHED IN
2. JAMMER switch - OFF
3. RWR switch - OFF
A1-F18EA-NFM-000
III-7-13 ORIGINAL
4. DISPENSER switch - OFF
5. AUX REL switch - NORM
6. RUD PED ADJ lever - ADJUST PEDAL POSITION
· Restrain the rudder pedals during adjustment. Unrestrained release of
the rudder pedals may damage the rudder pedal mechanism.
· Ensure the rudder pedals are locked in position after adjustment.
Failure to lock the rudder pedals may result in uncommanded forward
rudder pedal movement inflight.
Right console -
1. Circuit breakers - IN
2. GEN switches - NORM
3. BATT switch - OFF
4. ECS panel - SET
a. MODE switch - AUTO
Extended periods of ECS MAN mode operation, particularly at high
power settings, significantly reduces engine life. If the ECS is not DEGD
and temperatures are not out of limits, ensure the ECS MODE switch is
in the AUTO position.
b. CABIN TEMP knob - AS DESIRED
c. CABIN PRESS switch - NORM
d. BLEED AIR knob - OFF
e. ENG ANTI ICE switch - OFF
f. PITOT ANTI ICE switch - AUTO
5. DEFOG handle - MID RANGE
6. WINDSHIELD switch - OFF
7. INTR LT panel - SET
A1-F18EA-NFM-000
III-7-14 ORIGINAL
a. CONSOLES, INST PNL, and FLOOD knobs - AS DESIRED
b. CHART and WARN/CAUT knobs - AS DESIRED
c. MODE switch - DAY, NITE, or NVG (as required)
8. Sensor control panel - SET
a. FLIR, LTD/R, and LST/NFLR switches - OFF/SAFE/OFF
b. INS and RADAR knobs - OFF
9. NVG storage container - CHECK SECURE
7.1.6 Interior Checks - WSO.
1. Leads, leg restraints, and harness - SECURE/ADJUST
Connect oxygen, g suit, and communications leads. Fasten and secure leg restraint garters and lines.
Check leg garters buckled and properly adjusted with hardware on inboard side of the legs. Connect
and adjust lap belt straps. Attach parachute Koch fittings to harness buckles. Check operation of
shoulder harness locking mechanism. Check QDC is securely connected or stowed if not in use.
The leg restraint lines must be buckled at all times during flight to ensure
that the legs will be pulled back upon ejection. This enhances seat
stability and prevents leg injury by keeping the legs from flailing
following ejection.
2. Ejection control handle - CLEAR
3. Ejection control handle pin - VERIFY REMOVED
In trainer configured aircraft -
1. Control stick - CHECK SECURE
2. UFCD adapter - VERIFY NOT INSTALLED
Forward stick throw is restricted if a rear cockpit control stick and UFCD
adapter are both installed.
3. Throttles - CHECK CONDITION
4. RUD PED ADJ lever - ADJUST PEDAL POSITION
Left console -
1. OXY FLOW knob - OFF
A1-F18EA-NFM-000
III-7-15 CHANGE 1
2. Left hand controller - CHECK SECURE
3. CANOPY JETT handle - OUTBOARD AND DOWN
4. VOL panel - SET AS DESIRED
5. RECCE panel - SET
a. POD PWR knob - OFF
b. ATARS switch - OFF
Instrument panel -
1. EMERG LDG GEAR handle - STOWED
2. EMERG BRK handle - STOWED
The position of the EMERG BRK handle is the only indication that
emergency braking is selected: no warning or caution is displayed. The
EMERG BRK handle(s) must be fully stowed in both cockpits to ensure
that normal braking with anti-skid is available.
Due to friction in the EMERG BRK handle mechanism, the handle may
not return to the fully stowed position unless positively pushed.
3. L(R) DDI and MPCD knobs - OFF
NOTE
Power to the UFCD is controlled by the MPCD knob, so the UFCD
knob does not need to be OFF.
4. COMM 1 and 2 knobs - OFF
5. Standby attitude reference indicator - CAGED
6. EJECTION MODE handle - NORM
Right console -
1. Right hand controller - CHECK SECURE
2. INTR LT panel - SET
a. CONSOLES, INST PNL, and FLOOD knobs - AS DESIRED
A1-F18EA-NFM-000
III-7-16 ORIGINAL
b. CHART and WARN/CAUT knobs - AS DESIRED
3. NVG storage container - CHECK SECURE
7.2 ENGINE START
A self-contained (battery/APU) start is the primary method for starting the engines. The aircraft
also has provisions for starting on external power, external air, or opposite engine bleed air (crossbleed)
　
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本文鏈接地址：NATOPS Flight Manual 飛行手冊 1(132)