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· Probe retracts normally within 6 seconds.
· No PROBE UNLK caution when retracted.
c. PROBE switch - EMERG EXTD
· Probe extends normally within 6 seconds.
d. PROBE switch - RETRACT
· Probe retracts normally within 6 seconds.
· No PROBE UNLK caution when retracted.
7. HOOK - CHECK
a. HOOK handle - DOWN
· HOOK light on while hook in transit.
· HOOK light out when hook fully extended.
b. HOOK handle - UP
A1-F18EA-NFM-000
III-10-19 ORIGINAL
8. Fuel dump - CHECK
a. BINGO - CHECK/SET just below internal fuel level
b. DUMP switch - ON
· Fuel dumps from both vertical tails.
c. BINGO - Run above internal fuel level
· DUMP switch returns to OFF automatically.
· Fuel dump stops.
9. ATC cruise mode - CHECK
· ATC advisory in HUD when selected.
· Throttles respond correctly.
· ATC holds calibrated airspeed when straight-and-level and during turns, climbs, and descents.
10. HUD symbology - CHECK (both cockpits)
In NAV master mode with WYPT or TCN boxed -
· The following indications are present - heading, airspeed, altitude, AOA, Mach number,
aircraft g, bank angle scale, velocity vector, flight path/pitch ladder, steering arrow (TCN),
and distance to WYPT or TCN.
· WYPT # displayed to right of distance when WYPT boxed.
· Three-letter identifier displayed to right of distance when TCN boxed.
· HUD and MPCD distance agree.
· HUD format available on DDI, MPCD, or UFCD (both cockpits).
11. HSI symbology - CHECK on MPCD
a. HDG/TK set switch - SLEW (both cockpits)
· Heading bug moves in correct direction.
· Digital display and bug setting agree.
b. CRS set switch - SLEW (both cockpits)
· Steering arrow rotates in correct direction.
· Digital display and steering arrow agree.
c. TCN bearing and range - CHECK
· Symbol displayed at appropriate position when compared to a waypoint or known landmark.
· Digital display and symbol agree.
12. Standby flight instruments - CHECK (both cockpits)
a. Standby rate of climb indicator
· Indicates ±100 fpm or less during level 1g flight.
· Pointer movement smooth during climbs/descents.
b. Standby attitude reference indicator
(1) Perform a 360° roll right and left
· No gyro tumble.
A1-F18EA-NFM-000
III-10-20 ORIGINAL
(2) Perform a loop.
· Gyro indications are smooth thru bullseye.
c. Standby airspeed indicator
· Agrees with HUD.
· Pointer movement is smooth during airspeed changes.
d. Standby altimeter
· Agrees with HUD (except -100 to -400 feet of error since value is uncorrected by FCC air data
function.
· Pointer and drum movement is smooth and does not hang up during thousand-foot changes.
13. INS/GPS operation - CHECK
a. TCN update - PERFORM
· Proper update mechanization.
· Reject update.
b. DSG update - PERFORM
· Proper update mechanization.
· Reject update.
c. GPS HERR/VERR - CHECK
· Less than 100 feet inflight (with keyed MAGR).
14. ADF receivers - CHECK
a. ADF - BOX on COMM 1 and COMM 2 sub-levels (individually)
· Bearing within ± 5° off the nose.
· Bearing within ± 20° off the wing tip.
15. IFF operation - CHECK
· ATC reports valid mode 3 and C.
If/when possible -
a. IFF MASTER switch - EMERG
· ATC reports valid emergency squawk (7700).
16. Radar/HOTAS functionality - CHECK (both cockpits)
a. A/A master mode - CHECK
b. A/G master mode - CHECK
10.5.12 10,000 Feet Checks.
With an asymmetric FLIR pod on station 5 or 7 -
· Expect a gradually increasing amount of pod-induced roll-off during the accel to 500 KCAS on the FCS
RIG check or to 0.9 to 0.93 Mach on the LEF/HDU stall check.
· In this configuration, FCS rigging is considered acceptable if the 300 and 400 KCAS points are passed.
· If encountered on the LEF/HDU stall check, this ²gradual² roll-off is not indicative of an HDU stall.
A1-F18EA-NFM-000
III-10-21 ORIGINAL
1. FCS RIG check - 10,000 feet
Only perform if:
· Aircraft symmetrically loaded. (Asymmetric FLIR pod on station 5 or 7 acceptable for 300 and
400 KCAS points only.)
· External/internal wing tank fuel asymmetry less than 300 lb.
a. Autopilot mode - Disengage in 1g flight
b. T/O TRIM button - PUSH (4 seconds minimum)
· Do not retrim laterally or directionally for duration of check.
　
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本文鏈接地址：NATOPS Flight Manual 飛行手冊 1(165)