.  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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