737 ach fo procedures 10x21

7/29/2019 737 ACH FO Procedures 10x21

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737 NG

FIRST OFFICER PROCEDURES

Preflight and Postflight Scan Flow Areas of Responsability - Captain as Pilot Flying or Taxiing


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Verify that the ELEC light is extinguished.

Generator drive DISCONNECT switches Guards closed

Electrical Power Up supplementary procedure Completed Verify that the DRIVE lights are illuminated.

Exterior inspection Completed BUS TRANSFER switch Guards closed

Flight control panel Check Verify that the TRANSFER BUS OFF lights are extinguished.

Verify that the SOURCE OFF lights are extinguished.

FLIGHT CONTROL switches Guards closed Verify that the GEN OFF BUS lights are illuminated.

Verify that the flight control LOW PRESSURE lights are illuminated. Overheat and fire protection panel Check

Flight SPOILER switches Guards closed Do this check if the flight crew did not do the Electrical Power Up

supplementary procedure. This check is needed once per flight day.

YAW DAMPER switch ON Verify that the engine No. 1, APU and the engine No. 2 fire switches are in

Ver if y t hat the YAW DAMPER li ght is ex ti ngui shed. Al er t gr ound per sonnel befor e t he fol low ing test is accompl is hed.

Verify the standby hydraulic LOW QUANTITY light is extinguished OVERHEAT DETECTOR switches NORMAL

Verify the standby hydraulic LOW PRESSURE light is extinguished

Verify that the STBY RUD ON light is extinguished. TEST switch Hold to FAULT/INOP

ALTERNATE FLAPS master switch Guard closed Verify that the MASTER CAUTION lights are illuminated.

Verify that the OVHT/DET annunciator is illuminated.

ALTERNATE FLAPS position switch OFF Verify that the FAULT light is illuminated.

Ve ri fy tha t the F EEL D IF F PRESS l ig ht i s ex ting uishe d. If the F AULT li gh t fai ls to i ll um ina te , the fau lt moni tor ing s ys te m i s

Verify that the SPEED TRIM FAIL light is extinguished. inoperative.

Ver if y t hat t he MACH TRIM FAIL l ight is ext ingui shed. Ver if y that the APU DET INOP l ight is i ll uminated.

Ver if y t hat the AUT O SLAT FAIL li ght is exti ngui shed. Do not oper at e the APU if the APU DET INOP li ght fail s to il lumi nate.

NAVIGATION panel Set TEST switch Hold to OVHT/FIRE

Verify that the fire warning bell sounds.

VHF NAV transfer switch NORMAL Verify that the master FIRE WARN lights are illuminated.

Verify that the MASTER CAUTION lights are illuminated.

IRS transfer switch NORMAL Verify that the OVHT/DET annunciator is illuminated.

Master FIRE WARN light Push

FMC transfer switch NORMAL Verify that the master FIRE WARN lights are extinguished.

Verify that the fire warning bell cancels.

DISPLAYS panel Set Verify that the engine No. 1, APU and the engine No. 2 fire switches

stay illuminated.

SOURCE selector AUTO Verify that the ENG 1 OVERHEAT and ENG 2 OVERHEAT lights

stay illuminated.

CONTROL PANEL select switch NORMAL EXTINGUISHER TEST switch Check

TEST Switch Position to 1 and hold

Fuel panel Set Verify that the three green extinguisher test lights are illuminated.

Verify that the ENG VALVE CLOSED lights are illuminated dim. TEST Switch Release

Verify that the SPAR VALVE CLOSED l ights are il luminated d im. Verify that the three green ex tinguisher test l ights are ex tinguished.

Verify that the FILTER BYPASS lights are extinguished. Repeat for test position 2.

CROSSFEED selector Closed APU START Verify that the VALVE OPEN light is extinguished. If extended APU operation is needed on the ground, position an AC

FUEL PUMP switches OFF operated fuel pump ON.If fuel is loaded in the center tank, position the

Verify that the center tank fue l pump LOW PRESSURE ligh ts are lef t center tank fue l pump switch ON to prevent a fuel imbalance

extinguished. before takeoff.Verify that the main tank fuel pump LOW PRESSURE lights are When the APU GEN OFF BUS light is illuminated:

illuminated. APU GENERATOR bus switches ON

Electrical panel Set Verify that the SOURCE OFF lights are extinguished.

Verify that the TRANSFER BUS OFF lights are extinguished.

BATTERY switch Guard closed EQUIPMENT COOLING switches NORMVerify that the OFF lights are extinguished.

CAB/UTIL power switch ON EMERGENCY EXIT LIGHTS switch Guard closedVerify that the NOT ARMED light is extinguished.

IFE/PASS SEAT power switch ON Passenger signs Set

STANDBY POWER switch Guard closed NO SMOKING switch AUTO or ON

Verify that the STANDBY PWR OFF light is extinguished.

Verify that the BAT DISCHARGE light is extinguished. FASTEN BELTS switch AUTO or ON

Verify that the TR UNIT light is extinguished.

Areas of Responsability - First Officer as Pilot Flying Preflight Procedure


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Windshield WIPER selectors PARK ENGINE START switches OFF Clock Set

Verify that the windshield wipers are stowed.

WINDOW HEAT switches ON Lighting panel Set Display select panel Set

Position switches ON at least 10 minutes before takeoff.

Verify that the OVERHEAT lights are extinguished. LOGO light switch As needed MAIN PANEL DISPLAY UNITS selector NORM

PROBE HEAT switches OFF

Verify that all lights are illuminated. POSITION light switch As needed LOWER DISPLAY UNIT selector NORM

WING ANTIICE switch OFF

Verify that the VALVE OPEN lights are extinguished. ANTICOLLISION light switch OFF Disengage light TEST switch Hold to 1

ENGINE ANTIICE switches OFF A/P light Illuminated steady amber

Verify that the COWL ANTIICE lights are extinguished. WING illumination switch As needed A/T light Illuminated steady amber

Verify that the COWL VALVE OPEN lights are extinguished. FMC light Illuminated steady amber

Hydraulic panel Set WHEEL WELL light switch As needed Disengage light TEST switch Hold to 2A/P light Illuminated steady red

ENGINE HYDRAULIC PUMPS switches ON Mode control panel Set A/T light Illuminated steady red

Verify that the LOW PRESSURE lights are illuminated. FMC light Illuminated steady amber

ELECTRIC HYDRAULIC PUMPS switches OFF COURSE(S) Set Flight Instruments CheckVerify that the OVERHEAT lights are extinguished.

Verify that the LOW PRESSURE lights are illuminated. FLIGHT DIRECTOR switch ON Flight instrument indications Correct

Air conditioning panel Set Move the switch for the pilot flying to ON first. Flags shown :

EFIS control panel Set TCAS OFF

AIR TEMPERATURE source selector As needed NO VSPD

MINIMUMS reference selector RADIO or BARO Expected RMI flag

TRIM AIR switch ON Flight mode annunciations Correct

Verify that the ZONE TEMP lights are extinguished. MINIMUMS selector Set decision height or altitude reference autothrottle mode Blank

Temperature selectors As needed roll mode Blank

Verify that the RAM DOOR FULL OPEN lights are illuminated. FLIGHT PATH VECTOR switch As needed pitch mode Blank

RECIRCULATION FAN switches AUTO AFDS status FD

METERS switch As needed GROUND PROXIMITY panel Check

Air conditioning PACK switches AUTO or HIGHBAROMETRIC reference selector IN or HPA FLAP INHIBIT switch Guard closed

ISOLATION VALVE switch OPEN

BAROMETRIC selector Set local altimeter setting GEAR INHIBIT switch Guard closed

Engine BLEED air switches ON

VOR/ADF switches As needed TERRAIN INHIBIT switch Guard closed

APU BLEED air switch ON Verify that the INOP light is extinguished.

Verify that the DUAL BLEED light is illuminated. Mode selector As needed Landing gear panel SetVerify that the PACK lights are extinguished.

Verify that the WINGBODY OVERHEAT lights are extinguished. CENTER switch As needed LANDING GEAR lever DN Verify that the BLEED TRIP OFF lights are extinguished. Verify that the green landing gear indicator lights are illuminated.

Cabin pressurization panel Set Range selector As needed Verify that the red landing gear indicator lights are extinguished.

Verify that the AUTO FAIL light is extinguished. AUTO BRAKE select switch RTO

Verify that the OFF SCHED DESCENT light is extinguished. TRAFFIC switch As needed Verify that the AUTO BRAKE DISARM light is extinguished

FLIGHT ALTITUDE indicator Cruise altitude ANTISKID INOP light Verify extinguished

WEATHER RADAR Off LANDING ALTITUDE indicator Destination field elevation Verify that the weather radar indications are not shown on the MAP. Engine display control panel Set

Map switches As needed

Pressurization mode selector AUTO N1 SET selector AUTO

Verify that the ALTN light is extinguished. Oxygen Test and SetVerify that the MANUAL light is extinguished. SPEED REFERENCE selector AUTO

Lighting panel Set Crew oxygen pressure Check

FUEL FLOW switch RATE

LANDING light switches RETRACT and OFF Oxygen Mask Stowed and doors closed Move switch to RESET, t hen RATE.

Engine instruments Check

RUNWAY TURNOFF light switches OFF Reset/TEST switch Push and Hold Verify that the primary and secondary engine indications show existing

Yellow cross shown conditions.

TAXI light switch OFF Emergency/TEST selector Push and Hold Verify that no exceedance is shown.

Yellow cross shown

Ignition select switch IGN L or R ELECTRONIC FLIGHT BAG Set


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CARGO FIRE panel Check VR Correct

This check is needed once per flight day or following a flight crew V2+15 Correct

change. Flaps up maneuvering speed Correct Select the secondary engine indications.

DETECTOR SELECT switches NORM Taxi and takeoff brieffings Completed Air conditioning PACK switches OFF

It will contain the following information :

TEST switch Push Airport notam and taxi plan ENGINE START switch GRDVerify that the fire warning bell sounds. Flaps configuration N2 RPM Increase

Verify that the master FIRE WARN lights are illuminated. Runway condition After Engine start lever was move to ilde detent :

Master FIRE WARN light Push Bleeds and anti-ice (ON or OFF) Fuel flow Monitor

Verify that the master FIRE WARN lights are extinguished. Departure procedure(Vectors or SID, NADP) EGT indications Monitor

Verify that the fire warning bell cancels. Failure before 80kts (monitor braking or manual brake)

Ve ri fy tha t the F WD an d AF T l ig hts s ta y i ll umina ted . F ai lu re af ter 8 0k ts (Eng in e fai lu re, En gine f ire, T O c onf igu rat ion h orn, At 56% N2, verify that the ENGINE START switch moves to OFF.

Ver if y t hat the DETECTO R FAULT li ght stay s exti ngui shed. moni tor RTO, us e rever se thrust ) If not, move the ENGINE START switch to OFF.

Verify that the green EXTINGUISHER tes t ligh ts s tay il luminated. Fai lu re at fter VR (procedure to return airport) Verify that the START VALVE OPEN alert extinguishes when the

Verify that the DISCH light stays illuminated. Cabin altitude (don oxygen mask, Establish crew communication) ENGINE START switch moves to OFF.

HUD system As needed Cabin evacuation (Protect evacuation from fire and wind)

Exterior doors Verify closed Call STARTER CUTOUT.

Radio tuning panel SetOFF light Extinguished Flight Deck windows Closed and locked After starter cutout :

VHF communications radios Set N1 Normal indications

Start clearance Obtained N2 Normal indications

VHF NAVIGATION radios Set for departure Hydraulic system pressurization clearance Obtained EGT Normal indications

Start engine clearance Obtained Fuel flow Normal indications

Audio control panel Set Fuel panel Set Oil pressure Normal indications

ADF Radios Set LEFT and RIGHT CENTER FUEL PUMPS switches ON Starter duty cycle :If the center tank fuel quantity exceeds 1,000 pounds/460 kilograms Do not exceed 2 minutes during each start attempt

WEATHER RADAR Panel Set Verify that the LOW PRESSURE ligh ts i lluminate momentari ly A minimum of 10 seconds is needed between s tart at tempts

and then extinguish.

Transponder panel Set If the LOW PRESSURE light stays illuminated turn off the CENTER Normal engine start considerations :FUEL PUMPS switch. do not move an engine start lever to idle early or a hot start can occur

STABILIZER TRIM override switch Guard closed AFT and FORWARD FUEL PUMPS switches ON keep a hand on the engine start lever while monitoring RPM, EGT and

Verify that the LOW PRESSURE lights are extinguished. fuel flow until stable

Seat Adjust Hydraulic panel Set if fuel is shutoff accidentally (by closing the engine start lever) do not

reopen the engine start lever in an attempt to restart the engine

Rudder pedals Adjust Electric HYDRAULIC PUMP switches ON failure of the ENGINE START switch to stay in GRD until the starter

Verify that the electric pump LOW PRESSURE lights are extinguished. cutout RPM can cause a hot star t. Do not reengage the ENGINE START

Seat belt and shoulder harness Adjust Verify that the brake pressure is 2,800 psi minimum. switch until engine RPM is below 20% N2.

Verify that the system A and B pressures are 2,800 psi minimum.

Do the PREFLIGHT checklist on the captains command. ANTI COLLISION light switch ON Do the ABORTED ENGINE START checklist for one or more of the

following abort start conditions :

Do the BEFORE START checklist. the N1 or N2 does not increase or increases very slowly after the EGT

increases

there is no oil pressure indication by the time that the engine is stable

at idleStart the Before Start Procedure after papers are on board. the EGT does not increase by 10 seconds after the engine start lever is

moved to IDLE

Flight deck door Closed and locked The Engine Start procedure may be done during pushback or towing. the EGT quickly nears or exceeds the start l imit

Verify that the LOCK FAIL light is extinguished. Parking brake Released as directed

CDU display Set When pushack is complete :

Tow bar Disconnected

PF TAKEOFF ref page Nose gear steering lockout pin Removed

System A HYDRAULIC PUMPS switches ON

PNF LEGS page Verify that the system A pump LOW PRESSURE lights are GENERATOR 1 and 2 switches ONextinguished

N1 bugs Check Verify that the system A pressure is 2800 psi minimum. PROBE HEAT switches ONN1 reference bugs Correct

IAS bugs Set WING ANTIICE switch As NeededV1 Correct

Engine Start Procedure

Before Taxi Procedure

Before Start Procedure

Pushback or Towing Procedure


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ENGINE ANTIICE switches As needed

PACK switches AUTO Engage the autopilot when above the

Enter the runway offset on the CDU minimum altitude for autopilot

ISOLATION VALVE switch AUTO TAKEOFF REF page. engagement.

APU BLEED air switch OFF When entering departure runway, After flap retraction is complete:

set the STROBE light switch to ON. Set or verify engine bleeds and air

APU switch OFF Use other lights as needed. conditioning packs are operating

Set the AUTO BRAKE select switch

ENGINE START switches CONT Verify that the brakes are released. When cleared for takeoff, set the to OFF

Align the airplane with the runway. FIXED LANDING light switches to ON. Set the landing gear lever to OFF

Verify that the ground equipment is clear. Set the transponder mode selector to after landing gear retraction is

TA/RA. complete.

Flap lever Set takeoff flaps

Advance the thrust levers to Call AFTER TAKEOFF CHECKLIST. Do the AFTER T AKEOFF checklist.

Blank the lower display unit. approximately 40% N1.

Allow the engines to stabilize.

Transponder As neededAt airports where ground tracking is not avail able, select STBY. At Push the TO/GA switch. Takeoff Flap Retraction Speed Schedule :

airports equipped to track airplanes on the ground, select an active

transponder setting, but not a TCAS mode.

Recall CheckVerify that all system annunciator panel lights illuminate and then V2+15 Flaps 15extinguish. Monitor airspeed. Monitor airspeed and call out any Flaps 25 "15" Flaps 5

EFB AIRPORT MAP application Select Maintain light forward pressure on abnormal indications. "5" Flaps 1Select map as desired. the control column. "1" Flaps up

Do the BEFORE TAXI checklist. Verify 80 knots and call CHECK. Call 80 KNOTS. V2+15 Flaps 5

Flaps 15 or 10 "5" Flaps 1Verify V1 speed. Verify the automatic V1 callout or "1" Flaps up

call V1.

Flaps 5 V2+15 Flaps 1

Engine warm up requirement : At VR, rotate toward 15 pitch At VR, call ROTATE. "1" Flaps upEngine oil temperature Increase After liftoff, follow F/D commands. Monitor airspeed and vertical speed.

Engine warm up recommendations : Flaps 1 "1" Flaps uprun the engines for at least 2 minutes Establish a positive rate of climb.

use a thrust setting normally used for taxi operations

Verify a positive rate of climb on the

altimeter and call POSITIVE RATE.

Check the center tank fuel quantity. Verify a positive rate of climb on the

Both center tank fuel pump switches altimeter and call GEAR UP.

must be OFF for T/O if center tank

fuel is less than 5000 pounds/ Set the landing gear lever to UP2300 kilograms.

Above 400 feet radio altitude, call for Select or verify the roll mode.

Not ify the cabin crew to prepare for a rol l mode as needed. Veri fy VNAV engaged.

takeoff. Verify that cabin is secure.

Verify acceleration at acceleration

height.

Call FLAPS ___ according to the

flap retraction schedule.

Call "BEFORE TAKEOFF Do the BEFORE TAKEOFF checkli st.

CHECKLIST" Set the FLAP lever as directed.

Before Takeoff Procedure

Pilot Flying Pilot Monitoring

Takeoff At speed Select

Flaps (display) Flaps

Takeoff Procedure


After takeoff thrust is set, the captains hand must be on the thrust levers

until V1.

At thrust reduction height, verify that climb thrust is set.

needed.

Limit bank angle to 15 until reaching V2 + 15


The pilot who will do the takeoff updates changes to the takeoff briefing as

Set the weather radar display as needed.


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Complete the After Takeoff Checklis t before starting the Climb and Start the Descent Procedure before the airplane descends below

Cruise Procedure. the cruise altitude for arrival at destination.

Complete the Descent Procedure by 10,000 feet MSL.

If the center tank fuel pump switches

were OFF for takeoff and the center Set both center tank fuel pump

tank contains more than 1000pounds switches OFF when center tank fuel

500 kilograms, set both center tank quantity reaches approximately

fuel pump switches ON above 3000 pounds/1400 kilograms.

10,000 feet or after the pitch attitude

has been reduced to begin Verify that pressurization is set to

acceleration to a climb speed of landing altitude.

250 knots or greater.

Review the system annunciator Recal l and review the system

During climb, set both center tank lights. annunciator lights.

fuel pump switches OFF when

center tank fuel quanti ty reaches Ver ify VREF on the APPROACH Ent er VREF on the APPROACH

approximately 1000 pounds / REF page. REF page.

500 kilograms.

At or above 10,000 feet MSL, set the

LANDING light switches to OFF.

Set the passenger signs as needed.

Set the AUTO BRAKE select switch

to the needed brake setting

When established in a level attitudeat cruise, i f the center tank contains Do the approach brief ing.

more than 1000 pounds /

500 kilograms and the center tank Call DESCENT CHECKLIST. Do the DESCENT checklist.

fuel pump switches are OFF, set the

center tank fuel pump switches

ON again. Approach briefing will contain the following information :

Set both center tank fuel pump Approach procedure (Vector or STAR, type of approach : precision,

switches OFF when center tank fuel non precision, visual)

quantity reaches approximately Minimum Safe altitude

1000 pounds/500 kilograms. Runway condition

Bleeds and anti-ice (ON or OFF)

During an ETOPS flight, additional Flaps configuration

steps must be done. Autobrake configuration

See the ETOPS supplementary Heigh or altitude decision

procedure in SP.1. Missed approach procedureAirport notam and taxi plan

Before top of descent, modify the

active route as needed for the arrival Approach category :

and approach.

Verify or enter the correct RNP

for arrival.

Takeoff Profile using VNAV Climb and Cruise Procedure


Category IAS

C 121 knots or more but less than 141 knots

D 141 knots or more but less than 166 knots

At transition altitude, set and crosscheck the altimeters to standard.

Descent Procedure


Set the RADIO/BARO minimums as needed for the approach.

Set or verify the navigation radios and course for the approach.

Select FMC approach procedure


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The Approach Procedure is normally started at transition level.

Complete the Approach Procedure before :

the initial approach fix, or

the start of radar vectors to the final approach course, or

the start of a v isual approach

Set the passenger signs as needed.

At or above 10,000 feet MSL, set the

FIXED LANDING light switches to ON.

Update the approach briefing as

needed.

Call APPROACH CHECKLIST. Do the APPROACH checklist

Flap extension schedule :

"1"

Update the RNP as needed.

Current Flap At speedtape Select Flaps Command Speed for

Approach Procedure


At transition level, set and crosscheck the altimeters.

Update the arrival and approach procedures as needed.

ILS Approach Procedure VNAV Approach Procedure

Flaps 15 "15" Flaps 15(VREF30 or VREF40)

with wind additives

Flaps 1 "1" Flaps 1 "5"

Flaps 5 "5" Flaps 5 "15"

Position "display" selected flapsFlaps UP "UP" Flaps UP


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Visual Approach Procedure VS approach Procedure RNAV Approach Procedure


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Notify the cabin crew to prepare for At the same time : Position the FLAP lever to 15 and Disengage the autopilot. Control the

landing. push the TO/GA switch monitor flap retraction airplane manually.

Verify that the cabin is secure. call FLAPS 15.

Verify that thrust levers are closed Verify that the SPEED BRAKE lever

Call FLAPS ___ according to the Set flap lever as directed. Monitor Verify : Verify that the SPEED BRAKE lever is UP.

flap extension s chedule. flaps and slats extension. the rotation to goaround attitude is UP. Call SPEED BRAKES UP.

that the thrust increases. Without delay, fly the nose wheel If the SPEED BRAKE lever is not UP,

smoothly onto the runway. call SPEED BRAKES NOT UP.

Verify that the thrust is sufficient for Monitor the rollout progress.

the go-around or adjust as needed.

Verify correct autobrake operation.

Arm the APP mode. Verify a positive rate of climb on the Verify a positive rate of climb on the

alt imeter and cal l GEAR UP. alt imeter and cal l POSITIVE RATE. WARNING:After the reverse thrust levers are m oved, a ful l

Use HDG SEL to intercept the final Set the landing gear lever to UP. stop landin g mus t be made. If an engine stays in reverse,

approach course as needed. safe f l ight is not possible.

Verify that the missed approach

altitude is set. Without delay, move the reverse

thrust levers to the interlocks and

Call GLIDE SLOPE/GLIDE PATH If airspeed is below the top of the hold light pressure until the interlocks

ALIVE. amber band, limit bank angle to 15. release. Then apply reverse thrust

as needed.

At glide slope/glide path alive, call: Set the landing gear lever to DN. Above 400 feet, verify LNAV or Observe mode annunciation.

"GEAR DOWN" Verify that the green landing gear select HDG SEL as appropriate. By 60 knots, start movement of the Call 60 KNOTS.

"FLAPS 15" indicator lights are illuminated. Above 400 feet, select appropriate reverse thrust levers to be at the

Set the flap lever to 15. roll mode and verify proper mode reverse idle detent before taxi speed

annunciation.

Set the speed brake lever to ARM. After the engines are at reverse idle,Verify that SPEED BRAKE ARMED Verify that missed approach route move the reverse thrust levers

light is illuminated. is tracked. full down.

At glide slope/glide path capture, call Set the flap lever as directed. At acceleration height, call Set the FLAP lever as directed. Before taxi speed, disarm the

FLAPS ___ as needed for landing. FLAPS ___ according to the flap Monitor f laps and slats retraction. autobrake. Use manual braking

retraction schedule. as needed.

Set the missed approach altitude

on the MCP. After flap retraction to planned flap

setting, select LVL CHG. VNAV may

Call LANDING CHECKLIST. Do the LANDING checklist. be selected if the flaps are up.

Set the landing gear lever to OFF

after landing gear retraction is

complete.

Set the engine start switches

as needed.

Call AFTER TAKEOFF CHECKLIST. Do the AFTER TAKEOFF checklist.

Landing Roll Procedure

Pilot Flying Pilot Monitoring Pilot Flying Pilot Monitoring

verify that the deviation pointers are shown.

Verify that the localizer/final approach course is captured.

At the final approach fix or OM, verify the crossing altitude.

Monitor the approach.

Go-around and Missed Approach Procedure

Verify that climb thrust is set.

Verify that the missed approach altitude is captured.

Landing Procedure


When on localizer/final approach course intercept heading :

verify that the navigation radios are tuned and identified (as needed)


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IFE/PASS SEAT power switch As needed

Start the After Landing Procedure when clear of the active runway. WING ANTIICE switch OFF When making a no engine bleed takeoff or landing :

Engine cooldown recommendations : Takeoff

run the engines for at least 3 minutes ENGINE ANTIICE switches OFF

use a thrust setting normally used for taxi operations PACK Switches AUTO

routine cooldown times less than 3 minutes are not recommended. Hydraulic panel Set

ISOLATION VALVE Switch CLOSE

ENGINE HYDRAULIC PUMPS switches ON

The captain moves or verifies that Engine Bleed Air Switches OFF

SPEED BRAKE lever is DOWN. ELECTRIC HYDRAULIC PUMPS switches OFF

After Takeoff

Start the APU, as needed. RECIRCULATION FAN switches As needed If engine failure occurs, do not position engine BLEED air switches ON

until reaching 1500 feet or until obstacle clearance height has

Set the PROBE HEAT switches to Air conditioning PACK switches AUTO been attained.

OFF. At not less than 400 feet, and prior to 2000 feet above field elevation:

ISOLATION VALVE switch OPEN Engine N2 BLEED Air Switch ON

Set the exterior lights as needed. When CABIN rate of CLIMB indicator stabilizes:

Engine BLEED air switches ON Engine N1 BLEED Air Switch ON

Set the ENGINE START switches

to OFF. APU BLEED air switch ON ISOLATION VALVE Switch AUTO

Set the weather radar to OFF. Exterior lights switches As needed LandingWhen below 10,000 feet and starting the turn to final approach:

Set the AUTO BRAKE select switch FLIGHT DIRECTOR switches OFF Engine BLEED Air Switches OFF

to OFF. Avoid high rates of descent for passenger comfort.

Transponder mode selector STBY

Set the flap lever to UP.

Electronic Flight Bag Close flight

Set the transponder mode selectoras needed. APU switch As needed

At airports where ground tracking is The following procedure is accomplished to permit safe application

not available, select STBY. At Do the SHUTDOWN checklist. of electrical power.

airports equipped to track airplanes BATTERY Switch Guard Closed

on the ground, select an active

transponder setting, but not a STANDBY POWER Switch Guard Closed

TCAS mode.

ALTERNATE FLAPS Master Switch Guard Closed

IRS mode selectors OFF

Windshield WIPER Selector(s) PARK

EMERGENCY EXIT LIGHTS switch OFF

ELECTRIC HYDRAULIC PUMPS Switches OFF

WINDOW HEAT switches OFF

Electrical power Set LANDING GEAR Lever DN

If APU power is needed : Air conditioning PACK switches OFF Verify that the green landing gear indicator lights are illuminated.

Verify that the APU GENERATOR OFF BUS light is illuminated. Verify that the red landing gear indicator lights are extinguished.

APU GENERATOR bus switches ON EFB POWER switch Push If external power is needed:

Verify that the SOURCE OFF lights are extinguished. GRD POWER Switch ON

If external power is needed: Do the SECURE checklist. Verify that the SOURCE OFF lights are extinguished.

Verify that the GRD POWER AVAILABLE light is illuminated. Verify that the TRANSFER BUS OFF lights are extinguished.

GRD POWER switch ON Do the Electrical power down procedure Verify that the STANDBY PWR OFF light is extinguished.

Verify that the SOURCE OFF lights are extinguished. If APU power is needed:

FASTEN BELTS switch OFF Verify that the engine No. 1, APU and the engine No. 2 fire switches are in.

Alert ground personnel before the following test is accompl ished.

ANTI COLLISION light switch OFF OVERHEAT DETECTOR switches NORMAL

FUEL PUMP switches OFF TEST switch Hold to FAULT/INOP

Verify that the MASTER CAUTION lights are illuminated.

CAB/UTIL power switch As needed Verify that the OVHT/DET annunciator is illuminated.

SP 2.7 - Unpressurized Takeoff and Landing

SP 6.1 - Electrical Power Up

After Landing Procedure


Shutdown Procedure

Secure Procedure


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Verify that the FAULT light is illuminated.

If the FAULT light fails to illuminate, the fault monitoring system is

inoperative. Engine No. 1 must be started first. Icing conditions exist when OAT (on the ground) or TAT (in-flight) is

Verify that the APU DET INOP light is illuminated. When cleared to start: 10C or below and any of the following exist:

Do not operate the APU if the APU DET INOP light fails to illuminate. APU BLEED air switch OFF visible moisture (clouds, fog with visibility less than one statute mile

TEST switch Hold to OVHT/FIRE (1600m), rain, snow, sleet, ice crystals, and so on) is present,

Verify that the fire warning bell sounds. Engine No. 1 start Accomplish or

Verify that the master FIRE WARN lights are illuminated. Use normal start procedures. ice, snow, slush or standing water is present on the ramps,

Verify that the MASTER CAUTION lights are illuminated. WARNING : To minimize the hazard to ground personnel , the taxiways, or runways.

Verify that the OVHT/DET annunciator is illuminated. external air shou ld be d isconnected, and engine CAUTION : Do not use engine or wing antiice when OAT (GRD)

Master FIRE WARN light Push No. 2 star ted using the Eng ine Crossbleed or TAT (in-f light) is above 10C.Verify that the master FIRE WARN lights are extinguished. Start procedure.

Verify that the fire warning bell cancels. Prefl ight Procedu re - First Off icer

Verify that the engine No. 1, APU and the engine No. 2 fire switches Do the following step after completing the normal Preflight

stay illuminated. Procedure - First Officer:Verify that the ENG 1 OVERHEAT and ENG 2 OVERHEAT lights PROBE HEAT switches ONstay illuminated. Verify that all probe heat lights are extinguished.

EXTINGUISHER TEST switch Check Prior to using this procedure, ensure that the area is clear.

TEST Switch Position to 1 and hold Engine BLEED air switches ON Engine Start Procedu reVerify that the three green extinguisher test lights are illuminated. Do the normal Engine Start Procedure with the following

TEST Switch Release APU BLEED air switch OFF modifications:

Verify that the three green extinguisher test lights are extinguished. If the engine has been cold soaked for one or more hours at

Repeat for test position 2. PACK switches OFF ambient temperatures below -40C, do not start or motor the

APU START engine. Maintenance personnel should do appropriate

If extended APU operation is needed on the ground, position an AC ISOLATION VALVE switch AUTO procedures for adverse weather heating of the

operated fuel pump ON. If fuel is loaded in the center tank, position the Ensures bleed air supply for engine start. Hydro-Mechanical Unitleft center tank fuel pump switch ON to prevent a fuel imbalance Engine thrust lever(operating engine) Advance thrust lever If ambient temperature is below -35C, idle the engine for two

before takeoff. Advance thrust lever until bleed duct pressure indicates 30 PSI. minutes before changing thrust lever position

When the APU GEN OFF BUS light is illuminated: Nonoperating engine Start Up to three and onehalf minutes may be allowed for oil pressure

APU GENERATOR bus switches ON Use normal start procedures with crossbl eed air. to reach the minimum operating pressure. During this period,Verify that the SOURCE OFF lights are extinguished. After starter cutout, adjust thrust on both engines, as required. the LOW OIL PRESSURE light may remain illuminated,

Verify that the TRANSFER BUS OFF lights are extinguished. pressure may go above the normal range and the FILTER

Verify that the STANDBY PWR OFF light is extinguished. BYPASS light may illuminate. Operate the engine at idle thrust

Verify that the APU MAINT light is extinguished. until oil pressure returns to the normal range

Verify that the APU LOW OIL PRESSURE light is extinguished.

Verify that the APU FAULT light is extinguished. Engine Ant i - i ce Operat ion - On the Ground

Verify that the APU OVERSPEED light is extinguished. If an engine fuel leak is suspected: Do not rely on airframe visual icing cues before activating engine

Wheel well fire warning system Test Accomplish the ENGINE FUEL LEAK checklist. anti-ice. Use the temperature and visible moisture criteria because

Maintain main tank No. 1 and No. 2 fuel balance within limitations. late activation of engine anti-ice may allow excessive ingestion of

Test switch Hold to OVHT/FIRE Fuel pump pressure should be supplied to the engines at all times. ice and result in engine damage or failure.

Verify fire warning bell sounds, master FIRE WARN lights, MASTER At high altitude, without fuel pump pressure, thrust deterioration or engine ENGINE START switches CONT (F/O)CAUTION lights and OVHT/DET annunciator illuminate. flameout may occur.

Fire warning BELL CUTOUT switch Push If the center tank contains fuel: ENGINE ANTI-ICE switches ON (F/O)Verify that the master FIRE WARN lights extinguish. Center tank fuel pump switches OFF Verify that the COWL VALVE OPEN lights illuminate bright, then dim.

Verify that the fire warning bell cancels. Verify that the COWL ANTI-ICE lights are extinguished.

Verify that the WHEEL WELL fire warning light is illuminated. Crossfeed selector Open

Wing Ant i - i ce Operation - On the Grou nd

Fuel pump switches (low tank) OFF Use wing anti-ice during all ground operations between engine start

When quantities are balanced: and takeoff when icing conditions exist or are anticipated, unless

Fuel pump switches (main tank) ON the airplane is, or will be protected by the application of Type II or

Center tank fuel pump switches ON Type IV fluid in compliance with an approved ground de-icing

This procedure assumes the Secure procedure is complete. Crossfeed selector Close program. Do not use wing anti-ice as an alternative for ground

APU switch and/or GRD POWER switch OFF If the center tank contains no fuel: de-icing/anti-icing.

If APU was operating: Crossfeed selector Open When wing anti-ice is needed:

Delay approximately 2 minutes after the APU GEN OFF BUS WING ANTI-ICE switch ON (F/O)

light extinguishes before placing the BATTERY switch OFF. Fuel pump switches (low tank) OFF Verify that the L and R VALVE OPEN lights illuminate DIM

BATTERY switch OFF When quantities are balanced:

Fuel pump switches ON

Crossfeed selector Close

SP 6.4 - Electrical Power Down

SP 7.5 - Starting with Ground Air Source

SP 7.5 - Engine Crossbleed Start

SP 12.1 Fuel Balancing

SP 16.1 - Cold Weather Operation


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Before Taxi Procedu re When engine anti-ice is needed: Parking Brake Released ( C )

Do the normal Before Taxi Procedure with following modifications: ENGINE START switches CONT (PM) Reduces the possibility of frozen brakes.

GENERATOR 1 and 2 switches ON (F/O) Cold weather maintenance procedures for securing the

ENGINE ANTI-ICE switches ON (PM) airplane may be required.

Flight controls Check ( C ) Verify that the COWL VALVE OPEN lights illuminate bright, then dim.

An increase in control forces can be expected at low temperatures. Verify that the COWL ANTI-ICE lights are extinguished.

Flaps Check (F/O)Move the flaps from Flaps up to Flaps 40 back to Flaps up to ensure Wing An ti- ice Operation - In-Fl ight

freedom of movement. Ice accumulation on the flight deck window frames, windshield

If taxi route is in icing condit ion, taxi out with the flaps up. center post, or on the windshield wiper arm may be used as an Flights should be conducted to avoid thunderstorm or hail activity.

Taxi at a reduced speed. Use smaller nose wheel steering wheel indication of structural icing conditions and the need to turn on If visible moisture is present at high altitude, avoid flight over the

and rudder inputs and apply minimum thrust evenly and smoothly. wing anti-ice.The wing anti-ice system may be used as a de-icer or storm cell.

anti-icer in flight only. If moderate to heavy rain, hail or sleet is encountered:

De-ic ing/Ant i-ic ing CAUTION : Use of w ing anti-ice above approximately FL350 may ENGINE START switches CONT

If de-icing/anti-icing is needed: cause bleed t r ip of f and possible loss of cabinAPU As needed (F/O) pressure. Autothrottle Disengage

The APU should be shut down unless APU operation is necessary. When wing anti-ice is needed:

Call FLAPS UP. ( C ) WING ANTI-ICE switch ON (PM) Thrust Levers Adjust SlowlyVerify that the L and R VALVE OPEN lights illuminate bright, then dim.

Flaps UP (F/O) IAS/MACH Use a slower speed

Af ter Landing Procedure

Thrust levers Idle ( C ) Taxi at a reduced speed. Use smaller nose wheel steering wheel

Reduces the possibility of injury to personnel at inlet or exhaust areas. and rudder inputs and apply minimum thrust evenly and smoothly.

Stabilizer trim Full APL NOSE DOWN ( C )

Do the normal Procedure with the following modifications:

Engine BLEED air switches OFF (F/O) Do not retract the flaps to less than flaps 15 until the flap areas Yaw Damper ON

have been checked to be free of contaminants

APU BLEED air switch OFF (F/O) Autothrottle Disengage

Engine anti-ice must be selected ON and remain on during all

After de-icing/anti-icing is completed: ground operations when icing conditions exist or are anticipated. AUTOPILOT CWS

APU As needed (F/O) Shutdown Procedure ENGINE START switches FLT

Do the following step before starting the normal Shutdown

Engine BLEED air switches ON (F/O) Procedure: Thrust SetWait approximately one minute after de-icing is completed Stabilizer trim Set 0 to 2 units ( C ) Set thrust as needed for the phase of flight. Change thrust setting only if

Control column Move full forward/full aft ( C ) needed to modify an unacceptable speed trend.

Secure Procedur e Climb 280 Kts or .76 Mach

Stabilizer trim Set for takeoff ( C ) Do the following step before starting the normal Shutdown Cruise FMC Setting

APU Start (F/O) Descent .76 Mach/ 280 Kts/ 250 Kts

Before Takeoff Procedu re If an approach must be made into an area of severe turbulence,

Do the normal Procedure with the following modifications: APU GENERATOR bus switches ON (F/O) delay flap extension as long as possible.

Call FLAPS ___ as needed for takeoff. PF

PACK switches AUTO (F/O)

Flap lever Set takeoff flaps, as needed (PM)

ISOLATION VALVE switch OPEN (F/O)

Takeoff Procedu re

Do the normal Procedure with the following modifications: Pressurization mode selector MAN (F/O)When engine anti-ice is required and the OAT is 3C or below,

the takeoff must be preceded by a static engine run-up to a minimum of Outflow valve switch OPEN (F/O)70% N1 for approximately 30 seconds and confirm stable engine operate Prevents aircraft pressurization.

APU BLEED air switch ON (F/O)

Engine An ti-Ice Operation - In-f l ight If the airplane will not be attended, or if staying overnight,the flight

Engine antiice must be ON during all flight operations when crew must arrange for or verify that the following steps are done:

icing conditions exist or are anticipated, except during climb and Pressurization mode selector MAN (F/O)

cruise when the temperature is below -40C SAT. Engine antiice

must be ON before, and during descent in all icing conditions, Outflow valve CLOSE (F/O)

including temperatures below -40C SAT. Position the outflow valve fully closed to inhibit the intake of snow or ice.

When operating in areas of possible icing, activate engine antiice Wheel chocks Verify in Place (C or F/O)

before entering icing conditions.

SP 16.19 Mederate to Heavy Rain, Hail or Sleet

SP 16.20 Severe Turbulence


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737 ach fo procedures 10x21

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