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1. Airport B Displayed if the EFIS control panel ARPT map switch is selected on Origin and destination airports are always displayed regardless of map switch selection Airport and runway Displayed when selected as W the origin or destination and ND range is 10 20 or 40 NM Dashed runway centerlines extend 14 2 NM STA WPT Selected map MAP MAP CTR Displays EFIS control panel ARPT options B selected map options CDUL C R Map source MAP MAP CTR Displays ND source if CDU annunciation G is selected on respective navigation source select switch Both FMCs fail or A manually selected FMC fails North up arrow G Indicates map background is oriented and referenced to true north Weather radar MAP MAP CTR Weather radar returns show returns VOR APP when the WXR switch R A G M of the EFIS control panel is on Intense WXR returns show in red r Medium intensity show in amber a Low intensity show in green 9 5 Turbulence shows in magenta TCAS resolution RA pitch commands show on advisory RA or the PFD See note below relative altitude R MAP MAP CTR TCAS traffic APP VOR See note below advisory or TA A relative altitude www captainsim com 70 DO NOT USE FOR FLIGHT TCAS proximate See note below traffic W relative altitude TCAS other traffic See note below W relative altitude TCAS TA absolute See note below altitude The TCAS symbols above the arrow s
2. All items should work as described in this manual If something is not described as functional therefore it does not work or does not exist in the model it is not a system bug but a reasonable simplification www captainsim com DO NOT USE FOR FLIGHT AIRCRAFT GENERAL PRINCIPAL DIMENSIONS 199 feet 11 inches 60 9 meters 70 feet O 21 3 meters 4 L 84 feet 11 inches n 25 9 meters G eet S inches 18 4 meters x 209 feat 1 inch 63 7 meters r p www captainsim com DO NOT USE FOR FLIGHT CARGO COMPARTMENTS BULK CARGO COMPARTMENT FORWARD CARGO COMPARTMENT AFT CARGO COMPARTMENT BIN 4 BIN 3 The B777 has three cargo compartments forward aft and bulk Each compartment is accessed through its respective door The aft and bulk cargo compartments are separated only by a curtain The cargo compartments are administratively subdivided into five bins The forward and aft sections of the forward cargo compartment are bin 1 and bin 2 respectively Bin 3 and bin 4 are the forward and aft sections of the aft cargo compartment and the bulk compartment is bin 5 www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 9 DO NOT USE FOR FLIGHT INSTRUMENT PANELS FLIGHT DECK PANELS Maintenance Circuit Breaker Overhead Overhead Overhead Center Forward Left Forward Glareshield Va Right Forward Electroni
3. Flight Path Vector FPV Switch Meters MTRS Switch Barometric Standard BARO STD Switch inner Barometric BARO Selector middle Barometric BARO Reference Selector outer N 1 Minimums MINS Reference Selector outer RADIO Selects radio altitude as the PFD minimums reference BARO Selects barometric altitude as the PFD minimums reference 2 Minimums MINS Selector middle Rotate slew Adjusts the PFD radio or baro minimums altitude 3 Minimums Reset MINS RST Switch inner Push Resets the PFD minimums alert display e Blanks the minimums display when green 4 Flight Path Vector FPV Switch Push Displays the PFD flight path vector 5 Meters MTRS Switch Push Displays PFD altitude meters indications 6 Barometric Standard BARO STD Switch inner Push e Selects the standard barometric setting 29 92 inches Hg 1013 HPA for the PFD barometric reference e If STD is displayed selects the preselected barometric setting If no preselected barometric setting is displayed displays the last value before STD was selected 7 Barometric BARO Selector middle Rotate slew Adjusts the PFD barometric reference 8 Barometric BARO Reference Selector outer IN selects inches of mercury as the PFD barometric reference HPA selects Hectopascals as the PFD barometric reference 2014 Captain Sim www captainsim com 90 DO NOT USE FOR FLIGHT E
4. e The electric motor driven hydraulic pump operates e Pressurizes the center hydraulic system Off ON not visible The electric motor driven hydraulic pump off is turned off 6 9 Demand Pump Selectors ON the pump runs continuously AUTO the pump operates when system and or primary pump s pressure is low or when control logic anticipates a large system demand OFF the pump is off Note If both air driven pumps are selected to ON only air driven pump C1 operates the two air driven pumps cannot operate simultaneously when both are selected ON 10 13 Demand Pump Fault Lights Illuminated amber e Low demand pump output pressure Excessive demand pump fluid temperature or Demand pump is selected OFF www captainsim com FLIGHT MANUAL Part II Aircraft and Systems 112 DO NOT USE FOR FLIGHT MISCELLANEOUS HYDRAULIC SYSTEM CONTROLS P24 ENGINE FIRE PANEL 1 Engine Fire Switches Pull e Closes the engine driven pump hydraulic supply shutoff valve e Depressurizes the engine driven pump M02 FLIGHT CONTROL HYDRAULIC POWER SWITCHES Note No flight crew normal or non normal procedures require operation of the flight control shutoff switches These switches are for ground maintenance use only FLT su HYD POWER 1 Flight Control Hydraulic Power Shutoff TAL Switches NORM NORM NORM Hydraulic system power is available to the flight control actuators 1 SH 3H T EF zi SHUT OFF Hydrauli
5. LOCK OVRD Switch Push releases the landing gear lever lock www captainsim com 114 DO NOT USE FOR FLIGHT NOSE WHEEL STEERING TILLER 1 Nose Wheel Steering Tiller 2 Tiller Position Indicator 1 Nose Wheel Steering Tiller Rotate e Turns the nose wheels up to 70 degrees in either direction 2 Tiller Position Indicator Shows tiller displacement from the straight ahead neutral position BRAKE SYSTEM 1 Rudder Pedal Adjust Crank Adjusts the rudder pedals forward or aft 2 Rudder Brake Pedals Pushing the full pedal e Turns the nose wheel up to 7 degrees in either direction Does not activate main gear steering e Push the top of the pedals actuates the wheel brakes P12 PARKING BRAKE LEVER Pull Sets the parking brake when both brake pedals simultaneously depressed FULL Release Simultaneously depress both brake pedals www captainsim com 115 DO NOT USE FOR FLIGHT 04 BRAKE ACCUMULATOR PRESSURE INDICATOR 1 Brake Source Light Illuminated amber Both active brake hydraulic SOURCE sources right and center reserve hydraulic systems have low pressure 2 BRAKE ACCUMULATOR PRESSURE Indicator Indicates brake accumulator pressure www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 116 DO NOT USE FOR FLIGHT WARNING SYSTEMS SYSTEM WARNINGS MASTER WARNING CAUTION RESET SWITCHES AND LIGHTS mm
6. Other checklist steps are automatically checked off from sensed flight deck control positions aircraft system status or EICAS messages The CHECKLIST COMPLETE indicator is displayed at the bottom of all pages of the checklist when all of the line items are either complete inactive or overridden and every page has been displayed If the flight crew chooses not to perform a particular line item the line item can be overridden by selecting the ITEM OVRD key at the bottom of the page When a line item is overridden the text changes color from white to cyan and the current line item box moves down to the next incomplete line item If the flight crew chooses to not perform an entire checklist the checklist can be overridden by selecting the CHKL OVRD key at the bottom of the page When a checklist is overridden the text of the entire checklist changes color from white to cyan and the CHECKLIST OVERRIDDEN indicator is displayed at the bottom of all pages CHECKLIST STEPS Each step in a checklist is referred to as a line item After selecting a checklist a current line item box automatically encloses the text of the first incomplete line item When the cursor is on a line item a cursor selection box encloses the current line item box and the open loop indicator When line items are complete the cursor cursor selection box and current line item box move to the next incomplete line item Incomplete checklist line items appear as white text Com
7. PO1 P25 CDU PANEL P02 LOWER CENTER DISPLAY P04 CENTER PANEL BRIGHTNESS CONTROLS 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 17 DO NOT USE FOR FLIGHT INSTRUMENT PANELS AFT AND SIDE CONTROL STAND FLA l P08 P09 ENGINE CONTROLS P10 P15 FLAPS CONTROLS P12 ELEVATOR TRIM INDICATOR AND PARKING BRAKE LEVER P14 FUEL CONTROL SWITCHES 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 18 DO NOT USE FOR FLIGHT AFT AISLE STAND z 9 xz ust Ac mue mb sees n JP 53 Ed O HE Bis OOOO eee e ADA s 8 7 83 83 E 3 E E E EE 7 83 EAGER iile af P18 P21 P28 RADIO TUNING PANEL P19 P22 P29 501 AUDIO CONTROL PANEL P20 WEATHER RADAR PANEL P24 ENGINE AND APU FIRE PANEL P26 AILERON AND RUDDER TRIM CONTROLS P30 TRANSPONDER PANEL P32 LIGHTING CONTROLS 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems DO NOT USE FOR FLIGHT LEFT AND RIGHT SIDEWALL PANELS VO1 SHOULDER AND FOOT HEATERS V02 FORWARD PANEL BRIGHTNESS CONTROLS 2014 Captain Sim www captainsim com 19 777 Captain FLIGHT MANUAL Part II Aircraf
8. 3 FORWARD PANEL FLOOD Light Control Rotate map light ON OFF Independent controls for Captain s and F O lights 1 Outboard Display Light Control 2 Inboard Displays Lights Control 3 Forward Panel Flood Light Control The captain s and first officer s forward panel brightness controls have controls for their outboard and inboard display units These controls are on the sidewall panels There is a single control for the outboard display units There is a dual control knob for the inboard display units The outer knob controls display brightness and the inner knob controls WXR brightness DISPLAYS CONTROL VIA 2D POP UPS 2014 Captain Sim www captainsim com All 2D pop up displays have the following 3 control areas 1 Close 2D display left mouse click 2 Brightness adjustment Mouse wheel DOWN towards reduce brightness or mouse wheel UP outwards increase brightness 3 2D display drag area 777 Captain FLIGHT MANUAL Part II Aircraft and Systems DO NOT USE FOR FLIGHT O05 PASSENGER OXYGEN SWITCH PASS 1 Passenger Oxygen Switch OXYGEN 2 Passenger Oxygen ON Light 2 Passenger Oxygen ON Light Illuminated amber The passenger oxygen system is operating and the masks have dropped 2014 Captain Sim www captainsim com 23 24 DO NOT USE FOR FLIGHT ANTI ICE SYSTEM O13 PANEL 1 Wing Anti Ice Selector 2 Engine Anti Ice Selectors 1 WI
9. A P Engage Switches Autopilot master on off default key Z Push either switch can engage the autopilot If either flight director switch is ON the autopilot engages in the selected flight director mode s If both flight director switches are OFF the autopilot engages in default modes Vertical speed V S or flight path angle FPA as the pitch mode Attitude hold ATT heading or track hold HDG HLD TRK HLD as the roll mode WWW captainsim com 26 DO NOT USE FOR FLIGHT 2 3 Autothrottle A T ARM Switches The left autothrottle arm switch controls the left engine autothrottle The right autothrottle arm switch controls the right engine autothrottle L and or R Arms the selected autothrottle for mode engagement The selected autothrottle engages automatically when an AFDS mode VNAV or is selected OFF e Disconnects the selected autothrottle and e Prevents selected autothrottle engagement 4 IAS MACH Window Displays the speed selected by the IAS MACH selector Blank when the FMC controls the speed When changing from TO GA to V S FPA or ALT the window automatically displays e 250 knots flaps up or A speed value entered in the IAS MACH window The display range is e 100 399 KIAS e 0 40 0 95 MACH The selected speed is displayed as the PFD selected speed Displays 200 knots when power is first applied During climb automatically changes from IAS to MACH at 0 84 MACH Dur
10. AER 2 outer 1 Upper Display UPR DSPL Brightness Control Rotate Adjusts the brightness of the upper center display unit 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 92 DO NOT USE FOR FLIGHT 2 Lower Display LWR DSPL Brightness Control outer Rotate Adjusts the brightness of the lower center display unit PRIMARY FLIGHT DISPLAY PFD PFD INDICATIONS Flight Mode Annunciations Airspeed Mach Indications Attitude Steering and Miscellaneous Indications Autopilot Flight Director System Status Altitude Indications Vertical Speed Indication Heading and Track Indications e Q N Flight Mode Annunciations 2 Airspeed Mach Indications Displays Air Data Inertial Reference System ADIRS airspeed information and other airspeed related information 3 Attitude Steering and Miscellaneous Indications Displays ADIRS attitude information 4 Autopilot Flight Director System Status Refer to Automatic Flight 5 Altitude Indications Displays ADIRS altitude and other altitude related information 6 Vertical Speed Indication Displays ADIRS vertical speed and other vertical speed information 7 Heading and Track Indications Displays current ADIRS heading track and other heading information 2014 Captain Sim www captainsim com 93 DO NOT USE FOR FLIGHT PFD AIRSPEED INDICATIONS 1 Sele
11. Annunciations TFC TCAS is enabled TA ONLY all TAs and RAs are processed and displayed as TAs TCAS is e Turned on by selecting TA RA or TA ONLY on the transponder panel Enabled by pushing the EFIS control panel TFC switch Displayed in MAP MAP CTR APP and VOR modes 3 OFFSCALE Message Indicates a TCAS RA or TA is beyond the selected map range Displayed only if TCAS is enabled 4 TRAFFIC Alert Message Displayed whenever a TCAS RA or TA is active Displayed whether TCAS traffic information is being displayed or not Displayed in all ND modes and ranges G05 DISPLAY SELECT PANEL c 1 Status STAT Display Switch A 2 Cancel Recall CANC RCL Switch nm 1 GEAR mA Hoe 1 Status STAT Display Switch Push Displays the status display on the selected Subsequent pushes Displays the next page of status messages when additional pages exist The lower center MFD blanks after the last page of status messages is displayed The inboard MFDs return to the NAV display after the last page of status messages is displayed 2 Cancel Recall CANC RCL Switch Push when there are EICAS caution or advisory messages displayed e Displays the next page of EICAS messages when additional pages exist e Cancels caution and advisory messages when the last page is displayed warning memo and communications messages remain www captainsim com 120 DO NOT USE
12. COMPLETE If a pilot attempts to leave an incomplete checklist the text in the NORMAL checklist key changes color to amber to indicate that one or more unfinished normal checklists items exist Activating the amber NORMAL checklist key returns the display to the first unfinished step in the first unfinished normal checklist 2014 Captain Sim www captainsim com Aircraft and Systems 81 DO NOT USE FOR FLIGHT CONTROLS AND INDICATORS INBOARD DISPLAYS AND HEADING REFERENCE L06 R05 INBOARD DISPLAY SELECTORS EICAS Selects what is displayed on each inboard display unit INBOARD DSPL PFD Displays the PFD blanks the PFD on the outboard display unit and inhibits selections made from the display select panel NAV Displays the ND and inhibits selections made from the display select panel MFD displays the selection made on the display select panel Displays EICAS Inhibits most selections made from the display select panel limited ENG FUEL and AIR displays can be selected Blanks the upper center display unit Note The PFD automatically appears on an inboard display unit if the adjacent outboard display unit fails regardless of switch position LO6 HEADING REFERENCE SWITCH Pushing alternately selects the heading reference for the PFDs NDs AFDS and FMCs NORM Normally references magnetic north Automatically references true north when north of 82 N or south of 8
13. ELECTRONIC CHECKLIST ECL 81 CONTROLS AND INDICATORS 81 INBOARD DISPLAYS AND HEADING REFERENCE 82 G05 DISPLAY SELECT PANEL 89 G03 606 EFIS CONTROL PANELS 91 DISPLAY BRIGHTNESS CONTROLS 92 PRIMARY FLIGHT DISPLAY PFD 104 STANDBY FLIGHT INSTRUMENTS CLOCK 108 FLIGHT MANAGEMENT NAVIGATION 108 R05 FMC SELECTOR 109 FUEL 109 O12 FUEL SYSTEM 110 O11 FUEL JETTISON SYSTEM 111 HYDRAULICS 111 O07 HYDRAULIC PANEL 112 MISCELLANEOUS HYDRAULIC SYSTEM CONTROLS 112 M02 FLIGHT CONTROL HYDRAULIC POWER SWITCHES www captainsim com DO NOT USE FOR FLIGHT 113 LANDING GEAR 113 C03 LANDING GEAR PANEL 114 NOSE WHEEL STEERING TILLER 114 BRAKE SYSTEM 114 P12 PARKING BRAKE LEVER 115 104 BRAKE ACCUMULATOR PRESSURE INDICATOR 116 WARNING SYSTEMS 116 SYSTEM WARNINGS 117 TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM TCAS 119 G05 DISPLAY SELECT PANEL G AIR SYSTEMS 121 AIR CONDITIONING SYSTEM 122 PRESSURIZATION SYSTEM 123 O16 BLEED AIR SYSTEM 124 WEATHER RADAR 124 THEORY OF OPERATION 125 CONTROLS AND INDICATORS 127 CUSTOMER CARE www captainsim com DO NOT USE FOR FLIGHT SYSTEMS DESCRIPTION The 777 Captain is one of the most advanced complete and accurate airliner expansions for MSFS But the 777 Captain same as MSFS itself and any MSFS expansion is a flight simulation software game Therefore this product should not be used as flight training device FTD and or simulator for flight training purposes
14. FOR FLIGHT Pushing this switch cancels the red box color of any engine parameter exceedance box that remains after a red line exceeded parameter has cleared Pushing this switch when there are no EICAS messages displayed Displays the previously cancelled EICAS messages if the condition s still exist Displays the first page of messages when multiple pages exist Displays previously canceled red exceedance boxes www captainsim com FLIGHT MANUAL Part II Aircraft and Systems 121 DO NOT USE FOR FLIGHT AIR SYSTEMS AIR CONDITIONING SYSTEM O15 AIR CONDITIONING PANEL Equipment Cooling EQUIP COOLING Switch PACK Switches TRIM AIR Switches Air Conditioning Reset AIR COND RESET Switch Cabin Temperature CABIN TEMP Control Recirculation Fans RECIRC FANS Switches caus CONDITIONING x RECIRZ PAHS UPPER LOWER PLT DEGE TEMP ALTE OY QI Q N L TAIM A13 Cos ov 1 Equipment Cooling EQUIP COOLING Switch AUTO Equipment cooling mode is controlled automatically Off AUTO not visible Both equipment cooling supply fans are not operating The smoke override valve is open The forward cargo heat valve is closed and e OVRD illuminates OVRD override illuminated amber SMOKE OVRD mode is operating because e Off is selected manually e Both equipment cooling supply fans fail or e The smoke override mode is automatically selected by the
15. Options Settings Controls Button Keys Autopilot MCP operations like heading select sample press Ctrl Shift H release using or on keyboard spin the knob press any key or left mouse click to cancel selected option Known issues Ctri Shift K cannot be selected see p 32 Hotkeys can be used only when the MCP 2D panel is on screen or when you are in VC O a ranae BggB B8688 HE n B n KE o 19 4 05 19 02 62 CI G4 1 9 Autopilot A P Engage Switches 2 3 Autothrottle A T ARM Switches 4 IAS MACH Window IAS MACH Reference Switch 5 Lateral Navigation LNAV Switch 6 Heading Track HDG TRK Reference Switch Heading Track Window 7 Vertical Speed Flight Path Angle V S FPA Window V S FPA Reference Switch 8 Altitude Window 10 25 Flight Director F D Switches 11 Climb Continuous CLB CON Thrust Switch 12 Autothrottle A T Engage Switch 13 IAS MACH Selector 14 Vertical Navigation VNAV Switch 15 Flight Level Change FLCH SPD Switch 16 Autopilot A P Disengage Bar 17 BANK LIMIT Selector outer Heading Track Selector middle Heading Track Select SEL Switch inner 18 Heading Track Hold HOLD Switch 19 V S FPA Selector 20 V S FPA Switch Light 21 Altitude Selector 22 Altitude Hold Switch 23 Localizer LOC Switch 24 Approach APP Switch 1 9 Autopilot
16. RESETS NON NORMAL MENU BEFORE 5 4 FMC RADIOS PROG SET VERIF Vi ADIRU V HYDRAULIC PUMPS DEMAND AUTO PRIMARY N oe N EF LADIN Slt OXYGEN CHECK osasse COMPLETE CONTINUED ITEM CHKL CHKL NORMAL OVRD OVRD RESET Electronic checklists ECL support the following keys Alt Up Left Right Dn to navigate the ECL interface items Enter to set reset a checklist item or to click the ELC interface button INTRODUCTION Normal electronic checklists can be displayed on any selected Multifunction Display MFD The electronic checklist system is not required for dispatch a printed checklist must be available on the flight deck Electronic checklists can be displayed on any MFD by pushing the checklist display switch on the display select panel The checklists are controlled using either one of the two cursor control devices Cursor control devices CCD and MFD selection are described in the Display System Controls paragraph of this section 2014 Captain Sim www captainsim com DO NOT USE FOR FLIGHT ELECTRONIC CHECKLIST OPERATION GENERAL Pushing the checklist display switch on the display select panel displays the proper checklist Only one checklist is displayed at a time As each normal checklist is finished pushing the checklist display switch displays the next sequential normal checklist Some checklist steps must be checked off by the pilot
17. above the transition altitude or if STD is set and altitude descends below the transition flight level 2 Barometric Reference Indicates the barometric setting units selected on the EFIS control panel barometric reference selector e IN is inches of mercury HPA is Hectopascals 3 QFE Altitude Reference Indicates QFE altitude reference selected on the CDU APPROACH REF page When selected QFE is boxed for 10 seconds The altitude tape is shaded green during QFE operation When QNH is selected the green shading is removed QNH is displayed for 10 seconds then blanks 4 Autopilot Flight Director Barometric Source Lor R indicates that the left or right EFIS control panel is the barometric setting reference for the autopilot or flight director the same indication is displayed on both PFDs Displayed when a flight director switch is ON or the autopilot is engaged e F D One turned on and one not on determines L or R F D Both on Lis displayed e A P First one pushed on determines L or R 5 Preselected Barometric Setting A barometric setting can be preselected when STD is displayed The preset barometric setting is selected on the EFIS control panel barometric selector and is displayed below STD www captainsim com 97 DO NOT USE FOR FLIGHT 6 QFE When STD is selected a small QFE appears when QFE is selected PFD VERTICAL SPEED INDICATIONS 1 Vertical Speed Pointer 2 Selected Vertical Speed Bug 3 V
18. inoperative 4 Fault Indication amber BRAKE Indicates brake deactivation on the associated wheel ASKID Indicates antiskid fault on the associated wheel 5 Tire Pressure Indication Displays individual tire pressures White normal range e Amber abnormal high or low range www captainsim com II Aircraft and Systems 86 DO NOT USE FOR FLIGHT AIR SYNOPTIC DISPLAY The air systems synoptic is displayed by pushing the AIR synoptic display switch on the display select panel 1 Selected Temperatures magenta 2 Actual Temperatures white Displnyed when connected FAD flights deck WA wang antice valve ISLH scu eben 1 Selected Temperatures magenta Selected by the FLT DECK TEMP and the CABIN TEMP controls 2 Actual Temperatures white Actual temperature sensed on the flight deck or the passenger zone 2014 Captain Sim www captainsim com A green Door mode is armed M white Door mode is manual blank Door mode is not available w s 7 7 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 87 DOOR SYNOPTIC DISPLAY DO NOT USE FOR FLIGHT FWD ACCESS EE ACCESS ENTRY iL ENTRY 1R FWO CARGO ENTRY 2L ENTRY 2R ENTRY 3L ENTRY SR AFT CARGO BULK CARGO ENTRY 4L ENTRY 4R A M can appear inside door symbol O amber passeng
19. segment represents 30 seconds Based on bank angle and ground speed Selected range determines the number of segments displayed For range greater than 20 NM 3 segments 20 NM 2 segments 10 NM 1 segment Indicates actual position and track along the flight plan route in plan mode only Inhibited north of 829N latitude and south of 8295 latitude Indicates the active flight plan waypoint the next waypoint on the route of flight Active waypoint MAP MAP CTR Distance to the active distance W PLAN way point MAP MAP CTR 0835 4Z Active waypoint ETA W www captainsim com Waypoint active M inactive W PLAN MAP MAP CTR PLAN Indicates ETA at the active waypoint Time is based on distance to go and ground speed It does not consider FMC performance predictions and may differ from other FMC ETAs that do Active represents the waypoint the airplane is currently navigating to Inactive represents the waypoints on the active route A MLF 68 DO NOT USE FOR FLIGHT Off route waypoint MAP MAP CTR B Flight plan route MAP MAP CTR active M PLAN modified W inactive B Route data active waypoint M inactive waypoint W Selected reference point and bearing distance information G MAP MAP CTR AND PLAN Altitude profile point and identifier G VNAV path pointer MAP MAP M and deviation CTR scale W
20. side of the airplane and three static ports are located on the right side of the airplane Left and right static ports are paired through pneumatic tubing to each of the left center and right air data modules The air data modules convert static air pressure to a digital output for use by other systems The center static ports are also connected to an independent air data module to provide static pressure to the standby airspeed indicator and the standby altimeter Two pitot probes right and center are mounted on the right forward section of the airplane One pitot probe left is mounted on the left forward section of the airplane An air data module is connected to each pitot probe These air data modules convert dynamic air pressure to a digital output for use by other systems The center pitot probe also provides dynamic pressure to the standby air data module ANGLE OF ATTACK There are two angle of attack vanes one located on each side of the forward fuselage The vanes measure airplane angle of attack relative to the air mass TOTAL AIR TEMPERATURE A total air temperature probe is mounted outside the airplane to sense air mass temperature The temperature sensed by the probe is used by the ADIRU and the SAARU to compute total air temperature STATIC AIR TEMPERATURE Static air temperature displayed on the CDU PROGRESS page comes from the ADIRU using total air temperature probe information In the event the ADIRU value is invalid
21. smoke detection system 2 PACK Switches AUTO The pack is automatically controlled OFF AUTO not visible The pack flow control valves are commanded closed OFF illuminated amber The pack flow control valves are commanded closed e Automatically during engine start e Automatically due to a pack or compressor outlet high temperature both flow control valves failed closed no pneumatic air OFF is manually selected 3 TRIM AIR Switches ON The trim air valve is commanded open Off ON not visible e The trim air valve is commanded closed and e FAULT illuminates FAULT illuminated amber e The trim air valve is failed closed e The trim air valve is commanded closed because of a zone supply duct overheat or e The TRIM AIR switch is selected off 2014 Captain Sim www captainsim com FLIGHT MANUAL Part II Aircraft and Systems 122 DO NOT USE FOR FLIGHT 4 Air Conditioning Reset AIR COND RESET Switch Push e Resets any closed pack flow control valves or trim air valves held closed due to overheat control failure or valve failure e Attempts to reset a failed recirculation fan Resets fault protection 5 Cabin Temperature CABIN TEMP Control Provides automatic passenger cabin temperature control 6 Recirculation Fans RECIRC FANS Switches ON Provides automatic operation of the associated recirculation fans Off ON not visible The selected recirculation fans do not operate PRESSURIZAT
22. switch is in RUN CON This position has no function on CAL GE equipped aircraft Both ignitors operate continuously only when the respective FUEL CONTROL switch is in RUN and the PS3 compressor discharge pressure drops below a preset level regardless of switch position 2 AUTOSTART Switch ON Arms the autostart system OFF The autostart system is disabled e The start is manually controlled 3 AUTOSTART OFF Light Illuminated amber The AUTOSTART switch is OFF 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 49 DO NOT USE FOR FLIGHT AUXILIARY POWER UNIT APU O03 APU CONTROLS 1 APU Selector 2 APU FAULT Light 1 APU Selector OFF e Closes the APU bleed air isolation valve e Initiates normal shutdown Resets auto shutdown fault logic ON APU operating position e Opens the APU fuel valve and inlet door Activates AC or DC fuel pump e Powers the APU controller START momentary position spring loaded to ON Initiates automatic start sequence 2 APU FAULT Light Illuminated amber e APU fault and or fire is detected APU shutdown due to fault and or fire e Momentarily during APU controller self test 2014 Captain Sim www captainsim com Captain FLIGHT MANUAL Part II Aircraft and Systems 50 DO NOT USE FOR FLIGHT FIRE PROTECTION ENGINE FIRE PROTECTION P24 ENGINE AND APU FIRE PANEL 1 Engin
23. the bottom of the page Pressing the cursor select switch advances to the next checklist page When the last page is complete the cursor moves to the NORMAL checklist key as described above 1 WWW Captainsim com 79 DO NOT USE FOR FLIGHT CHECKLIST MENU OPERATION An alternate means of operating the checklist is through the use of menus The normal resets menus can be selected by the keys at the top of the checklist page using the cursor control device An EXIT MENU key is located in the lower right corner of all menu displays This exits the menu page to allow access to the NORMAL checklist keys CHECKLIST RESETS MENU Selecting RESETS displays miscellaneous information such as checklist database part number and revision information and the following selectable resets e RESET NORMAL e RESET ALL Selecting the resets menu and then the reset key labeled RESET ALL resets all normal and non normal checklists The flight crew is prompted to re accomplish all annunciated non normal checklists that were previously completed Use of the RESET ALL function in flight is not recommended This provides a way to reset multiple checklists CHECKLIST RESETS If a checklist is partially complete or complete and the pilot wishes to begin the checklist again the checklist must be reset Selecting the CHKL RESET key at the bottom of the page while the checklist is displayed resets the checklist and allows the checklist to be accomplished a
24. the target airspeed This is speed intervention 14 Vertical Navigation VNAV Switch Push e Arms disarms or engages VNAV as the pitch mode e Displays VNAV in white armed on the PFD pitch flight mode annunciator below 400 feet above runway elevation e VNAV engages 400 feet above runway elevation e If VNAV is selected and the FMC has insufficient data to provide VNAV guidance e VNAV SPD VNAV PTH or VNAV ALT pitch mode is displayed in green engaged on the PFD pitch flight mode annunciator In the VNAV PTH pitch mode the AFDS commands pitch to maintain FMC target altitude or the VNAV path The autothrottle maintains speed e In the VNAV ALT pitch mode the AFDS commands pitch to maintain the MCP selected altitude when that altitude is lower than the VNAV commanded altitude in climb or higher than the VNAV commanded altitude in descent e If VNAV is selected and VNAV commands a descent with the MCP altitude window above the current airplane altitude the autopilot maintains the altitude at which VNAV was selected When on a VNAV approach selecting the missed approach altitude does not interfere with the VNAV descent e If VNAV is selected and VNAV commands a climb with the MCP altitude window below the current airplane altitude the autopilot maintains the altitude at which VNAV is selected e With the VNAV PTH pitch mode engaged the autothrottle operates in the following modes climb or cruise Operates in the
25. what is displayed on the CANCEL RECALL switch functions display unit 5 The upper center display blanks The left inboard display cannot and the EICAS display moves to the display any selections made on the right inboard display unit display select panel Now there is ND visible Either 2 The left outboard display blanks pilot could use the display select and the PFD moves to the left panel to display an ND on the lower inboard display unit center display unit refer to the The left EFIS control panel following pages controls the 4 The right INBOARD DISPLAY selector is set to EICAS L T EI INBOARD DSPL INBOARD DSPL NORM NORM NAM P in MFD NAV www captainsim com 60 DO NOT USE FOR FLIGHT DISPLAY SELECT PANEL MFD SELECTION With the INBOARD DISPLAY selectors set to DOPL the display select panel display switches are MFD used to designate a display as an MFD The designated display L INBD CTR or R EICAS INED is then controlled by the other display select panel selections ENG STAT CHKL COMM NAY or one of the system synoptics www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems DO NOT USE FOR FLIGHT EFIS CONTROL PANEL MULTIPLE ND CONTROL This shows which EFIS control panel controls which ND when multiple NDs displayed or when the MD is displayed on the lower cen
26. within precipitation at calibrated gain level Turbulence display is available on displays of 40 miles or less MAP position selects the ground map mode GCS disabled 54 F d 2 a F m i 30 26 e Su m dof i TCAS TERR 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 126 DO NOT USE FOR FLIGHT 2 5 Tilt and Gain Control The left and right antenna tilt controls let you select antenna tilt from 15 degrees to 15 degrees The tilt controls also have the receiver gain control The gain control adjusts the system gain in the MAP mode only 3 6 System Select Switch The left LR T and right RR T select switches allows to select the left or right WXR for operation and activate appropriate Tilt Control and Mode Selectors 7 Test Switch The test switch lets you do a test of the WXR that is in operation The test results show on the NDs 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 127 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 777 Captain is one of the most advanced complete and accurate digital replica of the Boeing 777 aircraft ever available for any game platfo
27. 1 Master WARNING CAUTION Reset Switch 1 2 Master Warning Light 3 Master Caution Light 1 Master WARNING CAUTION Reset Switch Push Extinguishes the master WARNING lights Extinguishes the master CAUTION lights e Silences most associated aural alerts for exceptions see Master Warning Caution Reset Switches and Lights 2 Master WARNING Light Illuminated red A time critical warning or warning condition exists 3 Master CAUTION Light Illuminated amber A caution condition exists C03 GROUND PROXIMITY WARNING SYSTEM GPWS CONTROLS 1 Ground Proximity FLAP Override Switch 2 Ground Proximity GND PROX Glideslope G S ELAP Inhibit Switch OVRD RO 3 Ground Proximity Light 4 Ground Proximity GEAR Override Switch 5 Ground Proximity Terrain TERR Override Switch GND PROX 2014 Captain Sim www captainsim com DO NOT USE FOR FLIGHT TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM 5 P30 TCAS CONTROLS AND TRANSPONDER PANEL Transponder XPNDR Selector Altitude ALT SOURCE Selector Transponder Code Selectors Transponder Code Window Transponder Mode Selector TCAS Controls TCAS Test Switch Absolute Relative ABS REL Altitude Selector TCAS Airspace Selector Q N 1 Transponder XPNDR Selector Lor R selects desired transponder 2 Altitude ALT SOURCE Selector NORM normal selects ADIRU as source of transponder altitude r
28. 2 S latitude or within the vicinity of the magnetic poles PFDs NDs and FMCs Provides no reference for AFDS roll modes other than LNAV when north of 829 or south of 8295 latitude or in the vicinity of the magnetic poles TRUE References true north regardless of latitude 4 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 82 DO NOT USE FOR FLIGHT GO5 DISPLAY SELECT PANEL 1 Display Lights 2 Display Switches 3 Multifunction Display MFD Switches 4 Synoptic Switches 3 5 Cancel Recall CANC RCL Switch s 1 Display Lights Illuminates to show the display unit the display select panel controls 2 Display Switches Pushing the switch displays the associated display Pushing the same switch a second time blanks the display or left and right inboard display units redisplays the ND if there is only one page of messages If there are more than one page of messages pushing STAT pages through the messages ENG Secondary engine EICAS STAT Status page Hydraulic system indications e APU indications e Oxygen system indications Status messages for dispatch determination CHKL Checklist NAV Navigation display this section 3 Multifunction Display Switches Selects the active MFD left inboard lower center or right inboard display unit for display selection The appropriate left or right INBOARD DISPLAY selector must be in the MFD or EICA
29. 4 Commanded N1 Sector Displays momentary difference between engine N1 and N1 commanded by thrust lever position 5 Maximum N1 Line Displayed amber 6 Reference N1 Displayed digital green 7 N1 Digital N1 RPM displayed White Normal operating range Red Operating limit reached 8 N1 Indication N1 RPM displayed White Normal operating range Red Operating limit reached 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 42 DO NOT USE FOR FLIGHT EGT INDICATIONS EGT Red Line EGT Amber Band Start Limit Line EGT Indication gl WN 1 EGT Red Line Displayed red Maximum takeoff EGT limit 2 EGT Amber Band Displayed amber Maximum continuous EGT limit 3 EGT Start Limit Line Displayed red e With the FUEL CONTROL switch in CUTOFF or With the N2 RPM below idle 4 EGT EGT degrees C displayed White Normal operating range e Amber Maximum continuous limit reached Red Maximum start or takeoff limit reached 5 EGT Indication Displayed White Normal operating range e Amber Maximum continuous limit reached e Red Maximum start or takeoff limit reached ANTI ICE INDICATIONS 1 Engine Anti ice Indication 2 Wing Anti Ice Indication 758 1 Engine Anti ice Indication Displayed green Engine anti ice is on 2 Wing Anti I
30. AC B G appropriate navaids are displayed B Tuned VHF navaids are displayed in green regardless of switch selection When a navaid is manually tuned the selected course and reciprocal are displayed VOR DME raw data When the POS map switch is radial and distance selected on the station radial G extends to the airplane VOR G or ADF B MAP MAP CTR Located lower left or right selection VOR VOR CTR corner Represents positions of APP APP CTR the EFIS control panel VOR ADF switches VOR frequency or MAP MAP CTR Frequency is displayed before identifier G VOR VOR CTR identifier is decoded Decoded ADF frequency or APP APP CTR identifier replaces the frequency identifier B For VORs small size characters indicate only DME information is being received DME distance G MAP MAP CTR VOR VOR CTR APP APP CTR Indicates DME distance to the referenced navaid www captainsim com lt gt 9 Symbol Name ND Mode 67 DO NOT USE FOR FLIGHT Remarks Airplane symbol W Airplane symbol W Position trend vector W dashed line Airplane symbol W Active waypoint identifier M MAP MAP CTR VOR APP VOR CTR APP CTR MAP MAP CTR MAP MAP CTR PLAN Current airplane position is at the apex of the triangle Current airplane position is at the center of the symbol Predicts position at the end of 30 60 and 90 second intervals Each
31. ACCUMULATOR PRESSURE INDICATOR 05 LEFT INBOARD DISPLAY LO6 INBOARD DISPLAY SELECTOR HEADING REFERENCE SWITCH 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 13 DO NOT USE FOR FLIGHT RIGHT FORWARD PANEL R01 RIGHT INBOARD DISPLAY R02 INSTRUMENT SOURCE SELECT PANEL R03 RIGHT OUTBOARD DISPLAY R04 CLOCK R05 INBOARD DISPLAY SELECTOR HEADING REFERENCE SWITCH 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 14 DO NOT USE FOR FLIGHT GLARESHIELD PANEL II Cina mane lic e E Ber Oo 30 O gt En n 26 EH T ri o E ME em T e m e G01 G08 MAP LIGHT CONTROL G02 G07 MASTER WARNING CAUTION RESET SWITCHES AND LIGHTS G03 G06 EFIS CONTROL PANELS G04 MODE CONTROL PANEL MCP G05 DISPLAY SELECT PANEL 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 15 DO NOT USE FOR FLIGHT CENTER FORWARD PANEL C01 STANDBY INSTRUMENTS C02 UPPER CENTER DISPLAY C03 LANDING GEAR PANEL GROUND PROXIMITY WARNING SYSTEM GPWS CONTROLS 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 16 DO NOT USE FOR FLIGHT FORWARD AISLE STAND es F4 ojo on OI em Q O o O eeoo
32. APU Bleed Switch AUTO The APU bleed air valve is automatically controlled OFF AUTO not visible The valve is commanded closed OFF illuminated amber The APU bleed air valve is closed Automatically due to a duct leak e Because the switch is selected OFF e Due to the valve failing closed Because the APU fire switch is pulled out 3 Engine ENG Bleed Switches ON The engine bleed valves open when engine bleed air is available OFF ON not visible Valve is manually commanded closed OFF illuminated amber The engine bleed valves are closed Automatically due to a protective bleed shut down or duct leak Because the switch is selected OFF Because the engine is not running or Because the engine fire switch is pulled out www captainsim com y omy fi 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 124 DO NOT USE FOR FLIGHT WEATHER RADAR The primary use of this radar is to aid the pilot in avoiding thunderstorms and associated turbulence Since each operator normally develops specific operational procedures for use of weather avoidance radar the following information is presented for use at the operator s discretion Operational techniques for the radar are similar to earlier generation weather avoidance radars The proficient operator manages antenna tilt control to achieve best knowledge of storm height size and relative direction of movement RADAR PRINCIPLES Radar is fundamentally a distanc
33. DICATIONS Note The selected track bug and selected heading bug are not displayed at the same time 1 Current Heading Pointer 8 2 Selected Track Bug MCP Selection 3 Track Line 4 Selected Heading Track MCP Selection 5 Selected Heading Track Reference Selection 6 Selected Heading Bug MCP Selection 7 Heading Track Reference 1 Current Heading Pointer Indicates current heading 2 Selected Track Bug MCP Selection The selected track bug is displayed on the inside of the compass rose If selected track exceeds display range the bug parks on the side of the compass rose in the direction of the shorter turn to the track 3 Track Line Indicates the current track 4 Selected Heading Track MCP Selection Digital display of the selected heading or track bug 5 Selected Heading Track Reference MCP Selection When HDG heading is selected an H is displayed When TRK track is selected a T is displayed www captainsim com 102 DO NOT USE FOR FLIGHT 6 Selected Heading Bug MCP Selection The selected heading bug is displayed on the outside of the compass rose If selected heading exceeds display range the bug parks on the side of the compass rose in the direction of the shorter turn to the heading 7 Heading Track Reference Displays the automatic or manually selected heading track reference e MAG magnetic north e TRU true north www captainsim com 103 DO NOT USE FOR FLIGHT
34. DO NOT USE FOR FLIGHT 777 Captain FLIGHT MANUAL PART II Aircraft and Systems www captainsim com DO NOT USE FOR FLIGHT ABOUT THIS MANUAL VERSION 24 APRIL 2014 WARNING THIS MANUAL IS FOR MS FSX EXPANSION ONLY DO NOT USE FOR FLIGHT The 777 Captain FLIGHT MANUAL is organized into two Parts Each Part is provided as a separate Acrobat PDF document Part I User s Manual The User s Manual describes the 777 Captain product as a software title Part II Aircraft and Systems this document The Manuals are available free of charge online THIS MANUAL IS SUPPLEMENTAL TO THE 777 CAPTAIN WEB SITE WHICH WE HIGHLY RECOMMEND TO READ BEFORE USING THIS MANUAL www captainsim com DO NOT USE FOR FLIGHT 777 Captain FLIGHT MANUAL CONTENTS 6 SYSTEMS DESCRIPTION AIRCRAFT GENERAL 7 PRINCIPAL DIMENSIONS 8 CARGO COMPARTMENTS 9 INSTRUMENT PANELS 9 10 FLIGHT DECK PANELS INSTRUMENT PANELS OVERHEAD 10 OVERHEAD PANEL 11 OVERHEAD MAINTENANCE PANEL 12 INSTRUMENT PANELS FORWARD 12 LEFT FORWARD PANEL 13 RIGHT FORWARD PANEL 14 GLARESHIELD PANEL 15 CENTER FORWARD PANEL 16 FORWARD AISLE STAND 17 INSTRUMENT PANELS AFT AND SIDE 17 CONTROL STAND 18 AFT AISLE STAND 19 LEFT AND RIGHT SIDEWALL PANELS 20 PASSENGER SIGNS AND LIGHTING 20 O08 PASSENGER SIGNS AND LIGHTING 21 O14 LIGHTING PANEL 22 MISCELLANIOUS LIGHTING CONTROLS 23 O05 PASSENGER OXYGEN SWITCH 24 ANTI ICE SYSTE
35. ELECTRONIC CHECKLIST DISPLAYS NORMAL CHECKLIST HON HNORMAL MENJ A FLIGHT INSTRUMENTS ete ecce oor cA PARKING ete ete ne cen ceca FUEL CONTROL SWATCHES essen 8 5 S Left cursor MFD aL ar Right cursor 1 Cursor and Selection Box Highlights cursor selection area 2 Open Loop Indicator Indicates line item is an open loop action item Requires crew confirmation to become complete 3 Complete Indicator Indicates line item is complete 4 Normal Checklist NORMAL Key Select e Displays next incomplete normal checklist e Displays normal checklists menu page when all normal checklists are complete Displayed white Incomplete normal checklist has not been displayed Displayed amber Incomplete normal checklist has been displayed but is not currently displayed 5 Line Item Override ITEM OVRD Key Select Overrides action item in current line item box Item is displayed cyan 6 Checklist Line Item Displayed white e When action is required line item is incomplete e When action is not required line item remains white and is complete www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 104 DO NOT USE FOR FLIGHT Displayed green Line item is complete Displayed cyan Line item is inactive or overridden 7 Current Line Item Box Highlights current incomplete line i
36. FIS CONTROL PANEL ND CONTROLS ND Mode Selector outer ND Center CTR Switch inner VOR ADF Switches Map Switches ND Range Selector outer ND Traffic TFC Switch inner 1 ND Mode Selector outer Selects the desired ND map display APP Displays localizer and glideslope information in heading up format Displays reference ILS receiver ILS frequency or identification course and DME e Weather radar TCAS not displayed in APP mode VOR Displays VOR navigation information heading up format Displays reference VOR receiver VOR frequency or identification course DME and TO FROM indication e Weather radar and TCAS not displayed VOR mode MAP Displays FMC generated route and map information airplane position heading and track Displays waypoints including the active waypoint within the selected range Displays VNAV path deviation PLN Displays a nonmoving true north up route depiction The airplane symbol represents actual airplane position Allows route step through using the CDU legs page Weather radar and TCAS are not displayed in PLN mode 2 ND Center CTR Switch inner Push Displays the full compass rose centered for APP VOR and MAP modes Subsequent pushes alternate between expanded and centered displays VOR ADF Switches Displays VOR or ADF information on the respective ND VOR Displa
37. ION SYSTEM O17 PRESSURIZATION PANEL PAESSURIZATION 1 OUTFLOW VALVE Switches 2 OUTFLOW VALVE MANUAL Switches wave TART OPF ALS 3 Landing Altitude LDG ALT Selector 1 OUTFLOW VALVE Switches AUTO Outflow valve position is automatically controlled Manual AUTO not visible e Outflow valve position is controlled by the OUTFLOW VALVE MANUAL switch e MAN illuminates e Outflow valve position is displayed on EICAS an amber M is displayed on the outflow valve position indicator on EICAS MAN manual illuminated amber Outflow valve position is controlled by the associated OUTFLOW VALVE MANUAL switch 2 OUTFLOW VALVE MANUAL Switches Spring loaded to center Controls outflow valve position when MAN is illuminated in the OUTFLOW VALVE switch OPEN Moves the outflow valve toward open CLOSE Moves the outflow valve toward closed 2014 Captain Sim www captainsim com 123 DO NOT USE FOR FLIGHT O16 BLEED AIR SYSTEM BLEED AIR 1 Bleed Isolation ISLN Switches 2 APU Bleed Switch 3 Engine ENG Bleed Switches 1 Bleed Isolation ISLN Switches AUTO The bleed isolation valve is automatically controlled Off AUTO not visible Manually commands the respective bleed isolation valve to close CLOSED illuminated amber The isolation valve is closed due to a duct leak or bleed loss The valve is closed because the switch is selected to off or The valve fails closed 2
38. M 24 O13 ANTI ICE PANEL 24 O06 WINDOW HEAT PANEL 24 004 O18 WIPER PANEL 25 AUTO FLIGHT SYSTEM 25 G04 MODE CONTROL PANEL MCP 31 PO1 P03 CDU 33 CDU KEYBOARD CONTROL 34 09 TO GA AND AUTOTHROTTLE DISCONNECT SWITCHES 35 COMMUINICATIONS SYSTEM 35 P19 P22 P29 501 AUDIO CONTROL PANEL ACP 36 P18 P21 P28 RADIO TUNING PANEL 38 ELECTRICAL SYSTEM 38 O03 ELECTRICAL PANEL and AUXILIARY POWER UNIT APU 40 ENGINES amp APU 40 EICAS DISPLAY 40 MODE INDICATIONS 41 N1 INDICATIONS ALL MODES 42 EGT INDICATIONS 42 ANTI ICE INDICATIONS 43 SECONDARY ENGINE INDICATIONS www captainsim com DO NOT USE FOR FLIGHT 47 09 ENGINE CONTROLS 47 THRUST LEVERS 47 P14 FUEL CONTROL SWITCHES 48 O10 ENGINE CONTROL PANEL 49 AUXILIARY POWER UNIT APU 49 O03 APU CONTROLS 50 FIRE PROTECTION 50 ENGINE FIRE PROTECTION 50 P24 ENGINE AND APU FIRE PANEL 51 O09 APU AND CARGO FIRE PANEL 52 FLIGHT CONTROL 52 O02 THRUST ASYMMETRY COMPENSATION AND PRIMARY FLIGHT COMPUTERS CONTROLS 52 PITCH AND STABILIZER TRIM SYSTEMS 53 AILERON AND RUDDER TRIM CONTROLS 54 FLAP SYSTEM 2256 FLIGHT INSTRUMENTS 56 SYSTEM DESCRIPTION 56 DISPLAY SYSTEM CONTROLS 62 DISPLAY SYSTEM INFORMATION SOURCE 63 PRIMARY FLIGHT DISPLAY PFD 63 PFD INFORMATION 65 TYPICAL PFD DISPLAYS 68 NAVIGATION DISPLAY ND 68 ND MODES 71 ELECTRONIC FLIGHT BAG 72 MAIN MENU MODE 74 SPLIT MODE 75 DEFAULT SETUP AND CONTENT 76 USERS CUSTOMIZATION 77
39. ND e The Engine Indication And Crew Alerting System EICAS e The Multifunction Display MFD Detailed information on the following subjects is found in other parts of this section e PFD ND Electronic Checklist DISPLAY SYSTEM CONTROLS GENERAL During normal operations e inboard display selectors are set to MFD PFDs are displayed on the two outboard display units NDs are displayed on the two inboard display units EICAS is displayed on the upper center display unit The lower center display unit defaults to the secondary engine display at power up All Display Select Panel DSP functions may be displayed on the lower center display unit The flight crew should keep the secondary engine display selected if no other display is being used i e status checklist etc INBOARD DISPLAY SELECTORS The inboard display selectors are used to select PFD ND NAV position MFD or EICAS displays on the inboard display units The normal position is MFD With MFD selected ND information is displayed on the inboard display units if NAV is selected on the display select panel refer to Display Select Panel in this section In the ND PFD and EICAS positions only the selected displays can appear on the inboard display units With MFD selected on the inboard display selector the following ND and EFIS control logic applies e both pilots have an ND on the inboard displays then each EFIS control panel controls its correspondi
40. NG ANTI ICE Selector OFF Both wing anti ice valves are commanded closed AUTO In flight both wing anti ice valves are commanded opened or closed automatically by the ice detection system ON In flight both wing anti ice valves are commanded open 2 ENGINE ANTI ICE Selectors OFF The engine anti ice valve is commanded closed AUTO In flight the engine anti ice valve is opened or closed automatically by the ice detection system ON The engine anti ice valve is commanded open Note If the ENG ANTI ICE selector is in AUTO and the anti ice valve is commanded open or if the selector is in ON then approach idle is selected by the EEC 06 WINDOW HEAT PANEL WINDOW HEAT ON Window heat is applied to the selected windows PWD SILE INOP inoperative illuminated amber The switch is OFF An overheat is detected or A system fault has occurred O04 O18 WIPER PANEL OFF The wiper is stowed at the base of the L WIPER R WIPER window INT intermittent wiper operates intermittently LOW The wiper operates at low speed HIGH The wiper operates at high speed www captainsim com 25 DO NOT USE FOR FLIGHT AUTO FLIGHT SYSTEM Please note many MCP switches and buttons can be controlled using hotkeys The events for assignment are listed near each control s name in bold slanted font Any key combinations can be assigned for these controls using default FSX key assignment menu
41. S position The other display select panel switches determine what is displayed on the selected MFD 4 Synoptic Switches Pushing the switch displays the associated synoptic Synoptics present a simplified view of system status as an aid for crew situational awareness Pushing the same switch a second time blanks the display or left and right inboard display units redisplays the ND ELEC Electrical System HYD Hydraulic System FUEL Fuel System AIR Air Systems DOOR Doors GEAR Landing Gear and Brake Systems FCTL Flight Control System O 2014 Captain Sim www captainsim com 83 DO NOT USE FOR FLIGHT SYNOPTIC DISPLAYS FLIGHT CONTROL SYNOPTIC DISPLAYS The flight control synoptic is displayed by pushing the FCTL synoptic display switch on the display select panel NORMAL FLIGHT CONTROL SYNOPTIC The following display depicts the proper indication for full control wheel deflection left Spoiler Position Aileron Position Flaperon Position e III I F FLPRN F AIL Stabilizer Position k L AIL L FLPEM STAR RUDDER TRIM 6 50 LD LE R ELEY SEHEN RUDDER FLT CTRL MODE MORMAL MULTIFUNCTION DISPLAY Elevator Position Rudder Position Rudder Trim Position and Direction L Left R Right Primary Flight Control System Mode www captainsim com 84 DO NOT USE FOR FLIGHT FUEL SYNOPTIC DISPLAY The fuel synoptic is displayed by pushing the FUEL synoptic
42. ZOOM IN key Zoom the selected image in 37 ZOOM OUT key Zoom the selected image out 38 Scroll the selected image up Zoom must be IN enough for scrolling 39 SPLIT MODE indicator 40 Scroll the selected image down Zoom must be IN enough for scrolling 41 Scroll the selected image left Zoom must be IN enough for scrolling 42 Scroll the selected image right Zoom must be IN enough for scrolling 43 Return to the Main Menu DEFAULT SETUP AND CONTENT For educational purposes the EFB is setup and loaded with demo content DEFAULT SETUP Key 1 Enroute Key 2 SID Key 3 STAR Key 4 Approach Key 5 Airport Key 6 RNK Key 9 Setup Key 10 Whatever Key 14 Cameras Keys 7 11 12 13 15 Blank The default setup can be easily edited See USER CUSTOMIZABLE FUNCTION KEYS AND BOXES section DEFAULT CONTENT All content is provided for educational purposes only DO NOT USE FOR FLIGHT Captain Sim is not affiliated with any entity mentioned or pictured trademarks are the property of their respective owners Enroute Jeppesen EA7 H L enroute chart fragment Moscow Jeppesen EA9 H L enroute chart fragment St Petersburg SID Complete set of Jeppesen SID for UUDD Domodedovo Moscow STAR Complete set of Jeppesen STAR for UUDD Approach Complete set of Jeppesen approach charts for UUDD Airport Complete set of Jeppesen airport charts for UUDD RNK R 4A enroute c
43. arker Beacon Indication The marker beacon indication appears flashing when over one of the marker beacon transmitters e An airway or inner marker beacon e middle marker beacon OM An outer marker beacon The indication flashes in cadence with the beacon identifier 4 Glideslope Pointer and Scale The glideslope pointer e Indicates glideslope position relative to the airplane and e 5 in view when the glideslope signal is received e Fills in solid when within 2 1 2 dots from the scale center The scale is in view after the frequency is tuned At low radio altitudes with the autopilot or flight director engaged the scale turns amber and the pointer flashes to indicate excessive glideslope deviation www captainsim com 100 DO NOT USE FOR FLIGHT PFD LANDING ALTITUDE MINIMUMS INDICATIONS BARO Minimums Pointer Landing Altitude Indication Minimums Reference Minimums Landing Altitude Reference Bar Ul WN 1 BARO Minimums Pointer When BARO minimums are displayed the number is also represented as a pointer and line on the altitude scale Turns steady amber when the airplane descends below baro minimums 2 Landing Altitude Indication The crosshatched area indicates the FMC landing altitude for the destination runway or airport Indicates the landing altitude for the departure runway or airport until 400 NM or one half the distance to the destination whichever occurs first 3 Minimu
44. ated amber The extinguisher bottle is discharged or has low pressure 2 APU Fire Switch Override Switch In Normal position mechanically locked unlocks automatically for a fire warning Out Arms the APU fire extinguisher bottle Closes the APU fuel valve Closes the APU bleed air valves Closes the APU air inlet door Trips the APU generator field and generator breaker Shuts down the APU if automatic shutdown does not occur Rotate Either direction discharges the APU fire extinguisher into the APU compartment 3 APU Fire Warning Light Illuminated red An APU fire is detected or The APU automatically shuts down for a detected fire 4 CARGO FIRE Warning Lights Illuminated red e Associated cargo compartment smoke is detected or 5 CARGO FIRE Discharge DISCH Switch Push discharges the fire extinguisher bottles into the ARMED cargo compartment 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 52 DO NOT USE FOR FLIGHT FLIGHT CONTROL O02 THRUST ASYMMETRY COMPENSATION AND PRIMARY FLIGHT COMPUTERS CONTROLS SLAT LOAD RELIEF PRIMARY FLIGHT 1 Primary Flight Computers Disconnect Switch CORPUTERS 1 Primary Flight Computers Disconnect Switch DISC e Disconnects the Primary Flight Computers PFCs from the flight control system e Puts the flight control system in the direct mode e AUTO be reselected to attempt resto
45. aulically Secondary mode Positions the slats and or flaps electrically if hydraulic operation fails 3 Alternate Flaps Arm ALTN FLAPS ARM Switch Push ALTN displayed e Arms the alternate flap control mode e Arms the alternate flaps selector e Disables primary and secondary flap slat mode operation 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems DO NOT USE FOR FLIGHT 55 Asymmetry skew and uncommanded motion protection autoslat and flap slat load relief are not available e The flap lever is inoperative 4 Alternate Flaps Selector RET The slats and flaps are electrically retracted OFF Alternate flaps are deactivated EXT e The slats and flaps are electrically extended e Maximum extension is flaps 20 with the slats at the midrange sealed position FLAP LIMIT PLACARD and GROUND PROXIMITY WARNING SYSTEM GPWS CONTROLS FLAP LIMIT 1 Flap Limit Placard 1 255K Flaps extended speed limits O 22 15 215K 20 195K 29 185K 30 170K 2014 Captain Sim www captainsim com n FLIGHT MANUAL Part II Aircraft and Systems 56 DO NOT USE FOR FLIGHT FLIGHT INSTRUMENTS SYSTEM DESCRIPTION INTRODUCTION The flight instruments and displays supply information to the flight crew on six flat panel liquid crystal display units The units display four primary groups of information e The Primary Flight Display PFD e The Navigation Display
46. ay the following displays e ND NAV switch Status page STAT switch Secondary engine EICAS ENG switch System synoptics ELEC HYD FUEL AIR DOOR GEAR FCTL switches Electronic checklist CHKL switch EFIS CONTROL PANELS The EFIS control panels control display options mode and range for the respective PFDs and NDs Refer to the PFD and ND parts of this section If an EFIS control panel fails the displays can be controlled through the related CDU This CDU capability is available at all times but inhibits inputs from the respective EFIS control panel www captainsim com 58 DO NOT USE FOR FLIGHT NORMAL DISPLAY CONFIGURATION 1 The INBOARD DISPLAY 3 The outboard display units selectors are set to MFD display PFDs and the inboard The lower center display unit is display units display NDs The the preferred MFD controlled by the related EFIS control panel controls display select panel what is on the PFD and MD Ee ere E INBOARD DSPL INBOARD DSPL NORN x m NORMA NAV 7 D EICAS PFD WWW Captainsim com 59 DO NOT USE FOR FLIGHT INBOARD DISPLAY SWITCHING CD The left INBOARD DISPLAY right inboard display cannot selector is set to PFD display selections made on the With an INBOARD DISPLAY display select panel except for selector in any position other than compact engine air and fuel MFD the selector position alone synoptics anc the determines
47. c Flight Bag Electronic Flight Bag Control Stand Tem Right CF Forward Aisle Sidewall Aft Aisle Stand Stand 2014 Captain Sim www captainsim com LUTI MIFAINUAL rail 11 i and sYStems DO NOT USE FOR FLIGHT INSTRUMENT PANELS OVERHEAD OVERHEAD PANEL O01 AIR DATA INERTIAL REFERENCE UNIT ADIRU O02 THRUST ASYMMETRY COMPENSATION AND PRIMARY FLIGHT COMPUTERS CONTROLS O03 ELECTRICAL APU PANEL 004 018 WIPER PANEL O05 PASSENGER OXYGEN AND WINDOW HEAT PANEL O07 HYDRAULIC PANEL O08 PASSENGER SIGNS AND LIGHTING O09 APU AND CARGO FIRE PANEL 2014 Captain Sim www captainsim com O10 O11 O12 O13 LIGHTING PANEL O15 O16 O17 ENGINE CONTROL PANEL FUEL JETTISON SYSTEM FUEL SYSTEM ANTI ICE PANEL AIR CONDITIONING PANEL BLEED AIR SYSTEM PANEL PRESSURIZATION PANEL 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 11 DO NOT USE FOR FLIGHT OVERHEAD MAINTENANCE PANEL M01 BACKUP WINDOW HEAT PANEL M02 FLIGHT CONTROL HYDRAULIC POWER PANEL M03 SPEAKER M04 APU AND EEC MAINTENANCE PANEL M05 CARGO TEMPERATURE SELECT PANEL M06 GROUND TEST PANEL 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems DO NOT USE FOR FLIGHT INSTRUMENT PANELS FORWARD LEFT FORWARD PANEL LO1 INSTRUMENT SOURCE SELECT PANEL 102 CLOCK 03 LEFT OUTBOARD DISPLAY L04 BRAKE
48. c system power to the flight 2 AL VE EA aA control actuators is shut off L OS EC Note In flight the center system flight control shut off valves are isolated from electrical power and cannot be closed Wwk Y 2 Flight Control Hydraulic Power VALVE CLOSED Lights Illuminated amber The related valve is closed 2014 Captain Sim www captainsim com 113 DO NOT USE FOR FLIGHT LANDING GEAR C03 LANDING GEAR PANEL 1 Landing Gear Lever GND PROX 2 Autobrake Selector GEAR 3 Alternate Gear ALTN GEAR Switch 4 Landing Gear Lever Lock Override LOCK OVRD Switch 2 TOR ue LOCK Fa x TRD EXTEND 2 PX AUTOBRAKE 2 sas pm 4 RANK Auro 1 Landing Gear Lever UP The landing gear retracts DN The landing gear extends 2 AUTOBRAKE Selector OFF Deactivates and resets the autobrake system DISARM Disengages the autobrake system e Releases brake pressure 1 2 3 4 MAX AUTO Selects the desired deceleration rate RTO Automatically applies maximum brake pressure when the thrust levers are retarded to idle above 85 knots 3 Alternate Gear ALTN GEAR Switch NORM the landing gear lever operates normally DOWN the landing gear extends by the alternate extension system Note Alternate extension may be selected with the landing gear lever in any position 4 Landing Gear Lever Lock Override
49. ce Indication Displayed green Wing anti ice is on 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 43 DO NOT USE FOR FLIGHT SECONDARY ENGINE INDICATIONS SECONDARY ENGINE DISPLAY RR engine N ON ON 1 Secondary Engine Display Displays e N2 RPM Fuel Flow FF Oil pressure Oil temperature Oil quantity Vibration N2 INDICATIONS br 1 N2 N2 RPM 96 displayed White Normal operating range Red Operating limit reached 2 N2 Red Line N2 RPM operating limit displayed red 3 N2 Indication N2 RPM displayed White Normal operating range Red Operating limit reached 2014 Captain Sim www captainsim com GE and P 5 1 2 2 N2 Red Line 3 N2 Indication 44 DO NOT USE FOR FLIGHT FUEL FLOW INDICATIONS 1 Fuel Flow 1 Fuel Flow Displayed White Fuel flow to the engine pounds per hour x 1000 OIL PRESSURE INDICATIONS 1 Oil Pressure Engine oil pressure psi displayed White Normal operating range e Amber Caution range reached e Red Operating limit reached 2 Oil Pressure Pointer Engine oil pressure displayed White Normal operating range e Amber Caution range reached Red Operating limit reached 3 Oil Pressure Red Line Displayed red Oil pressure operating limit 4 Oil Pre
50. cimal point e Inner knob Selects the portion of the STANDBY frequency to the right of the decimal point www captainsim com DO NOT USE FOR FLIGHT 8 Radio Tuning Switches Push Selects the radio to be tuned The tuned frequency is displayed the ACTIVE frequency window The standby frequency is displayed in the STANDBY frequency window 9 Radio Tuning Lights Illuminated Indicates the selected radio www captainsim com 37 38 DO NOT USE FOR FLIGHT ELECTRICAL SYSTEM O03 ELECTRICAL PANEL and AUXILIARY POWER UNIT APU BATTERY Switch Battery OFF Light APU Generator APU GEN Switch APU Generator OFF Light BUS TIE Switches Bus Isolation ISLN Lights Generator Control GEN CTRL Switches Generator OFF Lights Drive Disconnect Switches 10 Generator DRIVE Lights Il wam 11 External Power EXT PWR Switches EXT PWR 12 External Power ON Lights t 13 External Power AVAIL Lights 14 Backup Generator BACKUP GEN Switches 15 Backup Generator OFF Lights ELECTRICAL OANA E ACAUP GE L R LL MAIN LLL LE AFR L DRIVE MSC 1 BATTERY Switch ON Unpowered airplane on the ground e Afew switch annunciator lights illuminate e Allows the APU to be started e displays are powered Powered airplane in flight or on the ground when AC power is removed or lost e The standby buses and emergency lighting are powered e The l
51. cted Speed 2 Speed Trend Vector 3 Current Airspeed 4 Current Mach 4 p 595 1 Selected Speed Displays the airspeed Mach selected in the mode control panel MCP IAS MACH window Displays the FMC computed airspeed Mach when the MCP IAS MACH window is blank 2 Speed Trend Vector Indicates predicted airspeed in ten seconds based on current acceleration or deceleration 3 Current Airspeed Indicates current ADIRS airspeed The box around the current airspeed indication turns amber when airspeed is below minimum maneuvering speed 4 Current Mach Displays current ADIRS Mach 5 Maximum Speed Indicates maximum permissible airspeed as limited by the lowest of the following Vmo Mmo e Landing gear placard speed or e Flap placard speed 6 Maximum Maneuvering Speed When displayed indicates maneuver margin to buffet May be displayed when operating at high altitude at relatively high gross weights 7 Speed Bug Points to the airspeed Mach selected in the MCP IAS MACH window Indicates FMC computed airspeed when the MCP IAS MACH window is blank The bug is five knots in height www captainsim com 94 DO NOT USE FOR FLIGHT When the selected speed is off scale the bug is parked at the top or bottom of the tape with only one half the bug visible PFD REFERENCE SPEEDS 143 1 Takeoff Reference Speeds 2 Flap Maneuvering Speeds 3 Landing Reference Speed 4 Minimum Maneuvering Speed 5 Minimum Sp
52. d Systems 47 DO NOT USE FOR FLIGHT P09 ENGINE CONTROLS THRUST LEVERS 1 Reverse Thrust Levers e Control engine reverse thrust e Reverse thrust can only be selected when the forward thrust levers are closed Actuates automatic speedbrakes 2 Forward Thrust Levers e Controls engine forward thrust e The thrust levers can only be advanced if 2 the reverse thrust levers are down P14 FUEL CONTROL SWITCHES 1 FUEL CONTROL Switch L FUEL CONTROL R RUM CUTOFF RUN AUTOSTART ON e Opens the spar fuel valve e Arms the engine fuel valve the EEC opens the valve when required e Arms the selected ignitors s the EEC turns the ignitors on when required RUN AUTOSTART OFF e Opens the spar fuel valve e Opens the engine fuel valve e Turns ignitors on CUTOFF e Closes the fuel valves e Removes ignitor power e Unlocks the engine fire switch 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 48 DO NOT USE FOR FLIGHT O10 ENGINE CONTROL PANEL EMGINE CONTROL ORM cor START EON D t AUTOS TART 1 START IGNITION Selector 2 AUTOSTART Switch 3 AUTOSTART OFF Light 1 START IGNITION Selector START e Initiates engine start by opening the start valve e Releases to NORM at start valve cutout NORM e he start valve closes Automatic ignition is provided for both ignitors if the FUEL CONTROL
53. display switch on the display select panel TOTAL an FEL 207 7 LES X 1000 CENTER MIN FUEL TEMP 37 C FUEL TEMP 13 C HYDRAULIC SYNOPTIC DISPLAY e ao D M M D D PRESS 3100 PRESS 3000 MULTIFUNCTION DISPLAY AIR air driven pump RAT ram air turbine pump ELEC electric dnven pump RF reservoir requires refilling EMS engine driven pump uy shuteff valve ILN value Closed vaie LO reservoir quantity low TE OF reservoir quantity over full B OVHT pump overheat indication Falsa pump www captainsim com 85 DO NOT USE FOR FLIGHT GEAR SYNOPTIC DISPLAY 1 Brake Temperature 2 Brake Symbol 3 Gear Door Status 4 Fault Indication amber 5 Tire Pressure Indication The landing gear synoptic is displayed by pushing the GEAR synoptic display switch on the display select panel 1 Brake Temperature Indicates a relative value of wheel brake temperature e Values range from 0 0 to 9 9 White normal range e Amber high range 2 Brake Symbol Blank box indicates any brake less than 3 0 Solid white box indicates hottest brake on each main gear within range of 3 0 to 4 9 Solid amber box indicates brake overheat condition on each wheel within range of 5 0 to 9 9 3 Gear Door Status Crosshatched The door is not closed CLOSED white The door is closed Empty box es white The associated landing gear door position indicators are
54. dures VNAV shows page to view or change vertical navigation path data FIX shows page to create reference points on ND map LEGS o Shows page to evaluate or modify lateral and vertical route data o Show page to control ND PLAN mode display HOLD shows page to create holding patterns and show holding pattern data PROG shows page to view dynamic flight and navigation data including waypoint and destination ETAs fuel remaining and arrival estimates NAV RAD shows page to monitor or control navigation radio tuning PREV PAGE shows previous page of related pages for example LEGS pages NEXT PAGE shows next page of related pages www captainsim com 32 DO NOT USE FOR FLIGHT 66 Brightness Control Rotate controls display brightness On some aircraft Push e increases brightness decreases brightness 67 Execute Key Push e Makes data modification s active Extinguishes execute light 68 Display Light Illuminated white e when RTE page 3 or greater RTE LEGS page 2 or greater RTE DATA page 2 or greater is shown e when airplane is not in holding pattern shown on HOLD page e when modification is in progress and RTE RTE LEGS RTE e DATA HOLD or VNAV page is shown 69 MSG Light Illuminated white e Scratchpad displays message e pushing CLEAR key extinguishes light and clears message 70 OFST Light Illuminated white LNAV gives guidance for lateral route offset 71 82 L
55. e Fire Switches 2 Engine Fire Warning Lights 3 Engine Bottle Discharged ENG BTL DISCH Lights 4 Engine and APU Fire Override Switches 1 Engine Fire Switches In normal position mechanically locked unlocks automatically for a fire warning Out Arms both engine fire extinguishers Closes the associated engine and spar fuel valves Closes the associated engine bleed air valves Trips the associated engine generator field and generator breaker Shuts off hydraulic fluid to the associated engine driven hydraulic pump Depressurizes the associated engine driven hydraulic pump Removes power from the thrust reverser isolation valve Rotate to position 1 or 2 discharges the selected fire extinguisher into the engine 2 Engine Fire Warning Lights Illuminated red Anengine fire is detected or 3 Engine Bottle Discharged ENG BTL DISCH Lights Illuminated amber The extinguisher bottle is discharged or has low pressure 4 Engine and APU Fire Override Switches Push Unlocks the fire switch 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 51 DO NOT USE FOR FLIGHT O09 APU AND CARGO FIRE PANEL 1 APU Bottle Discharge APU BTL DISCH Light D CARGO FIRE 2 APU Fire Switch Override Switch 3 APU Fire Warning Light 4 CARGO FIRE Warning Lights 5 CARGO FIRE Discharge DISCH Switch 1 APU Bottle Discharge APU BTL DISCH Light Illumin
56. e measuring system using the principle of radio echoing The term RADAR is an acronym for Radio Detecting and Ranging It is a method for locating targets by using radio waves The transmitter generates microwave energy in the form of pulses These pulses are then transferred to the antenna where they are focused into a beam by the antenna The radar beam is much like the beam of flashlight The energy is focused and radiated by the antenna in such a way that it is most intense in the center of the beam with decreasing intensity near the edge The same antenna is used for both transmitting and receiving When a pulse intercepts a target the energy is reflected as an echo or return signal back to the antenna From the antenna the returned signal is transferred to the receiver and processing circuits located in the receiver transmitter unit The echoes or returned signals are displayed on an indicator Radio waves travel at the speed of 300 million meters per second and thus yield nearly instantaneous information when echoing back Radar ranging is a two way process that requires 12 36 micro seconds for the radio wave to travel out and back for each nautical mile of target range As shown in the distance illustration below it takes 123 6 micro seconds for a transmitted pulse of radar energy to travel out and back from an area of precipitation 10 nautical miles away 20 NM ROUND TRIP IN 123 6 NN MICROSECONDS WEATHER RADAR PRINCIPLES Airborn
57. e receiver audio on or off 6 Approach APR Receiver Selector Selects the approach receiver to be monitored APP L Left ILS APP C Center ILS APP R Right ILS MKR Marker beacon P18 P21 P28 RADIO TUNING PANEL Radio Tuning Panel OFF Light Button Radio Tuning Panel PNL OFF Switch ACTIVE Frequency Window Frequency Transfer Switch STANDBY Frequency Window Frequency Selector Radio Tuning Switches Radio Tuning Lights 18010 I OA Q N 1 Radio Tuning Panel OFF Light Button Illuminated The radio tuning panel is off 2 Radio Tuning Panel PNL OFF Switch Push Disconnects the panel from the communication radios 3 ACTIVE Frequency Window Displays the tuned frequency of the selected radio Displays data if the selected radio is in the DATA mode not applicable for VHF L 5 Frequency Transfer Switch Push e Transfers the STANDBY window frequency to the ACTIVE window and tunes the selected radio to the new active frequency Transfers the ACTIVE window frequency to the STANDBY window 6 STANDBY Frequency Window Displays the preselected or previously tuned frequency of the selected radio With data link installed displays data when selection of the frequency transfer switch would reconfigure the selected radio to the DATA mode not applicable for VHF L 7 Frequency Selector Rotate e Outer knob Selects the portion of the STANDBY frequency to the left of the de
58. e weather avoidance radar as its name implies is for avoiding severe weather not for penetrating it Whether to fly into an area of radar echoes depends on echo intensity spacing between the echoes aircraft capabilities and pilot experience Remember that weather radar detects only precipitation drops it does not detect minute cloud droplets nor does it detect turbulence Therefore the radar provides no assurance of avoiding instrument weather in clouds and fog The indicator may be clear between intense echoes this clear area does not necessarily mean it is safe to fly between the storms and maintain visual sighting of them 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 125 DO NOT USE FOR FLIGHT CONTROLS AND INDICATORS P20 WEATHER RADAR PANEL To switch left or right WXR ON use WXR button on the corresponding EFIS panel Left Mode Selectors Left Tilt and Gain Control Left System Select Switch Right Mode Selectors Right Tilt and Gain Control Right System Select Switch Test Switch NO QI Q N Purpose The weather radar WXR panel has controls for WXR system operation 1 4 Mode Selector The left and right alternate action mode select switches have these functions TFR switch causes the RT to use the same mode tilt and gain as the other side WX shows weather radar returns at calibrated gain level WX T shows weather returns and turbulence
59. ed flight path angle window and PFD references between vertical speed and flight path angle Also changes the PFD pitch flight mode annunciator if the V S or FPA mode is engaged 8 Altitude Window Altitude bug select Displays the selected altitude The displayed altitude is the reference altitude for altitude alerting and level off The altitude range is 0 to 50 000 feet Displays 10 000 feet when power is first applied 10 25 Flight Director F D Switches Flight director on off default key Ctrl F The left flight director switch activates the flight director steering indications Pitch and Roll Bars on the left PFD The right flight director switch activates the flight director steering indications on the right PFD ON e On the ground with both flight director switches OFF the first flight director switch positioned ON arms the flight director in the takeoff TO GA roll and pitch modes and displays the flight direction steering indications on that PFD The flight mode annunciation TO GA appears on both PFDs Positioning the second switch ON e displays the flight direction steering indications on the second PFD e flight with the autopilot disengaged and both flight director switches OFF the first flight director switch positioned to ON engages the flight director in default modes e Vertical speed V S or flight path angle FPA as the pitch mode e Attitude hold heading or track hold HDG TRK HLD a
60. eed 1 Takeoff Reference Speeds Displays the takeoff reference speeds V1 VR displays R if VR is within 4 knots of V1 or V2 and V2 selected on the CDU Displayed for takeoff NO V SPD is displayed if V speeds are not selected on the CDU V1 is displayed at the top of the airspeed indication when selected and if the value is off the scale V1 and VR are removed at lift off V2 is removed on climb out When flap retraction begins or After 10 minutes have passed without flap lever movement or After VREF has been selected for a turn back 2 Flap Maneuvering Speeds Indicates flap maneuvering speed for flap retraction or extension Not displayed above approximately 20 000 feet altitude 3 Landing Reference Speed Displays the VREF speed as selected on the CDU VREF speed is displayed at the bottom of the airspeed indication when the value is off the scale 4 Minimum Maneuvering Speed Indicates maneuver speed margin to stick shaker or low speed buffet 5 Minimum Speed Indicates the airspeed where stick shaker activates www captainsim com 95 DO NOT USE FOR FLIGHT PFD ALTITUDE INDICATIONS 1 Selected Altitude Bug 2 Selected Altitude Meters 1550 2 3 Selected Altitude 5100 3 4 Current Altitude Meters 5 Current Altitude 5200 600 D E 5000 2 1463 4 4 8004 4600 2 4400 L 29 88 IN 1 Selected Altitude Bug Indicates the altitude set in the MCP a
61. eft inboard outboard and upper center displays and the left CDU are powered OFF turns battery power off In flight the EICAS message ELEC BATTERY OFF displays 2 Battery OFF Light Illuminated amber The battery switch is OFF 3 APU Generator APU GEN Switch ON Arms APU generator breaker to automatically close OFF Opens APU generator breaker 4 APU Generator OFF Light Illuminated with the APU running amber The APU generator breaker is open because of a fault or APU GENERATOR switch is selected OFF 5 BUS TIE Switches AUTO Arms automatic AC bus tie circuits ISLN isolation AUTO not visible Commands the bus tie open 1 WWW Captainsim com 39 DO NOT USE FOR FLIGHT 6 Bus Isolation ISLN Lights Illuminated amber Bustie breaker is locked open ISLN selected with bus tie switch or e A fault has occurred automatically opening the bus tie breaker 7 Generator Control GEN CTRL Switches ON Arms the generator breaker to close automatically when generator power is available OFF e Opens field and generator breakers Resets fault trip circuitry 8 Generator OFF Lights Illuminated amber The generator breaker is open 9 Drive Disconnect Switches Push Disconnects the integrated drive generator IDG input from the engine e Requires maintenance action on the ground to reconnect the IDG 10 Generator DRIVE Lights Illuminated amber IDG oil pressu
62. eporting ALTN alternate selects SAARU as source for transponder altitude reporting 3 Transponder Code Selectors Rotate Sets transponder code in transponder 4 Transponder Code Window Shows transponder code Shows operating transponder L or R 5 Transponder Mode Selector STBY standby does not transmit ALT RPTG altitude reporting OFF transponder operates without altitude reporting XPNDR transponder activates transponder with altitude reporting when airplane is in flight TA ONLY Allows the display of traffic advisory TA targets TA RA Allows the display of traffic advisory TA targets and resolution advisory RA targets with resolution advisory aurals and PFD vertical guidance pitch command and vertical speed command 6 Test Switch The test switch allows you to perform a TCAS test The test results are shown on the NDs 7 Absolute Relative ABS REL Altitude Selector Note The left selector controls the left TCAS display the right selector controls the right TCAS display ABS absolute Displays absolute altitude on the TCAS traffic display REL relative Displays relative altitude relative to own aircraft on the TCAS traffic display 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 118 DO NOT USE FOR FLIGHT 8 TCAS Airspace Selector Note The left selector controls the left TCAS display the right selector controls the right TCAS displa
63. er door open blank passenger door closed O white door status is not available n amber cargo access door open blank cargo access door closed n white door status is not available The doors synoptic is displayed by pushing the DOOR synoptic display switch on the display select panel AEN 2014 Captain S m www captainsim com 88 DO NOT USE FOR FLIGHT ELECTRICAL SYNOPTIC DISPLAY 010 L BUS TIE RBUSTIE L MAIN L UTIL RxFR L GEN Ros X CTRL CTRL pow E L N BACKUP L DRIVE L GEN R DRIVE MAIN BAT VOLTS 2B VOLTS 27 AMPS 13 CHG AMPS 13 CHG MULTIFUNCTION DISPLAY CHG battery charging Drive disconnected Mot supplyin CTRL control engine running power i failed 2 amber amber DRIVE oil pressure low On or available m amber green green Power not flowin Off white white The electrical synoptic is displayed by pushing the ELEC synoptic display switch on the display select panel www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 89 DO NOT USE FOR FLIGHT G03 G06 EFIS CONTROL PANELS The left EFIS control panel controls the left PFD and ND The right EFIS control panel controls the right PFD and ND EFIS CONTROL PANEL PFD CONTROLS Minimums MINS Reference Selector outer Minimums MINS Selector middle Minimums Reset MINS RST Switch inner
64. ertical Speed 1 Vertical Speed Pointer Indicates current vertical speed 2 Selected Vertical Speed Bug Indicates the speed selected in the MCP vertical speed window with the V S pitch mode engaged 3 Vertical Speed Displays vertical speed when greater than 400 feet per minute The display is located above the vertical speed indication when climbing and below when descending PFD ATTITUDE INDICATIONS Bank Pointer Slip Skid Indication Pitch Limit Indication Horizon Line and Pitch Scale Bank Scale Airplane Symbol Q N 1 Bank Pointer Indicates ADIRS bank in reference to the bank scale Fills and turns amber if bank angle is 35 degrees or more 2 Slip Skid Indication Displaces beneath the bank pointer to indicate slip or skid Fills white at full scale deflection Turns amber if bank angle is 35 degrees or more fills amber if the slip skid indication is also at full deflection www captainsim com 98 DO NOT USE FOR FLIGHT 3 Pitch Limit Indication Indicates pitch limit stick shaker activation point for the existing flight conditions Displayed when the flaps are not up or at slow speeds with the flaps up 4 Horizon Line and Pitch Scale Indicates the ADIRS horizon relative to the airplane symbol Pitch scale is in 2 5 degree increments 5 Bank Scale Fixed reference for the bank pointer Scale marks are at 0 10 20 30 45 and 60 degrees 6 Airplane Symbol I
65. fg atc flight numberz 21 Current FSX date 22 Aircraft type loads from aircraft cfg ui typez 23 User customizable logo located FSX NCaptain Sim EFB 24 Current FSX time 25 Current EFB version 26 Aircraft engine type loads from aircraft cfg engine typez www captainsim com and Systems 74 ect Captain FLIGHT MANUAL Part II Aircraf SPLIT MODE While in the Main Menu if you click any function key the EFB will open the selected function box folder in the Split Mode 27 28 29 30 31 3233 34 Approach UUDD 14L Fam nm Sere MOSCOW RUSSIA ame EL 15 2 Rwy 141 Ss fem CUNT 114 1 BS PLS ITIS TES HOE THD FIEL Han 00 FECE OALTCOHEIDST DEHA N zug Mat qnaa nem afr Bisa ee Fac GOA rat dees LOM es ae ARAM zit Dd CYCLE VIEW 27 Return to the Main Menu 28 Function box folder name 29 Page Up key Cycle the folder content up 30 Runway index see content files naming section 31 Page Down key Cycle the folder content down 32 Airport ICAO code see content files naming section 33 Current fine number total number of files in the selected folder 34 ENTER key Resizes the selected image fullscreen 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 75 DO NOT USE FOR FLIGHT 35 Cycle the folder content 36
66. gain For certain conditions resets are required to prepare the checklist for the next phase of flight There are automatic resets and manual resets CHECKLIST OVERRIDE Entire checklists can be overridden By pressing the CHKL OVRD key the displayed checklist turns to cyan indicating that it is overridden The message CHECKLIST OVERRIDDEN is displayed at the bottom of the page Normal checklist sequence is then resumed This allows for rapid skipping of checklists All associated operational notes and deferred line items are removed from their respective target areas and conditional statements within a checklist are overridden ITEM OVERRIDE Item override is used by the flight crew when an item in a checklist will not be accomplished or an item has been accomplished but the closed loop sensing is not functioning correctly Overridding an item when required allows the checklist to be completed The line item override function is available on all checklists Selection of the ITEM OVRD key turns the highlighted step to cyan indicating the step is not applicable and has been overridden Both closed loop and open loop steps can be overridden Conditional statements both closed and open loop cannot be overridden Individual steps within conditional statements can be overridden www captainsim com n FLIGHT MANUAL Part II Aircraft and Systems 80 DO NOT USE FOR FLIGHT NORMAL CHECKLISTS Normal electronic checklist use follows the sa
67. hart Setup Test pattern image Whatever Four movie posters Cameras Exterior cameras still image 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems DO NOT USE FOR FLIGHT 76 USERS CUSTOMIZATION USER CUSTOMIZABLE FUNCTION KEYS AND BOXES To make changes in the function keys boxes default setup 1 Open FSX NCaptain Sim EFB cs_efb xml file with any text editor All you need is the modes section s Notepad mode id 1 name path AIRCRAFT DIRXEFB N gt 1 function key number from 1 to 15 DO NOT use 0 and 8 2 function box name Whatever you want Any reasonable length 3 folder name you wish to use with the key e Thefolder name must match the key name e The folder must be created in FSX SimObjects Airplanes CS_B777 200 EFB Copy to the folder unlimited number of files in bmp jpg jpeg gif png tif ico formats Repeat for other keys folders you wish to edit Done CONTENT FILES NAMING For airport specific content four fist characters of the image file name must be the airport ICAO code Approach UUDD 14L Roeepezan MOSCOW RUSSIA a 31 1 DII ILS or 2 NUB Rw HAPI FUN 8 114 7 014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 77 DO USE FOR FLIGHT ELECTRONIC CHECKLIST ECL NORMAL MENU
68. he CDU LEGS pages ND SYMBOLOGY The following symbols can be displayed on each ND depending on EFIS control panel switch selections Colors indicate the following e W white Present status range scales G green Dynamic conditions M magenta or pink Command information pointers symbols fly to condition B blue or cyan Non active or background information A amber or yellow Cautions faults flags R red Warnings 2014 Captain Sim www captainsim com GENERAL 64 DO NOT USE FOR FLIGHT TRK 082 MAG HDG 263 MAG V GRID Track up ND Track orientation G current track W and track reference G Heading up ND Heading orientation G current heading W heading reference G and heading W Grid heading W Selected heading bug M Selected track bug M Track line and range scale W Heading track reference G box W in TRU box A if TRU displayed in descent Expanded compass W Current heading pointer W Shows track in MAP MAP CTR Shows HDG heading in VOR VOR CTR APP APP CTR All except PLAN All except PLAN MAP MAP CTR VOR VOR CTR APP APP CTR All except PLAN MAP APP VOR MAP MAP CTR Displays TRK as the orientation the current track and MAG or TRU as the reference and points to the heading on the compass rose Displays HDG as the display orientation current heading MAG or TRU as the
69. he maximum regardless of airspeed Heading Track Selector middle Rotate Sets heading or track in the heading track window and on the PFDs and NDs Heading Track Select SEL Switch inner Push Selects heading select HDG SEL or track select TRK SEL as the roll mode Displays HDG SEL or TRK SEL on the PFD roll flight mode annunciator The AFDS controls roll to fly the selected heading or track Bank is limited by the bank limit selector 18 Heading Track Hold HOLD Switch Autopilot heading hold on off Push e Selects heading hold HDG HOLD or track hold TRK HOLD as the roll mode e Displays HDG HOLD or TRK HOLD on the PFD roll flight mode annunciator e he AFDS commands wings level and holds the heading or track established when wings level is established 19 V S FPA Selector VSI bug select UP or DOWN Sets the vertical speed or flight path angle in the vertical speed flight path angle window and on the PFDs 20 V S FPA Switch Light Autopilot vertical speed hold on off V S FPA Switch Push Engages Vertical Speed V S or Flight Path Angle FPA as the pitch mode Displays V S or FPA on the PFD pitch flight mode annunciator Displays the current vertical speed or flight path angle in the vertical speed flight path angle window When the selected altitude is reached the pitch mode changes to altitude ALT AFDS commands pitch to maintain the vertical speed or flight path angle di
70. he respective transmitter radio or intercommunications for transmission from this crew station only one can be selected at a time for each crew station e Selects the receiver audio on if not already manually selected on e Pushing the CAB transmitter select switch twice within one second places a priority call to Door 1 Left Second push Deselects the transmitter Deselects receiver audio MIC Lights Illuminated Indicates the transmitter is selected CALL Lights Illuminated e Resets when the respective transmitter select switch is pushed or if already pushed by pressing a MIC INTERPHONE switch e Resets when the respective transmitter select switch is pushed or if already pushed by pressing a MIC INTERPHONE switch the SATCOM CALL light remains illuminated until the call ends e PA does not have a CALL light 2 MIC Interphone Switch MIC Keys the boom microphone or oxygen mask on the selected radio transmitter or other system Center Off position spring loaded to center INT Keys the boom microphone or oxygen mask on the flight interphone 3 VOR ADF Receiver Selector Selects the VOR or ADF receiver to be monitored VOR L Left VOR VOR R Right VOR ADF L Left ADF ADF R Right ADF 4 Receiver Lights Illuminated Indicates the respective receiver volume control is manually selected on www captainsim com 36 DO NOT USE FOR FLIGHT 5 Receiver Volume Controls Push Turns the respectiv
71. he standby airspeed bug Push inner Turns the standby airspeed display bug off and on Standby Altitude Indicator 7 Altimeter Pressure Set 8 Altimeter STD Pressure Button 1 WWW Ccaptainsim com 106 DO NOT USE FOR FLIGHT Rotate outer Adjusts the altimeter barometric reference Push inner Switches between standard and the last selected barometric reference 02 04 CLOCK Chronograph CHR or CLOCK Switch Chronograph Pointer Elapsed Time ET Selector Time Date Selector Time Date Window Elapsed Time ET Chronograph CHR Window Clock Set Selector Q N FORWARD PANELS 1 Chronograph CHR or CLOCK Switch Push Subsequent pushing starts stops resets the chronograph 2 Chronograph Pointer Indicates chronograph seconds 3 Elapsed Time ET Selector Controls the elapsed time function RESET Blanks ET display spring loaded to HLD HLD hold Stops the elapsed time display RUN Starts the elapsed time display 4 Date Selector MAN Manual The clock is manually set to a time and date UTC The clock is automatically set to the UTC date and time Push e Alternately displays the day month then year in the time date window e Subsequent selection displays only the time in the time date window 5 Time Date Window Displays time hours minutes when time is selected on the time date selector Alternately displays day month and year w
72. heading reference and points to the heading on the compass rose Displays above 70 degrees latitude Displays the MCP selected heading A dashed line M may extend from the marker to the airplane symbol In the MAP mode with LNAV LOC or ROLLOUT engaged the dashed line is removed 10 seconds after the selected heading bug is moved Displays the MCP selected track A dashed line M may extend from the marker to the airplane symbol Indicates current track Number indicates half the range VOR CTR and APP CTR do not display range Indicates heading track is referenced to magnetic north or true north Switching from TRU to MAG displays a box around MAG for 10 seconds Displays 90 degrees of compass rose Points to current heading on the compass rose www captainsim com 65 DO NOT USE FOR FLIGHT TAS312 x Current true airspeed displayed above 100 knots All Wind direction speed and wind arrow W 3207 15 RADIO NAVIGATION VOR L R ILS L C R 116 80 OR SEA ILS W VOR W Reference receiver frequency or identifier display Wasi Reference receiver VOR VOR CTR G APP APP CTR VOR VOR CTR APP APP CTR DME distance W VOR VOR CTR APP APP CTR VOR VOR CTR VOR course W APP APP CTR Left VOR G or ADF B pointer head and tail 14 A A All except PLAN Right VOR G or ADF B pointer head and tail ILS localizer or VOR course deviation
73. hen date is selected on the time date selector 6 Elapsed Time ET Chronograph CHR Window Displays elapsed time hours minutes or chronograph minutes The chronograph display replaces the elapsed time display Elapsed time continues to run in the background and will be displayed after the chronograph is reset 7 Clock Set Selector Sets the time and date when the time date selector is set to manual HD Hours Day e Advances hours when time is selected on the time date selector e Advances days when date is selected on the time date selector www captainsim com 107 DO NOT USE FOR FLIGHT MM Minutes Month Advances minutes when time is selected on the time date selector Advances months when date is selected on the time date selector HLDY Hold Year Stops the time indicator and sets the seconds to zero when time is selected on the time date selector Advances years when date is selected the time date selector RUN Starts the time indicator www captainsim com 108 DO NOT USE FOR FLIGHT FLIGHT MANAGEMENT NAVIGATION RO5 FMC SELECTOR FMC AUTO www captainsim com L selects left FMC to provide guidance commands AUTO automatically selects other FMC if one FMC fails R selects right FMC to provide guidance commands 109 DO NOT USE FOR FLIGHT FUEL O12 FUEL SYSTEM Fuel Pump Switches Forward and Aft Fuel Pump Pressure PRESS Lights Center Fuel Pump Pres
74. how that the traffic is climbing or descending no arrow indicates altitude of traffic in hundreds of feet relative to airplane position For absolute altitude symbols the numerics show altitude of traffic in hundreds and thousands of feet Relative versus absolute altitude display is selected by a switch on the TCAS control panel for both relative and absolute altitude the numeric shows below the traffic symbol when the traffic is below the airplane and above the traffic symbol when the traffic is above the airplane no numerics in both cases show altitude is unknown TCAS data shows when traffic TFC is selected on the EFIS CP TRAFFIC TCAS traffic alert Shows TCAS RA or TA is message active with or without the RA R TA A OFFSCALE TCAS offscale message TFC switch selected Shows RA or TA traffic is outside the traffic RA R TA A MAP MAP CTR area of the ND range TFC APP VOR switch needs to be on TCAS mode B Shows traffic mode is on TA ONLY Shows when TCAS computer is not computing RAS TCAS TEST B nes TCAS computer is operating in the test mode TFC is on EFIS CP TCAS OFF Shows a TCAS condition exists when TFC is on from the EFIS CP MAP MAP CTR TCAS FAIL APP VOR Shows a fault is present in TCAS data when TFC is on from the EFIS CP www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 71 DO NOT USE FOR FLIGHT ELECTRONIC FLIGHT The Electron
75. ic Flight Bag EFB is a major step toward e enabling the air transport system Through its integrated applications the EFB brings a new level of digital information delivery and management to the flight deck That results in flight operations cost savings improved safety and enhanced document accessibility and configuration control Captain Sim EFB is flexible and easily customizable application which can be loaded with unlimited data in bmp jpg jpeg gif png tif ico formats Two independently controlled EFBs are installed on the Captain s and F O s side shelves For better usability 2D version is also included It is synchronized with Captain s EFB 2014 Captain Sim www captainsim com MENU 4i Captain Sim 1 Enroute 2 SID 3 4 9 Approach 5 J Airport 6 7 0 15 User customizable function keys 16 Brightness control switch 17 Power ON OFF button 18 Index menu 19 User customizable function boxes Other buttons are INOP in the Main Menu mode www captainsim com setup Whatever Cameras e i MA TE a 6 1 4 1 M 1 Ri bea 4 1 el A J 1 l c T 72 11 12 13 14 15 73 DO NOT USE FOR FLIGHT INDEX MENU DETAILS 23 24 25 26 20 Flight number loads from aircraft c
76. inboard display unit regardless of the position of the inboard display selector Upper center display unit failure automatically switches the EICAS display to the lower center display unit A 2014 Captain Sim www captainsim com 57 DO NOT USE FOR FLIGHT subsequent EICAS selection on either of the inboard display selectors brings the EICAS display to that inboard display unit and assuming no latched condition exists the lower center display unit initially displays secondary engine instruments Following this initial display configuration the lower center display unit can be used in its usual MFD mode DISPLAY SELECT PANEL The display select panel controls the MFD format on the left and right inboard display units and the lower center display unit The selected display is indicated by the illuminated annunciator light on the display select panel L INBD R INBD LWR CTR After a display unit is selected the appropriate display is selected ENG STAT ELEC HYD FUEL AIR DOOR GEAR FCTL CHKL COMM or NAV A new display selection automatically replaces the previous one A second selection of the same display for the lower center display unit blanks the display A second selection of the same display on either inboard display causes display of the ND If there is more than one page of status messages pushing STAT pages through the messages When used as an MFD the lower center display unit and the two inboard display units can displ
77. indication M and scale W VOR VOR CTR APP APP CTR Selected course pointer W and line M VOR VOR CTR APP APP CTR www captainsim com Indicates wind bearing speed and direction with respect to display orientation and heading track reference Arrow not displayed in the PLAN map mode Indicates the selected receiver as the display reference Frequency displayed before the identifier is decoded The decoded identifier replaces the frequency Medium size characters for VOR small size characters for DME only Indicates DME distance to the reference navaid Indicates the VOR course or ILS localizer course Indicates bearing to head or from tail the tuned station if selected on the respective EFIS control panel Displays LOC or VOR course deviation Deviation indicator points in direction of VOR or ILS selected course For ILS deviation indicator fills M when less than 2 1 2 dots from center Displays CDU selected course 66 DO NOT USE FOR FLIGHT Glide slope pointer APP APP CTR Displays glideslope position and M and scale W deviation Deviation indicator fills M when less than 2 1 2 dots from center To from indication VOR CTR Located near airplane symbol W Displays VOR TO FROM indication _ Displays VOR to from indication indication VOR VOR CTR VOR B G MAP MAP CTR When the EFIS control panel DME TACAN B G STA map switch is selected on VORT
78. ine Select Keys Push moves data from scratchpad to selected line moves data from selected line to scratchpad selects page procedure or performance mode as applicable deletes data from selected line when DELETE is shown in scratchpad Conventions e Scratchpad must be blank for line select transfer e data cannot be transferred to a blank line e a blank scratchpad cannot be transferred to a line not all data can be modified e message displays if inappropriate entries attempted www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 33 DO NOT USE FOR FLIGHT CDU KEYBOARD CONTROL All CDU keys can be controlled using a keyboard To activate CDU keyboard control press Ctrl Shift K To deactivate CDU keyboard control press Note if activated the CDU keyboard control temporarily overrides those FSX management keys listed below ry kawan E 2 a D Wl T f 2 4 A Th i 4 jk jk Bh s rs LE EE EE LEE LEE LE s amp 8 amp T 2 F T 21 mW i Th i t B E RE nd Eme Aue env poe Eme ees novo got eros _ xe mmm mf mf maa mm mm mm s al I TES l ss LJEJEJEDIEJEUJUII IN 50 5 9 P 3
79. ine Vibration High Band Displayed white Vibration level at which automatic display of secondary engine indications occurs 3 Vibration Source Identifies the vibration source being displayed Displayed white Vibration source with the highest vibration N1 rotor vibration N2 rotor vibration If the vibration source BB broad band vibration is displayed the source is unknown and average vibration is displayed www captainsim com 46 DO NOT USE FOR FLIGHT 4 Engine Vibration Pointer Displayed white Engine vibration COMPACT ENGINE INDICATIONS TAT iu a CRZ 1 Compact Engine Indications 2 Crossbleed Start Indication NAT 81 5 8 0 3 1 FF 0 0 120 55 20 gt gt 120 TEMP 105 15 onaty 2 BB 1 2 VIF 1 0 Ne 1 Compact Engine Indications The following changes to EICAS and the normal secondary engine display occur N2 changes from round dial displays to a digital display An amber or red box frames the digital display if limits are exceeded FF OIL PRESS OIL TEMP are displayed as digital readouts only The digital displays turn amber or red if limits are exceeded e OIL QTY and VIB are displayed as digital readouts only Low oil quantity and high vibrations are displayed the same as in the normal format 2 Crossbleed Start Indication Displayed magenta www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft an
80. ing descent automatically changes from MACH to IAS at 310 KIAS IAS MACH Reference Switch Ctri M Push e Alternately changes the IAS MACH window between IAS and MACH displays MACH must be 0 4 or greater to switch from IAS to MACH Inoperative when the IAS MACH window is blank 5 Lateral Navigation LNAV Switch Autopilot NAV1 Hold default key Ctri N Push e Arms disarms or engages LNAV as the roll mode Displays LNAV in white armed on the PFD roll flight mode annunciator when armed The previous roll mode remains active e LNAV engages if the airplane is above 50 feet radio altitude and e Within 2 5 NM of the active leg e If not within 2 5 NM of the active leg and on an intercept heading to the active leg remains armed then engages when approaching the active leg e When engaged displays LNAV in green the PFD roll flight mode annunciator e Selection of LNAV when an active FMC route is not available displays NO ACTIVE ROUTE in the CDU scratchpad LNAV maintains current heading when Passing the last active route waypoint Passing the last waypoint prior to a route discontinuity Passing the last route offset waypoint Activating the inactive route or activating an airway intercept and not within LNAV engagement criteria LNAV green is disengaged By selecting heading hold HDG HOLD or track hold TRK HOLD By selecting heading select HDG SEL or track select TRK SEL When the localizer captu
81. lt J loj z eJ m 5 K bl le m E e elo CDU FUNCTION KEYS Ctri I INIT REF Ctrl R RTE Ctrl D DEP APR Ctri A ALTN Ctrl V VNAV Ctrl F FIX Ctri L LEGS Ctrl H HOLD Ctrl C FMC COMM Ctrl P PROG Ctrl M MENU Ctri N NAV RAD Ctri E EXEC 2014 Captain Sim www captainsim com 34 DO NOT USE FOR FLIGHT PO9 TO GA AND AUTOTHROTTLE DISCONNECT SWITCHES 1 Takeoff Go Around TO GA Switches 2 Autothrottle Disconnect Switches 1 Takeoff Go Around TO GA Switches default key Ctrl Shift When is armed On the ground autothrottles armed and leading edge slats extended First push either switch below 50 knots engages the autothrottle in THR REF mode e The autothrottle will not engage between 50 knots and 400 feet AGL Pushing either switch above 80 knots disarms LNAV and VNAV 2 Autothrottle Disconnect Switches Push either switch e Disconnects the autothrottle both left and right www captainsim com 35 DO NOT USE FOR FLIGHT COMMUINICATIONS SYSTEM 1 Transmitter Select Switches MIC Lights CALL Lights 2 MIC Interphone Switch 3 VOR ADF Receiver Selector 4 Receiver Lights 5 Receiver Volume Controls 6 Approach APR Receiver Selector 1 Transmitter Select Switches MIC Lights CALL Lights Transmitter Select Switches Push e The MIC light illuminates e The MIC light for any other transmitter extinguishes e Selects t
82. lt key Ctrl O The localizer mode can be disengaged after localizer capture by e Selecting another roll mode Pushing TO GA switch Disengaging the autopilot and turning both flight director switches off or Pushing the localizer switch a second time above 1 500 feet radio altitude reverts to the default roll mode The localizer mode can be disengaged after localizer capture by e Selecting another roll mode e Pushing a switch Disengaging the autopilot and turning both flight director switches off or Pushing the localizer switch a second time above 1 500 feet radio altitude reverts to the default roll mode 24 Approach APP Switch Autopilot approach mode on off default key Ctrl A Push Arms disarms engages or disengages localizer LOC as the roll mode and glideslope G S as the pitch mode Displays LOC and G S in white armed on the PFD roll and pitch flight mode annunciators prior to localizer and glideslope capture Displays LOC and G S in green engaged on the PFD roll and pitch flight mode annunciators after each one is captured The AFDS captures and tracks the localizer in the localizer LOC mode and captures the glideslope in the glideslope G S mode upon interception glideslope capture is inhibited until the localizer is captured Localizer captures when the intercept track angle is within 120 degrees of the localizer course Glideslope captures when the intercep
83. ltitude window When the selected altitude is off scale the bug is parked at the top or bottom of the tape with only one half the bug visible 2 Selected Altitude Meters Displayed when MTRS is selected on the EFIS control panel MTRS switch Indicates selected altitude in meters selected in feet in the MCP altitude window Displays in 10 meter increments 3 Selected Altitude Displays the altitude set in the MCP altitude window The selected altitude box is highlighted in white between 900 feet and 200 feet prior to reaching the selected altitude 4 Current Altitude Meters Displayed when MTRS is selected on the EFIS control panel MTRS switch Displays altitude in meters 5 Current Altitude Indicates current ADIRS altitude www captainsim com 96 DO NOT USE FOR FLIGHT PFD BAROMETRIC INDICATIONS 1 Barometric Setting 2 Barometric Reference 3 QFE Altitude Reference rh 4 Autopilot Flight Director Barometric Source lt 4800 lt 24800 5 Preselected Barometric Setting Ne uA 6 QFE o 24600 e 18 600 600 fa VU 24400 2986 QFE 4 STD 5 gt 29 86 INQFE 1 Barometric Setting Indicates the barometric setting selected on the EFIS control panel barometric selector STD is displayed when STD is selected on the EFIS control panel barometric STD switch The display is boxed and changes to amber if a barometric setting is set and altitude climbs
84. me philosophy as used with paper checklists The normal procedures are done from memory then the checklist is read to confirm the actions NORMAL CHECKLIST MENU Normal checklists are arranged in the menu by phase of flight If a normal checklist is selected out of sequence the original normal sequence can be resumed using the NORMAL MENU key or the checklist display switch NORMAL CHECKLIST ACCESS Normal checklist selection sequence follows progressive phases of flight Phases of flight are distinguished by completion of the previous phase checklist and not by air ground logic The checklist is automatically reset after completing the last checklist at power down or following a manual reset of all normal checklists The checklist order is BEFORE START BEFORE PUSHBACK BEFORE TAKEOFF AFTER TAKEOFF APPROACH DESCENT FINAL DESCENT PARKING As each normal checklist is completed the next unfinished normal checklist is displayed Any normal checklist can be accessed using the NORMAL MENU NORMAL CHECKLIST COMPLETING OR LEAVING At the completion of each checklist all steps are complete or overridden the appropriate message appears at the bottom of the page e CHECKLIST COMPLETE white text on green background e CHECKLIST OVERRIDDEN white text on cyan background After the checklist is complete but still displayed a change to the position of a closed loop sensed switch results in the checklist no longer showing CHECKLIST
85. ms Reference Displays BARO when the EFIS control panel MINS reference selector is set to BARO Displays RADIO when the EFIS control panel MINS reference selector is set to RADIO no corresponding pointer or line on the altitude scale Turns amber and flashes for 3 seconds when the airplane descends below selected minimum altitude 4 Minimums Displays the approach minimums altitude set using the EFIS control panel MINS selector BARO minimums are feet MSL RADIO minimums are radio altitude feet AGL Turns amber and flashes for 3 seconds when the airplane descends below selected minimum altitude 5 Landing Altitude Reference Bar Indicates the height above touchdown White bar 500 to 1000 feet above landing altitude Amber bar 0 to 500 feet above landing altitude www captainsim com 101 DO NOT USE FOR FLIGHT PFD EXPANDED LOCALIZER INDICATIONS 1 Expanded Localizer Scale Displays when the autopilot or flight director is in LOC mode and the airplane is close to the runway 177 9 center line Provides more sensitive display A rectangle equals 1 2 dot deviation PFD RISING RUNWAY INDICATIONS 1 Rising Runway Displayed below 2500 feet radio altitude when the localizer pointer is in view for both front and back courses Moves toward the airplane symbol below 200 feet radio altitude The stem of the rising runway symbol flashes when localizer deviations cause the diamond to flash PFD HEADING TRACK IN
86. ndicates airplane attitude with reference to the ADIRS horizon PFD RADIO ALTITUDE INDICATIONS 1 Radio Altitude Displays radio altitude below 2500 feet AGL The display box is highlighted in white for 10 seconds when passing below 2500 feet Turns amber when below radio altitude minimums www captainsim com 99 DO NOT USE FOR FLIGHT PFD INSTRUMENT LANDING SYSTEM INDICATIONS 130 1 Approach Reference V 3 4 2 Localizer Pointer and Scale 3 Marker Beacon Indication 4 Glideslope Pointer and Scale 1 Approach Reference Displays the selected ILS identifier or frequency approach front course and ILS DME distance If the tuned ILS frequencies disagree the frequency turns amber with an amber horizontal line through it If the approach courses in the ILS receivers disagree the course turns amber with an amber horizontal line through it 2 Localizer Pointer and Scale The localizer pointer e Indicates localizer position relative to the airplane e Is in view when the localizer signal is received e Fills in solid when within 2 1 2 dots from the center The scale is in view after the frequency is tuned At low radio altitudes with the autopilot or flight director engaged the scale turns amber and the pointer flashes to indicate excessive localizer deviation At low altitudes with LNAV engaged and LOC armed the localizer scale turns amber and the pointer flashes if the localizer is not captured 3 M
87. ng ND display e If there is ND display on one inboard display unit and on the lower center display unit then the pilot who does not have an ND on the inboard display unit controls the ND on the lower center display unit e If neither pilot has ND display on the inboard display unit and there is ND display on the lower center display unit then the left EFIS control panel controls the lower center display unit e If both pilots have an ND display on the inboard display unit and there is ND on the lower center display unit then the left EFIS control panel controls the left inboard display unit and the lower center display unit The ND on the left inboard and the lower center display units are identical When an inboard display selector is in the ND or PFD position new displays selected from the display select panel to that inboard display are inhibited The annunciator light above the associated display select panel switch is also inhibited When an inboard display selector is in the EICAS position only the ENG AIR and FUEL switches can affect the display Pushing one of those switches causes the display of the respective compacted blocks of information on the EICAS display The cancel recall switch operates normally Refer to these chapters for more information on compact EICAS displays The inboard display selectors have no effect on the inboard displays if an outboard display unit fails the PFD automatically moves to the
88. ode Expanded MAP mode Centered MAP mode If the mode selector is not in a correct mode when you push the TERR map switch the terrain display arms When armed the terrain display shows as soon as you change the ND selector to a correct mode The terrain display stays armed even if you push the TERR map switch again Push the WXR map switch to disarm the terrain display and arm the weather display 5 ND Range Selector outer The EFIS control panel has a 7 position range selector The range selections are 10 20 40 80 160 320 and 640 NM The terrain awareness display on the NDs uses dots to show terrain ahead of the airplane Dot color and dot pattern density compare terrain altitude with airplane altitude These are the dot colors and patterns the terrain display uses red Terrain more than 2 000 feet above airplane altitude yellow Terrain 500 feet below to 2 000 feet above airplane altitude Gear down changes the 500 feet to 250 feet green Terrain 500 feet below to 2 000 feet below airplane altitude Gear down changes the 500 feet to 250 feet Black Terrain more than 2 000 feet below airplane altitude Magenta Unknown terrain 6 ND Traffic TFC Switch inner Push displays TCAS ND information DISPLAY BRIGHTNESS CONTROLS P04 CENTER PANEL BRIGHTNESS CONTROLS CTR PHL BRIGHTNESS 1 Upper Display UPR DSPL Brightness Control LAR DSPL 2 Lower Display LWR DSPL Brightness Control UPRDSPL
89. ol module is automatically shut off CUTOUT shuts off the respective center or right hydraulic system power to the related stabilizer trim control module AILERON AND RUDDER TRIM CONTROLS 26 RUDDER CONTROLS 1 AILERON TRIM Indicator 2 RUDDER TRIM Indicator 3 AILERON Trim Switches 4 RUDDER Trim Selector 5 MANUAL TRIM CANCEL Switch RJGOER TRIB 1 AILERON TRIM Indicator Indicates units of aileron trim 2 RUDDER TRIM Indicator Indicates units of rudder trim 3 AILERON Trim Switches Push both switches Moves the control wheel ailerons flaperons and spoilers in the desired direction spring loaded to neutral 4 RUDDER Trim Selector Spring loaded to neutral 2014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 54 DO NOT USE FOR FLIGHT Rotate e Trims the rudder in the desired direction e The trim runs at high speed with the knob rotated past the first left or right detent The rudder pedals move with rudder trim operation 5 MANUAL TRIM CANCEL Switch Push Cancels manual rudder at high rate RUDDER BRAKE PEDALS 1 Rudder Pedals Push Deflects the rudder in the desired direction FLAP SYSTEM P10 P15 FLAP CONTROLS 1 Flap Lever 2 Flap Gates 3 Alternate Flaps Arm ALTN FLAPS ARM Switch 4 Alternate Flaps Selector 1 Flap Lever Primary mode Positions the slats and flaps hydr
90. pleted line items appear as green text with a green check mark to the left Overridden and inactive line items are displayed in cyan CHECKLIST OPEN LOOP AND CLOSED LOOP STEPS Open loop not sensed steps are checklist steps that require crew confirmation Open loop steps display a gray box open loop indicator in the left margin The CCD cursor select switch is used to confirm completed open loop steps When the cursor is positioned within the current line item box or open loop indicator and the CCD cursor select switch is pressed the checklist line item text color changes from white to green and a green check mark is displayed on the open loop indicator Closed loop sensed steps are checklist steps that can automatically be completed by system inputs Closed loop steps display check marks with no gray boxes CHECKLIST PAGES The checklist is displayed on one or more pages Page keys are located on the right side of each checklist containing more than one page Page keys are not shown on checklists containing only one page When a checklist is complete the cursor automatically moves to the NORMAL checklist key in the lower left corner of the display Pressing the cursor select switch causes the next appropriate checklist to appear When a checklist has more than one page and the checklist steps on the current page are complete the cursor automatically moves to the checklist page key corresponding to the next page CONTINUED is displayed on
91. ration of secondary or normal mode operation AUTO e The flight control system operates in the normal mode e System faults automatically cause the system to switch to the secondary or direct modes PITCH AND STABILIZER TRIM SYSTEMS STABILIZER TRIM SYSTEM 1 Alternate ALTN PITCH TRIM Levers 2 Stabilizer STAB Position Indicator 3 Takeoff Trim Green Band 4 Stabilizer STAB Cutout Switches 1 Alternate ALTN PITCH TRIM Levers Spring loaded to the neutral position Push pull both levers e In the normal mode changes trim reference airspeed and moves the stabilizer directly In the secondary and direct modes moves the stabilizer directly 2 Stabilizer STAB Position Indicator Indicates stabilizer position in units of trim 2014 Captain Sim www captainsim com FLIGHT MANUAL Part II Aircraft and Systems 53 DO NOT USE FOR FLIGHT 3 Takeoff Trim Green Band The green band indicates the allowable takeoff trim range based on gross weight takeoff thrust and CG information from the FMC When no information is available the green band defaults to midrange If the stabilizer signal is not present or is invalid the green band and the pointer are not displayed 4 Stabilizer STAB Cutout Switches NORM Hydraulic power is supplied to the related stabilizer trim control module e If unscheduled stabilizer motion is detected center and or right system hydraulic power to the related stabilizer trim contr
92. re is low 11 External Power EXT PWR Switches Push If AVAIL light is illuminated closes external power contactor Subsequent action opens external power contactor ON External power is connected to the bus ses OFF ON not visible External power is disconnected from the bus ses 12 External Power ON Lights Illuminated external power is powering the busses 13 External Power AVAIL Lights Illuminated e External power is plugged in and power quality is acceptable e Extinguishes when the ON light illuminates See Manual Part I for External Power Control details 14 Backup Generator BACKUP GEN Switches ON Backup generator operation is armed OFF e Opens the backup generator control relay e Resets the fault circuitry 15 Backup Generator OFF Lights Illuminated amber e The backup generator has failed or Acircuit fault has been detected or Backup generator switch selected off or e Both OFF lights illuminated backup system converter has failed www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 40 DO NOT USE FOR FLIGHT ENGINES amp APU EICAS DISPLAY GE engine RR ang PW engines PARKING BRAKE SET PARKING BRAKE SET MODE INDICATIONS 3 1 Total Air Temperature TAT 2 Thrust Reference Mode a gt TAT 13c D TO 30c 3 Assumed Temperature REW REV 4 4 4 Thrust Reverser Indication 1 Total Air Temperature TAT Di
93. res If there is a dual FMC failure LNAV white can be disarmed by pushing the LNAV switch a second time or by arming LOC or APP www captainsim com 27 DO NOT USE FOR FLIGHT 6 Heading Track HDG TRK Reference Switch Push Alternately changes the heading track window PFD and ND selected heading track references between heading and track Also changes the PFD roll flight mode annunciator if the HDG or TRK mode is engaged Heading Track Window Heading bug select Displays the selected heading or track The selected heading or track is displayed on the PFD and ND If approach APP or localizer LOC is armed the heading track in the MCP window automatically changes to the selected front course heading at LOC capture Displays 360 degrees when power is first applied 7 Vertical Speed Flight Path Angle V S FPA Window V S FPA Reference Switch Vertical Speed Flight Path Angle V S FPA Window Displays the selected vertical speed in 100 fpm increments or the selected flight path angle in 0 1 degree increments The display range is V S 8000 to 6000 fpm FPA 9 9 to 9 9 degrees Blank when the vertical speed V S or flight path angle FPA pitch mode is not engaged The selected vertical speed is displayed on the PFD vertical speed indication The selected flight path angle is displayed on the PFD attitude indicator V S FPA Reference Switch Push Alternately changes the vertical spe
94. rm 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 Lou Thieblemont 2014 Captain Sim www captainsim com
95. s the roll mode e In flight with the autopilot engaged and both flight director switches OFF the first flight director switch positioned to ON engages the flight director in the currently selected autopilot mode s OFF e The flight director steering indications are not displayed on the PFD e The flight director steering indications are displayed on the PFD if a TO GA switch is pushed when airspeed is greater than 80 knots on takeoff or on a go around with the leading edge slats extended www captainsim com 28 DO NOT USE FOR FLIGHT 11 Climb Continuous CLB CON Thrust Switch On the ground and below 400 feet AGL during takeoff the switch is inoperative Push e With two engines operating changes the engine thrust limit to the FMC selected climb thrust e With only one engine operating changes the thrust limit to maximum continuous CON 12 Autothrottle A T Engage Switch Autothrottle arm default key Shift R Push Above 400 feet AGL with the autothrottle armed engages the appropriate autothrottle mode for the selected AFDS pitch mode or if no pitch mode in the speed SPD mode 13 IAS MACH Selector When not in VNAV the IAS MACH window shows the current target airspeed Turn the IAS MACH selector to change the target airspeed In VNAV the IAS MACH window is normally blank If you push the selector the window unblanks to show the current FMC target airspeed You can then turn the IAS MACH selector to change
96. speed SPD mode For descent Operates in the IDLE HOLD or speed SPD mode VNAV pitch guidance is available with one engine inoperative VNAV green is disengaged e By engaging TO GA FLCH SPD V S FPA or ALT pitch mode e If there is a dual FMC failure VNAV white can be disarmed by e Pushing the VNAV switch a second time or Arming APP 15 Flight Level Change FLCH SPD Switch Push FLCH SPD is displayed on the PFD pitch flight mode annunciator as the pitch mode e If the IAS MACH window is blank the IAS MACH window opens to the FMC target speed if valid If not valid the IAS MACH window opens to the current speed www captainsim com 29 DO NOT USE FOR FLIGHT 16 Autopilot A P Disengage Bar default key Z Pull down e Prevents autopilot engagement Generates EICAS advisory message NO AUTOLAND Disables bank angle protection Exposes the amber and black stripes If an autopilot is engaged It disconnects Displays the EICAS warning message AUTOPILOT DISC Sounds an aural warning Illuminates the master warning lights Lift up e Permits autopilot engagement e Hides the amber and black stripes 17 Bank Limit Selector outer BANK LIMIT Selector outer Rotate Sets the AFDS commanded bank limit when in the heading select HDG SEL or track select TRK SEL roll mode as follows e AUTO Varies between 15 25 degrees depending on TAS 5 10 15 20 or 25 The selected value is t
97. splayed white TAT degrees C 2 Thrust Reference Mode Displayed green Selected FMS thrust reference mode e TO Maximum rated takeoff thrust D TO Assumed temperature derated takeoff thrust CLB Maximum rated climb thrust CLB 1 Derate one climb thrust CLB 2 Derate two climb thrust CON Maximum rated continuous thrust CRZ Maximum rated cruise thrust G A Maximum go around thrust 3 Assumed Temperature Displayed green Selected assumed temperature degrees C for reduced thrust takeoff 4 Thrust Reverser Indication Displayed REV amber Reverser in transit Displayed REV green Reverser fully deployed 2014 Captain www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 41 DO NOT USE FOR FLIGHT N1 INDICATIONS ALL MODES Note When reverse thrust is activated the following indications are not displayed Maximum NI1 line Commanded N1 Reference target N1 Reference N1 N1 Red Line Reference Target N1 Commanded N1 Commanded 1 Sector Maximum 1 Line Reference N1 N1 N1 Indication 1 N1 Red Line Displayed red N1 RPM operating limit 2 Reference Target N1 Displayed green Reference N1 limit Displayed magenta Target FMC commanded N1 when VNAV is engaged and e autothrottle is engaged in THR REF mode or e The autothrottle is not engaged 3 Commanded N1 Displayed white
98. splayed in the vertical speed or flight path angle window e If vertical speed or flight path angle is selected while FLCH or VNAV the autothrottle automatically engages in the speed SPD mode if engaged www captainsim com 30 DO NOT USE FOR FLIGHT V S FPA Light green Illuminated The vertical speed or flight path angle mode is engaged 21 Altitude Selector Rotate Sets the altitude in the altitude window and on the PFD altitude indication display Push e During climb or descent with altitude constraints each push deletes he next waypoint altitude constraint between the airplane altitude and the altitude window e During climb with no altitude constraints and the altitude window set above the FMC cruise altitude the FMC cruise altitude is changed to the altitude window value e During cruise With the altitude window set above or below FMC cruise altitude the FMC cruise altitude resets to the altitude window altitude Within 50 NM of the top of descent T D point with the altitude window set below cruise altitude the airplane initiates the descend now DES NOW feature 22 Altitude Hold Switch Autopilot altitude hold on off default key Ctrl Z Push e Engages altitude ALT as the pitch mode e ALT is displayed on the PFD pitch flight mode annunciator e he AFDS commands pitch to maintain the altitude when the switch was pushed 23 Localizer LOC Switch Autopilot localizer hold on off defau
99. ssure Amber Band Displayed amber Oil pressure caution range OIL TEMPERATURE INDICATIONS 179 1 20 iE 1 Oil Temperature Engine oil temperature 9C displayed White Normal operating range e Amber Caution range reached Red Operating limit reached www captainsim com 1 Oil Pressure 2 Oil Pressure Pointer 3 Oil Pressure Red Line 4 Oil Pressure Amber Band 1 Oil Temperature 2 Oil Temperature Pointer 3 Oil Temperature Red Line 4 Oil Temperature Amber Band 45 DO NOT USE FOR FLIGHT 2 Oil Temperature Pointer Engine oil temperature displayed White Normal operating range e Amber Caution range reached e Red Operating limit reached 3 Oil Temperature Red Line Displayed red Oil temperature operating limit 4 Oil Temperature Amber Band Displayed amber Oil temperature caution range OIL QUANTITY INDICATIONS OL QTY LO 3 1 Oil Quantity 1 Oil Quantity Usable oil quantity quarts Displayed e White Normal quantity Reverses the display to show black numbers on white background Low quantity Note LO Displayed white when quantity is low ENGINE VIBRATION INDICATIONS 1 Engine Vibration 2 Engine Vibration High Band 3 Vibration Source 4 Engine Vibration Pointer 1 Engine Vibration Engine vibration displayed White Normal operating range e Black numbers white background High vibration 2 Eng
100. sure PRESS Lights CROSSFEED Switches Crossfeed VALVE Lights FUEL CROSSFEED T _ FAD gl WN CENTER UMPS 1 Fuel Pump Switches ON The fuel pump is selected ON Off ON not visible The fuel pump is selected off 2 Forward and Aft Fuel Pump Pressure PRESS Lights Illuminated amber Fuel pump output pressure is low 3 Center Fuel Pump Pressure PRESS Lights Illuminated amber e Fuel pump output pressure is low with the pump selected ON e Illumination is inhibited when the center tank fuel pump switch is selected off 4 CROSSFEED Switches On bar visible The crossfeed valve is selected open Off bar not visible The crossfeed valve is selected closed 5 Crossfeed VALVE Lights Illuminated amber The crossfeed valve is not in the selected position www captainsim com 110 DO NOT USE FOR FLIGHT O11 FUEL JETTISON SYSTEM FUEL JETTIECN 1 2 Fuel Jettison NOZZLE Switches Fuel Jettison Nozzle VALVE Lights LONOEZLE Rpm dris 3 FUEL TO REMAIN Selector E kim 4 Fuel Jettison ARM Switch Fuel Jettison FAULT Light 5 FUEL TO REMAIN Selector 1 Fuel Jettison NOZZLE Switches ON e The jettison nozzle valve is selected open in flight e Ifin flight and jettison is armed turns on both main tank jettison pumps and opens both center tank jettison isolation valves Off ON not visible The jettison nozzle valve is selected closed 2 Fuel Je
101. t and Systems 20 DO NOT USE FOR FLIGHT PASSENGER SIGNS AND LIGHTING O08 PASSENGER SIGNS AND LIGHTING DASS SORS 1 Dome Light Control No oa T p 2 Master Switch 3 Glareshield Light Control outer 4 Landing Light Switches 1 DOME Light Control Controls overhead dome light brightness 2 MASTER Switch Shift L A black ring on the side of the inner switch is visible when the switch is out OFF Push ON in FSX panel light is on Push OFF out FSX panel light is off 3 GLARESHIELD Light Control outer Rotate controls glareshield panel light 4 LANDING Light Switches OFF The landing light is not illuminated ON The landing light is illuminated Note The nose gear landing lights cannot illuminate when the nose landing gear is not down and locked 014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 21 DO NOT USE FOR FLIGHT O14 LIGHTING PANEL Beacon Light Switch Navigation NAV Light Switch Wing Light Switch Indicator Lights IND LTS Switch Runway Turnoff Light Switches Taxi Light Switch Strobe Light Switch NO QI Q N RUNWAY TURHNOFF TAXI SIROBE 1 BEACON Light Switch ON the red anti collision beacon lights on the top and bottom of the fuselage operate 2 Navigation NAV Light Switch ON The red green and white navigation position lights are illuminated 3 WING Light S
102. t track angle is within 80 degrees of the localizer course and the localizer is captured e The approach mode can be disarmed before localizer or glideslope capture by selecting APP LOC LNAV or VNAV The approach mode disengages e With localizer captured and glideslope armed by selecting another roll mode including the localizer mode becomes a localizer approach e After localizer and glideslope are captured by engaging the TO GA mode www captainsim com 31 DO NOT USE FOR FLIGHT Disengaging the autopilot and turning both flight director switches OFF After localizer and or glideslope are captured by pushing the approach switch a second time above 1 500 feet radio altitude AFDS reverts to default pitch and roll modes PO1 PO3 CDU GED 0 9 Numeric Keys 11 40 Alpha Keys 41 42 Ll 51 64 Mode and Function Keys 66 Brightness Control Brightness Contro 67 Execute Key ez 68 FAIL Light 70 OFST Light 71 82 Line Select Keys EIE Lec Rr BEI 124 awm ABe e 9G rn Ej E DT 0 9 Numeric Keys 11 40 Alpha Keys 41 Numeric Key 42 Numeric Key 51 64 CDU Function Keys Push INT REF shows page for data initialization or for reference data RTE shows page to input or change origin destination or route DEP ARR shows page to input or change departure and arrival proce
103. tem 8 Checklist Reset CHKL RESET Key Select resets displayed checklist All open loop line items become incomplete and current line item box cursor selection box and cursor move to first incomplete line item STANDBY FLIGHT INSTRUMENTS CLOCK STANDBY MAGNETIC COMPASS 1 Standby Magnetic Compass 2 Standby Magnetic Compass Correction Card 1 Standby Magnetic Compass Displays magnetic heading 2 Standby Magnetic Compass Correction Card Provides appropriate heading corrections 2014 Captain Sim www captainsim com 105 DO NOT USE FOR FLIGHT CO1 STANDBY INSTRUMENTS DISPLAYS Standby Altitude Indicator 1 Bank Pointer 2 Airplane Symbol 3 Bank Scale 4 Horizon Line and Pitch Scale Standby Airspeed Indicator 5 Speed Bug Set 6 Speed Bug Set On Off Standby Altitude Indicator 7 Altimeter Pressure Set 8 Altimeter STD Pressure Button 1013 2352 Standby Altitude Indicator 1 Bank Pointer Indicates airplane bank 2 Airplane Symbol Indicates airplane attitude with reference to the SAARU horizon 3 Bank Scale Fixed reference for the bank pointer Scale marks are at 0 10 20 30 45 and 60 degrees 4 Horizon Line and Pitch Scale Indicates the SAARU horizon relative to the airplane symbol Pitch scale is in 2 5 degree increments Standby Airspeed Indicator 5 Speed Bug Set 6 Speed Bug Set On Off Rotate outer Adjusts t
104. ter display unit ursi m un DE 040 ga tht an r O uc A LC n EN rH E a l lo Dem 2014 Captain Sim www captainsim com 61 ANC stems 62 DO NOT USE FOR FLIGHT DISPLAY SYSTEM INFORMATION SOURCE AIR DATA INERTIAL REFERENCE SYSTEM ADIRS The ADIRS provides Primary secondary and standby air data Inertial reference information The major components of the ADIRS are One Air Data Inertial Reference Unit ADIRU e One Secondary Attitude Air Data Reference Unit SAARU e Eight air data modules Six static ports Three pitot probes Two angle of attack vanes One total air temperature probe AIR DATA INERTIAL REFERENCE UNIT ADIRU The ADIRU is the primary source for speed altitude attitude and inertial navigation position information The ADIRU processes information measured by its internal gyros and accelerometers and from air data module inputs angle of attack vanes and other systems SECONDARY ATTITUDE AIR DATA REFERENCE UNIT SAARU The SAARU is the secondary source for speed altitude and attitude information The SAARU processes information measured by its internal gyros and accelerometers and from air data module inputs angle of attack vanes and other systems The SAARU also transmits roll and pitch attitude information to the standby attitude display AIR DATA Three static ports are located on the left
105. the SAARU computed value is displayed 1 WWW Captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 63 DO NOT USE FOR FLIGHT NAVIGATION DISPLAY ND INTRODUCTION The NDs provide a mode selectable color flight progress display The modes are e MAP VOR e APP approach PLN plan The MAP VOR and APP modes can be switched between an expanded mode with a partial compass rose and a centered mode with a full compass rose MAP MODE The MAP mode is recommended for most phases of flight Presented track up this mode shows airplane position relative to the route of flight against a moving map background Displayed information can include e Selected and current track Selected and current heading Position trend vector Range to selected altitude Map range scale Ground speed True airspeed Wind direction and speed Next waypoint distance Waypoint estimated time of arrival Selected navigation data points Additional Navigation Facility STA Waypoint WPT Airport ARPT Route Progress DATA and Position POS data are available for display on the ND in both the expanded and center map modes VOR AND APPROACH MODES The VOR and APP modes are presented heading up The VOR and APP modes display track heading and wind speed and direction with VOR navigation or ILS approach information PLAN MODE The PLN mode is presented true north up The active route may be viewed using the STEP prompt on t
106. ttison Nozzle VALVE Lights Illuminated amber The jettison nozzle valve is not in the selected position 3 Fuel Jettison ARM Switch ARMED Arms the jettison system e Initializes fuel to remain at the MLW fuel quantity Off ARMED not visible Disarms the jettison system 4 Fuel Jettison FAULT Light Illuminated amber A system fault has occurred e Fuel jettison is inoperative 5 FUEL TO REMAIN Selector PULL ON changes the mode from MLW maximum landing weight to MAN manual Rotate e Rotate CW to increase CCW to decrease the MANUAL fuel to remain quantity e Sets the manual MAN fuel to remain quantity selection at the slow rate first detent or fast rate second detent Push automatically selects the MLW fuel to remain quantity www captainsim com DO NOT USE FOR FLIGHT HYDRAULICS 1 Ram Air Turbine Switch 2 5 Left Right Engine L R ENG Primary Pump Switches 3 4 C1 C2 Electrical C1 C2 ELEC Primary Pump Switches 6 9 Demand Pump Selectors 10 13 Demand Pump Fault Lights HYDRALLIC 1 ELEG 2 1 Ram Air Turbine Switch Push Deploys the RAT 2 5 Left Right Engine L R ENG Primary Pump Switches ON The engine driven hydraulic pump pressurizes the related left or right hydraulic system when the engine rotates Off ON not visible The engine driven hydraulic pump is turned off and depressurized 3 4 C1 C2 Electrical C1 C2 ELEC Primary Pump Switches ON
107. witch ON The wing leading edge illumination lights are illuminated 4 Indicator Lights IND LTS Switch TEST spring loaded e Iluminates all annunciator lights to full brightness for 10 seconds to check the bulbs then dims the lights as long as the switch is held e Causes test patterns to display on the stabilizer position indicators rudder trim indicator and radio tuning panel displays BRT sets all illuminated annunciator lights to full brightness DIM sets all illuminated annunciator lights to low brightness 5 RUNWAY TURNOFF Light Switches OFF The runway turnoff light is extinguished ON The runway turnoff light is illuminated 6 TAXI Light Switch OFF The taxi lights are extinguished ON The taxi lights are illuminated Note The taxi lights do not illuminate when the nose landing gear is not down and locked 7 STROBE Light Switch OFF The white anticollision strobe lights on the tips of each wing and the tail cone are off ON The strobe lights operate 014 Captain Sim www captainsim com 777 Captain FLIGHT MANUAL Part II Aircraft and Systems 22 DO NOT USE FOR FLIGHT MISCELLANIOUS LIGHTING CONTROLS 01 GOS MAP LIGHT CONTROL V02 FORWARD PANEL BRIGHTNESS CONTROLS PWD PANEL BRIGHTNESS OUTED wep OSPL FLOOD 1 Outboard Display Light Control Rotate Controls outboard display light 2 Inboard Displays Lights Control Rotate Controls inboard displays lights
108. www captainsim com When the EFIS control panel WPT map switch is selected on waypoints not on the selected route are displayed in ND ranges of 10 20 or 40 The active route is displayed with a continuous line M between waypoints Active route modifications are displayed with short dashes W between waypoints Inactive routes are displayed with long dashes B between waypoints When the EFIS control panel DATA map switch is selected on entered or procedural altitude and ETAs for route waypoints are displayed Shows the reference point selected on the FMCS CDU fix page bearing and or distance from the fix show with green dashes Indicates the approximate map position of the FMC calculated T C top of climb T D top of descent S C step climb and E D end of descent points Predicted altitude ETA points entered on the FIX page display the altitude ETA along with the profile point Deceleration points have no identifier Displays vertical deviation from selected VNAV PATH during descent only Scale indicates 400 feet deviation Digital display is provided when the pointer indicates more than 400 feet 69 DO NOT USE FOR FLIGHT Airport and runway The origin or airport shows W when the nd range is 10 20 OR 40 NM Runway dashes extend 14 2 NM Airport identifier Displayed when selected as and runway the origin or destination W and ND range is 80 160 320 or 640 NM
109. y This selector controls the vertical display range of other traffic and has no effect on the detection and display of proximate traffic TAs or RAs ABV Altitude range is set to 7000 ft above the aircraft and 2700 ft below the aircraft N Altitude range is set to 2700 ft above the aircraft and 2700 ft Below the aircraft BLW Altitude range is set to 2700 ft above the aircraft and 7000 ft below the aircraft VOR MAP APP uA PIN 29 D WXR STA WPT ARPT DATA POS TERR When selected allows TCAS traffic to be displayed on the ND TCAS TRAFFIC DISPLAYS 1 Traffic Targets 2 TCAS Mode Annunciations 3 OFFSCALE Message 4 TRAFFIC Alert Message 1 Traffic Targets Indicates the relative position of traffic targets A filled red square indicates a Resolution Advisory RA A filled amber circle indicates a Traffic Advisory TA A filled white diamond indicates proximate traffic An unfilled white diamond indicates other traffic The number represents the relative or absolute altitude of the traffic in hundreds and thousands of feet a missing number indicates the altitude is unknown The arrow indicates whether the traffic is climbing or descending at a rate of 500 feet per minute or greater a missing arrow means the traffic is flying relatively level 2014 Captain Sim www captainsim com 119 DO NOT USE FOR FLIGHT Displayed only when TCAS is enabled TCAS Mode
110. ys the VOR pointer VOR frequency or identification and associated DME information in all modes except PLAN OFF Removes VOR and ADF displays ADF Displays the ADF pointer and ADF frequency or identification in all modes except PLAN 4 Map Switches The map switches e Select detailed ND information displays Displays can be selected simultaneously Second push removes the information www captainsim com DO NOT USE FOR FLIGHT WXR Weather radar returns show when the WXR switch of the EFIS control panel is on Intense WXR returns show in red Medium intensity show in amber Low intensity show in green Turbulence shows in magenta STA station Displays high and low altitude navigation aids if the ND range selector is in the 10 20 or 40 NM range Displays high altitude navigation aids if the ND range selector is the 80 160 320 640 NM range WPT waypoint Displays waypoints if the ND range selector is in the 10 20 or 40 NM range APRT airport Displays airports on all ranges DATA Displays the FMC estimated time of arrival altitude at each waypoint and altitude constraints at each waypoint TERR Map When you push the TERR map switch on the EFIS control panel terrain data shows on the on side ND Push the TERR map switch again to remove the display Use the ND mode selector to select an ND mode The ND modes that show terrain data are Expanded APP approach mode Expanded VOR m

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