. IF Icing Conditions Are Encountered For More Than 2 Minutes:
Add 5 knots to all minimum maneuvering speeds. Do not extend flaps beyond 28° / EXT as a decrease in aircraft controllability may result.
Note: If on final approach with flaps 40° / EXT and aircraft in trim at time of electrical loss, flaps may be left at 40°.
Landing Data, Bugs........................ C+F.........................CHECKED, SET
CAB ALT Control
Lever, Wheel...................................................................LOCKED DOWN FULLY AFT (OPEN)
Approach Briefing, Harness...........................................COMPLETE, ON
- - - - - APPROACH - - - - -
Altimeters & Bugs........................... C+F.............................................. SET
VHF NAV-1 Radio, Course ............ C+F........................... I.D., INBOUND
(Continued)
- - - - - LANDING - - - - -
Gear Lever.................................. C+F............................................. DOWN
Check nose gear indicator is elevated.
Ignition .............................................................................................. OVRD
Flap / Slat Handle....................... C+F...........LANDING FLAP SETTING
Do not reduce approach thrust until landing flare has been initiated and sink rate has been reduced. After main gear touchdown, manually deploy ground spoilers. After nose wheel touchdown, use reverse thrust and manual braking as required.
Annunciator Panel, Cabin PA ........................CHECKED, COMPLETED
- - - - - 30 SECONDS PRIOR TO TOUCHDOWN - - - - -
EMER LTS Switch .................................................................................ON
* * * *
AIRCRAFT SYSTEMS STATUS DURING FLIGHT ON EMERGENCY POWER
AIR CONDITIONING / PRESSURIZATION
OPERATIVE PNEU press gauge / manual temp control / manual press control / air cond flow control valves / air cond regulator valves / max press relief valves / 8th stage bleed air / cabin altimeter/ max diff press gauge / cabin climb ind INOPERATIVE augmentation valves / AIR COND SHUTOFF system / radio rack fans / ram air valve / cabin press warning light & horn / primary & standby pressurization systems / FLOW light / transfer lockout / auto temp control
APU
OPERATIVE APU control / door control / fire warning / EGT / oil pressure / oil temp INOPERATIVE
ELECTRICAL
OPERATIVE AC EMER bus / DC EMER bus / DC transfer bus* / battery bus* / battery direct bus (* BATT switch must be on) INOPERATIVE L&R GEN bus / L&R AC bus / L&R DC bus / ground service bus
FIRE WARNING & PROTECTION
OPERATIVE all fire detection, warning & extinguishing INOPERATIVE agent low lights
FLIGHT CONTROLS / AUTOFLIGHT
OPERATIVE primary flight controls / OVRD function of mach trim / flaps / slats (mid only) / speed brakes / ground spoilers (manual only) / aileron & rudder trim INOPERATIVE stabilizer trim / autopilot trim / stall warning / stick pusher / airspeed warning / flap & slat indicator lights / auto ground spoilers / yaw damper / mach trim / autopilot / autothrotles / autoland
FUEL
OPERATIVE main tank fuel (suction feed) / DC start pump / crossfeed lever INOPERATIVE all AC boost pumps / fuel heat / center & aux tank fuel / all fuel gauges & lights
HYDRAULICS / LANDING GEAR / BRAKES
OPERATIVE engine hyd pumps HI press only / transfer pump (if on at time of electrical power loss) / landing gear with normal extension / nose gear indicator / manual brakes INOPERATIVE aux hyd pump / transfer pump (if off at time of electrical power loss) / all hyd gauges & lights / landing gear lights & warning horn / anti-skid / autobrakes
(Continued)
AIRCRAFT SYSTEMS STATUS DURING FLIGHT ON EMERGENCY POWER
ICE & RAIN PROTECTION
OPERATIVE Capt pitot heat / engine anti-ice if on at time of electrical power loss INOPERATIVE all pitot & vane heaters except Capt / engine anti-ice if off at time of electrical power loss / windshield anti-fog & anti-ice / airfoil anti-ice
INSTRUMENTS / NAVIGATION / COMMUNICATION
OPERATIVE Capt HSI, ADI, altimeter, IVSI, airspeed, mach / FO RMI / DG-1 / VG-1 / air data computer-1 / VHF NAV-1 / VHF COMM-1 / glideslope-1 / flight interphone / PA / MAG compass / standby ADI / compass, radio nav, aux vert gyro switching (if installed) / autopilot & autothrottle OFF lights / master warning & caution lights INOPERATIVE Capt RMI / FO HSI, ADI, altimeter, IVSI, airspeed, mach / DG-2 / VG-2 / air data computer-2 / VHF NAV-2 / VHF COMM-2&3 / glideslope-2 / ADF-1&2 / DFGC-1&2 / flight directors / all ATS & FGS functions / both FMA’s / all digital lights / altitude alert lights & aural warning / DME / PMS / marker beacon / SELCAL / transponder / flight recorder / radar / TCAS / CVR
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本文链接地址：MD-80 Flight Manual 麦道80飞行手册 1(45)
