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8. BLEED AIR knob - NORM
9. ENG CRANK switch - L
10. Left throttle - IDLE
· RPM 10% minimum
· TEMP 871°C maximum transient
· OIL 10 psi within 30 seconds
11. ENG CRANK switch - CHECK OFF
12. EFD - CHECK
10.5.5 Post-Start Checks.
1. APU automatic shutdown - CHECK
· APU shutdown 1 minute after second generator online.
2. WINDSHIELD ANTI ICE/RAIN removal - CHECK
a. WINDSHIELD switch - ANTI ICE
· High airflow across windshield.
b. WINDSHIELD switch - RAIN
· Reduced airflow across windshield.
c. WINDSHIELD switch - OFF
· Airflow stops.
3. Canopy operation - CHECK
a. CANOPY switch - CLOSE (half way)
· Canopy stops when switch is released.
b. CANOPY switch - OPEN then release
· Switch returns to HOLD position.
· Canopy moves to full open position.
c. Position canopy as desired.
4. WINGFOLD switch - SPREAD
A1-F18EA-NFM-000
III-10-7 ORIGINAL
5. FCS RESET button - PUSH (verify RSET advisory displayed)
· No flight control surface Xs.
· No BLIN codes.
· No complete FCC channel failures.
After successful FCS reset -
6. GAIN ORIDE - CHECK
With flaps FULL -
a. GAIN switch - ORIDE
· LAND advisory displayed.
· Amber FLAPS light on.
b. FLAP switch - AUTO
· CRUIS advisory displayed.
· Amber FLAPS light out.
c. GAIN switch - NORM/GUARD DOWN
7. FCC keep-alive circuitry - CHECK
a. FCS CH circuit breakers - Pull in sequence 1, 2, 3, and 4
b. Immediately reset in sequence 1, 2, 3, 4
· Complete within 7 seconds for valid test.
· No FCC channel completely Xd out.
· No FCS surface Xs and no BLIN codes.
8. Mission computer operation - CHECK
a. SUPT MENU - SELECT ON LDDI
b. MC switch - 1 OFF
· MC1 and NO RATS cautions displayed.
· BIT, CHKLST, ENG, and ADI options removed from SUPT MENU
· ACL option appears on HSI.
c. MC switch - NORM
· MC1 and NO RATS cautions removed.
· SUPT MENU options return.
d. TAC MENU - SELECT ON LDDI
e. MC switch - 2 OFF
· MC2 caution displayed.
· STORES option removed from TAC MENU.
f. MC switch - NORM
· MC2 caution removed.
· STORES option returns.
A1-F18EA-NFM-000
III-10-8 ORIGINAL
Steps 9 thru 13 are to be performed on both engines (RIGHT then LEFT).
9. Engine FIRE light shutdown - PERFORM
a. Throttle affected engine - IDLE
b. FIRE light affected engine - PUSH
When rpm decay noted (up to 60 seconds) but NLT 50% -
c. Throttle affected engine - OFF
d. FIRE light affected engine - IMMEDIATELY RESET
With affected engine secured -
10. Fuel/air heat exchanger leak check - PERFORM
a. BIT/STATUS MONITOR/XFR page - SELECT ON RDDI
· XCOOL line reads ²0² (open)
b. RBYP or LBYP option (affected side) - PUSH to read ²HX²
· Signal: Pull tip of nose with thumb and index finger.
· No fuel leaking from the heat exchanger drains (forward lower inboard side of the inlet on the
affected side) (thumbs up from PC).
c. FXFR/RESET option - PUSH
· RBYP or LBYP option (affected side) reads ²BP².
11. Verify proper switching valve operation.
a. Note hydraulic pressure decay through 500 psi on the affected side.
b. Cycle lateral stick and rudder pedals and verify aileron and rudder surface movement.
c. If aileron, rudder, or LEF surfaces X, maintenance action is required.
12. GEN/electrical system checks - PERFORM
With affected GEN inoperative -
· Opposite GEN picks up all three busses
· GEN TIE caution light out.
· All displays operative.
· No FCS Xs or channel failures.
a. BATT switch - OFF (opens bus tie)
· Busses are isolated on affected side.
· BATT SW and GEN TIE caution lights on.
With R GEN off -
· HUD and RDDI inoperative.
· LDDI, MPCD, and UFCD operative.
A1-F18EA-NFM-000
III-10-9 ORIGINAL
With L GEN off -
· HUD and RDDI operative.
· LDDI, MPCD, and UFCD inoperative.
b. BATT switch - NORM
· BATT SW and GEN TIE caution lights out.
· All displays operative.
c. GEN switch opposite side - OFF (for at least 30 seconds)
· PMGs pickup essential bus.
· Battery gauge reads >24 vdc (26.5 vdc nominal).
· BATT SW caution light out.
d. GEN switch opposite side - NORM
· Essential bus picked up FCS channels on affected side.
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NATOPS Flight Manual 飞行手册 1(161)
