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· No complete FCC channel failures on FCS page.
· ENGINE LEFT/RIGHT voice alert and BLIN code 260 can be expected and are normal in the
conduct of this check.
13. Shutdown engine - CROSSBLEED START
Advance operating engine to a minimum of 80% rpm.
14. Repeat steps 9 thru 13 for the left engine.
· Restart left engine within 15 minutes, else motor for 1 minute at 29% rpm or greater before
restart (to preclude engine damage).
15. GEN TIE operation - CHECK
a. GEN TIE switch - RESET
· GEN TIE caution light on.
b. GEN TIE switch - NORM/GUARD DOWN
· GEN TIE caution light out.
16. Fuel system checks - PERFORM
On the RDDI -
a. SDC/transducer operation - CHECK
(1) BIT/STATUS MONITOR format - SELECT
(2) SDC BIT option - SELECT
· SDC BIT status indicates GO.
(3) FXFR format - SELECT
· No parameters flashing.
(4) FQTY format - SELECT/LEAVE
· No parameters flashing.
A1-F18EA-NFM-000
III-10-10 ORIGINAL
On the LDDI -
b. FUEL page - SELECT
· No fuel cautions or advisories displayed.
· No CG DEGD, EST, INV, INVALID, or INVALID TIMER.
· BINGO, TOTAL, and INTERNAL fuel quantities agree with EFD.
c. FLBIT option - SELECT
· On RDDI, TK(2)FL indicates GO within 2 seconds.
· On RDDI, TK(3)FL indicates GO within 12 seconds.
· FUEL LO caution and voice alert activated within 12 seconds.
· FUEL LO caution removed after 60 seconds.
d. SDC RESET option - SELECT
· CAUT DEGD caution displayed for 3 seconds.
On the EFD -
e. BINGO caution - CHECK
(1) BINGO - SET 200 lb above INTERNAL fuel
· BINGO caution and voice alert activated.
(2) BINGO - SET 200 lb below INTERNAL fuel
· BINGO caution removed.
(3) BINGO - SET as desired
17. Hydraulic pressure gauge - CHECK (2,600 to 3,300 psi)
18. ECS system checks - PERFORM
a. DEFOG - CHECK
(1) DEFOG handle - LOW
· Minimum defog airflow and maximum cabin airflow.
(2) DEFOG handle - HIGH
· Progressively decreasing cabin airflow and increasing defog flow.
b. ECS modes - CHECK
· Signal: Punch open palm with fist.
(1) ECS MODE switch - OFF/RAM
· Cockpit airflow stops.
· ECS ram air scoop opens (thumbs up from PC).
(2) ECS MODE switch - AUTO
· Cockpit airflow resumes.
· ECS ram air scoop closes (thumbs up from PC).
A1-F18EA-NFM-000
III-10-11 ORIGINAL
c. CABIN TEMP knob - ROTATE between COLD and HOT
· Air temperature changes to agree with setting.
19. ENG ANTI ICE system - CHECK
a. ENG ANTI ICE switch - ON
· LHEAT and RHEAT advisories displayed.
b. ENG ANTI ICE switch - TEST
· INLET ICE caution displayed when switch held.
20. BLEED AIR system - CHECK
a. Throttles - IDLE
b. BLEED AIR knob - L OFF and R OFF (individually)
· Opposite engine TEMP increases 5° to 90°C.
c. BLEED AIR knob - NORM
d. FIRE test switch - TEST A (for at least 2 seconds)
· L and R BLEED warning lights on while switch held.
· Voice alert sequence initiated.
· L and R BLD OFF cautions displayed.
· Cockpit airflow stops.
e. BLEED AIR knob - CYCLE THRU OFF TO NORM
· L and R BLD OFF cautions removed.
· Cockpit airflow resumes.
f. Repeat steps d and e for the TEST B position.
10.5.6 Before Taxi Checks.
1. WYPT 0 and MVAR - CHECK/SET
2. GPWS - CHECK BOXED
3. INS knob - CV OR GND (PARK BRK SET)
4. RADAR knob - OPR
5. FLIR and LST/FLR switches - AS DESIRED
6. UFCD avionics - TURN ON
a. RALT - ON/SET
b. TCN - ON, T/R, CH SET
c. IFF - ON/MODES BOXED
A1-F18EA-NFM-000
III-10-12 ORIGINAL
7. MPCD/UFCD - ENTER DESIRED WAYPOINTS
8. Throttle position related cautions - CHECK
a. PARK BRK handle - SET
b. FLAP switch - AUTO
c. Stabilator trim - SET LESS THAN 3° NU
d. Ejection seat SAFE/ARMED handle(s) - SAFE (both cockpits)
e. Throttles - Advance to MIL momentarily. Do not allow engine RPM to exceed 80%.
· CK FLAPS and PARK BRK cautions displayed momentarily.
· CHECK TRIM and CHECK SEAT cautions displayed.
· CHECK SEAT caution does not clear until seat(s) armed for takeoff.
f. T/O TRIM button - PRESS UNTIL TRIM ADVISORY DISPLAYED
· CHECK TRIM caution removed.
9. WINGFOLD system - CHECK
With wings spread and locked -
a. WINGFOLD switch - HOLD
· Ailerons fair and beer cans pop up.
· WING UNLK cautions displayed.
b. NWS button - PUSH (twice if required)
　
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