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· Full-time NWS HI available.
c. WINGFOLD switch - FOLD
· Wingfold system and locking pins operate properly.
· Both ailerons Xd out.
d. WINGFOLD switch - SPREAD then HOLD
· Wings stop at intermediate position.
With NWS HI selected -
e. WINGFOLD switch - SPREAD
· Wings spread fully.
· Beer cans go down.
· WING UNLK caution removed.
· NWS HI reverts to NWS (low).
To the maximum extent possible, make sure wings are spread and locked prior to FCS
IBIT to make sure all aileron related tests are performed.
10. FCS RESET button - PUSH (if required)
· RSET advisory displayed.
· If wings are folded, both ailerons Xd out.
A1-F18EA-NFM-000
III-10-13 ORIGINAL
11. FCS IBIT - PERFORM
a. FCS BIT consent switch - HOLD UP THEN PRESS THE FCS OPTION
b. AOA warning tone - VERIFY ANNUNCIATION AT FCS IBIT COMPLETION
c. FCS A and FCS B BIT status - VERIFY GO
d. FCS display - VERIFY NO BLIN CODES
12. Trim - CHECK
a. Trim - FULL LEFT and UP (ailerons, rudders, and stabs)
· Control surfaces respond correctly.
b. T/O TRIM button - PRESS UNTIL TRIM ADVISORY DISPLAYED
c. Trim - FULL RIGHT and DOWN (ailerons, rudders, and stabs)
· Control surfaces respond correctly.
13. T/O TRIM button - PRESS UNTIL TRIM ADVISORY DISPLAYED (stabilators 4° NU)
14. Controls - CHECK (tolerance ±1°)
a. Control stick - CYCLE
(1) Full aft - CHECK 24° NU stabilator
(2) Full fwd - CHECK 20° ND stabilator
(3) Full L/R - CHECK 30° differential stabilator (21° with tanks or A/G stores on
any wing station)
- CHECK differential TEFs
b. FLAP switch - HALF
c. Rudder pedals - CYCLE 40° L/R
d. FLAP switch - FULL (carrier-based)
e. TRIM - SET FOR CATAPULT LAUNCH (carrier-based)
15. PROBE, speedbrake, LAUNCH BAR switches and HOOK handle - CYCLE
· Spoilers extend to 60° ±3° and retract in 3 seconds.
· SPDBRK light on when spoilers not fully retracted.
· Hook extends within 2 seconds and retracts within 4 seconds.
· Probe extends and retracts within 6 seconds.
· Probe light is on with the probe extended (thumbs up from PC).
· Launch bar extends (leave extended).
· Green LBAR advisory light on.
16. Pitot and AOA heat check - PERFORM
A1-F18EA-NFM-000
III-10-14 ORIGINAL
a. PITOT ANTI ICE switch - ON
b. Make sure ground crew verify proper operation.
c. PITOT ANTI ICE switch - AUTO
17. CHECK TRIM caution - CHECK
With launch bar extended -
a. Stabilator trim - SET LESS THAN 6° NU
b. Throttles - Advance to MIL momentarily. Do not allow engine rpm to exceed 80%.
· CHECK TRIM caution displayed.
c. Stabilator trim - SET ABOVE 7° NU
· CHECK TRIM caution removed.
d. T/O TRIM button - PRESS UNTIL TRIM ADVISORY DISPLAYED
e. LAUNCH BAR switch - RETRACT
18. CVRS - AS DESIRED (both cockpits)
19. Standby attitude reference indicator - UNCAGE AND ERECT (both cockpits)
20. Altimeter setting - SET (both cockpits)
· Altimeter setting displayed on HUD.
· HUD altitude displayed within ±30 feet of parking spot elevation.
· Standby altimeter within ±60 feet of parking spot elevation.
21. INS - CHECK
a. PARK BRK handle - CYCLE
· INS alignment time flashes when PARK BRK released.
· Stops flashing after PARK BRK reset.
b. Alignment status - VERIFY COMPLETE
· QUAL ²OK² displayed within 6 minutes.
c. GPS HERR/VERR - VERIFY WITHIN LIMITS
When clear of overhead obstructions for 6 to 12 minutes -
· HERR and VERR less than 100 feet (with keyed MAGR).
d. INS knob - NAV (to check unaided drift)
22. MUMI/ID - SELECT/ENTER DATE and FLT
23. Stores page - Verify proper store inventory and station status.
24. ZTOD/LTOD - BOX TO ENABLE HUD DISPLAY (if desired)
A1-F18EA-NFM-000
III-10-15 ORIGINAL
25. Weapons/sensors - ON/BIT CHECK (as required)
26. BIT page - NOTE DEGD/FAIL INDICATIONS
27. Standby attitude data - CHECK
a. ATT switch - STBY
· Velocity vector disappears.
· Pitch ladder referenced to the W .
· INS ATT caution displayed.
b. Standby attitude reference indicator - ERECT
· HUD pitch ladder moves/coincides with the standby attitude reference indicator.
c. ATT switch - AUTO
28. OBOGS system - CHECK
a. OBOGS control switch - ON
b. OXY FLOW knob - ON/MASK(S) (both cockpits)
· System provides oxygen on demand.
· No excessive backpressure.
　
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本文鏈接地址：NATOPS Flight Manual 飛行手冊 1(163)