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c. OBOGS monitor pneumatic BIT plunger - PRESS AND HOLD (do not rotate)
· OBOGS DEGD caution displayed within 65 seconds.
· Release plunger.
· Caution removed within 30 seconds.
d. OBOGS electronic BIT button - PRESS AND RELEASE
· OBOGS DEGD caution displayed within 10 seconds.
· Caution removed within 3 seconds.
e. OXY FLOW knob(s) - OFF (both cockpits)
· OBOGS flow stops.
29. Engine status/FADEC channel transfer - CHECK
a. ENG format - SELECT ON LDDI
· LEFT and RIGHT engine STATUS is NORM.
b. FADEC channel transfers - A to B and B to A on each engine
· FADEC channels change with selection.
· No channel line-outs.
10.5.7 Taxi Checks.
1. Canopy - EITHER FULL UP OR FULL DOWN FOR TAXI
2. Braking system - CHECK
A1-F18EA-NFM-000
III-10-16 ORIGINAL
a. Normal brakes - CHECK
· Nominal braking performance at taxi speed.
b. ANTI SKID switch - OFF
· SKID advisory displayed
· Nominal braking performance at taxi speed.
c. ANTI SKID switch - ON
· SKID advisory clears.
d. EMERG BRK handle - PULL TO DETENT (both cockpits - separately)
· Handle latches securely in detent.
· Nominal braking performance at taxi speed.
e. EMERG BRK handle - NORM
3. Nosewheel steering - CHECK IN HIGH MODE L/R
· NWS responds appropriately in NWS and NWS HI.
· NWS disengages when paddle switch pressed.
10.5.8 Before Takeoff Checks.
For MAX power catapult launches only -
1. ABLIM option - BOX
2. ABLIM advisory - VERIFY DISPLAYED
For all takeoffs -
3. Checklist page
a. FUEL TYPE - VERIFY
b. T.O. checklist - COMPLETE
4. Canopy - CHECK CLEAR/CLOSED
5. OXY FLOW knob(s) - ON/MASK(S) ON
6. IFF sublevel - BOX REQUIRED MODES
7. PARK BRK handle - FULLY STOWED
At position and hold -
8. Engine run-ups - PERFORM (individually)
a. Throttle affected engine - IDLE to MIL
A1-F18EA-NFM-000
III-10-17 ORIGINAL
b. ENG page - CHECK ENGINES AT MIL
· N2 rpm 88 to 100%
· N1 rpm 86 to 98%
· EGT 720 to 932°C
· FF 11,000 pph maximum
· NOZ POS 0 to 35% open
· OIL PRESS 80 to 150 psi
· THRUST 100% minimum
c. Throttle affected engine - MIL to IDLE, pause 1 second, IDLE to MIL
· Engines respond with normal acceleration characteristics.
· No stall or stagnation.
d. Throttle affected engine - IDLE
e. Repeat steps a thru d for the opposite engine.
10.5.9 Takeoff Checks.
1. Heading sources - CHECK
After runway lineup -
· HSI heading within ±3° of known runway heading.
· Standby magnetic compass within limits of compass card.
2. Afterburner takeoff - PERFORM IAW Chapter 7
· Both nozzles open correctly.
· Feed tanks stay full during and immediately following climb.
10.5.10 After Takeoff Checks.
When definitely airborne -
1. LDG GEAR handle - UP
· Gear retracts within 7 seconds.
2. Flap auto retract - CHECK
a. Airspeed - Increase through 250 KCAS
· Flaps retract to AUTO scheduling.
· Amber FLAPS light on.
b. FLAP switch - AUTO
· Amber FLAPS light out.
3. RALT operation - CHECK
· Radar altitude tracks correctly during climbout.
When above 5,000 feet AGL -
· HUD ²R² changes to flashing ²B².
A1-F18EA-NFM-000
III-10-18 CHANGE 1
10.5.11 Medium Altitude Checks (above 10,000 feet).
Altitude blocks are suggested ONLY to provide a logical sequence for the FCF procedures. Deviations
from these block altitudes are acceptable unless specified.
1. Cabin pressurization - CHECK (both cockpits)
Aircraft Altitude Cabin Altitude
· <8,000 feet Aircraft altitude (+0, -3,000 feet)
· 8,000 to 24,500 feet 8,000 feet (±500 feet)
2. Fuel transfer - CHECK INTERNAL and EXTERNAL
3. RALT - CHECK SET to 5,000 FEET
4. COMM - CHECK (both cockpits)
· Comm switches function normally.
· Both radios operative in transmit and receive.
· Preset and manual frequency selection operative.
5. 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.
6. Air refueling probe - CHECK
· Airspeed - Maintain below 300 KCAS.
a. PROBE switch - EXTEND
· Probe extends normally within 6 seconds.
b. PROBE switch - RETRACT
　
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