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.
----------------------------------------------------------------------------------------------------
RED
ANTI-COLL LTS . . . . . . . . . . . . . . ON
IRS . . . .
. . . . . . . . . . . . . . . . . . . . . . . . ALIGNED
CDU . . . .
. . . . . . . . . . . . . . . . . . . . . . . SET
MCP . . . .
. . . . . . . . . . . . . . . . . . . . . . . SET
FLIGHT
INSTRUMENTS . . . . . . . . . . . SET
SPEED BUGS
. . . . . . . . . . . . . . . . . . . . SET
STAB TRIM .
. . . . . . . . . . . . . . . . . . . . . SET
----------------------------------------------------------------------------------------------------
ENG PARAMS
. . . . . . . . . . . . . . . . . . . CKD
APU . . . .
. . . . . . . . . . . . . . . . . . . . . . . . OFF
ENG / WING
ANTI-ICE . . . . . . . . . . . . . A/R
PACKS . . .
. . . . . . . . . . . . . . . . . . . . . . AUTO
L & R
ISOL SWITCHES . . . . . . . . . . . . OFF
GROUND
EQUIPMENT . . . . . . . . . . . . CLEAR
AUTOBRAKE .
. . . . . . . . . . . . . . . . . . . RTO
FLIGHT
CONTROLS . . . . . . . . . . . . . . CKD
TAKEOFF
BRIEFING . . . . . . . . . . . . . . DONE
COCKPIT WINDOWS
. . . . . . . . . . . . . LOCKED
FLAPS . . .
. . . . . . . . . . . . . . . . . . . . . . SET
AFDS T/O
MODE . . . . . . . . . . . . . . . . . ACTIVE
LDG LTS . .
. . . . . . . . . . . . . . . . . . . . . . ON
LANDING
GEAR . . . . . . . . . . . . . . . . . . UP
& OFF
FLAPS . . .
. . . . . . . . . . . . . . . . . . . . . . . UP
AFDS
LAT/VERT MODES . . . . . . . . . . ACTIVE
CLB THRUST
. . . . . . . . . . . . . . . . . . . . SET
SEAT BELTS
. . . . . . . . . . . . . . . . . . . . AUTO
LDG LTS . .
. . . . . . . . . . . . . . . . . . . . . . OFF
ALTIMETERS
. . . . . . . . . . . . . . . . . . . . STD
SEAT BELTS
. . . . . . . . . . . . . . . . . . . . ON
FUEL
QUANTITY/BALANCE . . .. . . CKD
MCP / MSA
ALT . . . . . . . . . . . . . . . . . . SET / CKD
AUTOBRAKE .
. . . . . . . . . . . . . . . . . . . SET
APP
BRIEFING . . . . . . . . . . . . . . . . . . . DONE
CDU . . . .
. . . . . . . . . . . . . . . . . . . . . . . SET
SPEED BUGS
. . . . . . . . . . . . . . . . . . . . SET
LDG LTS . .
. . . . . . . . . . . . . . . . . . . . . . ON
ALTIMETERS
. . . . . . . . . . . . . . . . . . . . SET
QNH
RECALL . .
. . . . . . . . . . . . . . . . . . . . . . CKD
LANDING
GEAR . . . . . . . . . . . . . . . . . . DOWN,
3
GREEN
FLAPS . . .
. . . . . . . . . . . . . . . . . . . . . . . SET
SPEEDBRAKE
. . . . . . . . . . . . . . . . . . . ARMED
MAP ALT
& G/A BRIEFING . . . . . . . . . SET
& DONE
LDG
CLEARANCE….. . . . . . . . . . . . . .
RECEIVED
EMERGENCY
LANDING BRIEFING….. DONE
APU . . . .
. . . . . . . . . . . . . . . . . . . . . . . . A/R
AUTOBRAKE .
. . . . . . . . . . . . . . . . . . . OFF
SPEEDBRAKE
. . . . . . . . . . . . . . . . . . . DOWN
FLAPS . . .
. . . . . . . . . . . . . . . . . . . . . . . UP
LDG LTS . .
. . . . . . . . . . . . . . . . . . . . . . OFF
STAB TRIM .
. . . . . . . . . . . . . . . . . . . . . 4
UNITS
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
IRS . . . .
. . . . . . . . . . . . . . . . . . . . . . . . OFF
PACKS . . .
. . . . . . . . . . . . . . . . . . . . . . OFF
APU . . . .
. . . . . . . . . . . . . . . . . . . . . . . . OFF
once APU
OFF and no external power selected
STBY PWR .
. . . . . . . . . . . . . . . . . . . . . OFF
BATTERY SW .
. . . . . . . . . . . . . . . . . . . OFF
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
than
used at Captain's discretion.Arm Speed Brakes.Extend
landing gear at first indication of G/S
movement.When landing is assured (
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
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
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
altitude is below
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
level-off altitude.
- Retract speed brakes approximately
altitude, or as desired to control
airspeed and level-off.
3. Level-Off (Using FL CH mode)
- Retract speed brakes approximately
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
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.