在线看免费❗_日本免费中文字幕一区_.手.动.输.入.网.址.联.系.客.服.人.员.lanan_shell
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. A1-F18EA-NFM-000 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) A1-F18EA-NFM-000 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. www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：NATOPS Flight Manual 飞行手册 2
