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a. Note hydraulic pressure decay through 500 psi.
b. Cycle lateral stick and rudder pedals.
c. If aileron, rudder, or LEF surfaces X, maintenance action is required.
7. FCS page - Verify no channel is completely X'd out.
8. COMM 1 and 2 knobs - OFF (both cockpits)
9. L (R) DDI, HUD, and MPCD knobs - OFF (both cockpits)
10. Other throttle - OFF
When amber FLAPS light illuminates -
11. BATT switch - LEAVE ON
· Battery gauge reads 23 to 24 vdc (nominal).
· Automatic battery cutoff operates at 2 minutes (1 minute on aircraft 165533 thru 165544).
12. FCF Profile A - COMPLETE
10.6 FCF CHECKLIST - PROFILE C
1. Perform engine start, taxi, and takeoff IAW NATOPS
10.6.1 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-10-27 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.
c. Airspeed - Maintain 300 KCAS
d. Stick - RELEASE from wings level
· Time to roll through 30° AOB must be £ 10 seconds.
· Roll rate £ 3°second.
e. Repeat steps c and d at 400 KCAS
f. Repeat steps c and d at 500 KCAS
2. LEF/HDU stall check - 10,000 feet
a. G-warm - PERFORM
· 4g for 90°.
· 6g for 90°.
· -1g pushover to check for cockpit foreign objects.
b. FCS page - CHECK
· G-LIM value not Xd out.
· No G-LIM 7.5G caution.
c. Speed - Accelerate to 0.9 to 0.93 Mach
d. Roll to 90° AOB, retard throttles to IDLE, and smoothly pull to g-limiter.
At 25° AOA -
e. Terminate the maneuver.
· No ²abrupt² rolling tendency.
· No FLAP SCHED caution.
· No BLIN code 256 (channel identifies weak HDU).
3. FCF Profile C - COMPLETE
10.7 FCF CHECKLIST - PROFILE D (REAR COCKPIT)
1. When a profile D is required solely by the reconfiguration of the rear cockpit, perform engine
start, taxi, and takeoff IAW NATOPS.
A1-F18EA-NFM-000
III-10-28 ORIGINAL
10.7.1 Preflight Checks.
1. UFCD adapter - VERIFY NOT INSTALLED
10.7.2 Before Taxi Checks.
1. Rudder pedal adjustment - CHECK
· Smooth through full range of travel.
· Locks securely when RUD PED ADJ lever released.
2. Stick and rudder pedals - CYCLE
· No binding through full travel.
3. Throttles - Advance to MIL momentarily. Do not allow engine rpm to exceed 80%.
· No binding or sticking through range of travel.
· No engine shutdowns when pulled to IDLE.
10.7.3 Taxi Checks.
1. Braking system - CHECK
a. Normal brakes - CHECK
· Nominal braking performance at taxi speed.
b. EMERG BRK handle - PULL TO DETENT
· Handle latches securely in detent.
· Nominal braking performance at taxi speed.
c. EMERG BRK handle - NORM
2. Nosewheel steering - CHECK IN HIGH MODE L/R
· NWS responds appropriately in NWS and NWS HI.
· NWS disengages when paddle switch pressed.
10.7.4 Medium Altitude (above 10,000 feet).
1. Flight control damping - CHECK
a. Airspeed - Maintain 300 to 350 KCAS
b. Make small, abrupt pitch, roll, and yaw inputs.
· Aircraft response is appropriate.
· No oscillation tendencies noted.
2. Throttles - CYCLE INTO AB
· Nominal engine response to throttle position.
· Afterburners light off normally and cancel when MIL selected.
3. COMM switch - CHECK
· Comm switch functions normally.
· Both radios operative in transmit and receive.
A1-F18EA-NFM-000
III-10-29 ORIGINAL
4. Speedbrakes - CHECK
a. Speedbrake switch - HOLD AFT
· Speedbrake surfaces extend normally.
· SPD BRK light on when surfaces not fully retracted.
b. Speedbrake switch - RELEASE
· Speedbrake surfaces retract fully.
In front cockpit -
c. Speedbrake switch - HOLD AFT
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NATOPS Flight Manual 飞行手册 2(2)
