Normal Procedures
Contents
1. OFF nue EA ERREUR MAE F O LEFT and RIGHT ISOLATION switches ON omm V ME F O PLIGHT DIRECTOR SWIEGDBS uuu ara e dca n au OFF C F O SUALUS MESSAGES veta textu tandi a KR ERR EAE DEA Check F O APU Selector awe vanae a d E a 8 V n Set F O If APU power is no longer required APU selector OFF Call for SHUTDOWN CHECKLIST C Accomplish SHUTDOWN checklist F O SECURE PROCEDURE IRS mode 5 6 F O EMERGENCY LIGHTS SWICK qvos F O WINDOW HEAT F O CARGO HEAT Swit MES ue mia na Rete MR eA E a E Eb b ibi DEF F O PACK CONTROL Selectors ean Wn D e e Y V Pos OFF taa aaa ww da F O Call Tor SECURE CHECKLIST T uuu uu u sasshusakapaqadaqaqaqaqusadupaqaqu C Accomplish SECURE checklist F O 2009 Captain Sim www captainsim com DO NOT USE FOR FLI GHT 767 CHECKLISTS NORMAL PROCEDURES PREFLIGHT 1 OXYGEN TESTED 100 3 FLIGHT INSTRUMENTS 4 PARKING BRAKES 5 FUEL CONTROL SWITC2. OFF Verify VALVE light extinguished Standby ard Check Standby ADI Check ILS selector OFF Verify no flags displayed Airspeed indicator Check Verify instrument indications are correct Altimeter Set Set local altimeter setting Verify instrument indications are correct Standby engine indicator selector AUTO AUTO BRAKES selector r OFF J Adjust Position seat for optimum eye reference WARNING Do not place objects between the seat and the aisle stand Injury can occur when the seat is adjusted forward BEFORE START PROCEDURE This procedure is accomplished after papers are on board and flight crew is ready for push back and or engine start Takeoff thrust reference r Set C F O Verify correct thrust reference mode displayed INITREF key Push Verify fuel quantities agree e upload fuel quantity e fuel quantity indicator e CDU Enter e Zero fuel weight e reserve fuel e cruise altitude e COSt index Check e Step size TAKEOFF line select key Push Enter e takeoff flap setting e CG e position shift value if required e wind if required e Slope if required Check e thrust line e acceleration height NNAQ fantain Ci Wana ZUUY Ca prain oim WwWW captall SIm c
3. As desired MAP light control As desired Left INSTRUMENT SOURCE SELECT panel Set FLIGHT DIRECTOR selector L NAVIGATION SOURCE selector FMC L ALTERNATE SOURCE switches Off Left flight S 1 DITE Set Note IRS alignment must be complete before AUTOLAND STATUS VSI ADI HSI and RDMI checks Airspeed indicator Correct Verify instrument indications are correct Verify no flag displayed RDMI Correct VOR ADF switches As desired Verify instrument indications are correct Verify no inappropriate flag displayed ADI Correct Flight mode annunciations Verify e autothrottle mode is blank e roll mode is TO e pitch mode is TO e AFDS status is F D Flight instrument indications are correct Verify no flags displayed HSI Correct Verify magnetic track correct Verify present heading correct Verify map mode displayed Verify no flags displayed Route Displayed correct ALTIMETER Correct Set the local altimeter setting Verify instrument indications are correct Verify no flag displayed VERTICAL SPEED INDICATOR Correct Verify instrument indications are correct Captain Sim FLIGHT MANUAL Part III Normal Procedures 17 DO NOT USE FOR FLI GHT Verify no flag displayed Clock Correct DATE switch GMT AUTOLAND STATUS annunciator enn m mnm Check Verify blank indications RESERVE BRAKES AND STEERING switch
4. CEA REN AF E VU VENUE UENUE C F O Call Tor AFTER START CHECKLIST ba rna C Accomplish AFTER START checklist F O 2009 Captain Sim www captainsim com f 767 Captain Sim FLIGHT MANUAL Part III Normal Procedures 21 DO NOT USE FOR FLI GHT BEFORE TAKEOFF PROCEDURE Obtain taxi clearance sese Hee nnn nnn F O Brier taxi ClealanCe sesir sirinin nina anin r rE AA C cin li E Release C Call for FLAPS A as required for takeoff C Position flap lever to takeoff setting F O Takeo br etig 2u u u u o aysayan kanka Accomplish C Flight attendants Notify F O Call for BEFORE TAKEOFF C Accomplish BEFORE TAKEOFF checklist F O TAKEOFF PROCEDURE Pilot Flying Pilot Not Flying Release brakes Position LEFT and RIGHT WING LANDING and WHITE ANTI COLLISION light switches ON Align airplane with runway Position transponder mode selector to TA RA Advance thrust levers to approximately 1 10 EPR Push THR switch Verify correct takeoff thrust set Monitor engine instruments throughout takeoff Adjust takeoff thrust prior to 80 knots if required N
5. if required e Set missed approach altitude e Select HDG SEL Missed approach I ntercepting landing profile Bu c e Disconnect autopilot and icc autothrottle Make climbing turn in the shortest direction toward the landing runway Execute the missed approach 33 DO NOT USE FOR FLI GHT Visual Traffic Pattern Entering downwind e Flap 5 Base O Ly il e Landing flaps T 2 engine e Landing checklist 1500 FT pr Prior to turning base P d Gear down e Flaps 20 landing flaps for 1 P d engine un c d e Arm speedbrake d e Start descent as required wee 700 500 FT SO Stabilized on profile Go around e Push GA switch Go around thrust Go around attitude Flaps 20 flap 5 for 1 engine Positive rate of climb gear up Retract flaps on schedule e After Takeoff checklist So gt 2 25 NM ku su Sa ls diag rem SO 34 CUSTOMER SUPPORT For Customer Support please visit http www captainsim com support Thank you Enjoy your flight Captain Sim Team www captainsim com 2008 Captain Sim www captainsim com
6. CLP Set Set panel As desired CARGO FIRE Dane Lu uu Ted EE IUE Set CARGO FIRE ARM switches Off Verify FWD and AFT fire warning lights extinguished CARGO FIRE BTL DISCH light Extinguished APU Te par BERTI o STU Set APU BTL DISCH light Extinguished APU fire switch In Verify APU fire warning light extinguished Right VHP communications panel Set First officer s audio control panel Set Set panel As desired 13 Verify the lock lever is in the locked forward position and the WINDOW NOT CLOSED decal is not in WINGOW 2 PIQhlu Locked view First officer s HEATERS ceeeee nmm hh nnns Set FOOT and SHOULDER switches As desired DO NOT USE FOR FLI GHT First Officer s Lighting panel Set PANEL light control As desired CHART light control As desired FLOOD light control As desired MAP light control As desired Right INSTRUMENT SOURCE SELECT panel Set FLIGHT DIRECTOR selector R NAVIGATION SOURCE selector FMC R ALTERNATE SOURCE switches Off Right flight instruments nme nnn Set Note IRS alignment must be complete before AUTOLAND STATUS VSI ADI HSI and RDMI checks ALTIMETER Correct Set the local altimeter setting Verify instru
7. GHT ELECTRICAL panel Set BUS TIE switches AUTO Verify AC BUS OFF and utility bus OFF lights extinguished APU GENERATOR switch ON GENERATOR CONTROL switches ON OFF and DRIVE lights remain illuminated until respective engine is started APU Sel 0 Puuu d Wie START then ON Position the APU selector back to the ON position Do not allow the APU selector to spring back to the ON position Lighting panel uuu Z Set GLARESHIELD panel light controls As desired AISLE STAND panel light controls As desired LIGHT OVERRIDE switch As desired RUNWAY TURNOFF light switches OFF EMERGENCY LIGHTS switch s icc rarae cec ec ARMED Verify UNARMED light extinguished PASSENGER OXYGEN ON au uuu Extinguished CAUTI ON Switch activation causes deployment of passenger oxygen masks RAM AIR TURBINE UNLKD light Extinguished WARNING Switch activation may cause deployment of the ram air turbine ENGINE CONTROL panel r Set Engine ignition selector 1 or 2 Engine start selectors AUTO FUEL JETTISON panel r nnns Set NOZZLE switches OFF Selector OFF POE Pane u ua u UU DUDEN Set CROSSFEED switches O
8. Push IDENT line select key Push IDENT page Check Verify active date current Verify Fuel Flow Factor is 1 7 or greater for PW4000 series engines 12 DO NOT USE FOR FLI GHT POS INIT line select key Push Verify time correct Inertial position Enter Enter inertial position using the most accurate latitude and longitude ROUTE line select key Push Select company route or load route manually ACTIVATE line select key Push EXEC key Push DEPARR key Push Select runway and SID ROUTE line select key Push Verify SID and route are correct EXEC key Push RONCES control quas duda eR vacuae teda Ud quaa Ra au Ed a a Set Decision height selector As desired TERRAIN switch As desired HSI RANGE selector As desired HSI TRAFFIC switch As desired HSI mode selector MAP HSI CENTER switch As desired WEATHER RADAR switch Off MAP switches As desired WEATHER RADAR Datel pO ftre dca OR NR Set Set panel As desired Left VHF communications panel Set Center VHF communications panel Set Engine Ire DanC ce che CERE EXE EX EX X Ev vd da wb Run M arr Set ENG BTL 1 DISCH and ENG BTL 2 DISCH lights Extinguished Engine fire switches In Verify LEFT and RIGHT fire warning lights extinguished ADF MEN Set Set panel As desired Trensponder pabhlel u un y REPE REX AAAA AAAA EE d AA Set
9. altitude Call for LANDING CHECKLIST Accomplish LANDING checklist Monitor approach progress Verify Autoland status at 500 feet radio altitude GO AROUND PROCEDURE Pilot Flying Pilot Not Flying Push go around switch Position flap lever to 20 Call for FLAPS 20 Verify rotation to go around attitude and thrust increase Verify thrust adequate for go around adjust if necessary After positive rate of climb established call for Verify positive rate of climb then position landing GEAR UP gear lever UP Above 400 feet radio altitude select LNAV or HDG SEL 80 At flap retraction altitude set speed to VREF 30 Push CLIMB thrust reference mode select switch Call for CLIMB THRUST Call for FLAPS according to flap retraction Position flap lever as directed schedule After flap retraction select FLCH or VNAV as required Verify missed approach route being tracked and missed approach altitude captured Call for AFTER TAKEOFF CHECKLIST Position landing gear lever OFF after GEAR and DOORS lights extinguish Accomplish AFTER TAKEOFF checklist CEREREM En re Cink a 2009 Captain Sim www captainsim com 767 Captain Sim FLIGHT MANUAL Part III Normal Procedures 24 DO NOT USE FOR FLI GHT LANDING ROLL PROCEDURE Pilot Flying Pilot Not Flying Monitor rollout progress and proper auto brakes operation Verify thrust levers closed and speedbrake lever up Verify speedbr
10. tank temperature is 3 C 5 F above the freeze point of the fuel being used The center tank may contain up to 2000 pounds of fuel with less than full main tanks provided center tank fuel weight plus actual zero fuel weight does not exceed the maximum zero fuel weight and center of gravity limits are observed REVERSE THRUST Reverse thrust is for ground use only Backing the airplane with use of reverse thrust is prohibited FLIGHT CONTROLS The maximum altitude for flap extension is 20 000 ft NAVI GATI ON Do not operate under IFR or at night into airports north of 73 North or south of 60 South latitude whose navigation aids are referenced to magnetic north 2009 Captain Sim www captainsim com DO NOT USE FOR FLI GHT NORMAL PROCEDURES INTRODUCTION GENERAL This chapter contains Normal Procedures It incorporates routine normal procedures and associated flight patterns NORMAL PROCEDURES Normal procedures are used by the trained flight crew to ensure airplane condition is acceptable and that the flight deck is correctly configured for each phase of flight These procedures assume all systems are operating normally and automated features are fully utilized Procedures are performed from recall and follow a panel flow These procedures are designed to minimize crew workload and are consistent with flight deck technology If the correct indication is not observed during accomplishment of procedures verify contro
11. this section describe each crewmember s area of responsibility for pre post flight and phase of flight Pre post flight duties are apportioned between the captain and first officer while phase of flight duties are apportioned between the pilot flying PF and pilot not flying PNF A normal panel flow is encouraged however certain items may be handled in the most logical sequence for existing conditions Actions outside the crewmember s area of responsibility are initiated at the direction of the captain General phase of flight responsibilities are as follows Pilot flying e flight path and airspeed control e airplane configuration navigation Pilot not flying e checklist reading e communications e tasks requested by PF e fuel shutoff and fire switches with PF concurrence Phase of flight duties beginning with the takeoff procedure and ending with the landing roll procedure are presented in table form in the appropriate procedures section The first officer when flying the airplane performs the duties listed under pilot flying and the captain performs those duties listed under pilot not flying Note Although the mode control panel is designated as the pilot flying s responsibility the pilot not flying should operate the controls on the mode control panel at the direction of the pilot flying when the airplane is being flown manually DO NOT USE FOR FLI GHT Autopilot Flight Director System and Flight Management System Moni
12. 10 PREFLIGHT PROCEDURE FIRST OFFICER 15 PREFLIGHT PROCEDURE CAPTAIN 17 BEFORE START PROCEDURE 20___ NORMAL PROCEDURES AMPLIFIED PROCEDURES 20 ENGINE START PROCEDURE 20 AFTER START PROCEDURE 21 BEFORE TAKEOFF PROCEDURE 21 TAKEOFF PROCEDURE 22 CLIMB PROCEDURE 22 CRUISE PROCEDURE 22 DESCENT PROCEDURE 22 APPROACH PROCEDURE 23 LANDING PROCEDURE 23 GO AROUND PROCEDURE 24 LANDING ROLL PROCEDURE 24 AFTER LANDING PROCEDURE 25 SHUTDOWN PROCEDURE 25 SECURE PROCEDURE P26 767 CHECKLISTS P l X D l l 88 26 NORMAL PROCEDURES W WI FLIGHT PATTERNS eC 28 TAKEOFF 29 ILS APPROACH 30 INSTRUMENT APPROACH USING VNAV 31 INSTRUMENT APPROACH USING V S 32 CIRCLING 33 VISUAL TRAFFIC PATTERN P34 CUSTOMER SUPPORT ee 2009 Captain Sim www captainsim com 67 Captain Sim FLIGHT MANUAL Part III Normal Procedures 4 DO NOT USE FOR FLI GHT OPERATING LIMITATIONS GENERAL This chapter contains Airplane Flight Manual AFM limitations and Boeing recommended operating limitations Limitations that are obvious shown on displays or placards or incorporated within an operating procedure are not contained in this chapter Al RPLANE GENERAL OPERATIONAL LIMITATIONS Runway slope K Maximum Operating Altitude 43 100 feet pressure altitude Maximum Takeoff and Landing Altitude 8 400 feet pressure altitude Maximum Takeoff and Landing Tailwind 10 knots Component NON AFM OPERATIONAL INFORMATION Note The following items are not AFM limitation
13. DO NOT USE FOR FLI GHT 167 Captain FLIGHT MANUAL PART III Normal Procedures DO NOT USE FOR FLI GHT ABOUT THI S MANUAL VERSION 23 JULY 2009 WARNING THIS MANUAL IS DESIGNED FOR MICROSOFT FSX USE ONLY DO NOT USE FOR FLIGHT The 767 Captain FLIGHT MANUAL is organized into five Parts Each Part is provided as a separate Acrobat PDF document Click START Programs Captain Sim 767 Captain Part User s Manual e Partll Aircraft Systems e Part III Normal Procedures this document Part IV Flight Characteristics and Performance Data e PartV Flight Management System Adobe Acrobat 9 Reader Required FOR GENERAL INFORMATION ON THE 767 CAPTAIN PRODUCT PLEASE USE WWW CAPTAINSIM COM THIS MANUAL PROVIDES ADDITIONAL INFORMATION ONLY WHICH IS NOT AVAILABLE ON THE WEB SITE 767 Captain Sim FLIGHT MANUAL Part III Normal Procedures 3 DO NOT USE FOR FLI GHT CONTENTS Page Po 4 COPERATINGLIMITATIONS aaa 4 GENERAL 4 AIRPLANE GENERAL 4 OPERATIONAL LIMITATIONS 4 NON AFM OPERATIONAL INFORMATION 4 AIRPLANE WEIGHT RESTRICTIONS 5 AUTO FLIGHT 5 ENGINE 5 ENGINE FUEL SYSTEM 5 REVERSE THRUST 5 FLIGHT CONTROLS 5 NAVIGATION WI I NORMAL PROCEDURES ee NTRODUCTION eee 6 GENERAL 6 NORMAL PROCEDURES 8 PREFLIGHT AND POSTFLIGHT AREAS OF RESPONSIBILITY AND PANEL FLOW 9 PILOT FLYING AND PILOT NOT FLYING AREAS OF RESPONSIBILITY W i i AMPLIFIED PROCEDURES sts gsgt2tb2u 10 EXTERIOR INSPECTION
14. EDURES AMPLI FI ED PROCEDURES ENGINE START PROCEDURE Announce start sequence Normal start sequence is right then left Call START ENGINE Position START selector to GROUND Observe oil pressure increase Position FUEL CONTROL switch to RUN when e at maximum motoring and a minimum of 15 N2 Observe initial EGT rise and EGT within limits Abort start if EGT fails to rise within 20 seconds of selecting RUN or if EGT rising rapidly or approaching limit Abort start if N1 fails to increase at EGT rise Abort start if N2 fails to reach stabilized idle within 120 seconds of selecting RUN Do not advance thrust beyond that required for taxi until 50 C oil temperature Repeat procedure to start remaining engine AFTER START PROCEDURE T TT T Tm OFF F O ENGINE ANTI ICE switches As required F O LEFT and RIGHT ISOLATION OET ne F O PACK CONTROL 5 UTC F O REGAL Check C F O If any message displayed refer to Minimum Equipment List and Dispatch Deviation Guide or airline equivalent to determine if dispatch relief is available AUTO BRAKES RIO C Ground EGUIPIMENE
15. FF Verify VALVE lights extinguished FUEL PUMP switches OFF Left and right pump PRESS lights are illuminated Left forward pump PRESS light is extinguished if the APU is running Both center pump PRESS lights are extinguished ANTI ICE panel seeeeeeeeenn nnnm n nnn nnns Set WING anti ice switch OFF ENGINE anti ice switches OFF WIPER selector eeeee nennen hem hh hh hh hh nnn OFF LIGNGING PANG eee Set POSITION light switch As required RED and WHITE ANTI COLLISION light switches OFF WING light switch OFF LANDING light switches OFF WINDOW HEAT switches Verify INOP lights extinguished AF a EP Set PASSENGER SIGNS parell aaa aba ra aa iil Set NO SMOKING selector AUTO or ON SEATBELTS selector AUTO or ON CABIN ALTITUDE CONTROL panel Set DO NOT USE FOR FLI GHT AUTO RATE control Index LANDING ALTITUDE selector Destination airport elevation MODE SELECTOR AUTO 1 or AUTO 2 EQUIPMENT COOLING mode selector AUTO Noii NO u CN AN Set CIRCUIT BREAKER panel light control As desired OVERHEAD PANEL light control As desired DOME LIGHT control As desired LOGO light switch As desired INDICATOR LIGHT selector As desired BLEED ALR DOS suseszu xc FERTIG dad Pda Set ENGINE bleed air switch
16. GROUND PROXIMITY GEAR OVERRIDE switch Off GROUND PROXIMITY TERRAIN OVERRIDE switch Off RONE SO L rep Adjust Position seat for optimum eye reference WARNING Do not place objects between the seat and the aisle stand Injury can occur when the seat is adjusted forward Right seat belt and shoulder harness Adjust Accomplish PREFLIGHT checklist on captain s command PREFLIGHT PROCEDURE CAPTAIN Normally this procedure is accomplished by the captain However it does not preclude the first officer from completing the procedure if time and conditions dictate Left VOR DME SWIiL Ch uuu nua y ERTARAEREREDARERKRRRERERMEKESRERARE TERN MEE AUTO Mode contFol Dallelisseseses sooo sacs me Qu a UR MERE unt Ud nC m nA CRAS GA Und CE dE Set Left FLIGHT DIRECTOR switch ON AUTOTHROTTLE ARM switch ARM BANK LIMIT selector As desired Autopilot DISENGAGE bar UP Esa bCM o Set If MENU page displayed FMC line select key Push If IDENT page not displayed INITREF key Push INDEX line select key Push IDENT line select key Push IDENT page Check Verify active date current Verify Fuel Flow Factor is 1 7 or greater for PW4000 series engines POS INIT line select key Push Verify present position and time correct ROUTE line select key Push Verify e flight number correct e route correct Left EFIS con
17. HES BEFORE START 1 2 3 4 5 6 7 8 9 FLIGHT DECK DOOR PASSENGER SIGNS WINDOWS MCP TAKEOFF SPEEDS CDU PREFLIGHT TRIM TAXI AND TAKEOFF BRIEFING RED ANTI COLLISION LIGHT SET HEADING ALTIMETER CUTOFF CLOSED AND LOCKED LOCKED V2 HDG ALT Vi VR V2 COMPLETED UNITS ZERO ZERO COMPLETED ON BEFORE TAXI ANTI ICE L and R ISOLATION SWITCHES 1 2 3 RECALL 4 OFF CHECKED AUTOBRAKE RTO 5 GROUND EQUIPMENT CLEAR BEFORE TAKEOFF 1 FLAPS AFTER TAKEOFF 1 LANDING GEAR FLAPS DECSENT PRESSURIZATION RECALL LANDING DATA 1 2 3 AUTOBRAKE 4 5 APPROACH BRIEFING APPROACH 1 ALTIMETERS LANDI NG 1 SPEEDBRAKE 2 LANDING GEAR FLAPS UP and OFF UP LDG ALT CHECKED VREF MINIMUMS COMPLETED 27 DO NOT USE FOR FLI GHT SHUTDOWN HYDRAULIC PANEL FUEL PUMPS FLAPS PARKING BRAKE FUEL CONTROL SWITCHES WEATHER RADAR SECURE 1 IRSs 2 EMERGENCY LIGHTS SWITCH 3 WINDOW HEAT 4 PACK SWITCHES FLIGHT PATTERNS Takeoff Flap Retraction Schedule Select next flap position when within 20 knots of the Maneuvering speed for that Position and accelerating Monitor airspeed Thrust set Manually advance thrust to stabilize Engage autothrottle VR Verify takeoff thrust set by 80 knots Rotate i 28 DO NOT USE FOR FLI GHT 3000 feet AGL One or 2 engine climb speed V2 15 to V2 25 knots Or V2 to V2 15 kn
18. III Normal Procedures 25 DO NOT USE FOR FLI GHT SHUTDOWN PROCEDURE Parking brake ssssssseeeee e enhn nnnm nena nnn Set C Verify PARK BRAKE light illuminated Electrical Establish F O If APU power is required Check APU RUN light is illuminated If external power is desired EXTERNAL POWER AVAIL light Illuminated EXTERNAL POWER switch Push ENGINE ANTISICE SWITCHES ERVERYFERIEMRS EON REA D e jr F O FUEL CONTROL switches CUT OFF C Verify ENG VALVE and SPAR VALVE lights extinguished Peng Release C When wheel chocks in place release the parking brake SEATBELIS selector ceni caido OPE u u oaa F O PANG SURE EEERE UMEN c PR RR F O Note Depressurize right system last to prevent fluid transfer between systems Left ELECTRIC DEMAND pump selector OFF C1 and C2 ELECTRIC PRIMARY pump switches OFF Center AIR DEMAND pump selector OFF Right ELECTRIC DEMAND pump selector OFF FUEL PUMP sssaauanaqa F O RED ANTI COLLISION light switch
19. NTER FUEL PUMP switches ON Note Both PRESS lights will not be extinguished due to load shedding Indications will be normal after engine start RED ANTI COLLISION light SWILCH oes i C a nu ON F O PACK CONTROL 5 OFF F O T eee 9 Q X Units zero zero C F O Stabilizer trim UNITS Set for takeoff Check in greenband Aileron trim ZERO Rudder trim ZERO alelgiueieip dao qute Check C Displace control wheel and control column to full travel in both directions and verify e freedom of movement e controls return to center e proper flight control movement on EICAS status display Hold the nose wheel steering tiller during rudder check to prevent undesired nose wheel movement Displace rudder pedals to full travel in both directions and verify e freedom of movement 19 DO NOT USE FOR FLI GHT e rudder pedals return to center e proper flight control movement on EICAS status display Secondary ENGINE DISPLAY switch PUSH as F O Call for BEFORE START CHECKLIST ced C Accomplish BEFORE START checklist F O 767 Captain Sim FLIGHT MANUAL Part III Normal Procedures 20 DO NOT USE FOR FLI GHT NORMAL PROC
20. OT USE FOR FLI GHT Instrument Approach Using V S On Approaching intercept heading n e Appropriate pitch mode Flaps 5 at LZ cw n k Enroute to fix O S e LNAV or appropriate 4 nZ roll mode e Flaps 1 i N e VNAV or appropriate 4 es pitch mode Se Flaps 5 O BN O Missed approach Q e Push GA switch e Flap 20 flap 5 for 1 engine I ntercept Heading e Go around attitude e Arm LNAV or appropriate Descend to MDA H Go around thrust roll mode Set V S e Positive rate of climb gear up Q e Above 400 feet select roll mode e At flap retraction altitude set Approaching MDA H speed for desired flap setting Set missed approach e Select CLB thrust 2 engine altitude in MCP e Retract flaps on schedule wa Jl e After flap retraction select u eM FLCH or VNAV as required k eS e Select CON thrust 1 engine kis c e Verify tracking route and Ec altitude capture I nbound 2NM kau e After Takeoff checklist Gear down B c Flap 20 landing flaps for 1 ie oe O engine Bic Arm speedbrake i Set MDA H e Intercept landing profile and disengage autopilot and disconnect autothrottle Landing flaps 2 engine DO NOT USE FOR FLI GHT Circling Configuration at MDA H e Gear down e Flaps 20 landing flaps for 1 engine e Arm speedbrake Turning base e Landing flaps if not previously selected e Landina checklist 32 Minimum Descent Altitude e Select ALT HLD
21. ake lever UP and call SPEEDBRAKES UP If speedbrake lever not UP Without delay raise reverse thrust levers to the call SPEEDBRAKES NOT UP interlocks hold light pressure until release and then apply reverse thrust as required By 60 knots initiate movement of reverse thrust Call 60 KNOTS levers to reach reverse idle detent prior to taxi speed Position levers full down forward thrust when engines have decelerated to reverse idle Prior to taxi speed disarm the auto brakes and continue manual braking as required WARNING After reverse thrust is initiated a full stop landing must be made AFTER LANDI NG PROCEDURE Accomplished when clear of the active runway AP O REESE ER START then ON F O Position the APU selector back to the ON position Do not allow the APU selector to spring back to the ON position ExLGrior MONTS u uu lu Position WHITE ANTI COLLISION light switch OFF and LANDING TAXI light switches as required Speedbrake lever enean nnne nn DOWN C Weather radar ccccccccccccccceeecueeeeeeeeeeeeeeaeeeeeaeeeneueeennuueenanenens OM kausai C F O AUTO BRAKES selector eeesssseeen nne iz yuyu E F O ce T ns F O Tane PONIO D F O 2009 Captain Sim www captainsim com 767 Captain Sim FLIGHT MANUAL Part
22. efines Captain s area of responsibility Unshaded area is First Officer s responsibility 2009 Captain Sim www captainsim com 767 Captain Sim FLIGHT MANUAL Part III Normal Procedures DO NOT USE FOR FLI GHT FLYING AND NOT FLYING AREAS OF RESPONSIBILITY Weather Radar WX Audio Control Panel ACP and trim location may vary EX area of Responsibility PNF area of Responsibility __ Unshaded areas are the responsibility of the pilot seated on the respective side 2009 Captain Sim www captainsim com 767 Captain Sim FLIGHT MANUAL Part III Normal Procedures 10 DO NOT USE FOR FLI GHT AMPLIFIED PROCEDURES EXTERI OR I NSPECTI ON Prior to each flight a flight crewmember or the maintenance crew must verify the airplane is acceptable for flight Check Flight control surfaces unobstructed and all surfaces clear of ice snow or frost Door and access panels not in use properly secured Ports and vents unobstructed Airplane free of damage and fluid leakage Wheel chocks in place ground locking pins removed and nose gear steering lever in normal position Tire condition Gear struts not fully compressed PREFLIGHT PROCEDURE FIRST OFFICER This procedure assumes the supplementary power up procedure has been accomplished and electrical power is established The following procedures are accomplished in their entirety on each originating trip or crew change or following ma
23. es ON Verify OFF lights illuminated APU bleed air switch ON Verify VALVE light extinguished LEFT CENTER and RIGHT ISOLATION switches ON Verify VALVE lights extinguished Air conditioning Ban l u uuu u kt rh rea eese sid i die Set PACK CONTROL selectors AUTO Verify PACK OFF lights extinguished FLIGHT DECK temperature control AUTO Set as desired Verify INOP lights extinguished TRIM AIR switch ON RECIRCULATION FAN switches ON Verify INOP lights extinguished CABIN temperature controls AUTO Set as desired Verify INOP lights extinguished CARGO HEAT switches eese nennen nnne nnn nnn ON Right VOR DME SWiIlchu vs vins visa pria dcin AUTO Right FLIGHT DIRECTOR switch EICAS y iu Check Secondary ENGINE DISPLAY switch Push Indications Normal Verify e primary and secondary engine indications display existing conditions e noexceedance values are displayed e quantity adequate for flight STATUS DISPLAY switch Push STATUS display Verify e hydraulic quantities do not display RF If any status message is displayed refer to the Minimum Equipment List and Dispatch Deviation Guide to determine if dispatch relief is available COMPUTER selector AUTO Set If MENU page displayed FMC line select key Push If IDENT page not displayed INITREF key Push INDEX line select key
24. for arrival and approach Verify pressurization set to landing altitude Set DH as required for approach Set DH ADF and ILS as required for approach Review all alert messages Recall and review all alert messages Set airspeed reference bugs to VREF 30 VREF 30 Set airspeed reference bugs to VREF 30 VREF 30 40 and VREF 30 80 40 and VREF 30 80 Set AUTO BRAKES selector to desired brake setting When cleared to descend set clearance limit altitude on MOP APPROACH PROCEDURE Pilot Flying Pilot Not Flying At transition level set altimeters Verify correct arrival and approach procedures selected At 10 000 feet position LEFT and RIGHT WING LANDING light switches ON Call for APPROACH CHECKLIST Accomplish APPROACH checklist 2009 Captain Sim www captainsim com 4772 767 Captain Sim FLIGHT MANUAL Part III Normal Procedures 23 DO NOT USE FOR FLI GHT LANDING PROCEDURE Pilot Flying Pilot Not Flying Call for FLAPS _ according to flap extension Position flap lever as directed schedule When on localizer intercept heading verify ILS tuned and identified and localizer and glideslope pointers displayed arm APP mode At glideslope alive call for Position landing gear lever DN GEAR DOWN Position flap lever to 20 FLAPS 20 At glideslope capture call for Position flap lever as commanded FLAPS as required for landing At final approach fix OM verify crossing
25. intenance action Normally this procedure is accomplished by the First Officer However it does not preclude the captain from completing the procedure if time and conditions dictate Maintenance documents cexeeswxrkaacakuakadazadasudeizdazudadadududude bees Check FLIGHT DECK ACCESS SYSTEM switch NORM RESERVE BRAKES amp STRG RESET DISABLE guard Closed Verify ISLN light extinguished Circuit 5 cosas Check Emergency equipment ar nnn Check TRS mode SSlBCEOES uu QU DEVE TREND DEED DERE EHP IE BE OFF then NAV Verify ALIGN lights illuminated For all flights a full alignment is recommended YAW DAMPER CREATES UA ON INOP lights remain illuminated until IRS alignment is complete EEC du RA REA QUK dead M NORM HYDRAULIC DaFigl 22222 y dbi Set LEFT and RIGHT ENGINE PRIMARY pump switches ON Left and right engine pump PRESS lights remain illuminated until the respective engine is started ELECTRIC PRIMARY pump switches OFF DEMAND pump selectors OFF HF Pai NR Set BATTERY STANDBY CONTROL panel Set BATTERY switch ON Verify DISCH light extinguished STANDBY POWER selector AUTO Verify standby power bus OFF light extinguished 2009 Captain Sim www captainsim com 11 DO NOT USE FOR FLI
26. ls are positioned correctly If necessary check the appropriate circuit breaker s and test the related system light s Before engine start lights or indications verify the systems condition or configuration Review the EICAS status display before engine start to determine if messages are displayed which may affect dispatch and require maintenance action or compliance with the Minimum Equipment List MEL After engine start it is not necessary to check status messages as any message having an adverse effect on safe continuation of the flight and requiring crew attention will appear as an EICAS alert message warning caution or advisory EICAS alert messages are the primary means of alerting the flight crew to non normal conditions or improper configuration During engine start and prior to takeoff any alert message requires accomplishment of the appropriate non normal procedure Upon completion of the procedure and prior to takeoff the Dispatch Deviations Guide DDG should be consulted to determine if MEL relief is available Exterior lighting flight deck lighting and personal comfort items such as shoulder heaters are systems assumed to have obvious procedural requirements and are not addressed in this section Flight crew duties are organized in accordance with an area of responsibility concept Each crewmember is assigned a flight deck area where the crewmember initiates actions for required procedures The panel illustrations in
27. ment indications are correct Verify no flag displayed VERTICAL SPEED INDICATOR Correct Verify instrument indications are correct Verify no flag displayed Clock Correct DATE switch GMT ADI Correct Flight mode annunciations Verify e autothrottle mode is blank e roll mode is TO e pitch mode is TO e AFDS status is F D Flight instrument indications are correct Verify no flags displayed HSI Correct Verify magnetic track correct Verify present heading correct Verify map mode displayed Verify no flags displayed Route Displayed correct Airspeed indicator Correct Verify instrument indications are correct Verify no flag displayed RDMI Correct VOR ADF switches As desired Verify instrument indications are correct Verify no inappropriate flag displayed AUTOLAND STATUS annurclatOFxssiiezetexsbensiadadade eeiam Rara auae Check Verify blank indications HEADING REFERENCE switch rrr rr NORM or TRUE FLAP position indication and FLAP lever Agree ALTERNATE FLAPS vidc Set ALTERNATE FLAPS selector NORM ALTERNATE FLAPS switches OFF Landing gear Panel uu odd ga ERRISPAREREDERRIXERGN ERR Ra rXPGga Pd cuin Set Landing gear lever DN ALTERNATE GEAR EXTEND switch OFF guarded position 14 art J rme cedures 15 DO NOT USE FOR FLI GHT GROUND PROXIMITY FLAP OVERRIDE switch Off
28. om 18 DO NOT USE FOR FLI GHT Verify PRE FLT COMPLETE displayed CDU display Set Usually one pilot on LEGS page and the other on CLB page Note If required for noise abatement reasons enter a speed restriction on the CLIMB page of VREF 30 80 to 3 000 feet above field elevation IAS MACH selector Rotate Set V2 speed in the IAS MACH window Initial heading Set Initial altitude Set Airspeed bugs sssssssseeeeeennn nnne nennen aaa ena ann nnn nnn Set C F O Set bugs at VI VR VREF 30 40 and VREF 30 80 r CE iid Obtain C F O Obtain clearance to pressurize hydraulic systems and start engines HYDRAULIC panal u dena dena dena deca F O Note Pressurize right system first to prevent fluid transfer between systems Right ELECTRIC DEMAND pump selector AUTO Verify PRESS lights extinguished C1 and C2 ELECTRIC PRIMARY pump switches ON Verify C1 PRESS light extinguished Center AIR DEMAND pump selector AUTO Verify PRESS lights extinguished Left ELECTRIC DEMAND pump selector AUTO Verify PRESS lights extinguished Note C2 PRESS light will not be extinguished due to load shedding Indication will be normal after engine start PUL E Cu n 9 I Aaa F O LEFT and RIGHT FUEL PUMP switches ON Verify PRESS lights extinguished If center tank contains fuel CE
29. ote After takeoff thrust is set the captain s hand must be on the thrust levers until VI Monitor airspeed Monitor airspeed indications and call out any abnormalities Verify 80 knots Call 80 KNOTS Verify V1 speed Call V1 Rotate at VR At VR call ROTATE Establish a positive rate of climb Monitor airspeed and vertical speed Call for GEAR UP when positive rate of climb Verify positive rate of climb then position landing established gear lever UP Call for LNAV when climb stabilized Push L NAV switch Call for VNAV at flap retraction altitude Push VNAV switch Push A P ENGAGE COMMAND switch Call for FLAPS according to flap retraction Position flap lever as directed schedule Verify climb thrust set Call for AFTER TAKEOFF CHECKLIST Position landing gear lever OFF after GEAR and DOORS lights extinguish Accomplish AFTER TAKEOFF checklist 2009 Captain Sim www captainsim com 767 Captain Sim FLIGHT MANUAL Part III Normal Procedures 22 DO NOT USE FOR FLI GHT CLI MB PROCEDURE Pilot Flying Pilot Not Flying 10 000 feet position LANDING light switches OFF At transition altitude set altimeters to 29 92 in Hg 1013 mb CRUISE PROCEDURE Pilot Flying Pilot Not Flying When CTR L and CTR R FUEL PUMP messages are displayed push CENTER FUEL PUMP switches OFF DESCENT PROCEDURE Pilot Flying Pilot Not Flying Prior to top of descent modify active route as required
30. ots 1 engine Accelerate and climb at VREF 30 80 knots Flap up Continuous thrust 1 engine After Takeoff checklist Acceleration height Flap retraction altitude normally 1000 feet Select pitch mode 2 engines Select V S 0 to 200 fpm 1 engine Select verify climb thrust Engage autopilot Retract flaps on schedule Climb stabilized Select roll mode Positive rate of climb Gear up DO NOT USE FOR FLI GHT ILS Approach 29 On RADAR vectors e HDG SEL AFDS Approaching intercept heading Appropriate pitch mode AFDS n 2 e Flaps 5 dit SU Nu D o l X OS I Tz ze Flaps 1 ot L I E Missed approach 9 Flaps 5 O gt e Push GA switch AFDS e Flap 20 flap 5 for 1 eng O e LNAV or appropriate e Go around attitude roll mode AFDS e Go around thrust e VNAV or appropriate e Positive rate of climb pitch mode AFDS gear up e Above 400 feet select roll mode AFDS O e Atflap retraction altitude set Glideslope intercept A e Landing flaps 2 engine e Set missed approach altitude e Landing checklist Localizer capture e Final Approach Course heading LOM MKR DME Verify crossing altitude B Intercept Heading I B c e ILS tuned and identified Glideslope alive ku e LOC and GVS pointers Gear down e Flap 20 landing flaps for 1 engine e Arm speedbrake displayed e Arm APP mode speed for desired flap setting e Select climb
31. s but are provided for flight crew information Turbulent air penetration speed is 290 KIAS 78 Mach The navigation and display system does not support operations at latitudes greater than 87 North or South AIRPLANE WEIGHT RESTRICTIONS MAXIMUM WEIGHT LIMITATIONS Weights Pounds Maximum Taxi Weight MTW 413 000 Maximum Take Off Weight MTOW 412 000 Maximum Landing Weight MLW 320 000 Maximum Zero Fuel Weight MZFW 295 000 OTHER WEI GHT RESTRI CTI ONS Note These weights may be further restricted by field length limits climb limits tire speed limits brake energy limits obstacle clearance or enroute and landing requirements CEREREM En re Cink AnA Pu rAr 2009 Captain Sim www captainsim com 767 Captain Sim FLIGHT MANUAL Part III Normal Procedures 5 DO NOT USE FOR FLI GHT AUTO FLIGHT After takeoff the autopilot must not be engaged below 200 feet AGL Use of aileron trim with the autopilot engaged is prohibited Maximum allowable wind speeds when landing weather minima are predicated on autoland operations Continuous ignition must be on engine start selector in the CONT position while operating in severe turbulence Note Continuous ignition is automatically provided in icing conditions when engine anti ice is on Flight crew shall not blank engine vibration display during takeoff ENGINE FUEL SYSTEM The maximum fuel temperature is 49 C 120 F The minimum inflight fuel
32. thrust 2 engine e Retract flaps on schedule e After flap retraction select FLCH or VNAV as required e Select continuous thrust 1 engine e Verify tracking route and altitude capture e After Takeoff DO NOT USE FOR FLI GHT I nstrument Approach Using VNAV Approaching intercept heading f i P f e Flaps 5 aie E a O De gt b Flaps 5 O O Intercept Heading Arm NAV or appropriate Descend to DA H or MDA H e Monitor VNAV path e Landing checklist O Y E i Inbound 2NM n c Gear down B c e Flap 20 landing flaps for 1 O engine EMEND Arm speedbrake At DA H or MDA H Lu Set DA H or MDA H Select VNAV Speed intervention Landing flaps 2 engine e Intercept landing profile and disengage autopilot and disconnect autothrottle 30 On RADAR vectors e HDG SEL e Appropriate pitch mode Enroute to fix n e LNAV or appropriate j n roll mode VNAV or appropriate Ae pitch mode Missed approach e Push GA switch Flap 20 flap 5 for 1 eng Go around attitude Go around thrust Positive rate of climb gear up e Above 400 feet select roll mode e At flap retraction altitude set speed for desired flap setting e Select CLB thrust 2 engine e Retract flaps on schedule e After flap retraction select FLCH or VNAV as required e Select CON thrust 1 engine e Verify tracking route and altitude capture 31 DO N
33. toring When the autopilot flight director or autothrottle is in use and a mode change is selected or is scheduled to occur the annunciation must be verified on the flight mode annunciation display Airplane course vertical path and speed must always be monitored Similarly when a thrust reference mode change is selected or is scheduled to occur the annunciation must be verified on the EICAS display In LNAV and VNAV all airplane course vertical path thrust and speed changes must be verified CDU Operation On the ground the control display unit CDU manipulations are normally performed by the first officer and verified by the captain In flight CDU entries are accomplished by the pilot not flying and verified by the pilot flying prior to execution CDU manipulations should be accomplished prior to high workload periods such as departure arrival or holding During high workload periods using autopilot modes such as heading select flight level change and the altitude and speed intervention features along with the map switches may be more efficient than entering complex route modifications into the CDU 767 Captain Sim FLIGHT MANUAL Part III Normal Procedures DO NOT USE FOR FLI GHT PREFLIGHT AND POSTFLIGHT AREAS RESPONSIBILITY AND PANEL FLOW mir ELIT jem IOS ei ens Audio Control Panel ACP and trim location may vary s Captain First Officer LEGEND Shaded area d
34. trol panel rr nn nn Set Decision height selector As desired TERRAIN switch As desired HSI RANGE selector As desired HSI TRAFFIC switch As desired HSI mode selector MAP HSI CENTER switch As desired WEATHER RADAR switch Off MAP switches As desired SPEEDBRAKE EVE ccm DOWN ALTERNATE STABILIZER TRIM switches Neutral Reverse thrust levers 16 DO NOT USE FOR FLI GHT WARNI NG Movement of the reverse thrust lever could result in operation of the engine thrust reverser TOUSE IOVIS ue m m IT Closed ii wc Set Position lever to agree with flap position Parking Set Verify PARK BRAKE light illuminated STABILIZER TRIM Cutout switches NORM guarded position FUEL CONTROL 5 CUT OFF Captains audio control DaFrielsweeeeneweweaateu sr hw y bata v Set Set panel As desired Window Ne T Locked Verify the lock lever is in the locked forward position and the WINDOW NOT CLOSED decal is not in view Captain S HEATERS uuu Set FOOT and SHOULDER switches As desired Captain s aut Tu dd qd Set PANEL light control As desired CHART light control As desired FLOOD light control
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