In rear cockpit -
g. EMERG LDG GEAR handle - ROTATE 45° CCW and PUSH FULL IN
6. AOA warning tone - CHECK
With gear down and flaps HALF -
a. Increase AOA toward 15°.
· AOA warning tone comes on at 14 ± 0.5°
7. PA throttle transients - 10,000 feet (INDIVIDUALLY)
With gear down, flaps HALF, and at onspeed AOA -
a. Throttle affected engine - IDLE to MAX
· Afterburner lights within 8 seconds.
b. Throttle affected engine - MAX to IDLE, pause 3 seconds, IDLE to MAX
· Afterburner lights within 8 seconds.
· Engine responds smoothly with no stall, stagnation, or flameout.
c. Repeat steps a and b for opposite engine
8. LDG GEAR handle - UP
9. Wheels warning - CHECK
a. Descend below 7,500 feet MSL
b. Reduce airspeed below 175 KCAS.
c. Establish rate of descent greater than 250 fpm.
· Landing gear warning light flashes.
· Landing gear warning tone sounds.
10.5.13 High Altitude (above 30,000 feet).
1. Cabin pressurization - MONITOR
Above 24,500 feet MSL, cabin pressurization shall remain within 5 psi differential of actual
altitude. A rule of thumb is altitude x 0.4.
Aircraft Altitude Cabin Altitude
· Less than 30,000 feet 10,000 to 12,000 feet
· 40,000 feet 15,000 to 17,000 feet
2. Throttle transients - 35,000 ± 2,000 feet (INDIVIDUALLY)
a. ENG ANTI ICE switch - CHECK OFF
b. Airspeed - Maintain 200 to 220 KCAS
A1-F18EA-NFM-000
III-10-24 ORIGINAL
c. Throttle affected engine - IDLE to MAX
· Afterburner lights within 12 seconds.
d. Throttle affected engine - MAX to IDLE, pause 3 seconds, IDLE to MAX
· Afterburner lights within 12 seconds.
· Engine responds smoothly with no stall, stagnation, or flameout.
e. Repeat steps a thru d for opposite engine
10.5.14 10,000 Feet to Landing.
1. Fuel transfer - CHECK (throughout flight)
With external fuel available -
· External fuel transfers normally.
· Internal tanks fill/stay near full.
With external tanks empty -
· Tank 1 depletes to approximately 1,000 lb prior to wing tanks depleting.
When wing tanks are empty -
· Tanks 1 and 4 fall in approximately ¼ ratio.
· No FUEL XFER caution.
With fuel in tanks 1 and 4 -
· Feed tanks stay at or near full (2,100 to 2,450 lb).
2. RALT operation - CHECK
During descent through 5,000 feet AGL -
· Low altitude warning correctly comes on.
· Radar altitude tracks correctly during descent.
3. TCN or WYPT course intercept - PERFORM
· Course deviation indicator in HUD corresponds with steering arrow on MPCD
4. ILS/ACLS operation - CHECK (if available)
· Proper ILS and/or ACLS indications.
10.5.15 Landing Checks.
1. Landing checklist - COMPLETE
2. ATC approach mode - CHECK
· ATC advisories in HUD when selected.
· Throttles respond correctly.
· Holds onspeed AOA during turns and on approach.
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III-10-25 ORIGINAL
10.5.16 After Landing Checks.
1. Anti-skid system - CHECK
Above 75 KGS on landing -
a. Brake pedals - Apply full brake pressure
· Anti-skid cycles smoothly.
· No left or right pulling tendencies.
When clear of active runway -
2. Ejection seat SAFE/ARMED handle(s) - SAFE (both cockpits)
3. EJECTION MODE handle - NORM (rear cockpit)
4. Landing gear handle mechanical stop - FULLY ENGAGED
5. FLAP switch - AUTO
6. T/O TRIM button - PRESS UNTIL TRIM ADVISORY DISPLAYED
7. Mask(s) - OFF (both cockpits)
8. OXY FLOW knob(s) - OFF (both cockpits)
9. OBOGS control switch - OFF
10. Canopy - EITHER FULL UP OR FULL DOWN FOR TAXI
10.5.17 Before Engine Shutdown Checks.
1. PARK BRK handle - SET
2. BIT display - RECORD DEGD/FAIL INDICATIONS
3. BIT/HYDRO-MECH page - VERIFY absence of FADEC fault codes
4. Radar maintenance (BOA) codes - RECORD IF PRESENT
5. RADAR knob - OFF
6. FCS display - RECORD BLIN CODES
7. EFD - RECORD MSP CODES
8. INS - PERFORM POST FLIGHT UPDATE
· Maximum error is 1.5 nm per hour of operating time.
9. INS knob - OFF
10. Sensors, avionics, and CVRS - OFF (both cockpits)
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III-10-26 ORIGINAL
11. EXT and INTR lights knobs - OFF (both cockpits)
12. Canopy - CHECK CLEAR/OPEN
10.5.18 Engine Shutdown Checks.
1. Brake accumulator gauge - CONFIRM 3,000 PSI
2. Paddle switch - PRESS (disengage NWS)
3. Confirm 5 minute engine cool down.
4. BLEED AIR knob - OFF
5. Throttle - OFF (alternate sides)
6. Verify proper switching valve operation.
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本文链接地址：NATOPS Flight Manual 飞行手册 2
