***** Boeing 767 Normal Procedure Checklist *****

                               

                                             

 

PRE-FLIGHT

 

(ELCTRICAL POWER NOT ESTABLISHED)

 

Battery Switch                                              ON

 

Standby Power Selector                             AUTO

      Verify battery DISCH light illuminated and standby bus OFF light extinguishes.

 

Hydraulic  Electric Pump Switches          OFF

 

Hydraulic Demand Pump Selectors         OFF

 

Landing Gear Lever                                    DN

 

Alternate Flaps Selector                             NORM

 

Electrical Power                                           ESTABLISHED

  

APU Selector                                                START   

   or  

External Power Switch                               PUSH 

 

APU GEN Switch                                         ON

 

(ELECTRICAL POWER ESTABLISHED)

 

IRS                                                                 OFF, THEN  NAV

      Verify ALIGN Lights illuminated.

  

YAW Damper Switches                              ON

.

Electronic Engine Control Switches        ON

 

Hydraulic System                                         SET

  

Primary Engine Pump Switches               ON

  

Primary Electric Pump Switches               OFF

  

Demand Pump Selectors                           OFF

 

Electrical System                                         SET

  

Battery Switch                                              ON

      Verify DISCH Light extinguished.

 

Standby Power Selector                             AUTO

      Verify standby power bus OFF Light extinguished.

 

Bus Tie Switches                                         AUTO

      Verify AC BUS OFF and utility bus OFF Lights extinguished.

 

Generator Control Switches                      ON

 

Utility Bus Switches                                    ON

 

Ram Air Turbine UNLKD Light                  EXTINGUISHED

 

CAUTION:  SWITCH  ACTIVATION  WILL  CAUSE DEPLOYMENT OF RAM AIR TURBINE.

 

Engine Ignition Selector                             SINGLE

  Set on position 1 or 2

 

Fuel System                                                  SET

 

Fuel Pump Switches                                   OFF

 

Crossfeed Valve Switches                         OFF

      Verify VALVE Lights extinguished.

 

Wing  And Engine Anti-Ice Switches       OFF

 

Passenger Signs Selectors                       SET

 

No Smoking Selector                                  AUTO or ON

 

Seatbelts Selector                                        AUTO or ON

 

Air Conditioning System                            SET

 

APU and Engine Bleed Air Switches  ON 

      Verify APU VALVE Light extinguished.

 

Left, Center and Right Isolation Switches        ON

      Verify VALVE lights extinguished.

 

Pack Control Selectors                               AUTO 

      Verify PACK OFF lights extinguished.

 

Trim Air Switch                                             ON

 

Recirculation Fan Switches                      ON 

      Verify INOP Lights extinguished.

 

Compartment Temperature Controls        AUTO

      Set as desired and verify INOP Lights extinguished.

 

Flight Director Switch                                  ON

 

EICAS Display                                             CHECK

 

Secondary Engine Display                        ON 

      Verify primary and secondary engine indicators display existing conditions,

      oil quantity adequate for flight and no exceedance values displayed.

 

Status Display                                              ON 

      Verify  hydraulic  quantity  indications  do  not  display  RF

 

FMC                                                               ROUTE SET

  

Flight Instrument Control Panel                SET

 

HSI Range Selector                                    AS DESIRED

 

HSI Mode Selector                                       MAP

 

Map Switches                                               AS DESIRED

 

Speedbrake  Lever                                      DOWN

 

Thrust Levers                                                IDLE

 

Flap Lever                                                     SET

       Position lever to agree with flap position indicator.

 

Parking Brake                                               SET

      Observe PARK BRAKE light illuminated and indication on upper EICAS.

 

Stabilizer Trim Cutout Switches                NORM

 

Fuel Control Switches                                CUT OFF

 

Fire Extinguishing System                         CHECK

 

Engine and APU Fire Switches                IN

 

Cargo Fire Switches                                    OFF

 

Engine, Cargo, and APU

Fire Bottle Discharge Lights                      EXTINGUISHED 

 

Reserve Brake and Steering Switch        OFF

 

Standby Flight Instruments                        SET

 

Attitude Indicator                                          CHECK

      Verify proper attitude.

 

Airspeed Indicator                                        CHECK

      Verify proper speed.

 

Altimeter                                                        SET

      Set barometric indication. Verify Proper altitude.

  

Standby  Engine  Indicator Selector         AUTO

 

Auto Brakes Selector                                  OFF

 

VHF  Comms                                                SET

 

Instrument  Sources                                    CHECK

 

Flight Director Source Selector                 L *

 

NAV Source Selector                                  FMC L *

 

Alternate Source Switches                        OFF *

 

Flight Instruments                                        SET

 

Altimeter                                                        SET 

      Set barometric indication. Verify proper altitude and no flag .

 

Vertical Speed Indicator                             CHECK 

      Verify indication zero and OFF flag not in view.

 

Clock                                                              SET

 

ADI                                                                 CHECK 

      Verify proper attitude, flight director command bars, flight mode displays

      T0, T0, FD, proper airspeed, and no flags.

HSI                                                                 CHECK 

      Verify  magnetic  track,  present  heading,  appropriate  route  and  no  flags.

 

Airspeed Indicator                                        CHECK 

      Verify proper speed and no flags.

 

RDMI                                                              CHECK 

      Position  ADF/VOR  selectors,  as  desired.  Verify  present  heading  and  no

      inappropriate flags.

 

Autoland Status Annunciator                    CHECK

      Press on Test 1 then Test 2, verify indications then blank.

 

Alternate  Gear Extend Switch                  OFF

 

Alternate Flaps                                             CHECK

 

Alternate Flaps Selector                             NORM

 

Alternate Flaps Switches                           OFF

 

Ground Proximity / Configuration

Gear Override Switch                                  OFF

 

Ground  Proximity Flap Override Switch OFF

 

COCKPIT PREPARATION  FINAL

 

(This procedure is accomplished after papers are aboard and crew is ready for engine start.)

 

Fuel Loading                                                CHECK

 

Takeoff Thrust Reference                          SET

      Verify correct thrust reference mode displayed.

 

FMC                                                               SET

 

Wind (If required)                                         ENTER

 

Slope/Condition (If req)                              ENTER*

 

Acceleration Height                                     CHECK

 

Command Airspeed Bugs                          SET

 

Start Clearance                                            OBTAIN

  

Hydraulic System                                         SET

 

Electric Primary Pump Switches               ON

      Verify PRESS lights extinguished. 

 

Demand Pump Selectors                           AUTO

      Verify PRESS Lights extinguished.

 

Fuel Pump Switches                                   ON

      Position  switches  ON  for  all  tanks  containing  fuel  and  verify  left  and  right

      pump PRESS  Lights extinguished.

 

Pack  Control Selectors                              OFF

 

Trim                                                                SET

 

Flight Controls                                              CHECK

 

Secondary Engine Display                        ON

 

Accomplish remaining items on BEFORE START checklist.

 

PRE-FLIGHT CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

BEFORE START

 

RED ANTI-COLL LTS . . . . . . . . . . . . . .     ON

 

IRS . . . . . . . . . . . . . . . . . . . . . . . . . . . .         ALIGNED                 

 

CDU . . . . . . . . . . . . . . . . . . . . . . . . . . .         SET

 

MCP . . . . . . . . . . . . . . . . . . . . . . . . . . .         SET

 

FLIGHT INSTRUMENTS . . . . . . . . . . .      SET

 

SPEED BUGS . . . . . . . . . . . . . . . . . . . .      SET

 

STAB TRIM . . . . . . . . . . . . . . . . . . . . . .       SET

 

BEFORE START CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

AFTER START

 

ENG PARAMS . . . . . . . . . . . . . . . . . . .       CKD

 

APU . . . . . . . . . . . . . . . . . . . . . . . . . . . .        OFF

 

ENG / WING ANTI-ICE . . . . . . . . . . . . .      A/R

 

PACKS . . . . . . . . . . . . . . . . . . . . . . . . .        AUTO

 

L & R ISOL SWITCHES . . . . . . . . . . . .      OFF

 

GROUND EQUIPMENT . . . . . . . . . . . .     CLEAR

 

AFTER START CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

TAXI

 

AUTOBRAKE . . . . . . . . . . . . . . . . . . . .       RTO

 

FLIGHT CONTROLS . . . . . . . . . . . . . .       CKD

 

RECALL . . . . . . . . . . . . . . . . . . . . . . . .        CKD

 

TAXI CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

BEFORE TAKEOFF

 

TAKEOFF BRIEFING . . . . . . . . . . . . . .      DONE

 

COCKPIT WINDOWS . . . . . . . . . . . . .       LOCKED

 

FLAPS . . . . . . . . . . . . . . . . . . . . . . . . .         SET

 

AFDS T/O MODE . . . . . . . . . . . . . . . . .       ACTIVE

 

LDG LTS . . . . . . . . . . . . . . . . . . . . . . . .        ON

 

BEFORE TAKEOFF CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

AFTER TAKEOFF

 

LANDING GEAR . . . . . . . . . . . . . . . . . .      UP & OFF

 

FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . .       UP

 

AFDS LAT/VERT MODES . . . . . . . . . .     ACTIVE

 

CLB THRUST . . . . . . . . . . . . . . . . . . . .       SET

 

AFTER TAKEOFF CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

CLIMB

 

SEAT BELTS . . . . . . . . . . . . . . . . . . . .        AUTO

 

LDG LTS . . . . . . . . . . . . . . . . . . . . . . . .        OFF

 

ALTIMETERS . . . . . . . . . . . . . . . . . . . .       STD

 

CLIMB CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

DESCENT

 

SEAT BELTS . . . . . . . . . . . . . . . . . . . .        ON

 

FUEL QUANTITY/BALANCE . . .. . .         CKD

 

MCP / MSA ALT . . . . . . . . . . . . . . . . . .       SET / CKD

 

AUTOBRAKE . . . . . . . . . . . . . . . . . . . .       SET

 

DECENT CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

APPROACH

 

APP BRIEFING . . . . . . . . . . . . . . . . . . .      DONE

 

CDU . . . . . . . . . . . . . . . . . . . . . . . . . . .         SET

 

SPEED BUGS . . . . . . . . . . . . . . . . . . . .      SET

 

LDG LTS . . . . . . . . . . . . . . . . . . . . . . . .        ON

 

ALTIMETERS . . . . . . . . . . . . . . . . . . . .       SET QNH

 

RECALL . . . . . . . . . . . . . . . . . . . . . . . .        CKD

 

APPROACH CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

LANDING

 

LANDING GEAR . . . . . . . . . . . . . . . . . .      DOWN, 3

GREEN

 

FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . .       SET

 

SPEEDBRAKE . . . . . . . . . . . . . . . . . . .      ARMED

 

MAP ALT & G/A BRIEFING . . . . . . . . .      SET & DONE

 

LDG CLEARANCE….. . . . . . . . . . . . . .  RECEIVED

 

EMERGENCY LANDING BRIEFING….. DONE

 

LANDING CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

AFTER LANDING

 

APU . . . . . . . . . . . . . . . . . . . . . . . . . . . .        A/R

 

AUTOBRAKE . . . . . . . . . . . . . . . . . . . .       OFF

 

SPEEDBRAKE . . . . . . . . . . . . . . . . . . .      DOWN

 

FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . .       UP

 

LDG LTS . . . . . . . . . . . . . . . . . . . . . . . .        OFF

 

STAB TRIM . . . . . . . . . . . . . . . . . . . . . .       4 UNITS

 

AFTER LANDING CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

PARKING

 

PARKING BRAKE . . . . . . . . . . . . . . . . .     SET

 

ELECTRICAL POWER . . . . . . . . . . . . .     ESTD

 

LIGHTS . . . . . . . . . . . . . . . . . . . . . . . . .        ALL OFF

 

FUEL CONTROL SWITCHES . . . . . . .     CUTOFF

 

IRS . . . . . . . . . . . . . . . . . . . . . . . . . . . .         CHECK

 

HYDRAULIC SYSTEM . . . . . . . . . . . . .     SET

 

PASS SIGNS . . . . . . . . . . . . . . . . . . . .        OFF

 

FUEL PUMPS . . . . . . . . . . . . . . . . . . . .      OFF

 

ENG / WING ANTI-ICE . . . . . . . . . . . . .      OFF

 

PACKS . . . . . . . . . . . . . . . . . . . . . . . . .        A/R

 

L & R ISOL SWITCHES . . . . . . . . . . . .      ON

 

FLIGHT DIRECTORS . . . . . . . . . . . . . .     OFF

 

PARKING CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

SECURE

 

IRS . . . . . . . . . . . . . . . . . . . . . . . . . . . .         OFF

 

PACKS . . . . . . . . . . . . . . . . . . . . . . . . .        OFF

 

APU . . . . . . . . . . . . . . . . . . . . . . . . . . . .        OFF

 

once APU OFF and no external power selected

 

STBY PWR . . . . . . . . . . . . . . . . . . . . . .       OFF

 

BATTERY SW . . . . . . . . . . . . . . . . . . . .      OFF

 

SECURE CHECKLIST COMPLETED

 

----------------------------------------------------------------------------------------------------

 

----------------------------------------------------------------------------------------------------

 

 

       Abnormal Procedure Checklist

 

 

ELECTRICAL

 

AC BUS(ES) OFF

Message:       L or R AC BUS                                 OFF

Light:              L and/or R BUS                                OFF

 

GENERATOR CONTROL SWITCH(ES)             OFF THEN ON

            Attempt one reset of the generator control switch(es).

 

APU (If Available)                                                    START

            After APU RUN Light illuminates and APU GEN OFF Light remains extinguished:

 

BOTH BUS TIE SWITCHES                                  OFF THEN AUTO

            Attempt one reset of the Bus Tie switches.

            If both BUS OFF Lights were illuminated and AC power is restored:

            Reactivate FMC route and reenter performance data. Select ATT mode on IRS(s)

            with ALIGN Light(s) illuminated.

            If one BUS OFF Light remains illuminated:

            Flight in icing conditions may result in some erroneous flight instrument

            indications. [Associated probe heat inoperative.]

            Left BUS OFF Light illuminated:

            L and C autopilots inoperative. L and C flight directors inoperative.

            Right BUS OFF Light illuminated:

            R autopilot/flight director inoperative.

            If both BUS OFF Lights remain illuminated:

            If EEC Inoperative Lights illuminated:

 

THRUST LEVERS                                                   RETARD TO MID

 

ELECTRONIC ENGINE

CONTROL SWITCHES                                          OFF*

            Turn both EEC switches to OFF*.

            Accomplish this action methodically, one switch at a time*.

            If engine inoperative:

 

FUEL CROSSFEED VALVE SWITCHES           OPEN

 

FLIGHT DECK TEMPERATURE CONTROL      MAN*

            Master caution inoperative.

            Antiskid for outboard wheels inoperative braking effectiveness reduced, brake

            with caution.

            Auto speedbrake inoperative - deploy speedbrakes manually after Landing.

 

STANDBY BUS OFF

Message:                                                                   STANDBY BUS OFF

Light:                                                                          OFF

 

STANDBY POWER SELECTOR                          BAT

            The battery will provide standby bus power for approximately 30 minutes.

            If standby power bus OFF light remains illuminated and right AC bus power is

            available:

 

STANDBY POWER SELECTOR                          AUTO

 

GENERATOR DRIVE

Message:                                                                   L or R GEN DRIVE

Light:                                                                          DRIVE

 

GENERATOR DRIVE

DISCONNECT SWITCH                                         PUSH

 

APU (If Available)                                                    START

 

GENERATOR OFF

Message:                                                                   L or R GEN OFF

or APU GEN OFF

Light:                                                                          OFF

 

H

 

GENERATOR CONTROL SWITCH

(APU/Engine)                                                           OFF THEN ON

            If engine generator control OFF light remains illuminated:

 

----------------------------------------------------------------------------------------------------

 

HYDRAULIC

 

HYDRAULIC OVERHEAT

E

 

Message:                                                                   L, C, or R DEM HYD OVHT, L

or         R PRIM HYD OVHT,C HYD 1

or         C HYD 2 OVHT

Light:                                                                          OVHT

 

PUMP SWITCH/SELECTOR                                 OFF

 

HYDRAULIC PUMP

 

Message:                                                                   L, C or R HYD DEM PUMP,L

or         R HYD PRIM PUMP,

C HYD PRIM 1

or         2

 

Light:                                                                          PRESS

            If primary pump PRESS Light illuminated:

 

PRIMARY PUMP SWITCH                                    OFF

            If demand pump PRESS light illuminated:

 

DEMAND PUMP SELECTOR                               ON

            If PRESS light remains illuminated:

 

DEMAND PUMP SELECTOR                               OFF

 

HYDRAULIC SYSTEM(S) PRESSURE

 

Message:                                                                   L, C

or         R HYD SYS PRESS

 

Light:                                                                          SYS PRESS

 

DEMAND PUMP SELECTOR(S)

(Affected System(s))                                                ON

            If SYS PRESS light remains illuminated:

 

PUMP SWITCH(ES) & SELECTOR(S)

(Affected Pumps)                                                     OFF

            Turn off pumps with PRESS lights illuminated.

 

If L system only inoperative:

            L autopilot inoperative

 

If C system only inoperative:

            Automatic speedbrake inoperative

            C autopilot inoperative

            R autopilot stabilizer trim inoperative.

            Use flaps 20 and VREF 20 for landing Accomplish C SYSTEM INOPERATIVE

            LANDING PREPARATION

 

If R system only inoperative:

            Auto brakes inoperative

            R autopilot inoperative

 

If L and R systems inoperative:

            Auto brakes inoperative

            L and R autopilots inoperative

            Crosswind limit 20 knots.

            Use flaps 20 and VREF 30 + 20 knots for landing

 

GROUND PROXIMITY FLAP

OVERRIDE SWITCH                                              OVRD

 

If L and C systems inoperative:

            Automatic speedbrake inoperative

            Elevator feel inoperative

            ALL autopilots inoperative

            Crosswind Limit 20 knots

            Use flaps 20 and VREF 30 + 20 knots for landing

            Accomplish C SYSTEM INOPERATIVE LANDING PREPARATION

 

If C and R systems inoperative:

            Automatic speedbrake inoperative

            Normal brakes inoperative

            Primary source to alternate brakes inoperative

            Auto brakes inoperative

            C and R autopilots inoperative

            Crosswind limit 20 knots

            Use flaps 20 and VREF 30 + 20 knots for landing.

            Accomplish C SYSTEM INOPERATIVE LANDING PREPARATION

            C SYSTEM INOPERATIVE LANDING PREPARATION

            ALTERNATE FLAP OPERATION:

 

GROUND PROXIMITY FLAP

OVERRIDE SWITCH                                              OVRD

 

ALTERNATE FLAPS SELECTOR                        SET

            Position to agree with flap Lever.

 

ALTERNATE FLAPS SWITCHES                        ALTN

 

ALTERNATE FLAPS SELECTOR                        SET

            Extend or retract flaps as required.

 

ALTERNATE GEAR EXTENSION:

 

LANDING GEAR LEVER                                       OFF

 

ALTERNATE GEAR EXTENSION

SWITCH (Max 250K-.75M)                                     DN

            After gear down Lights illuminate:

 

LANDING GEAR LEVER                                       DN

 

RESERVE BRAKES/STEERING SWITCH        ON

            NOTE: If No. 1 Center Primary Hydraulic pump PRESS Light remains

            illuminated, Reserve Brakes and Nose Wheel Steering are inoperative.

 

ANTISKID (FAULT)*

 

Message:                                                                   ANTISKID*

 

Light:                                                                          ANTISKID*

            Braking effectiveness is reduced, brake with caution*.

 

BRAKE SOURCE

 

Message:                                                                   BRAKE SOURCE

 

Light:                                                                          BRAKE SOURCE

 

RESERVE BRAKES/STEERING SWITCH        ON

 

If BRAKE SOURCE light remains illuminated:

AUTO BRAKES SELECTOR                                 OFF

            Only accumulator pressure available for brakes; apply steady increasing

            brake pressure and hold to full stop.

 

GEAR DISAGREE

 

Message:                                                                   GEAR DISAGREE

 

Light:                                                                          GEAR

            NOTE: Do not use FMC fuel predictions with Landing gear extended If gear Lever UP:

            bserve EXTEND OR EXTENDED Limit speed (270K.82M).

            If gear Lever DN and all gear down (green) Lights illuminated:

            Accomplish normal Landing.

            If gear Lever DN and any gear down (green) Light(s) not illuminated:

 

LANDING GEAR LEVER                                       OFF

 

ALTERNATE GEAR EXTENSION SWITCH

(Maximum 250K-.75M)                                            DN

            If all gear down Lights illuminated:

 

LANDING GEAR LEVER                                       DN

            If any gear down (green) light(s) not illuminated:

            - Use flaps 30 for Landing.

            - Use manual speedbrake after landing.

 

LANDING GEAR LEVER                                       DN

 

GROUND PROXIMITY/CONFIGURATION

GEAR OVERRIDE SWITCH                                   OVRD

            At pattern altitude:

 

PACK CONTROL SELECTORS                           OFF

 

FUEL PUMP SWITCHES                                       OFF

 

----------------------------------------------------------------------------------------------------

 

FLIGHT CONTROLS

 

LEADING EDGE SLAT DISAGREE

 

Message:                                                                   LE SLAT DISAGREE

 

Light:                                                                          LEADING EDGE

 

GROUND PROXIMITY FLAP

OVERRIDE SWITCH                                              OVRD

            If indicated flap position greater than 20:

            Use existing flaps and VREF 20 for Landing.

            If indicated flap position 20 or less:

            Use flaps 20 and VREF 20 for landing.

 

ALTERNATE FLAPS SELECTOR                        SET

            Position to agree with flap Lever.

 

LEADING AND TRAILING EDGE

ALTERNATE FLAPS SWITCHES                        ALTN

 

CAUTION: IF, AFTER SELECTING ALTN, THE LEADING EDGE OR TRAILING

EDGE LIGHT REMAINS ILLUMINATED, POSITION THE ASSOCIATED ALTERNATE

FLAPS SWITCH OFF AND ACCOMPLISH THE APPLICABLE ASYMMETRY PROCEDURE.

 

ALTERNATE FLAPS SELECTOR                        SET

            Extend or retract flaps as required.

 

TRAILING EDGE FLAP DISAGREE

 

Message:       TE FLAP DISAGREE

 

Light:              TRAILING EDGE

 

GROUND PROXIMITY FLAP

OVERRIDE SWITCH                                              OVRD

            If indicated flap position greater than 20:

            Use existing flaps and VREF 20 for landing

            If indicated flap position 20 or less:

            Use flaps 20 and VREF 20 for Landing.

 

ALTERNATE FLAPS SELECTOR                        SET

            Position to agree with flap Lever.

 

LEADING AND TRAILING EDGE

ALTERNATE FLAPS SWITCHES                        ALTN

 

CAUTION: IF, AFTER SELECTING ALTN, THE LEADING EDGE OR TRAILING

EDGE LIGHT REMAINS ILLUMINATED, POSITION THE ASSOCIATED ALTERNATE

FLAPS SWITCH OFF AND ACCOMPLISH THE APPLICABLE ASYMMETRY PROCEDURE.

 

ALTERNATE FLAPS SELECTOR                        SET

            Extend or retract flaps as required.

 

LEADING EDGE SLAT ASYMMETRY

 

Message:                                                                   LE SLAT ASYM

 

Light:                                                                          LEADING EDGE

 

CAUTION: DO NOT ARM ALTERNATE LEADING EDGE FLAPS

 

GROUND PROXIMITY FLAP

OVERRIDE SWITCH                                              OVRD

            NOTE: Do not use FMC fuel predictions with flaps extended.

            If indicated flap position greater than 20:

            Use existing flaps and maintain VREF 30 + 20 knots minimum for landing.

            If indicated flap position 20 or less:

            Use trailing edge flaps 20 and VREF 30 + 30 knots for landing.

 

ENGINE START SELECTORS                             CONT

 

ALTERNATE FLAPS SELECTOR                        SET

            Position to agree with flap Lever.

 

ALTERNATE FLAPS SWITCH

(Trailing Edge)                                                          ALTN

 

ALTERNATE FLAPS SELECTOR                        SET

            Extend or retract trailing edge flaps as required.

 

TRAILING EDGE FLAP ASYMMETRY

 

Message:                                                                   TE FLAP ASYM

 

Light:                                                                          TRAILING EDGE

 

CAUTION: DO NOT ARM ALTERNATE TRAILING EDGE FLAPS.

 

GROUND PROXIMITY FLAP

OVERRIDE SWITCH                                              OVRD

            NOTE: Do not use FMC fuel predictions with flaps extended.

            If indicated flap position 5 or Less, use VREF 30 + 30 knots for landing.

            If indicated flap position between 5 and 20, use VREF 30 + 20 knots for Landing.

            If indicated flap position at or greater than 20, use VREF 20 for Landing.

 

NO FLAP AND NO SLAT LANDING

This procedure is to be used when no flaps and no slats are extended (ALTNextension failed).

 

ENGINE START SELECTORS                             FLT

 

GND PROX FLAP OVRD SWITCH                      OVRD

            The Too Low Terrain and Too Low Flaps advisories are inhibited.

APPROACH PREPARATION

            Maneuver at Flaps 30 VREF + 80 knots until on final approach.

            Use longest runway available. Recommend a 10-mile final.

            If ILS available, the autopilot may be used for approach. Autoland is not

            recommended.

LANDING PREPARATION

            Use Flaps 30 VREF + 50 knots for landing. Autobrakes, if operative, must be

            used when braking action is reported to be less than good, or on wet/slippery

            runways, or on runways 7,000 feet or less in length. On dry runways greater

            than 7,000 feet in length, the autobrake system is not required but may be

            used at Captain's discretion.Arm Speed Brakes.Extend landing gear at first indication of             G/S movement.When landing is assured (100 feet AFL), retard throttles to idle.

 

----------------------------------------------------------------------------------------------------

 

PNEUMATICS

 

BLEED DUCT LEAK

 

Message:                                                                   L or R BLD DUCT LEAK

 

Light:                                                                          DUCT LEAK

            Condition: Bleed air Leak detected in the Left or right pneumatic duct.

 

ENGINE BLEED AIR SWITCH

(Affected side)                                                          OFF

 

ISOLATION SWITCH (Affected side)                   OFF

 

WING ANTI-ICE SWITCH                                       OFF

            Avoid icing conditions.

            Do not use wing anti-ice.

 

CAUTION: Flight beyond 6 hours with a DUCT LEAK Light illuminated may result in structural damage.

 

ENGINE BLEED OFF

 

Message:                                                                   L or R ENG BLEED OFF

 

Light:                                                                          OFF

            If wing anti-ice required:

 

ONE PACK CONTROL SELECTOR                    OFF

 

ISOLATION SWITCH (Affected Side)                   ON

            Return to OFF when wing anti-ice is no Longer required.

            Thrust reverser (affected side) may be inoperative.

 

ENGINE BLEED OVERHEAT*

 

Message:       L or R ENG BLD OVHT*

 

Light:              OVHT*

 

ENGINE BLEED AIR SWITCH

(Affected side)                                                          .OFF THEN ON*

            Select to ON after thrust is reduced for cruise.

            If OVHT Light remains illuminated or re-illuminates*:

 

ENGINE BLEED AIR SWITCH

(Affected side)                                                          OFF*

            If wing anti-ice required*:

 

ONE PACK CONTROL SELECTOR                    OFF*

 

ISOLATION SWITCH (Affected side)                   ON*

            Return to OFF when wing anti-ice is no longer required*.

            Thrust reverser (affected side) inoperative*.

 

----------------------------------------------------------------------------------------------------

 

RAPID DEPRESSURIZATION /CABIN ALTITUDE

            NOTE: CABIN ALTITUDE EICAS message and CABIN ALT light will display if cabin

            altitude exceeds 10,000 feet.

 

C ISLN VALVE                                                         CLOSE

 

ENGINE BLEED VALVES                                     CHECK OPEN

 

PACK CONTROL SELECTORS                           CHECK AUTO

 

L AND R ISLN VALVES                                         CHECK CLOSED

            If not arrested by 10.000 ft cabin altitude:

            INITIATE EMERGENCY DESCENT

 

EMERGENCY DESCENT

 

AUTOTHROTTLE                                                    AS DESIRED

 

THROTTLES                                                             CLOSE

 

SPOILER HANDLE                                                 FULL AFT

 

NO SMOKING AND SEAT BELT SIGN               ON

            Descent straight ahead or initiate moderate bank (max 30°)

 

TARGET SPEED                                                     MAX Vmo

 

ENGINE START SELECTORS                             FLT

            - Advise passengers to: Use oxygen; Fasten seat belts; No smoking. Make the

            following announcement: "Ladies and gentlemen, pull down and use your

            oxygen masks. Fasten your seatbelts and no smoking please."

            - When time permits: Advise Flight Attendants if cabin altitude remains above

            10,000 feet for an extended period. Advise Flight Attendants when cabin

            altitude is below 10,000 feet.

NOTES:

            1. The above procedure assumes structural integrity of the aircraft. If

            structural integrity is in doubt, limit airspeed as much as possible and avoid

            high maneuvering loads until structural integrity has been verified.

            2. Level-Off (If not in FL CH mode)

            - Start reducing rate of descent approximately 2,000 feet above desired

            level-off altitude.

            - Retract speed brakes approximately 1,000 feet above desired level-off

            altitude, or as desired to control airspeed and level-off.

            3. Level-Off (Using FL CH mode)

            - Retract speed brakes approximately 1,000 feet above desired level-off

            altitude, or as desired to control airspeed and level-off.

            4. After Level-Off

            - Speed Brakes - Check retracted

            - Engine Start Selectors - As Required

 

----------------------------------------------------------------------------------------------------

 

ENGINES

 

ENGINE FIRE, SEVERE DAMAGE OR SEPARATION

 

Message:                                                       L or R ENGINE FIRE

 

Light:                                                              LEFT or RIGHT engine fire switch

and associated fuel control switch.

            Condition: Airframe vibrations with abnormal engine indications.

 

THRUST LEVER                                         CLOSE

            Disengage autothrottle if on.

 

FUEL CONTROL SWITCH                        CUT OFF

 

ENGINE FIRE SWITCH                              PULL

            If engine fire warning light remains illuminated:

 

ENGINE FIRE SWITCH                              ROTATE

            Rotate to the stop and hold for 1 second.

            After 30 seconds, if engine fire warning Light remains illuminated:

 

ENGINE FIRE SWITCH                               ROTATE TO

 

REMAINING BOTTLE

            Rotate to the stop and hold for 1 second.

            If high airframe vibration occurs and continues after engine is shut down:

            Without delay, reduce airspeed and descend to a safe altitude which results in

            an acceptable vibration level. If high vibration returns and further airspeed

            reduction and descent is not practical, increasing the airspeed may reduce the

            vibration.

 

APU (If Available)                                        START

 

GROUND PROXIMITY FLAP

OVERRIDE SWITCH                                  OVRD

            If wing anti-ice required:

 

ONE PACK CONTROL SELECTOR        OFF

 

ISOLATION SWITCH (Affected Side)       ON

            Return to OFF when wing anti-ice is no longer required.

            LANDING PREPARATION

            Use flaps 20 and VREF 20 for landing and flaps 5 for go-around.

            Condition: - Engine failure or flameout

            - Engine parameters cannot be maintained within Limits

            - When prescribed by other non-normal procedure

 

THRUST LEVER                                         CLOSE

            Engine conditions permitting, operate at idle for 2 minutes to allow engine

            to cool and stabilize. Disengage autothrottle if on.

 

FUEL CONTROL SWITCH                        CUT OFF

 

APU (If Available)                                        START

 

GROUND PROXIMITY FLAP

OVERRIDE SWITCH                                  OVRD

            If wing anti-ice required:

 

ONE PACK CONTROL SELECTOR        OFF

 

ISOLATION SWITCH (Affected Side)       ON

            Return to OFF when wing anti-ice is no longer required.

            LANDING PREPARATION

            Use flaps 20 and VREF 20 for landing and flaps 5 for go-around.

 

 

LOSS OF THRUST ON BOTH ENGINES

            Condition: Thrust or thrust lever response is Lost from both engines.

 

ENGINE START SELECTORS                 FLT

            NOTE: Takoff EGT limit is in-flight start EGT Limit.

 

RAM AIR TURBINE                                     UNLKD

 

AIRSPEED                                                   KTS

            Above 30,000 ft - 240 kts

            30,000 ft or below - 220 kts minimum

NOTE: OVSPD light and associated aural warning will indicate Vmo/Mmo exceedances.

            If engines do not recover:

 

THRUST LEVERS                                       CLOSE

 

FUEL CONTROL SWITCHES                   CUT OFF THEN RUN

Repeat until engine start achieved; remain approximately 30 seconds in each position during start attempts.

 

APU (If Available)                                        START

            After restoring AC power, reactivate FMC route and reenter performance data.

            Select ATT mode on IRS(s) with ALIGN lights) illuminated.

NOTE: Cabin altitude warning may occur during descent.

 

 

ENGINE IN-FLIGHT START

Condition: Following a shutdown or flameout when fire or apparent damage has not occurred.

 

ALTITUDE AND AIRSPEED                     CHECK

            Starts not assured outside EICAS envelope.

            If X-BLD not displayed:

 

ENGINE START SELECTOR                    FLT

 

FUEL CONTROL SWITCH                        RUN

            Abort start if EGT fails to rise within 45 seconds.

            If X-BLD displayed:

 

ONE PACK CONTROL SELECTOR        OFF

 

ISOLATION SWITCH (Affected Side)       ON

 

IGNITION SELECTOR                                BOTH

 

ENGINE START SELECTOR                    GND

 

FUEL CONTROL SWITCH                        RUN

            Select when N2 exceeds Fuel On Command bug [15%]. Abort start if EGT

            fails to rise within 45 seconds.

            After engine started:

 

ENGINE START SELECTOR                    AUTO

 

PACK CONTROL SELECTORS               AUTO

 

LEFT AND RIGHT ISOLATION

SWITCHES                                                   OFF

 

GROUND PROXIMITY FLAP

OVERRIDE SWITCH                                  OFF

 

----------------------------------------------------------------------------------------------------

 

TAKE OFF AND LANDING

 

PASSENGER EVACUATION

            Condition: The situation requires the evacuation of the passengers and crew.

 

PARK BRAKE                                              SET

 

ALL ENGINE AND APU FIRE

SWITCHES                                                   OVERRIDE,

 

PULL & ROTATE

            Rotate engine fire switches in opposite directions

 

PASSENGER EVACUATION                   INITIATE

            Initiate the evacuation by informing the tower and flight attendants of

            passenger evacuation.

 

DITCHING PREPARATION

            Condition: The flight conditions require airplane ditching and evacuation

 

DISTRESS SIGNAL                                    TRANSMIT

 

CREW AND PASSENGERS                     ADVISE

            Below 5,000 feet:

 

GROUND

PROXIMITY/CONFIGURATION

GEAR OVERRIDE SWITCH                      OVRD

 

PACK CONTROL SELECTORS               OFF

 

NO SMOKING SIGNS SELECTOR          ON

 

Final Approach

(Omit LANDING CHECKLIST):

 

PASSENGER CABIN                                 SECURED

 

LANDING GEAR LEVER                           UP & OFF

 

FLAPS                                                           30

            Advise cabin crew of imminent touchdown.

            Maintain airspeed at VREF. Flare airplane to achieve minimum rate of descent

            at touchdown.