Normal Procedures
Contents
1. 737 Captain FLIGHT MANUAL Part III Normal Procedures 6 DO NOT USE FOR FLIGHT ENGINE LIMIT DISPLAY MARKINGS Maximum and minimum limits are red Caution limits are amber GENERAL ENGINE LIMITATIONS Maximum Start EGT Ambient Temperature above 15 C momentary 420 C Ambient Temperature below 15 C 350 Q Maximum Oil Temperature continuous 120 q 15 minutes 121 C 157 C OIL PRESSURE Maximum Oil Pressure Minimum Oil Pressure age ENGINE IGNITION Engine ignition must be on during takeoff and landing REVERSE THRUST Intentional selection of reverse thrust in flight is prohibited Maximum start EGT is 760 C Maximum continuous EGT is 710 C With APU bleed electrical load maximum altitude is 10 000 ft With APU bleed maximum altitude is 17 000 ft With APU electrical load maximum altitude is 35 000 ft APU bleed valve must be closed when e ground air connected and isolation valve open e engine no 1 bleed valve open e isolation valve and engine no 2 bleed valve open APU bleed valve may be open during engine start but avoid engine power above idle 2012 Captain Sim www captainsim com 737 Captain FLIGHT MANUAL Part III Normal Procedures 7 DO NOT USE FOR FLIGHT FLIGHT CONTROLS Flap extension altitude is 20 000 ft In flight do not extend the SPEED BRAKE lever beyond the FLIGHT DETENT Avoid rapid and large alternating control inputs especial2. 737 Captain FLIGHT MANUAL Part III Normal Procedures 17 DO NOT USE FOR FLIGHT LEFT WING AND LEADING EDGE WING SUurfaces s asrang aana anaa KAEN ENE KAB a KAANANE EEE aa ENE EEE NEK Check Leading edge Slats 5 sasinan aka naka Ai aia a AKA aa dake ai KANG kaa Check NUMBER 1 ENGINE Exhaust area and tailcone ssssrssesssssssrsssrrenssesnssrsesrrensonrsoeenossnnse Check Thrust reverse Saeimos aa aba a e A Aa NG ee NE E a Ga AA Ga ka Stowed Fan blades probes and SPiNNEL ccc cece cece cece eee eee eee e eens nett en ene Check Probes sensors ports vents and drains as applicable Check ACCESS PANES sawakane aa aa aa ga a aii aaa KANAAN ANA aaa aaa na an Latched LEFT WING ROOT PACK AND LOWER FUSELAGE Leading edge apsara aana a Dagan agan NA as Check Probes sensors ports vents and drains as applicable Check Exterior Meja EEE E A EN TE KAT E a AR EN GN E ERRES Check PREFLIGHT PROCEDURE FIRST OFFICER The first officer normally does this procedure The captain may do this procedure if needed Flight control Panel sasarane aaa anna nenesa ag a Kan EA Sia ais Check FLIGHT CONTROL switches Guards closed Flight SPOILER switches Guards closed YAW DAMPER switch ON NAV transfer SwitcheS s ssssssssrrerresssossssrrernsenseeussssasananssoans NORMAL Verify that the FUEL VALVE CLOSED lights are illuminated dim Verify that the FILTER ICING lights are extingu
3. DO NOT USE FOR FLIGHT __4 FFI Captain FLIGHT MANUAL PART III Normal Procedures www captainsim com DO NOT USE FOR FLIGHT ABOUT THIS MANUAL VERSION 04 MAY 2012 WARNING THIS MANUAL IS DESIGNED FOR MICROSOFT FSX USE ONLY DO NOT USE FOR FLIGHT The 737 Captain FLIGHT MANUAL is organized into four Parts Each Part is provided as a separate Acrobat PDF document e Part I User s Manual o The User s Manual describes the 737 Captain Sim product as a software title e Part II Aircraft Systems e Part III Normal Procedures this document Part IV Flight Crew Training Manual Adobe Acrobat Reader Required FOR GENERAL INFORMATION ON THE 737 CAPTAIN PRODUCT PLEASE USE WWW CAPTAINSIM COM THIS MANUAL PROVIDES ADDITIONAL INFORMATION ONLY WHICH IS NOT AVAILABLE ON THE WEB SITE www captainsim com DO NOT USE FOR FLIGHT 737 Captain FLIGHT MANUAL PART III CONTENTS 3 OPERATING LIMITATIONS WEIGHT LIMITATIONS 737 200 AIRPLANES AIR SYSTEMS ANTI ICE RAIN AUTOPILOT ELECTRICAL POWER ENGINES APU FLIGHT CONTROLS FLIGHT MANAGEMENT NAVIGATION FUEL LANDING GEAR 8 NORMAL PROCEDURES INTRODUCTION NINININIGOG OO UUUU 8 NORMAL PROCEDURES PHILOSOPHY AND ASSUMPTIONS 8 CREW DUTIES 9 SCAN FLOW AND AREAS OF RESPONSIBILITY 10 PREFLIGHT AND POSTFLIGHT SCAN FLOW 11 AREAS OF RESPONSIBILITY CAPTAIN AS PILOT FLYING OR TAXIING 12 AREAS OF R
4. Set the speed bugs at VREF VREF 15 and flaps up maneuvering speed Set radio altimeter minimums as needed for the approach Check and set EPR bugs for the GO AROUND corrected for the bleed configuration Set or verify the navigation radios and course for the approach Set the AUTOBRAKE selector to the needed brake setting Call DESCENT CHECKLIST Do the DESCENT checklist www captainsim com 33 DO NOT USE FOR FLIGHT APPROACH PROCEDURE The Approach Procedure is normally started at transition level Complete the Approach Procedure before e the initial approach fix or e the start of radar vectors to the final approach course or e the start of a visual approach If a flaps 15 landing is needed because of performance GROUND PROXIMITY flap gear inhibit switch FLAP GEAR INHIBIT F O Pilot Flying Pilot Monitoring Set the passenger signs as needed At or above 10 000 feet MSL set the INBOARD LANDING light switches to ON At transition level set and crosscheck altimeters Update changes to the arrival and approach as needed Update the approach briefing as needed Call APPROACH CHECKLIST Do the APPROACH checklist FLAP EXTENSION SCHEDULE At Speed knots lected Flaps 140 VREF30 or VREF40 wind additives As needed www captainsim com 34 DO NOT USE FOR FLIGHT LANDING PROCEDURE Pilot Flying Pilot Monitoring Notify the cabin crew to prepare for l
5. AIL Vertical stabilizer and rudder saanane noni iniii aaa aa naa naa Check Elevator feel ProDGS isinsin sipi i innn n a Es a EEES Check Horizontal stabilizer and elevator eee een Check Static discharge WICKS saanane aaa naa aan aa pa ae a a a Ta NG Ka a gka BA Check APU exhaust outlet asas saa sa aana a ag EEE aa EEE a Na aa nes Check Verify that there is no indication of scorch marks on the outlet LEFT AFT FUSELAGE Doors and access panels NOt iN USE cceeeeeeeeee eee e eee etna eae ee eee Latched Probes sensors ports vents and drains as applicable Check LEFT MAIN WHEEL WELL VIEW PONG anaing kini kaa aa ika aring aje ag m jana an ninen aa Be a Clear and clean Wheel well ss anainaira kiai aas aja anana aka naga th aa a maa a a aa a Ka eaaa a palana d aa kani Check Verify that the wheel chocks are in place as needed Gear strut actuators and do0ors sarsa rese eee eeeeeeaeeeeeeeaeeeeeaeegs Check Hydraulic IMCS anaa ka aaa aaa aE BADE a aa aa a Baal AK a Ka Secure LEFT WING TIP AND TRAILING EDGE Aileron and trailing edge flapS s ssssssrsserrsssresssssressrsosressssosssosssene Check Static discharge WICKS c cceccsaicteceercetinas ss NEGEN E aaa Kg TAG ka KE A aia ahead seazen Check POSiItIOM OATS ii ennaa a aa BANGGA GA NGAEN A ESEA EES Check ENKterio0rlightSa sasana nani KA NANAS SENEN NENGNA NEGEN EEE a GE KH ENG aa e Check 2012 Captain Sim www captainsim com
6. saranane ee ee ene ee ee eee OFF F O FUEL PUMP SWitChES cies eee cece eee eee ee eeeeeee aan gain OFF F O CAUTION Do not use the center tank fuel pumps with the flight deck unattended GALLEY power SWITCH siii aaa ag aaa aa aa kaa a aaa a in kaag aia As needed F O WING ANTI ICE swWIiteh 4s445a5s5a 855 aaaa nana eee aaa na eee tees OFF F O ENGINE ANTI ICE switches OFF F O FY draulic Panels sasana aana a aaa aaa a aaa aaa aaa b ajaka ba Set F O ENGINE HYDRAULIC PUMPS switches ON www captainsim com 39 DO NOT USE FOR FLIGHT ELECTRIC HYDRAULIC PUMPS switches OFF GASPER FAN SWIitCH ccccceeceeeeseeeeeaeeeeeaee As needed F O Air conditioning PACK SWItCHES ccceeeeeeeeee eee ne eee eaee Set F O One air conditioning PACK switch ON Other air conditioning PACK switch OFF ISOLATION VALVE SWItCH cccceseeeee eee e teen nenen AUTO F O Engine BLEED air switches ss aranana anna ON F O APU BLEED aif SWItCH rana asana naa aana a aaa aa aan aga eet ON F O Exterior lights switches sanane eaaa anane As needed F O Flight director mode selector sasana ee eens OFF C F O After the wheel chocks are in place Parking brake Release C APUHSWIt hi iii naa a aaa kna ab ada aik ad aja D ga a ATEK iga aa As needed F O Flight deck door Unlock F O Verify that the CAB DOOR UNLOCKED light as installed is illuminated OXYGEN regulators sss ccccwcecstondhi
7. 11 DO NOT USE FOR FLIGHT AREAS OF RESPONSIBILITY CAPTAIN AS PILOT FLYING OR TAXIING f ji Sasa TYPICAL PANEL LOCATIONS ARE SHOWN CAPTAIN ITEMS INCLUDING AUDIO CONTROL TRIM First OFFICER ITEMS JOINT RESPONSIBILITY TEMS 2012 Captain Sim www captainsim com 737 Captain FLIGHT MANUAL Part III Normal Procedures 12 DO NOT USE FOR FLIGHT AREAS OF RESPONSIBILITY FIRST OFFICER AS PILOT FLYING OR TAXIING TYPICAL PANEL LOCATIONS ARE SHOWN caran TEMS JOINT RESPONSIEBILITY ITEMS FIRST OFFICER MEMS INCLUDING AUDIO CONTROL TRIM 2012 Captain Sim www captainsim com DO NOT USE FOR FLIGHT NORMAL PROCEDURES AMPLIFIED PROCEDURES PRELIMINARY PREFLIGHT PROCEDURE CAPTAIN OR FIRST OFFICER The Preliminary Preflight Procedure assumes that the Electrical Power Up supplementary procedure is complete Electronic master Switches ssasinisas spg ea K anana aa ANGGON AANE ANANE ON Circuit breakers P6 panel szsisisuwssssesisisasia page degan de Egen aga NANGEN ENENG Check Circuit breakers P18 panel 0seaeaaaeae ana nen nean anana nana n nenen ne Check Parking brak saienitisi aaae gga Ga sa EE Na As needed EKTERIOR INSPECTION Before each flight the captain first officer or maintenance crew must verify that the airplane is satisfactory for flight Items at each location may be checked in any sequence Use the detailed inspe
8. DO NOT USE FOR FLIGHT Start the Shutdown Procedure after taxi is complete Parking Drake nininini pa Waa ag aga rain NAGA UN EA EE LEE i Set C Verify that the parking brake warning light is illuminated Electrical POW saa adaa anara nh apanas AKARANA NGA AKEH aga NA GAE Eeh an aeai aaraa Set F O If APU power is needed Verify that the APU GENERATOR OFF BUS light is illuminated APU GENERATOR bus switches ON Verify that the BUS OFF lights are extinguished If external power is needed Verify that the GND POWER AVAILABLE light is illuminated GROUND POWER switch ON Verify that the BUS OFF lights are extinguished Before engine shutdown consider engine cooldown recommendations Engine start Evers sasada dai aia a aa aaa aaa a aaa CUTOFF C If towing is needed Establish communications with ground handling personnel C System A HYDRAULIC PUMP switches OFF Verify that the system A pump LOW PRESSURE lights are illuminated CAUTION Do not hold or turn the nose wheel steering wheel during pushback or towing This can damage the nose gear or the tow bar CAUTION Do not use airplane brakes to stop the airplane during pushback or towing This can damage the nose gear or the tow bar Set or release parking brake as directed by ground handling personnel When towing is complete System A HYDRAULIC PUMP switches ON FASTEN BELTS swit h sworo sarana anaa nem sang aa seen aa aas OFF F O ANTI COLLISION light switch
9. as installed has been accomplished according to approved procedures once each flight day On revenue flights the escape slide retention bar girt bar must be installed during taxi takeoff and landing www captainsim com 737 Captain FLIGHT MANUAL Part III Normal Procedures 5 DO NOT USE FOR FLIGHT WEIGHT LIMITATIONS 737 200 AIRPLANES CHARACTERISTICS 737 200 737 100 737 200ADV 737 200C F TAKEOFF WEIGHT POUNDS 116 000 111 000 128 100 116 000 ZERO FUEL WEIGHT POUNDS 95 000 90 000 95 000 95 000 OPERATING EMPTY WEIGHT POUNDS 59 800 62 000 65 700 65 700 AIR SYSTEMS The makimum cabin differential pressure relief valves is 8 65 psi ANTI ICE RAIN Engine TAI must be on when icing conditions exist or are anticipated except during climb and cruise below 40 C SAT Minimum N1 RPM for operating in icing conditions except for landing 40 when TAT between 0 and 10 C 55 when TAT below 0 C 70 in moderate to severe icing conditions when TAT below 6 5 C Window heat inop max speed 250 KIAS below 10 000 ft AUTOPILOT Use of autopilot not authorized for takeoff or landing Do not use autopilot roll channel above 30 000 feet with yaw damper inoperative Do not use autopilot pitch channel above 81M with hydraulic system A or B depressurized ELECTRICAL POWER Max engine driven generator load 111 amps Maximum generator drive oil temperature 157 C 2012 Captain Sim www captainsim com
10. n nenen n anane nenen Set for departure Audio selector pan lz s asasi iaasas an aa a EN eaaa iiis Set WARNING Do not put objects between the seat and the aisle stand Injury can occur when the seat is adjusted Adjust the seat for optimum eye reference Verify a positive horizontal fore and aft seat lock Rudder pedalai Pagagan ne Nan Tan E aana ga ah Kaga KAE Adjust Adjust the rudder pedals to allow full rudder pedal and brake pedal movement Seat belt and shoulder NarneSS cccccceeeeeeeeeeeeeeeeeeeseeeeeeaees Adjust Call PREFLIGHT CHECKLIST www captainsim com 24 DO NOT USE FOR FLIGHT BEFORE START PROCEDURE Start the Before Start Procedure after papers are on board light deck dOOMs necra a iin eee Closed and locked F O Verify that the CAB DOOR UNLOCKED light as installed is extinguished Verify that the LOCK FAIL light as installed is extinguished Do the Performance Data Computer System as installed Preflight Supplementary Procedure PDCS CDU flight mode selector as installed As needed C F O Takeoff data asana aia aaa ika Dak anes naya ss Sam d a aana aa dn Complete C F O Verify the takeoff data to include EPR N1 V1 VR and V2 flap setting zero fuel weight temperature altimeter setting gross weight stabilizer trim setting Fuel quantity indicators sasak saa naa ag aaa aaa a GAE Check C F O Verify that the fuel on the dispatch papers and fuel quantity in
11. stop landing must be made If an engine stays in reverse safe flight is not possible AUTION start to lower the nose before selecting reverse thrust to prevent the reverser doors from touching the runway Without delay move the reverse thrust levers to the interlocks and hold light pressure until the interlocks release Then apply reverse thrust as needed By 60 knots start movement of the reverse thrust levers to be at the reverse idle detent before taxi Call 60 KNOTS speed After the engines are at reverse idle move the reverse thrust levers full down Before taxi speed disarm the autobrakes Use manual braking as needed www captainsim com 37 DO NOT USE FOR FLIGHT AFTER LANDING PROCEDURE Start the After Landing Procedure when clear of the active runway Engine cooldown recommendations e Run the engines for at least 5 minutes e Use a thrust setting no higher than that is normally used for all engine taxi operations Pilot Flying Pilot Monitoring he captain moves or verifies that the SPEED BRAKE lever is DOWN Start the APU as needed Set the PITOT STATIC HEAT switches to OFF Set the Flight Ground switch to GRD Set the LANDING and TAXI light switches as needed Set the ENGINE START switches to OFF Set the AUTOBRAKE selector to OFF Set the flap lever to UP Set the weather radar to OFF Set the transponder mode selector as needed www captainsim com 38
12. thrust Set climb EPR to approximately 90 N1 and call SET CLIMB THRUST erify that climb thrust is set At acceleration height Set the flaps up maneuvering speed call SET FLAPS SPEED Verify acceleration Set the FLAP lever as directed Monitor flaps Call FLAPS according to the and slats retraction flap retraction schedule After flap retraction is complete and above After flap retraction is complete minimum altitude for autopilot Set or verify engine bleeds and air conditioning engagement packs are operating e engage the autopilot Set the engine start switches as needed Set the AUTOBRAKE selector to OFF Set the landing gear lever to OFF after landing gear retraction is complete Call AFTER TAKEOFF CHECKLIST Do the AFTER TAKEOFF checklist www captainsim com 737 Captain FLIGHT MANUAL Part III Normal Procedures 30 DO NOT USE FOR FLIGHT AKEOFF FLAP RETRACTION SPEED SCHEDULE Takeoff Flaps At and Below Above 117 000 LB 15 or 10 V2 15 170 190 117 000 LB Limit bank angle to 15 until reaching V2 15 2012 Captain Sim www captainsim com 31 DO NOT USE FOR FLIGHT CLIMB AND CRUISE PROCEDURE Complete the After Takeoff Checklist before starting the Climb and Cruise Procedure Pilot Flying Pilot Monitoring At or above 10 000 feet MSL set the LANDING light switches to OFF Set the passenger signs as needed At transition altitude set and cross
13. A anaa naa Check View POPE anana ei ain aa ag jera a E Sapa nd aaa ah anih aa ina da a NE KK A Aa Clear and clean Nose wheel steering assembly sssssssssrsssrerssesossssosnsernossososesnranreonse Check RIGHT FORWARD FUSELAGE Probes sensors ports vents and drains as applicable Check Doors and access panels NOt iN Use sesa eee teeta teeta neta nean nane Latched RIGHT WING ROOT PACK AND LOWER FUSELAGE Ram air deflector door sasasi a ag aa Da aaa aga aa alaa aan Masa AG Extended Pack and pneumatic ACCESS GOOFS cicecceeee cette este e eee teeta neta eee naen Secure Probes sensors ports vents and drains as applicable cceeeeee Check Exterior iIgh Ss wawan awanan ans Na KA KN KENAA ANK KATARA NGE EN NINEN Check Leading dge flaps s sasaran as aan aa EEN aa aaa aa aaa NE KANANE NE kaa Kai aan Check NUMBER 2 ENGINE ACCESS Ppan lS ss anas aaa na nona aa sag ENE NG KENE KANANG Dara E E Ke ea naa iE Latched Probes sensors ports vents and drains as applicable Check Fan blades probes And SPiNNEL ccceceee cece eaaa Kanan anana anana ane Check 2012 Captain Sim www captainsim com 737 Captain FLIGHT MANUAL Part III Normal Procedures 15 DO NOT USE FOR FLIGHT WMPUSEFEVEFSELS 5 ss sicctcsencnas rai aAA ED aED Stowed Exhaust area and tailCOne ssssrsssrrrrrrrrrerrrrrrrrrrrrrrrrenrrrrrrrrrrrrere Check Position IQHE
14. E FLAPS EXT green light is illuminated Make slow and deliberate inputs one direction at a time Move the control wheel and the control column to full travel in both directions and verify e freedom of movement e that the controls return to center Hold the nose wheel steering wheel during the rudder check to prevent nose wheel movement www captainsim com 28 DO NOT USE FOR FLIGHT Move the rudder pedals to full travel in both directions and verify e freedom of movement that the rudder pedals return to center Transpond r sasama snang a Alaga Ka a ANARA AKEN KENA caves As needed F O Recall Check C F O Verify that all system annunciator panel lights illuminate and then extinguish Update changes to the taxi briefing as needed C or PF Call BEFORE TAXI CHECKLIST C Do the BEFORE TAXI checklist F O BEFORE TAKEOFF PROCEDURE Engine warm up recommendations there is no need to delay the takeoff for these recommendations When the engines have been shut down more than 2 hours run the engine for 5 minutes e when taxi time is expected to be less than 5 minutes start the engines as early as feas ible use a thrust setting normally used for taxi operations Pilot Flying Pilot Monitoring Notify the cabin crew to prepare for takeoff Verify that the cabin is secure The pilot who will do the takeoff updates changes to the takeoff briefing as needed Set the weather radar display as needed Call BE
15. EE Verify closed F O Flight deck WINdOWS cceeeeeee eee e teen teens Closed and locked C F O Start ClearanC iviecteds ftewcaasddscnie E a a a a a ang an Ba alenia Ka Bian a Obtain C F O Obtain a clearance to pressurize the hydraulic systems Obtain a clearance to start the engines ANTI COLLISION light SWitCh cece eee ee ee eaaa anna ON F O Check each trim for freedom of movement Stabilizer trim UNITS Set the trim for takeoff Verify that the trim is in the green band Aileron trim 0 units Rudder trim 0 units Call BEFORE START CHECKLIST C Do the BEFORE START checklist F O www captainsim com 26 DO NOT USE FOR FLIGHT The Engine Start procedure may be done during pushback or towing Establish communications with ground handling personnel C CAUTION Do not hold or turn the nose wheel steering wheel during pushback or towing This can damage the nose gear or the tow bar CAUTION Do not use airplane brakes to stop the airplane during pushback or towing This can damage the nose gear or the tow bar Set or release the parking brake as directed by ground handling personnel C When pushback or towing is complete Verify that the tow bar is disconnected C Verify that the nose gear steering lockout pin is removed C System A HYDRAULIC PUMPS switches ON F O ENGINE START PROCEDURE Air conditioning PACK switcheS sssssssersserrerrerererreree OFF F O Start presSUre saraat na raa naga e A
16. ESPONSIBILITY FIRST OFFICER AS PILOT FLYING OR TAXIING 13 NORMAL PROCEDURES AMPLIFIED PROCEDURES 13 PRELIMINARY PREFLIGHT PROCEDURE CAPTAIN OR FIRST OFFICER 13 EXTERIOR INSPECTION 17 PREFLIGHT PROCEDURE FIRST OFFICER 22 PREFLIGHT PROCEDURE CAPTAIN 24 BEFORE START PROCEDURE 26 PUSHBACK OR TOWING PROCEDURE 26 ENGINE START PROCEDURE 27 BEFORE TAXI PROCEDURE 28 BEFORE TAKEOFF PROCEDURE 30 TAKEOFF FLAP RETRACTION SPEED SCHEDULE 31 CLIMB AND CRUISE PROCEDURE 32 DESCENT PROCEDURE 33 APPROACH PROCEDURE 33 FLAP EXTENSION SCHEDULE 34 LANDING PROCEDURE 35 GO AROUND AND MISSED APPROACH PROCEDURE 36 LANDING ROLL PROCEDURE 37 AFTER LANDING PROCEDURE 38 SHUTDOWN PROCEDURE 39 SECURE PROCEDURE 40 CUSTOMER CARE 40 SPECIAL THANKS TO www captainsim com DO NOT USE FOR FLIGHT OPERATING LIMITATIONS This chapter contains Airplane Flight Manual AFM limitations and Boeing recommended operating information Limitations that are obvious shown on displays or placards or incorporated within an operating procedure are not contained in this chapter Maximum Takeoff and Landing Tailwind Com 15 knots ponent Maximum speeds Observe Vmo_ pointer and gear flap placards Turbulent airspeed 280 KIAS 70M Mach trim inoperative imax speed 74M Maximum Operating Altitude 37 000 feet Maximum Takeoff and Landing Altitude 8 300 feet Verify that an operational check of the flight deck door access system
17. FORE TAKEOFF CHECKLIST Do the BEFORE TAKEOFF checklist Pilot Flying Pilot Monitoring hen entering the departure runway use lights as needed Verify that the brakes are released Align hen cleared for takeoff set the the airplane with the runway INBOARD LANDING light switches to ON Set the transponder mode selector to Advance the thrust levers to approximately 1 4 EPR levers in vertical position Allow the engines to stabilize Advance thrust levers to takeoff EPR Verify that the correct takeoff thrust is set Monitor the engine instruments during the takeoff Call out any abnormal indications Adjust takeoff thrust before 60 knots as needed After takeoff thrust is set the captain s hand must be on the thrust levers until V1 www captainsim com 29 DO NOT USE FOR FLIGHT Monitor airspeed Monitor airspeed and call out any abnormal incitations Maintain light forward pressure on the control column Verify 80 knots and call CHECK Call 80 KNOTS Verify V1 speed Call Vi At VR rotate toward 15 pitch attitude At VR call ROTATE Establish a positive rate of climb Monitor airspeed and vertical speed Verify a positive rate of climb on Verify a positive rate of climb on the altimeter the altimeter and call GEAR UP and call POSITIVE RATE Maintain a minimum of V2 15 to 25 Set the landing gear lever to UP after the initial climb is established At thrust reduction height reduce
18. GT does not increase by 20 seconds after the engine start lever is moved to IDLE the N1 or N2 does not increase or increases very slowly after the EGT increases the EGT quickly nears or exceeds the start limit BEFORE TAXI PROCEDURE Fuel HEAT switcheS sssssssssssssrssssrssrrrerssrrrrnsees As needed F O Before takeoff with tank fuel temperature 0 C or below set the fuel HEAT switches to ON for one cycle Fuel heat must be OFF for takeoff GENERATOR 1 and 2 SWItCHES cece eee eect ee ee eee ee eee eee ON F O PITOT HEAT SWItCheS sis aasma a anjajari na a a ajaa aaa da a ajara daraa Na ON F O WING ANTI ICE switch saranane anana anae nana As needed F O ENGINE ANTI ICE switches senare nenen eran As needed F O Flight recorder REPEAT switch s seke ae een anna a nane Push F O PACK Switche Srii iii anan anaa sara aaae ien a ag a a aan ON F O ISOLATION VALVE SWitCN c cccee aee teeta eee eeeeeeee nana AUTO F O APU BLEED alr SWitCh a aaa is aana ana a aia Ag a aaa aa aaa a aga gana anadah OFF F O Flight Ground SWItCH zssssas ass anana aa EE eee teens FLT F O APU SWICK ani a ir aaa aja Ka AKEH nara EEN EYES SENENG KAN OFF F O ENGINE START switCches senene anna ranne na nann LOW IGN F O Engine start Eversince IDLE detent C Verify that the ground equipment is clear C F O Call FLAPS____ as needed for takeoff C Flap LAA EN ae E a Set takeoff flaps F O Verify that the L
19. RENA a nang S ERES PSI F O The minimum start pressure at sea level is 30 psi Decrease the minimum start pressure 0 5 psi for each 1 000 feet above sea level Start SEQUENCE sisia aaa nana desa aaa AJA dia Kjai ja naa Ga Announce C Call START__ ENGINE C ENGINE START SWIt h 5s sasama 55 amana cece eee NA SER aa Aa naga tees GRD F O Verify that the N2 RPM increases C F O Verify that the oil pressure increases and call OIL PRESSURE RISING F O When N1 rotation is seen and N2 is at 20 or if 20 N2 is not possible at maximum motoring and a minimum of 15 N2 Engine start l Ver cccsseccessscecssneeeenecereeeseceneenenenes IDLE C Monitor fuel flow and EGT indications C F O At 35 40 N2 verify that the ENGINE START switch moves to OFF If not move the ENGINE START switch to OFF F O Verify that the duct pressure increases when the ENGINE START switch moves to OFF F O Verify that the START VALVE OPEN light extinguishes when the ENGINE START switch moves to OFF F O Call STARTER CUTOUT F O www captainsim com 27 DO NOT USE FOR FLIGHT Monitor N1 N2 EGT fuel flow and oil pressure for normal indications while the engine accelerates to a stable idle C F O Do the ABORTED ENGINE START checklist for one or more of the following abort start conditions there is no N1 rotation by 20 N2 there is no oil pressure increase by 30 seconds the fuel flow is greater than 1100 pph 500kgph at start the E
20. S arrsa a AAK SANGKA a ANA NE a SAN Ee a Check Static discharge WICKS is sarsa sasisaning ea naa NA aaa aaa aaa Na a NE gan Check Aileron and trailing edge flaps sesek aane nenen nenen nena eae a nenen Check Exterior lights e0s0nennnenao ena nan aane e nengan a aaa a A GN NA Agng enG ANG aana n naen enkes Check RIGHT MAIN GEAR Tires brakes and WhEEIS cccceccceeeeese senses sees ee aane n eaaa nana ne naen naen Check Verify that the wheel chocks are in place as needed Gear strut actuators ANd doors ss sssee rare e eaaa eeeeeaeeeaeeeaeeeaeegs Check Hydraulic NeSSie aaa EEN EAE EEE EEEE Secure RIGHT MAIN WHEEL WELL VIGW alon ANK EE EN NA A A NA E HEEE RE A ned D AE EE TENA ia Clear and clean Wheel well sisa aaa aatinaa krn Beng ajaa ka aana aga Ka aa aja a grana ena ara asaba alaa engeta ki Check RIGHT AFT FUSELAGE Doors and access panels NOt in Use kesesa a aane naen nean ena ene Latched Negative pressure relief door ssassaana anae naen anna n anana aane nane Closed Outflow Va lVe cnnan Pana ENE YAE E SENAT NANGEN ENG nga Ta EE KENEH E NENENG NG NENG Check Probes sensors ports vents and drains as applicable Check APU aira aaa ae aa saa aja aa agaran kata ils ja a DA aa a aan aana aaa aaa a aaa maap ea Aa Open 2012 Captain Sim www captainsim com 737 Captain FLIGHT MANUAL Part III Normal Procedures 16 DO NOT USE FOR FLIGHT
21. airplane configuration and navigation PF and PM duties may change during a flight For example the captain could be the PF during taxi but be the PM during takeoff through landing Normal procedures show who does a step by crew position C F O PF or PM in the procedure title or in the far right column or www captainsim com DO NOT USE FOR FLIGHT 6 in the column heading of a table The mode control panel is the PF s responsibility When flying manually the PF directs the PM to make the changes on the mode control panel The captain is the final authority for all tasks directed and done SCAN FLOW AND AREAS OF RESPONSIBILITY The scan flow and areas of responsibility diagrams shown below are representative and may not match the configuration of your airplane The scan flow diagram provides general guidance on the order of each flight crew member should follow when doing the preflight procedures Specific guidance on the items to be checked are detailed in the amplified Normal Procedures Preflight Procedure Captain and Preflight Procedure First Officer www captainsim com 737 Captain FLIGHT MANUAL Part III Normal Procedures 10 DO NOT USE FOR FLIGHT PREFLIGHT AND POSTFLIGHT SCAN FLOW TYPICAL PANEL LOCATIONS ARE SHOWN D CAPTAIN ITEMS OO FIRST OFFICER ITEMS 2012 Captain Sim www captainsim com 737 Captain FLIGHT MANUAL Part III Normal Procedures
22. anding Verify that the cabin is secure Call FLAPS according to the Set the flap lever as directed Monitor flaps and slats flap extension schedule extension When on localizer intercept heading verify that the ILS is tuned and identified verify that the LOC and G S pointers are shown eur Padangan NGA imaman approach course as needed ee NIIII At glide slope alive call Set the landing gear lever to DN GEAR DOWN Verify that the green landing gear indicator lights are FLAPS 15 illuminated Set the flap lever to 15 Set the engine start switches to LOW IGN Set the speedbrake lever to ARM Verify that the SPEED BRAKE ARMED light is illuminated At glide slope capture call FLAPS Set the flap lever as directed as needed for landing Set the missed approach altitude on the ALTITUDE ALERT controller Call LANDING CHECKLIST Do the LANDING checklist At the final approach fix or OM verify the crossing altitude Monitor the approach Disengage the autopilot prior to landing www captainsim com 35 DO NOT USE FOR FLIGHT GO AROUND AND MISSED APPROACH PROCEDURE Pilot Flying Pilot Monitoring At the same time Monitor EPR indication e push either go around switch e disengage autopilot Set the FLAP lever to 15 and monitor flap retraction e advance the thrust levers to go around EPR e Rotate to go around attitude e call FLAPS 15 Adjust thrust as neede
23. are extinguished Verify that the LOW OIL QUANTITY light is extinguished Verify that the APU LOW OIL PRESSURE light is extinguished Verify that the APU HIGH OIL TEMP light is extinguished Verify that the APU OVERSPEED light is extinguished EQUIPMENT COOLING SWItCH ccccceeeee eee e eee eee eee ee eaeeeee teens NORMAL Verify that the OFF light is extinguished EMERGENCY EXIT LIGHTS SWitCh cece eeeeeeeee ee ee nara aan a NAN Guard closed Verify that the NOT ARMED light is extinguished Pass ng r SIGNS asasaran nika aaa NENG Nak naa Naga Ka Set NO SMOKING switch AUTO or ON www captainsim com 19 DO NOT USE FOR FLIGHT FASTEN BELTS switch AUTO or ON Windshield WIPER SQIOCtOM 5 siswa Wk ara a a aka a aaa aa aaa OFF If the windshield wipers are not stowed place the selector to PARK then OFF WINDOW HEAT SWItCHES ccccsscenteceeceeesnecrsnsasscesntaeeessenenenes ON Position the switches ON at least 10 minutes before takeoff Verify that the OVERHEAT lights are extinguished Verify that the ON lights are illuminated except at high ambient temperatures PITOT STATIC HEAT SWitChES c cccee cece eee eee tees eee teen teenie OFF Verify that all PROBE HEATER lights are illuminated WING ANTI ICE SWItCh is ass 455554995 a aaa nain EE aaa nag na ag KAN a aan E Naga a OFF Verify that the VALVE OPEN lights are extinguished ENGINE ANTI ICE SWItChHES c cccccccsssecseteeseeetsnecrsnsceeesanseeenes OFF V
24. check the altimeters to standard During climb set both center tank fuel pump switches to OFF when both center tank fuel pump LOW PRESSURE lights illuminate During the last hour of cruise on ETOPS flights do a Fuel Crossfeed Valve check Before the top of descent modify the route as needed for the arrival and approach When established in a level flight attitude if the center tank contains usable fuel and the center tank fuel pump switches are OFF set both center tank fuel pump switches to ON again Set both center tank fuel pump switches to OFF when both center tank fuel pump LOW PRESSURE lights illuminate www captainsim com 32 DO NOT USE FOR FLIGHT DESCENT PROCEDURE Start the Descent Procedure before the airplane descends below the cruise altitude for arrival at destination Complete the Descent Procedure by 10 000 feet MSL Pilot Flying Pilot Monitoring Set both center tank fuel pump switches to OFF when both center tank fuel pump LOW PRESSURE lights illuminate If in level flight for an extended time with usable fuel in the center tank and the center tank fuel pump switches OFF both center tank fuel pump switches may be set to ON again Set both center tank fuel pump switches to OFF when both center tank fuel pump LOW PRESSURE lights illuminate Verify that pressurization is set to landing altitude Review the system annunciator lights Recall and review the system annunciator lights
25. ction route below to check that the surfaces and structures are clear not damaged not missing parts and there are no fluid leaks the tires are not too worn not damaged and there is no tread separation the gear struts are not fully compressed the engine inlets and tailpipes are clear the access panels are secured the exterior is not damaged and the reversers are stowed the doors and access panels that are not in use are latched the probes vents and static ports are clear and not damaged the skin area adjacent to the pitot probes and static ports is not wrinkled the antennas are not damaged the light lenses are clean and not damaged INSPECTION ROUTE www captainsim com 737 Captain FLIGHT MANUAL Part III Normal Procedures 14 DO NOT USE FOR FLIGHT LEFT FORWARD FUSELAGE Probes sensors ports vents and drains as applicable esa Check Doors and access panels NOt iN Use sesauran naen nean anaa ee nee Latched Main deck cargo door as installed sesa senene nean nenen eaaa anan ane Check Conductor straps Secure Forward E and E dodi saa aka ajaa aa a a a aa ADA ii aa ka AA a eja ga aa marga ajang aa Secure NOSE WHEEL WELL Tires and WAGES cs stan nia wajan alay E a aja TE EEN EN a aaa aaa maja EA aa Ee snare Check Exterior light aaa aaa da AANE NA Kae EE NEGEN AE NEGEN GEN Ba NANG BA a a ete Check Gear strut and dOO0FS asarana sakan AKNG AAN ani a aan A SAN
26. d the rotation to go around attitude that the thrust increases Verify that the thrust is sufficient for the go around or adjust as needed Verify a positive rate of climb on the Verify a positive rate of climb on the altimeter and call altimeter and call GEAR UP POSITIVE RATE Set the landing gear lever to UP ee Verify that the missed approach altitude is set Call TUNE RADIOS FOR MISSED Tune the navigation radios as directed APPROACH Verify that the missed approach route is tracked At acceleration height call Position the FLAP lever as directed Monitor flaps and FLAPS according to the flap slats retraction retraction schedule Verify that climb thrust is set Verify that the missed approach altitude is captured Set the landing gear lever to OFF after landing gear retraction is complete Set the engine start switches as needed all AFTER TAKEOFF CHECKLIST Do the AFTER TAKEOFF checklist www captainsim com 36 DO NOT USE FOR FLIGHT LANDING ROLL PROCEDURE Pilot Flying Pilot Monitoring erify that the thrust levers are closed erify that the SPEED BRAKE lever is UP erify that the SPEED BRAKE lever is UP all SPEED BRAKES UP Without delay fly the nose wheel smoothly onto the runway If the SPEED BRAKE lever is not UP call SPEED BRAKES NOT UP Monitor the rollout progress erify correct autobrake operation ARNING after the reverse thrust levers are moved a full
27. dicators agree Verify that the fuel is sufficient for flight Note Do not push the QUANTITY TEST switch when the airplane is being refueled This will cause incorrect indications at the external fueling panel Total fuel and VREF indicator ccccececeeeeeeeeeeeeseeeeeeaeees Set C Zero fuel weight Set Flap selector As needed Verify VREF on the VREF pointer On airplanes without PDCS EPR reference SClCCtOIS cccccsceeceeeeeeceeeeeeeeeeseeesaeeneeseeaeee Set C Verify that the EPR reference bugs and digital readouts are correct On airplanes with PDCS EPR reference selectOrS s sssissrssesssessssrrsnrennnosnssrrornsesssenss In C Verify that the PDCS reference bugs and digital readouts are correct DAS DUG SE ie aaa agan aaa es aaa aa ajaja a EE PE aaa ea aE Set C F O Set the speed bugs at V1 VR V2 15 and flaps up maneuvering speed Airspeed cursor COntrols ccccceee eee cece tees eee eee eeneeeae Set V2 C F O HSI HEADING SClECtOIrS is isa aaa aaa aa ba SSA KN aa a a E Ka gi anaa Set C F O www captainsim com 25 DO NOT USE FOR FLIGHT HSI COUrSe SEI CHOIS saanak tannin Kaanan KA KK Ka ajaa ina Aak Aa Set C F O ALTITUDE alert COntroller cccccceeeeee eee ee eee tees eee teen eae eee Set C Taxi and Takeoff DriefingS cccceeceeeeeeeeeeeeeea eee Complete C F O The pilot who will do the takeoff does the taxi and takeoff briefings gt Ana go gila jojo MAN ANNA NE E
28. erify that the VALVE OPEN lights are extinguished Hydrauli PAaMmel sis sccccesearacnrscadeecccesstecaeiandeannetage aaa naa Kn aa Set GROUND INTERCONNECT switch CLOSE HYDRAULIC PUMPS switches ON Verify that the LOW PRESSURE lights are illuminated ELECTRIC HYDRAULIC PUMPS switches OFF Verify that the OVERHEAT lights are extinguished Verify that the LOW PRESSURE lights are illuminated Cabin altitude panel ss sasasi ni nabi Nana Naah aa EE AGE EA Ba AE SN aa NG Set SMOKE CLEARANCE switch Guard closed Ait conditioning panel sisan sawara Asa aaa ag NANA aa NE ga Aa A gak Set AIR TEMPERATURE source selector As needed Verify that the DUCT OVERHEAT lights are extinguished Temperature selectors As needed Verify that the RAM DOOR FULL OPEN lights are illuminated GASPER FAN switch As needed Air conditioning PACK switches Set One switch ON Other switch OFF ISOLATION VALVE switch AUTO Engine BLEED air switches ON APU BLEED air switch ON Verify that the DUAL BLEED light is illuminated www captainsim com 20 DO NOT USE FOR FLIGHT Verify that the PACK TRIP OFF lights are extinguished Verify that the WING BODY OVERHEAT lights are extinguished Verify that the BLEED TRIP OFF lights are extinguished Cabin pressurization panel ccccceceeeeeee eee ee teen eee eee eeeeee ee ee es Set Verify that the AUTO FAIL light is extinguished Verify that the OFF SCHED DESCENT light is extinguished FAILURE ALTITUDE ind
29. features Normal procedures also assume coordination with the ground crew before e hydraulic system pressurization or e flight control surface movement or e airplane movement Normal procedures do not include steps for flight deck lighting and crew comfort items Normal procedures are done by recall and scan flow The panel illustration in this section shows the scan flow The scan flow sequence may be changed as needed CREW DUTIES Preflight and postflight crew duties are divided between the captain and first officer Phase of flight duties are divided between the Pilot Flying PF and the Pilot Monitoring PM Each crewmember is responsible for moving the controls and switches in their area of responsibility The phase of flight areas of responsibility for both normal and non normal procedures are shown in the Area of Responsibility illustrations in this section Typical panel locations are shown The preflight and postflight areas of responsibility are defined by the Preflight Procedure Captain and Preflight Procedure First Officer The captain may direct actions outside of the crewmember s area of responsibility The general PF phase of flight responsibilities are taxiing flight path and airspeed control airplane configuration navigation The general PM phase of flight responsibilities are checklist reading communications 6 tasks asked for by the PF monitoring taxiing flight path airspeed
30. icator Cruise altitude LANDING ALTITUDE indicator Destination field elevation CABIN RATE selector Index CABIN ALTITUDE indicator 200 feet below destination field elevation FLIGHT GROUND switch GRD Pressurization mode selector AUTO Verify that the STANDBY light is extinguished Verify that the MANUAL light is extinguished Lighting PaMel i ssisiivesensess KN a na EEE aa aa a Set LANDING light switches RETRACT and OFF RUNWAY TURNOFF light switches OFF TAKI light switch OFF ENGINE START SWItCHES aas 555 isnin ka jian nk ka Sai aria Ka ba aa aa OFF Lighting pah las asin aaa sasana ni a DES Set POSITION light switch As needed ANTI COLLISION light switch OFF WING illumination switch As needed WHEEL WELL light switch As needed Flight director panel ss asas aaa aeng ajara ara a Kaga aja aa a NA mah jan Na BAE Ag A Set Mode selector OFF ALTITUDE HOLD switch OFF PITCH COMMAND control Full clockwise OXYGEN isiscntacenacegienaeeneceisitcddeemseaegesreeerededscdcs n AARO AAAA Test and set STATIC SOURCE SELECTOR SWILGh lt 5 45555 450552555855 nga 595 dhap anan pada gk ag an ng nanginin NORMAL Marker beacon lights sarasa sadana aan KAG a aja ER agawa una ANAKE BENTEN KOE age NENGGE ani Test Cloke AE Aa ese a a esa dS ANA EA PANI KN eee ees Set Autopilot disengage light niiina iannu Push to test Verify that the AUTOPILOT disengage light is illuminated Flight iMStrunmnents c6 cc05 scans tesssasaanstesssvsee
31. ify that the flight instrument indications are correct www captainsim com 23 DO NOT USE FOR FLIGHT Verify that only these flags are shown TCAS as installed expected RMI flags Standby InStrumentSy isis cee esieenwacieineiannenanenc Check Verify that the flight instrument indications are correct Verify that no flags are shown STAB OUT OF TRIM OPU enaner eaaa asinan Laa nein re aga gag akan Verify extinguished SPEED BRAKE lOVCriviccscisccssscesscstisssessccadssstersasaasentestensecesteosaseas DOWN detent Verify that the SPEED BRAKE ARMED light is extinguished Verify that the SPEED BRAKE DO NOT ARM light is extinguished Reverse thrust IQVEPS cccccccccscccseeeesscesseecsseccsseecseeestseeseeesss Down Forward thrust l VEPS ccccccsceccscsssessssessseesseeesseeesseeesssessnaes Closed FLAPEV 5 aaa sage anaa e agan aaa ag e a ag aaa gae ajag aaa sia Set Set the flap lever to agree with the flap position Parking Drak Ges 5 4 area nganani wat ana naga Handed inah a aaa gaga Set Verify that the parking brake warning light is illuminated Note Do not assume that the parking brake will prevent airplane movement Accumulator pressure can be insufficient Engine start Jever Sinni ieai A aa gag a abaan dak kekiatan CUTOFF STABILIZER TRIM cutout switches 0ananenenan nenen e anana nei NORMAL VHF COMMUNICATIONS radios Set VHF NAVIGATION radios sesanan nenen en anna n anana
32. ished Fuel HEAT switches OFF Verify that the VALVE OPEN lights are extinguished CROSSFEED selector CLOSED Verify that the VALVE OPEN light is extinguished FUEL PUMP switches OFF Verify that the center tank fuel pump LOW PRESSURE lights are extinguished 2012 Captain Sim www captainsim com 18 DO NOT USE FOR FLIGHT Verify that the auxiliary tank fuel pump LOW PRESSURE lights as installed are extinguished Verify that the main tank fuel pump LOW PRESSURE lights are illuminated Electrical panel sasa sasa naka ana ag aaa kih kaa a ia a AA E Ka gan aa anaa kri aka E Set BATTERY switch Guard closed GALLEY power switch ON STANDBY POWER switch Guard closed Verify that the STANDBY PWR OFF light is ektinguished Generator drive DISCONNECT switches Guards closed Verify that the LOW OIL PRESSURE lights are illuminated Verify that the HIGH OIL TEMP lights are extinguished DRIVE TEMPERATURE switch As needed BUS TRANSFER switch Guard closed Verify that the TRANSFER BUS OFF lights are extinguished Verify that the BUS OFF lights are extinguished Verify that the GEN OFF BUS lights are illuminated Overheat and fire protection panel Passenger airplanes Check APU Switch as Needed sia nia gig saa aaa Na Raka ng aa ga Ka cae NGE feces START When the APU GEN OFF BUS light is illuminated APU GENERATOR bus switches ON Verify that the BUS OFF lights are extinguished Verify that the TRANSFER BUS OFF lights
33. lanes seses Push ENJINS INSECUMEUS renees aenea raaa AnA ENAU CAEN AEAN SNAN EESE Check Verify that the REVERSER UNLOCKED lights are extinguished Verify that the START VALVE OPEN lights are extinguished Verify that the LOW OIL PRESSURE lights are illuminated Verify that the OIL FILTER BYPASS lights are extinguished Verify that the primary and secondary engine indications show existing conditions ENGINE OIL QUANTITY TEST switch a0nenannen ane a nne a nenen n anana nenen Push Verify that the oil guantity indicators move toward zero and return to the original position when the switch is released VHF COMMUNICATIONS Fadi0s 255455557055 agan gegana Lagna anana g aaa Set VHF NAVIGATION radios sss0105esen0s0a senen ng nereg er an anapa tenenan panenan aana Set for departure Audio Selector panel ass5as aa ak aka NAN E SER DAKA Ha NA NEH GAN a a Tag Ea A sa AAK ak RER anaie Set ADF TACOS Fos sasadan anae gawan ea anaa nana naba niesie idinan nik E ga aga ENE SENA Set WEATHER RADAR panel issic a 55 Yaaa nagan Kana KUASA Tan Kae ian Set www captainsim com 22 DO NOT USE FOR FLIGHT TRANSPONGER PANO aaa aaananana aia kadanin ae aan nan eibbanses engedueeeeeneds Set STABILIZER BRAKE RELEASE knob uu eee Verify released WARNING Do not put objects between the seat and the aisle stand Injury can occur when the seat is adjusted Adjust the seat for optimum eye reference Verify a positive horiz
34. ly in combination with large changes in pitch roll or yaw e g large side slip angles as they may result in structural failure at any speed including below VA FLIGHT MANAGEMENT NAVIGATION Do not operate the weather radar in a hangar or within 50 feet of fueling operations or fuel spills Do not operate the weather radar within 160 feet of personnel Warm up radar in STBY position only Do not reset a tripped fuel pump circuit breaker Maximum fuel temperature is 49 C Minimum fuel temperature is fuel freeze point 3 C or 45 C whichever is higher FUEL LOADING On the ground main tanks 1 and 2 must be full if center tank contains more than 1000 Ibs LANDING GEAR Do not apply brakes until after touchdown 2012 Captain Sim www captainsim com DO NOT USE FOR FLIGHT NORMAL PROCEDURES INTRODUCTION This chapter gives e an introduction to the normal procedures philosophy and assumptions e step by step normal procedures NORMAL PROCEDURES PHILOSOPHY AND ASSUMPTIONS Normal procedures verify for each phase of flight that e the airplane condition is satisfactory e the flight deck configuration is correct Normal procedures are done on each flight Refer to the Supplementary Procedures SP chapter for procedures that are done as needed for example the adverse weather procedures Normal procedures are used by a trained flight crew and assume e all systems operate normally e the full use of all automated
35. ontal fore and aft seat lock Rudder pedalsi asana gana asa ba E naga pantaka gina aas Adjust Adjust the rudder pedals to allow full rudder pedal and brake pedal movement Seat belt and shoulder harneSS cccceseeteseeeeeees Adjust Do the PREFLIGHT checklist on the captain s command The captain normally does this procedure The first officer may do this procedure if needed LATS ga AA AE AA a KANA ANG KAN WA Aa AKP A PI A Set Flight director panel ss sasana aa Gaga baanga nnna Set Mode selector OFF ALTITUDE HOLD switch OFF PITCH COMMAND control Full clockwise A t pilot panel arar ng Kana a panan aged Set Autopilot mode selector MAN Autopilot system select switch As needed Autopilot heading switch Centered position Autopilot AILERON engage switch DISENGAGED Autopilot ELEVATOR engage switch DISENGAGED Autopilot pitch mode selector OFF OXYGEN sasinan nana et nining banene k nig bangi kah aka aga dag ag iiini Test and set STATIC SOURCE SELECTOR switch ceceseeeeteeeeeeeeeteeeees NORMAL Marker beacon NiGhts ee eseceeeeeeeeeeeeneeseeeeeeseeeeeseeeeeeneeaee Test ClOCK SANAN ANNA AN ANGEN E KN KA na A a chained EN AN TE E a Set Autopilot disengage light 0a0esenneaean enere anana n anna n anana n nee Push to test Verify that the AUTOPILOT disengage light is illuminated Flight IASEFUNMN NES adasa aaa aa anganaki ga gabag naka Naga abaan a ak AA Check Set the altimeter Ver
36. sactedseantenceastbacendiaaaseeneisenaa Check Set the altimeter www captainsim com 21 DO NOT USE FOR FLIGHT Verify that the flight instrument indications are correct Verify that only these flags are shown TCAS as installed disengage light is illuminated expected RMI flags Hydraulic system B LOW QUANTITY light eects Verify extinguished SYSTEM A HYDRAULIC QUANTITY indicator cccceceeeeeeeteeeeees Above RF GROUND PROXIMITY panel 0a0ananeneneae anana anana nana anana nen nananen Check FLAP GEAR INHIBIT switch Guard closed Verify that the INOP light is extinguished Landing gear panel sissien ariaa na anana a a Aa apapa babag ndane pan pe anana sapan ana nai Set LANDING GEAR lever DN Verify that the green landing gear indicator lights are illuminated Verify that the red landing gear indicator lights are extinguished TAKEOFF CONFIG light as installed asaaeaeenan nenen n anna anana naen en ene Verify extinguished CABIN ALTITUDE light as installed 0asaseneneneanene nana an nenen nana nn anna anen Verify extinguished ANTISKIDSWIL h Ss seisena aren sanan ng pinan i naa pakap an nadi depang Kaanan ikan ina nenika api nganan Guards closed Verify that the ANTISKID INOP lights are extinguished AUTOBRAKE s le koh yini kat sanga ran cad ea aaa a ieee OFF Verify that the AUTO BRAKE DISARM light is extinguished EPR reference selectors on PDCS equipped airp
37. sdecseeetateariaieidnqeacdvecaaeegnies Set C F O Do the SHUTDOWN checklist F O SECURE PROCEDURE EMERGENCY EXIT LIGHTS switch OFF F O WINDOW HEAT switches ccceeeee eee eee eee eee ee eee ee ee nne OFF F O Air conditioning PACK SWItCHES ccececeeeeeeeeeeeeeeeeeeenaee OFF F O Call SECURE CHECKLIST C Do the SECURE checklist F O www captainsim com 737 Captain FLIGHT MANUAL Part III Normal Procedures 40 DO NOT USE FOR FLIGHT CUSTOMER CARE You are invited to join Captain Sim community forum DAILY NEWS For Captain Sim daily news please follow us at Twitter or Facebook VIDEO CHANNEL For Captain Sim videos please watch our YouTube channel TECH SUPPORT The 737 Captain is one of the most advanced complete and accurate digital replica of the Boeing 737 aircraft ever available for any game platform Our product is not perfect unfortunately nothing is But we are working on improvements If you have some important issue to report please check in to Your Profile then click Product Name gt Customer Support gt and use the Trouble Ticket System We process all tickets and consider the most significant issues for the next service packs SPECIAL THANKS TO Mark Fletcher Dirceu Seabra Paul Sweeney Brendan Downie Marko Raicevic Peter Orosz Wilfredo Tour 2012 Captain Sim www captainsim com
Download Pdf Manuals
Related Search