BOEING 737NG PROCEDURES CHECKLIST
ACTIVE SKY
EXTERIOR SAFETY INSPECTION
CHOCKS
SURFACES
MAINTENANCE STATUS
SHIPS LIBRARY
ELECTRICAL POWER UP
BATTERY SWITCH
STANDBY POWER
ALTERNATE FLAPS
WIPERS
ELECTRIC HYDRAULIC PUMPS
LANDING GEAR LEVER
>Verify green landing gear lights
>Verify red landing gear lights
*If external power is needed:
GROUND POWER AVAILABLE LIGHT
GROUND POWER
>Verify source off lights
>Verify transfer bus off lights
*If APU power is needed:
>VerifyENG 1, APU, ENG 2 fire switches
OVERHEAT DETECTOR
TEST SWITCH
>Verify MASTER CAUTION lights
>Verify OVHT/DET annunciator
>Verify FAULT light
>Verify APU DET INOP light
TEST SWITCH
>Verify fire warning bell sounds
>Verify Master FIRE WARN lights
>Verify MASTER CAUTION lights
>Verify OVHT/DET annunciator
MASTER FIRE WARN LIGHT
>Verify Master FIRE WARN lights
>Verify fire warning bell cancels
>Verify ENG 1, APU, ENG 2 fire swiches
>Verify ENG 1 OVERHEAT/ENG 2 OVERHT
EXTINGUISHER TEST SWITCH
>Test switch to position 1
>Verify 3 green extinguisher test lights
>Test switch
>Verify 3 green extinguisher test lights
>*Repeat for test position 2
APU
When APU GEN OFF BUS light illuminated:
APU GENERATOR bus switches
>Verify SOURCE OFF lights
>Verify TRANSFER BUS OFF lights
>Verify STANDBY PWR OFF light
>Verify APU MAINT light
>Verify APU LOW OIL PRESSURE light
WHEEL WELL FIRE WARNING SYSTEM
TEST SWITCH
>Verify fire warning bell sounds, master
Fire Warn, Master Caution, Ovht/Det
FIRE WARNING BELL CUTOUT switch
>Verify the master FIRE WARN lights
>Verify the fire warning bell cancels
>Verify WHEEL WELL fire warning light
Created by: SIM737PILOT
LOADED /SET
(checkbox use VATSIM weather, VATSIM interval update to zero)
Captain or First Officer
SET
(verify in place-AVITAB)
CHECKED
(verify all moveable surfaces are clear)
CHECKED
(acceptable or agreement with dispatch deviations if required)
CHECKED
GUARD CLOSED
GUARD CLOSED
GUARD CLOSED
PARKED
OFF
DOWN
ILLUMINATED
EXTINGUISHED
.
ILLUMINATED
ON
EXTINGUISHED
EXTINGUISHED
IN
NORMAL
FAULT/INOP
ILLUMINATED
ILLUMINATED
ILLUMINATED
ILLUMINATED
OVHT/FIRE
ILLUMINATED
ILLUMINATED
ILLUMINATED
PUSH
EXTINGUISHED
ILLUMINATED
ILLUMINATED
CHECK
HOLD
ILLUMINATED
RELEASE
EXTINGUISHED
START
ON
EXTINGUISHED
EXTINGUISHED
EXTINGUISHED
EXTINGUISHED
EXTINGUISHED
Test
OVHT/FIRE
ILLUMINATED
PUSH
EXTINGUISHED
ILLUMINATED
(Run for 1 minute before using as bleed air)
PRELIMINARY PREFLIGHT PROCEDURE
Captain or FO
IRS MODE SELECTORS
OFF, NAV
>Verify ON DC lights illuminate then extinguish
>Verify ALIGN lights illuminated
VOICE RECORDER SWITCH
AS NEEDED
>Verify following sufficient for flight:
. Oxygen Pressure
. Hydraulic quanitity
. Engine oil quantity
Do remaining actions after crew change/maintenance
MAINTENANCE DOCUMENTS
CHECK
FLIGHT DECK ACCESS SYSTEM SWITCH
GUARD CLOSED
EMERGENCY EQUIPMENT
CHECK
>Fire extinguisher
CHECKED/STOWED
>Crash Axe
STOWED
>Escape Ropes
STOWED
>Other needed equipment
CHECKED/STOWED
ELT SWTICH
GUARD CLOSED
>Verify ELT light
EXTINGUISHED
PSEU LIGHT
EXTINGUISHED
GPS LIGHT
EXTINGUISHED
SERVICE INTERPHONE switch
OFF
ENGINE PANEL
Set
>Verify REVERSER lights
EXTINGUISHED
>Verify ENGINE CONTROL lights
EXTINGUISHED
EEC SWITCHES
ON
OXYGEN PANEL
Set
PASSENGER OXYGEN switch
GUARD CLOSED
>Verify PASS OXY ON light
EXTINGUISHED
LANDING GEAR INDICATOR LIGHTS
ILLUMINATED
FLIGHT RECORDER SWITCH
GUARD CLOSED
MACH AIRSPEED WARNING TESTS
PUSH
>Verify clacker sounds
STALL WARNING TESTS
PUSH
>Verify each control column vibrates
EMERGENCY EVACUATION SWITCH
GUARD CLOSED
>Verify EVAC light
EXTINGUISHED
CIRCUIT BREAKERS
CHECKED
PARKING BRAKE
SET
CDU PREFLIGHT PROCEDURE
Captain or FO
Initial Data
Set
IDENT PAGE:
>Verify MODEL is correct
>Verify ENG RATING is correct
>Verify nav data base ACTIVE range current
POS INIT PAGE:
>Verify time is correct
>Enter present position on SET IRS POS line
Navigation Data
Set
ROUTE PAGE:
>Enter ORIGIN
>Enter route
>Enter flight number
>ACTIVATE and Execute route
DEPARTURES PAGE:
>Select runway and departure routing
>Execute runway and departure routing
LEGS PAGE:
>Verify correct RNP for departure
>Verify route correct on RTE pages
Performance Data
Set
PERF INIT PAGE:
>Enter ZFW
>Verify fuel sufficient for flight
(Requires AC bus powered 4 min)
(Verify fuel on CDU, dispatch, and fuel qty agree)
(Verify gross weight and cruise CG (GW/CRZ CG) on CDU and dispatch agree)
>Thrust Mode Display
N1 LIMIT PAGE:
>Confirm OAT value correct and reasonable for ambient conditions
>Select assumed temp or fixed derate takeoff, or both as needed
>Select full or derated climb thrust as needed
TAKEOFF REF PAGE:
>Make data entries on pg2 before page 1/2
>Enter the CG
>Verify a trim value is shown
>Select or enter the takeoff V speeds
>Verify or enter engine out acceleration height
>Verify or enter thrust reduction altitude
>Verify preflight is complete
PREFLIGHT PROCEDURE- FIRST OFFICER
FLIGHT CONTROL PANEL
Check
FLIGHT CONTROL SWITCHES
GUARD CLOSED
>Verify flight control LOW PRESS lights
ILLUMINATED
FLIGHT SPOILER SWITCHES
GUARDS CLOSED
YAW DAMPER
ON
>Verify yaw damper light
EXTINGUISHED
>Verify standby hydraulic LOW QTY light
EXTINGUISHED
>Verify standby hydraulic LOW PRESS light
EXTINGUISHED
>Verify STBY RUD ON light
EXTINGUISHED
ALTERNATE FLAPS MASTER SWITCH
GUARD CLOSED
ALTERNATE FLAPS POSITION SWITCH
OFF
>Verify FEEL DIFF PRESS light
EXTINGUISHED
>Verify SPEED TRIM FAIL light
EXTINGUISHED
>Verify MACH TRIM FAIL light
EXTINGUISHED
>Verify AUTO SLAT FAIL light
EXTINGUISHED
NAVIGATION PANEL
Set
VHF NAV TRANSER SWITCH
NORMAL
IRS TRANSFER SWITCH
NORMAL
FMC SOURCE SELECT SWITCH
NORMAL
DISPLAYS PANEL
Set
SOURCE SELECTOR
AUTO
CONTROL PANEL SELECT SWITCH
NORMAL
FUEL PANEL
Set
>Verify ENG VALVE CLOSED lights
ILLUM DIM
>Verify SPAR VALVE CLOSED lights
ILLUM DIM
>Verify FILTER BYPASS lights
EXTINGUISHED
CROSSFEED SELECTOR
CLOSED
>Verify VALVE OPEN light
EXTINGUISHED
FUEL PUMP SWITCHES
OFF
>Verify center tank LOW PRESS lights
EXTINGUISHED
>Verify main tank LOW PRESS lights
ILLUMINATED
ELECTRICAL PANEL
Set
BATTERY SWITCH
GUARD CLOSED
CAB/UTIL POWER SWITCH
ON
IFE/PASS SEAT POWER SWITCH
ON
GALLY POWER SWITCH
ON
STANDBY POWER SWITCH
GUARD CLOSED
>Verify STANDBY PWR OFF light
EXTINGUISHED
>Verify BAT DISCHARGE light
EXTINGUISHED
>Verify TR UNIT light
EXTINGUISHED
>Verify ELEC light
EXTINGUISHED
GEN DISCONNECT SWITCHES
GUARDS CLOSED
>Verify DRIVE lights
ILLUMINATED
BUS TRANSFER SWITCH
GUARD CLOSED
>Verify TRANSFER BUS OFF lights
EXTINGUISHED
>Verify SOURCE OFF lights
EXTINGUISHED
>Verify GEN OFF BUS lights
ILLUMINATED
OVERHEAT/FIRE PROTECTION PANEL
Check
(Procedure listed above)
EQUIPMENT COOLING SWITCHES
NORMAL
(Verify TO or dashes are shown) *dashes normal model
(If flight crew didn't complete. Required once per flight day)
>Verify OFF lights
EMERGENCY EXIT LIGHTS
>Verify NOT ARMED light
NO SMOKING SWITCH
FASTEN BELTS
WIPERS
WINDOW HEAT
>Verify OVHT lights are extinguished
PROBE HEAT
WING ANTI ICE
>Verify VALVE OPEN light
ENGINE ANTI ICE
>Verify COWL ANTI ICE lights
>Verify COWL VALVE OPEN lights
START FLIGHT LEG
HYDRAULIC PANEL
ENGINE HYDRAULIC PUMPS
>Verify LOW PRESSURE lights
ELECTRIC HYDRAULIC PUMPS
>Verify OVERHEAT lights
>Verify LOW PRESSURE lights
AIR CONDITIONING PANEL
AIR TEMPERATURE SOURCE SELECTOR
TRIM AIR
>Verify ZONE TEMP lights
TEMPERATURE SELECTORS
>Verify RAM DOOR FULL OPEN lights
RECIRCULATION FAN SWITCHES
PACKS
ISOLATION VALVE
ENGINE BLEEDS
APU BLEED
>Verify DUAL BLEED
>Verify PACK lights
>Verify WING-BODY OVERHEAT lights
>Verify OFF SCHED DESCENT light
FLIGHT ALTITUDE INDICATOR
LANDING ALTITUDE
PRESSURIZATION MODE SELECTOR
>Verify ALTN light
>Verify MANUAL light
LIGHTING PANEL
LANDING LIGHTS
RUNWAY TURNOFF LIGHTS
TAXI LIGHT
IGNITION SELECTOR SWITCH
ENGINE START SWITCHES
LIGHTING PANEL
LOGO LIGHT
POSITION LIGHT
ANTI-COLLISION LIGHT
WING ILLUMINATION LIGHT
WHEEL WELL SWITCH
MODE CONTROL PANEL
COURSES
FLIGHT DIRECTORS
EFIS CONTROL PANEL
MINIMUMS REFERENCE SELECTOR
MINIMUMS SELECTOR
FLIGHT PATH VECTOR SWITCH
METERS SWITCH
BAROMETRIC REFERENCE SELECTOR
BAROMETRIC SELECTOR
VOR/ADF SWITCHES
EXTINGUISHED
GUARD CLOSED
EXTINGUISHED
AUTO or ON
AUTO or ON
PARKED
ON
OFF
OFF
EXTINGUISHED
OFF
EXTINGUISHED
EXTINGUISHED
AVITAB
Set
ON
ILLUMINATED
OFF
EXTINGUISHED
ILLUMINATED
Set
AS NEEDED
ON
EXTINGUISHED
AS NEEDED
ILLUMINATED
AUTO
AUTO or HIGH
OPEN
ON
ON
ILLUMINATED
EXTINGUISHED
EXTINGUISHED
EXTINGUISHED
CRUISE ALT
DEST ELEV
AUTO
EXTINGUISHED
EXTINGUISHED
Set
RETRACT and OFF
OFF
OFF
L or R
AUTO
Set
AS NEEDED
AS NEEDED
OFF
AS NEEDED
AS NEEDED
Set
SET
ON
Set
RADIO OR BARO
Set DH or ALT REF
AS NEEDED
AS NEEDED
IN OR HPA
SET LOCAL ALT
AS NEEDED
(Must be ON prior to boarding passengers)
(Position on at least 10 min prior to takeoff)
(Zibo Mod)
(Alternate switch position on subsequent starts)
(Or OFF depending on model options)
(Move switch for pilot flying to ON first.)
(STD is 29.92 or 1013)
MODE SELECTOR
MAP
CENTER SWITCH
AS NEEDED
RANGE SELECTOR
AS NEEDED
TRAFFIC SWITCH
AS NEEDED
WEATHER RADAR
OFF
>Verify wx radar indications not shown on MAP
MAP SWITCHES
AS NEEDED
OXYGEN
Test and Set
>Note crew oxygen pressure
(Min 1100 psi for dispatch)
OXYGEN MASK
STOWED
RESET/TEST SWITCH
PUSH and HOLD
>Verify yellow cross shows in flow indicator
EMERGENCY TEST SELECTOR
PUSH and HOLD
>Continue to hold the RESET/TEST switch down and push the emergency
test selector for 5 sec. Verify yellow cross shows continuously in flow indicator.
>Verify crew oxygen pressure doesn't drop more than 100 psig.
*If oxy cylinder is not in full open position, pressure can:
. Decrease rapidly
. Decrease more than 100 psig, or
. Increase slowly back to normal
>Release the RESET/TEST switch and EMERGENCY TEST selector.
>Verify yellow cross doesn't show in flow indicator.
(Normal/100% switch- 100%)
CREW OXYGEN PRESSURE
CHECK
(Verify pressure sufficient for dispatch- 1100psi)
CLOCK
SET
TIME/DATE
UTC TIME
DISPLAY SELECT PANEL
Set
MAIN PANEL DISPLAY UNITS
NORMAL
LOWER DISPLAY UNIT
NORMAL
TAKEOFF CONFIG LIGHT
EXTINGUISHED
(if installed)
CABIN ALTITUDE LIGHT
EXTINGUISHED
(if installed)
LIGHT TEST SWITCH
HOLD to 1
>Verify A/P light steady amber.
>Verify A/T light steady amber.
>Verify FMC light steady amber.
TEST LIGHT SWITCH
HOLD to 2
>Verify A/P light steady red.
>Verify A/T light steady red.
>Verify FMC light steady amber.
?? Amber or red?
*Do Initial Data and Nav Data steps from the CDU Preflight Procedure and verify IRS
alignment is complete before checking flight instruments.
FLIGHT INSTRUMENTS
Check
>Verify TCAS OFF flag shown
>Verify NO VSPD until V-speeds are selected
>Verify expected RMI flags are shown
>Verify flight mode annunciators correct:
. Autothrottle mode is blank
. Roll mode is blank
. Pitch mode is blank
. ADFS status is FD
*Select MAP Mode
BRAKE TEMP LIGHT
EXTINGUISHED
GROUND PROXIMITY PANEL
Check
FLAP INHIBIT
GUARD CLOSED
GEAR INHIBIT
GUARD CLOSED
TERRAIN INHIBIT
GUARD CLOSED
>Verify GROUND PROXIMITY INOP light
EXTINGUISHED
LANDING GEAR PANEL
Set
LANDING GEAR LEVER
DOWN
>Verify green landing gear lights
ILLUMINATED
>Verify red landing gear lights
EXTINGUISHED
AUTOBRAKE
RTO
>Verify AUTOBRAKE DISARM light
EXTINGUISHED
ANTI-SKID INOP LIGHT
EXTINGUISHED
ENGINE DISPLAY CONTROL PANEL
Set
N1 SET SELECTOR
AUTO
SPEED REFERENCE SELECTOR
AUTO
FUEL FLOW SWITCH
RATE
>Move switch to RESET, then RATE
ENGINE INSTRUMENTS
CHECK
>Verify primary/secondary indications show existing conditions
>Verify no exceedance is shown
>Verify hydraulic qtys don't show RF.
CARGO FIRE PANEL
CHECK
(This check is needed once per flight day)
DETECTOR SELECT SWITCHES
NORMAL
TEST SWITCH
PUSH
>Verify fire warning bell sounds.
>Verify FIRE WARN lights
ILLUMINATED
MASTER FIRE WARN LIGHT
PUSH
>Verify Master FIRE WARN lights
EXTINGUISHED
>Verify fire warning bell cancels.
>Verify green EXTINGUISHER lights
ILLUMINATED
>Verify FWD/AFT lights
ILLUMINATED
>Verify DETECTOR FAULT light
EXTINGUISHED
>Verify DISCH light
ILLUMINATED
HUD SYSTEM
AS NEEDED
RADIO TUNING PANEL
Set
>Verify OFF light
EXTINGUISHED
VHF RADIOS
SET
VHF NAV RADIOS
SET
AUDIO CONTROL PANEL
SET
ADF RADIOS
SET
WEATHER RADAR CONTROL PANEL
SET
TRANSPONDER PANEL
SET
STABILIZER TRIM OVERRIDE SWITCH
GUARD CLOSED
SEAT
ADJUSTED
(Align view angle with red ball covering white)
RUDDER PEDALS
ADJUSTED
SEAT BELT / SHOULDER HARNESS
ADJUSTED
*Preflight checklist on Captain's command.
PREFLIGHT PROCEDURE- CAPTAIN
MASTER LIGHTS AND DIM SWITCH
TEST
EFIS CONTROL PANEL
Set
MINIMUMS REFERENCE SELECTOR
RADIO OR BARO
MINIMUMS SELECTOR
DH or ALT REF
FLIGHT PATH VECTOR SWITCH
AS NEEDED
METERS SWITCH
AS NEEDED
BAROMETRIC REFERENCE SELECTOR
IN OR HPA
BAROMETRIC SELECTOR
LOCAL ALT
VOR/ADF SWITCHES
AS NEEDED
MODE SELECTOR
MAP
CENTER SWITCH
AS NEEDED
RANGE SELECTOR
AS NEEDED
TRAFFIC SWITCH
AS NEEDED
WEATHER RADAR
OFF
>Verify wx radar indications not shown on MAP
MAP SWITCHES
AS NEEDED
MODE CONTROL PANEL
Set
COURSES
SET
FLIGHT DIRECTOR SWITCH
ON
(Move switch for pilot flying to ON first.)
BANK ANGLE INDICATOR
AS NEEDED
AUTOPILOT DISENGAGE BAR
UP
OXYGEN
TEST and SET
>Oxygen mask
STOWED
RESET/TEST SWITCH
PUSH and HOLD
>Verify yellow cross shows in flow indicator
EMERGENCY TEST SELECTOR
PUSH and HOLD
>Continue to hold the RESET/TEST switch down and push the emergency
test selector for 5 sec. Verify yellow cross shows continuously in flow indicator.
>Verify crew oxygen pressure doesn't drop more than 100 psig.
>Release the RESET/TEST switch and EMERGENCY TEST selector.
>Verify yellow cross doesn't show in flow indicator.
NORMAL/100% SWITCH
100%
CREW OXYGEN PRESSURE
CHECK
>Verify pressure sufficient for dispatch
CLOCK
SET
NOSEWHEEL STEERING
GUARD CLOSED
DISPLAY SELECT PANEL
Set
MAIN PANEL DISPLAY UNITS
NORMAL
LOWER DISPLAY UNIT
NORMAL
TAKEOFF CONFIG LIGHT
EXTINGUISHED
(if installed)
CABIN ALTITUDE LIGHT
EXTINGUISHED
(if installed)
LIGHT TEST SWITCH
HOLD to 1
>Verify A/P light illuminated steady amber
>Verify A/T light illuminated steady amber
LIGHT TEST SWITCH
HOLD to 2
>Verify A/P light is illuminated steady red.
>Verify the A/T light is illuminated steady red.
>Verify the FMC light is illuminated steady amber.
STAB OUT OF TRIM LIGHT
EXTINGUISHED
*Do Initial Data and Nav Data steps from the CDU Preflight Procedure and verify IRS
alignment is complete before checking flight instruments.
FLIGHT INSTRUMENTS
Check
>Verify flight instrument indications are correct.
>Verify only these flags are shown:
. TCAS OFF
. NO VSPD until V-SPEEDS are selected
. Expected RMI flags
>Verify flight mode annunciators correct:
. Autothrottle mode is blank
. Roll mode is blank
. Pitch mode is blank
. AFDS status is FD
>Select MAP mode
STANDBY INSTRUMENTS
Check
STANDBY HORIZON
SET
GYRO CAGING CONTROL
PULL then RELEASE
APPROACH MODE SELECTOR
AS NEEDED
>Verify flight instrument indications are correct.
>Verify no flags are shown.
STANDBY ALTIMETER
SET
>Verify flight instrument indications are correct.
>Verify no flags are shown.
STANDBY RMI
SET
>Select VOR or ADF
SPEED BRAKE LEVER
DOWN DETENT
>Verify SPEED BRAKE ARMED light
EXTINGUISHED
>Verify SPEED BRAKE DO NOT ARM light
EXTINGUISHED
>Verify SPEEDBRAKES EXTENDED light
EXTINGUISHED
REVERSE THRUST LEVERS
DOWN
FORWARD THRUST LEVERS
CLOSED
FLAP LEVER
SET
>Set flap lever to agree with flap position.
>Verify FLAP LOAD RELIEF light
EXTINGUISHED
PARKING BRAKE
SET
>Verify parking brake warning light
ILLUMINATED
ENGINE START SWITCHES
CUTOFF
STABILIZER TRIM CUTOUT SWITCHES
NORMAL
HUD SYSTEM
AS NEEDED
RADIO TUNING PANEL
SET
>Verify OFF light
EXTINGUISHED
VHF RADIOS
SET
VHF NAV RADIOS
SET
AUDIO CONTROL PANEL
SET
SEAT
ADJUSTED
RUDDER PEDALS
ADJUSTED
SEAT BELT / SHOULDER HARNESS
ADJUSTED
Request ATC clearance
RECEIVED
*Taxi Brief
*Departure Brief- Plate#, DEP freq, ELEV, initial ALT, initial HDG, threats, wx. Brief SID routing.
*Route review in FMC
START ACARS PROGRAM
AS NEEDED
(If you belong to a VA)
*Call "PREFLIGHT CHECKLIST"
PREFLIGHT CHECKLIST
PINS AND COVERS
REMOVED
OXYGEN
TESTED, 100%
NAV TRANSFER DISPLAY SWITCHES
NORM, AUTO
WINDOW HEATS
ON
PRESSURIZATION MODE SELECTOR
AUTO
FLIGHT INSTRUMENTS
TRACK, BARO, ELEV
PARKING BRAKE
SET
ENGINE START LEVERS
CUTOFF
ELEVATOR TRIM
SET
"Taxi and Takeoff Briefing Completed"
(Now 10 min prior to departure)
PA Welcome Message
AVITAB
*DEST wx brief, ALTN wx brief, takeoff calculator
ZFW, TOW, V1, VR, V2, derate used if applicable
Call "PREFLIGHT CHECKLIST BELOW THE LINE"
FUEL
SET
PASSENGER SIGNS
SET
TAKEOFF SPEEDS
V1__, VR__, V2
MCP
V2, RWY HDG, INIT ALT
"Preflight Checklist Complete"
"Request PUSH and START"
RECEIVED
BEFORE START PROCEDURE
FLIGHT DECK DOOR
CLOSED and LOCKED
>Verify CABIN DOOR UNLOCKED light
EXTINGUISHED
>Verify LOCK FAIL light
EXTINGUISHED
*Do the CDU Preflight Procedure- Performance Data
steps before completing this procedure.
CDU DISPLAY
SET
*Normally PF selects TAKEOFF REF PAGE
*Normally PM selects LEGS PAGE
N1 BUGS
CHECK
>Verify N1 reference bugs correct.
IAS BUGS
SET
MCP
Set
AUTOTHROTTLE ARM SWITCH
ARM
IAS/MACH SELECTOR
SET V2
ARM LNAV
AS NEEDED
ARM VNAV
AS NEEDED
INITIAL HEADING
SET
INITIAL ALTITUDE
SET
Taxi and Takoff Briefings
COMPLETED
(Pilot who does takeoff does taxi and takeoff brief.)
EXTERIOR DOORS
CLOSED
FLIGHT DECK WINDOW
CLOSED/LOCKED
START CLEARANCE
OBTAINED
(Request push and start)
>Obtain clearance to pressurize hydaulics
>Obtain clearance to start engines
*If pushback needed, verify nose gear lockout pin installed, equipment removed
FUEL PANEL
Set
*If center tank exceeds 460kg/1000 lbs then:
LEFT, RIGHT, CENTER FUEL PUMPS
ON
>Verify LOW PRESSURE lights illuminate momentarily then extinguish
AFT and FWD FUEL PUMP SWITCHES
ON
>Verify LOW PRESSURE lights
EXTINGUISHED
HYDRAULIC PANEL
Set
SYSTEM A HYDRAULIC PUMPS
SYSTEM B HYDRAULIC PUMPS
>Verify brake pressure is 2800 psi minimum.
>Verify system B pressure is 2800 psi minimum.
ANTI-COLLISION LIGHT
STAB TRIM
>Verify trim is in green band.
AILERON TRIM
RUDDER TRIM
Call "BEFORE START CHECKLIST to the LINE"
BEFORE START CHECKLIST
ON
ON
ON
SET
(triggers cabin crew to shut door in ZIBO)
ZERO
ZERO
Captain
*Request ATC push and start clearance*
RECEIVED
PUSHBACK / TOWING PROCEDURE
REVIEWED
>Establish comms with ground personnel
ESTABLISHED
CPT
TRANSPONDER
AS NEEDED
FO
PARKING BRAKE
RELEASED
*When pushback complete:
>Verify tow bar disconnected
>Verify nose gear steering lockout pin removed.
SYSTEM A HYDRAULIC PUMPS
ON
>Verify system A LOW PRESS lights extinguished
>Verify system A pressure is 2800 psi minimum.
ENGINE START PROCEDURE
>Select secondary engine indications
FO
PACK SWITCHES
OFF
FO
START SEQUENCE
ANNOUNCE
CPT
Call "START ENGINE ___"
ENGINE START SWITCH
GRND
FO
>Verify N2 RPM increases
FO
*When N1 rotation seen and N2 is at 25% :
ENGINE START LEVER
IDLE DETENT
CPT
*Monitor fuel flow and EGT indications
CPT, FO
*At 56% N2, verify ENG START SWITCH moves to AUTO.
FO
>Verify the START VALVE OPEN altert extinguishes when ENG START moves to AUTO
Call "STARTER CUTOUT"
FO
*Monitor N1, N2, EGT, fuel flow, and oil pressure for normal indications
while engine accelerates to stable idle.
CPT, FO
*After engine stable at idle, start other engine.
BEFORE TAXI PROCEDURE
GENERATOR 1 AND 2 SWITCHES
ON
FO
PROBE HEAT
ON
FO
WING ANTI-ICE
AS NEEDED
FO
ENGINE ANTI-ICE
AS NEEDED
FO
PACK SWITCHES
AUTO
FO
ISOLATION VALVE
AUTO
FO
APU BLEED AIR
OFF
FO
APU SWITCH
OFF
FO
ENGINE START SWITCHES
CONT
FO
ENGINE START LEVERS
IDLE DETENT
CPT
*Verify ground equipment is clear.
Call "FLAPS ___" as needed for takeoff.
FLAP LEVER
T/O SET
FO
>Verify LE FLAPS EXT green light
ILLUMINATED
FLIGHT CONTROLS
CHECK
*Push MFD SYS to display flight control surface indications on lower display unit.
*Blank the lower display unit
FO
TRANSPONDER
AS NEEDED
(Set active setting but not TCAS mode)
RECALL
CHECK
*Update changes to taxi brief as needed.
Call "BEFORE TAXI CHECKLIST"
CPT
BEFORE TAXI CHECKLIST
Operator/Company
ENGINE GENERATORS
ON
PROBE HEAT
ON
ANTI ICE
OFF
AC PRESSURIZATION
PACKS ON, AUTO
ENGINE START SWITCHES
CONT
THRUST LEVERS
IDLE DETENT
FLIGHT CONTROLS
CHECKED
GROUND EQUIPMENT
CLEAR
FLAPS
SET
"Before taxi checklist complete."
BEFORE TAKEOFF PROCEDURE
>Verify increase in engine oil temp before takeoff.
>Run engine for at least 2 minutes
>Use thrust setting normal used for taxi operations.
CABIN CREW
NOTIFIED
(Use trigger switch WING LIGHT or WHEEL WELL LT as set in AVITAB)
WEATHER RADAR
ON
TERRAIN RADAR
AS NEEDED
Call "BEFORE TAKEOFF CHECKLIST"
BEFORE TAKEOFF CHECKLIST
(On Yoke Clipboard)
CONFIG
CHECKED
FLAPS
___, GRN LIGHT
STAB TRIM
___UNITS, SET
TAKEOFF BRIEFING
RECEIVED
CABIN
SECURE
MCP
SET
TRANSPONDER
TA/RA
STROBE LIGHTS
ON
LANDING LIGHTS
ON
"Before Takeoff Checklist Complete"
TAKEOFF PROCEDURE
>Update FMC position to rwy threshold on CDU TAKEOFF REF page.
>Before entering RWY, verify RWY and entry point are correct.
>When entering RWY
STROBES
ON
EXTERIOR LIGHTS
AS NEEDED
TRANSPONDER
TA/RA
BRAKES
RELEASED
>When cleared for T/O, set FIXED landing lights to ON.
>Advance thrust to 40% N1
>Allow engines to stabilize
>Push TOGA
Call "THRUST SET"
(Adjust before 60kts)
Call "80 KNOTS"
CHECK
Call "V1"
At VR Call "ROTATE"
Call "POSITIVE RATE"
Call "GEAR UP"
LANDING LEVER
UP
Above 400 ft RA, call for roll mode
SELECTED
At thrust reduction altitude, verify climb thrust set.
At acceleration height, call for flaps up maneuvering speed.
Verify acceleration, Call "FLAPS" on schedule.
After flaps/slats retracted Call "VNAV"
Engage AP above min altitude for engagement.
(400 ft AGL per Boeing, but operator may set higher limit)
After flap retraction complete, verify engine bleeds and packs operating.
ENGINE START SWITCHES
AUTO / OFF
LANDING GEAR LEVER
OFF
(After landing gear retraction is complete)
AUTOBRAKE
OFF
Call "AFTER TAKEOFF CHECKLIST"
AFTER TAKEOFF CHECKLIST
(Yoke Clipboard)
AIR CONDITIONING & PRESSURIZATION
SET
ENGINE START SWITCHES
AUTO
(Or OFF if not equipped)
LANDING GEAR
UP and OFF
AUTOBRAKE
OFF
FLAPS
UP, NO LIGHTS
ALTIMETERS
SET
"After takeoff checklist completed"
Pilot Monitoring
CLIMB AND CRUISE PROCEDURE
>At or above 10,000 MSL, set LND lights
OFF
PASSENGER SIGNS
AS NEEDED
>At transition altitude:
ALTIMETERS
SET/CROSSCHECKED
(FL180 in USA)
Level Off Announcement
AVITAB
(ZIBO Mod)
>Center fuel tank pumps
OFF
(when LOW PRESS light on)
>ETOPS flight: Additional steps- see suppliment
>Prior to TOD, modify active route as needed for arrival and approach
*Prior to TOD, conduct Approach Brief
RWY, ILS freq, course, threats, chart #, MSA, APT ELEV, AIR TEMP, RWY calculator, FUEL
Descent PA Announcement
AVITAB
(ZIBO Mod)
DESCENT PROCEDURE
>Verify RNP
AS NEEDED
>Set center fuel tank when LOW press light
OFF
PRESSURIZATION - LAND ALT
SET
RECALL
PUSH
(review any lights)
>Verify VREF on APPROACH BRIEF PAGE
CHECKED
RADIO/BAROMETER minimums
SET
NAV RADIOS
SET
AUTOBRAKE
AS NEEDED
Give Approach Briefing
Call "DESCENT CHECKLIST"
DESCENT CHECKLIST
PRESSURIZATION - LAND ALT
SET
ANTI ICE
AS NEEDED
AUTOBRAKE
SET
APPROACH BRIEF & FUEL
DISCUSSED
IAS & ALT BUGS
CHECKED & SET
"Descent checklist complete"
APPROACH PROCEDURE
*Normally started at transition level. Complete before initial approach fix,
start of radar vectors to final, or start of visual approach.
>Verify localizer frequency
>Update approach briefing as needed.
Call "APPROACH CHECKLIST"
APPROACH CHECKLIST
ALTIMETERS & INSTRUMENTS
SET, CROSSCHECKED
APPROACH AIDS
CHECKED, SET
"Reading xxxx feet- NOW"
XCHECKED
"Approach Checklist Complete"
LANDING PROCEDURE- ILS
*If on radar vectors
HDG SEL
*If enroute to fix
LNAV
(or other roll mode)
CABIN CREW
NOTIFIED
AVITAB
(Prepare Landing PA Announcement)
>Verify cabin is secure
Call "FLAPS ___" according to extension schedule.
*When on localizer intercept heading:
>Verify ILS tuned and identified
>Verify LOC and G/S pointers shown
APPROACH MODE
ARM
*If dual mode approach is desired, engage second AP.
NOTE: When using LNAV to intercept final approach course, LNAV
might parallel the localizer without capturing it.
>Verify localizer is captured.
>Verify final approach course heading.
Call "GLIDESLOPE ALIVE"
GEAR DN, FL15
>Verify green gear lights illuminated
ENGINE START SWITCHES
CONT
SPEEDBRAKE
ARM
>Verify SPEEDBRAKE ARMED light
ILLUMINATED
*At glideslope capture, call "FLAPS __" as needed for landing.
MISSED APP ALTITUDE
SET
Call "LANDING CHECKLIST"
LANDING CHECKLIST
Yoke Clipboard
START SWITCHES
CONT
RECALL
CHECKED
SPEEDBRAKE
ARMED, LT ON
LANDING GEAR
DN, 3 GREEN
AUTOBRAKE
____SET
FLAPS
____, GRN LIGHT
LANDING LIGHTS
ON
"Landing Checklist Complete"
*At final approach fix, verify altitude.
*If autoland planned, verify AFDS status at 500 feet AGL.
*For SINGLE CHANNEL approach, disengage AP and autothrottle no later
than the min use height for single autopilot operation.
*For DUAL CHANNEL approach, disengage AP after touchdown.
MISSED APPROACH PROCEDURE
PUSH TOGA, call "FLAPS 15"
>Verify rotation to go around attitude and thrust increases.
>Verify thrust sufficient or adjust as necessary.
>Verify positive rate, call "GEAR UP"
>Verify Missed Approach altitude set.
NOTE: If airspeed within amber band, limit bank to 15 degrees.
>Above 400 ft RA, verify LNAV or HDG SEL as appropriate
>Verify missed approach route is tracked.
*At acceleration height, call "FLAPS ___" according to schedule.
*After flaps set to planned flap setting at or above flap maneuvering speed,
select LVL CHG. VNAV may be selected if flaps are up.
>Verify CLIMB THRUST
SET
>Verify missed approach ALT captured
LAND GEAR
OFF
ENGINE START SWITCHES
AS NEEDED
Call "AFTER TAKEOFF CHECKLIST"
LANDING ROLL PROCEDURE
*If autoland accomplished, disengage AP.
THRUST LEVERS
CLOSED
Call "SPEEDBRAKE UP"
>Verify correct autobrake operation
WARNING: After reverse thrust levers are moved, a full stop
landing MUST be made.
REVERSE THRUST
APPLY
Call "REVERSERS NORMAL"
Call "60 KNOTS"
*Disarm autobrake prior to taxi speed
AFTER LANDING PROCEDURE
*Run engine for at least 3 minutes.
*Use thrust setting normally used for taxi
SPEEDBRAKE
DOWN
APU
START
PROBE HEAT
OFF
EXTERIOR LIGHTS
AS NEEDED
STROBES
OFF
LANDING LIGHTS
OFF
RUNWAY TURNOFF LIGHTS
ON
TAXI LIGHT
ON
ENGINE START SWITCHES
AUTO
WEATHER RADAR
OFF
AUTOBRAKE
OFF
FLAPS
UP
TRANSPONDER
AS REQUIRED
*Turn off taxi light during final turn to stand.
SHUTDOWN PROCEDURE
PARKING BRAKE
SET
(400 ft AGL)
(Alt Off setting, but ON for VATSIM)
>Verify parking brake light
ILLUMINATED
ELECTRICAL POWER
SET
*If APU needed:
>Verify APU GEN BUS OFF lights
ILLUMINATED
APU GENERATOR SWITCHES
ON
>Verify SOURCE OFF lights
EXTINGUISHED
*If external power is needed:
>Verify GRD POWER AVAILABLE light
ILLUMINATED
GROUND POWER SWITCH
ON
>Verify SOURCE OFF lights
EXTINGUISHED
ENGINE START LEVERS
CUTOFF
*Operate engines at or near idle for 3 min to thermally
stabilize and reduce undercowl soak-back temperatures.
SEAT BELTS
OFF
ANTI COLLSION LIGHT
OFF
FUEL PUMPS
OFF
CAB/UTIL SWITCH
AS NEEDED
IFE/PASS SEAT SWITCH
AS NEEDED
GALLEY POWER SWITCH
AS NEEDED
WING ANTI-ICE
OFF
ENGINE ANTI-ICE
OFF
ENGINE HYDRAULIC PUMPS
ON
ELECTRIC HYDRAULIC PUMPS
OFF
RECIRCULATION FANS
AS NEEDED
PACKS
AUTO
ISOLATION VALVE
OPEN
ENGINE BLEEDS
ON
APU BLEED
ON
EXTERIOR LIGHTS
AS NEEDED
>Logo light
AS NEEDED
>Nav lights
ON
FLIGHT DIRECTORS
OFF
TRANSPONDER
STANDBY
*Once wheel chocks in place- brake
RELEASED
APU SWITCH
AS NEEDED
FLIGHT DECK DOOR
UNLOCKED
>Verify CABIN DOOR UNLOCKED light
ILLUMINATED
Call "SHUTDOWN CHECKLIST"
Do SHUTDOWN checklist.
SECURE PROCEDURE
IRS MODE SELECTORS
OFF
EMERGENCY EXIT SWITCH
OFF
WINDOW HEAT SWITCHES
OFF
PACK SWITCHES
OFF
Call "SECURE CHECKLIST"
SECURE CHECKLIST
IRS MODE SELECTORS
OFF
CAB/UTIL, IFE/GALLEY PWR
ON
EMERGENCY EXITS
OFF
AIR COND PACKS
OFF
TRIM AIR
OFF
APU/GROUND POWER
OFF
BATTERY
OFF
(Triggers Flight Attendant Cabin PA Announcement)
(Normally on after dusk if not last flight of the day)
(Nav lights remain on when power is supplied to aircraft)
FO
FO
FO
FO
CPT
FO