Boeing ALTEON 777 Training Manual
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Boeing ALTEON 777 Training Manual

Boeing ALTEON 777 Training Manual

This manual is for training purposes only
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777
Training Manual
THIS MANUAL IS FOR TRAINING PURPOSES ONLY.
NO MAINTENANCE ACTION SHOULD BE TAKEN AS A RESULT OF INFORMATION CONTAINED IN THIS MANUAL.
ALTEON PROPRIETARY RIGHTS ARE INCLUDED IN THE INFORMATION DISCLOSED HEREIN. R
,
,
ECIPIENT
BY ACCEPTING THIS DOCUMENT
AGREES
THAT NEITHER THIS DOCUMENT NOR THE INFORMATION DISCLOSED HEREIN NOR ANY PART THEREOF SHALL BE REPRODUCED OR TRANSFERRED TO OTHER DOCUMENTS
A
.
OR USED OR DISCLOSED TO OTHERS FOR MANUFACTURING OR FOR ANY OTHER PURPOSE EXCEPT AS SPECIFICALLY AUTHORIZED IN WRITING BY
LTEON
UNPUBLISHED, ALL RIGHTS RESERVED UNDER COPYRIGHT LAWS (
) 2003 A
T
L.L.C
C
LTEON
RAINING
This manual has been prepared by Alteon Seattle, Washington for the
Boeing Commercial Airplane Group.

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  • Page 1 OR USED OR DISCLOSED TO OTHERS FOR MANUFACTURING OR FOR ANY OTHER PURPOSE EXCEPT AS SPECIFICALLY AUTHORIZED IN WRITING BY LTEON UNPUBLISHED, ALL RIGHTS RESERVED UNDER COPYRIGHT LAWS ( ) 2003 A L.L.C LTEON RAINING This manual has been prepared by Alteon Seattle, Washington for the Boeing Commercial Airplane Group.
  • Page 2 This page is intentionally left blank...
  • Page 3 777 TRAINING MANUAL Alteon FS733 Chapter TABLE OF CONTENTS Section Subject Subject Page 777 GENERAL -- INTRODUCTION ........00-00-00 . . 1 PRINCIPAL DIMENSIONS .
  • Page 4 777 TRAINING MANUAL Alteon FS733 Chapter TABLE OF CONTENTS Section Subject Subject Page EXTERNAL POWER OPERATION ........
  • Page 5 777 TRAINING MANUAL Alteon FS733 Chapter TABLE OF CONTENTS Section Subject Subject Page ARINC 629 SIGNAL GATEWAY (ASG) CARDS ....... . .
  • Page 6 777 TRAINING MANUAL Alteon FS733 Chapter TABLE OF CONTENTS Section Subject Subject Page MESSAGE STRUCTURE FUNCTIONAL DESCRIPTION .......
  • Page 7 777 TRAINING MANUAL Alteon FS733 Chapter TABLE OF CONTENTS Section Subject Subject Page LSCF POWER INTERFACES ........

  • Page 9: General Introduction

    777 TRAINING MANUAL 777 GENERAL -- INTRODUCTION Introduction - auxiliary power unit ARINC - Aeronautical Radio, Inc. The 777 is designed for ETOPS (extended range - ARINC signal gateway operations with two-engine airplanes). It is for medium - air traffic control and long range flights.

  • Page 10: Training Manual

    777 TRAINING MANUAL 777 GENERAL -- INTRODUCTION - integrated drive generator - very high frequency - instrument landing system - VHF omni range ISFD - integrated standby flight display - words per second KBPS - kilobits per second - local area network - line replaceable unit - maintenance access terminal MBPS...
  • Page 11 777 TRAINING MANUAL 777 GENERAL - INTRODUCTION 777 GENERAL - INTRODUCTION 00-00-00 - 3 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 12 777 TRAINING MANUAL 777 GENERAL -- PRINCIPAL DIMENSIONS 777 Principal Dimensions These are the principal dimensions of the 777-300ER airplane on a front and side view. 00-00-00 - 4 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 13 777 TRAINING MANUAL 212 FT 7 IN (64.8 M) 70 FT 7.5 IN (21.5 M) 2 FT 11 IN (MIN) 36 FT (0.9 M) (11 M) 20 FT 4 IN (6.2 M) 60 FT 8 IN (MAX) (18.5 M) 19 FT 4 IN 102 FT 5 IN (5.9 M) 7 FT 9 IN (MIN)
  • Page 14 777 TRAINING MANUAL 777 GENERAL -- GENERAL ARRANGEMENT THIS PAGE INTENTIONALLY LEFT BLANK 00-00-00 - 6 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 15 777 TRAINING MANUAL 777 GENERAL -- GENERAL ARRANGEMENT General Arrangement Section 44 (Sta 1035 - 1434) The fuselage has these six manufacturing sections: Section 44 is the upper center part of the fuselage. It contains these: Section 41 Section 43 Main entry doors (2) - overwing Section 44 Section 45...
  • Page 16 777 TRAINING MANUAL 777 GENERAL -- GENERAL ARRANGEMENT Aft pressure bulkhead Stabilizer compartment access door Auxiliary power unit (APU) firewall APU inlet and exhaust APU access doors Aft access door. 00-00-00 - 8 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 17 777 TRAINING MANUAL ENTRY ENTRY ENTRY ENTRY ENTRY AFT PRESSURE DOOR 1 DOOR 2 DOOR 3 DOOR 4 DOOR 5 BULKHEAD FIREWALL FORWARD PRESSURE INLET BULKHEAD 1434 1437 1886 2062 DOOR PLUG PLUG 332.5 210 IN 189" EXHAUST WL 343 WL 200.5 WL 99 ACCESS...
  • Page 18 777 TRAINING MANUAL 777 GENERAL -- AIRPLANE SERVICING General The locations of doors, service connections, and access panels make it possible to do servicing of many systems at the same time. 00-00-00 - 10 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 19 777 TRAINING MANUAL UTILITY GALLEY TRUCK HYDRANT TUG AND DOOR NO. 2 FUEL TRUCK TRAILERS LOWER CARGO UTILITY TUG HOLD LOADER AND TRAILERS UTILITY TUG AND TRAILERS BULK CARGO LOWER CARGO LOADER HOLD LOADER GALLEY TRUCK GALLEY TRUCK ELECTRICAL POWER TRACTOR PASSENGER BRIDGE...
  • Page 20 777 TRAINING MANUAL 777 GENERAL -- FLIGHT CONTROL SURFACES General There are two flight controls systems. They are the primary flight control system and the high lift control system. Primary Flight Control System (PFCS) These are the control surfaces of the PFCS: One aileron on each wing One flaperon on each wing Seven spoilers on each wing...
  • Page 21 777 TRAINING MANUAL RUDDER RUDDER TAB ELEVATOR (2) OUTBOARD SPOILER (10) FLAPERON (2) INBOARD HORIZONTAL FLAP (2) STABILIZER INBOARD SPOILER (4) OUTBOARD FLAP (2) AILERON (2) KRUEGER OUTBOARD INBOARD FLAP (2) SLAT (12) SLAT (2) 777 GENERAL - FLIGHT CONTROL SURFACES 00-00-00 - 13 - ALTEON PROPRIETARY.
  • Page 22 777 TRAINING MANUAL 777 GENERAL -- ANTENNA LOCATIONS Antenna Locations These are the communication and navigation system antennas: Weather radar TCAS (traffic alert and collision avoidance system) ATC (air traffic control) GPS (global positioning system) VHF (very high frequency) communication SATCOM (satellite communication) ADF (automatic direction finder) HF (high frequency) communication...
  • Page 23 777 TRAINING MANUAL SATCOM HI GAIN SATCOM LO GAIN VHF C VHF L TCAS ILS GLIDESLOPE CAPTURE (3) AND LOCALIZER (3) WEATHER RADAR GLIDESLOPE DME R TELEPHONE (L,R) TRACK (3) MARKER BEACON VHF R TCAS DME L RA (6) OPTIONAL SYSTEM TOP OR SIDE MOUNTED OPTIONAL 777 GENERAL - ANTENNA LOCATIONS 00-00-00...
  • Page 24 777 TRAINING MANUAL 777 GENERAL -- ZONE DIAGRAMS - AIRPLANE MAJOR ZONES General The 777 airplane has 8 major zones to help you find and identify airplane components and parts. These are the major zones: 100 - lower half of the fuselage 200 - upper half of the fuselage 300 - empennage and body section 48 400 - power plants and nacelle struts...
  • Page 25 777 TRAINING MANUAL 777 GENERAL - ZONE DIAGRAMS - AIRPLANE MAJOR ZONES 00-00-00 - 17 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 26 777 TRAINING MANUAL 777 GENERAL -- ZONE DIAGRAMS - SUBZONES AND ZONES General Fourth digit - a letter that identifies each access door or panel in a zone; if there are more The eight major zones have subzones, and the subzones than one access panel in a zone, they have letters have zones.
  • Page 27 777 TRAINING MANUAL SUBZONE 510 ZONE 541 SUBZONE 530 SUBZONE 540 543AB 543BB ZONE 542 SUBZONE 520 ZONE 543 ZONE 544 543CB 543DB ZONE 543 ACCESS PANELS (BOTTOM OF THE WING) SUBZONES OF MAJOR ZONE 500 - LEFT WING ZONES OF SUBZONE 540 777 GENERAL - ZONE DIAGRAMS - SUBZONES AND ZONES 00-00-00 - 19 -...
  • Page 28 777 TRAINING MANUAL 777 GENERAL -- FLIGHT DECK Flight Deck Major Panels These are the major panels in the flight deck: P1 left forward panel P2 center forward panel P3 right forward panel P5 overhead panel P7 glareshield panel P8 aft aisle stand panel P9 forward aisle stand panel P10 control stand P11 overhead circuit breaker panel...
  • Page 29 777 TRAINING MANUAL 777 GENERAL - FLIGHT DECK 00-00-00 - 21 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 30 777 TRAINING MANUAL 777 GENERAL -- MAIN INSTRUMENT PANELS General The main instrument panels (P1 and P3) have these displays and controls: Display units (4) Instrument source select panels (2) Clocks (2) Inboard display selectors (2) FMC selector Heading reference switch Brake accumulator pressure indicator.
  • Page 31 777 TRAINING MANUAL LEFT INBOARD RIGHT INBOARD DISPLAY UNIT DISPLAY UNIT INSTRUMENT SOURCE LEFT OUTBOARD RIGHT OUTBOARD SELECT PANEL (2) DISPLAY UNIT DISPLAY UNIT CLOCK (2) HEADING REFERENCE SWITCH SELECTOR BRAKE ACCUMULATOR INBOARD DISPLAY INBOARD DISPLAY PRESSURE INDICATOR SELECTOR SELECTOR P1 LEFT FORWARD PANEL P3 RIGHT FORWARD PANEL 777 GENERAL - MAIN INSTRUMENT PANELS...
  • Page 32 777 TRAINING MANUAL 777 GENERAL -- GLARESHIELD PANELS General The glareshield panels have these controls: Master warning and caution lights (2) Master warning and caution reset switches (2) Mode control panel EFIS control panels (2) Display select panel Data uplink switches (2) Map light controls (2) MIC switches (2) Clock switches (2).
  • Page 33 777 TRAINING MANUAL MASTER WARNING MODE DISPLAY EFIS CONTROL DATA UPLINK ACCEPT, AND CAUTION LIGHTS CONTROL SELECT PANEL (2) REJECT, AND CANCEL AND RESET SWITCH (2) PANEL PANEL SWITCHES (2) SWITCH (2) MINS BARO MINS BARO MAP LIGHT RADIO BARO RADIO BARO MTRS...
  • Page 34 777 TRAINING MANUAL 777 GENERAL -- P2 CENTER FORWARD AND P9 FORWARD AISLE STAND PANELS General The P2 center forward and P9 forward aisle stand panels have these controls: Integrated standby flight display Display units (2) Ground proximity light and override switches Landing gear lever Autobrake selector Control display units (2)
  • Page 35 777 TRAINING MANUAL UPPER CENTER GROUND PROXIMITY P2 CENTER FORWARD PANEL DISPLAY UNIT LIGHT AND OVERRIDE SWITCHES LEVER LOCK GND PROX OVERRIDE FLAP GEAR OVRD OVRD INHIBIT SWITCH INTEGRATED OVRD OVRD PROX STANDBY TERRAIN G/S INHB RETRACT OVERIDE SWITCH FLIGHT TERR 270K-.82M OVRD...
  • Page 36 777 TRAINING MANUAL 777 GENERAL -- P10 CONTROL STAND General The P10 control stand has these controls and indications: Speedbrake lever Thrust levers(2) Stabilizer position indicators (2) Alternate flaps arm switch Alternate flaps selector Fuel control switches (2) Stabilizer cutout switches (2) Parking brake lever Alternate pitch trim levers Cursor control devices (2)
  • Page 37 777 TRAINING MANUAL SPEEDBRAKE THRUST LEVER LEVERS CURSOR CONTROL FLAP LEVER DEVICE (2) ALTERNATE PITCH TRIM LEVERS STABILIZER POSITION INDICATOR (2) ALTERNATE FLAPS ARM SWITCH PARKING BRAKE LEVER ALTERNATE FLAPS SELECTOR STABILIZER FUEL CONTROL CUTOUT SWITCHES SWITCHES P10 CONTROL STAND 777 GENERAL - P10 CONTROL STAND 00-00-00 - 29 -...
  • Page 38 777 TRAINING MANUAL 777 GENERAL -- P8 AFT AISLE STAND PANEL General The P8 aft aisle stand panel has these controls: Control display unit Engine fire panel Radio tuning panels (3) Audio control panels (3) Transponder panel Emergency evacuation panel Aileron/rudder trim panel Light controls Flight deck printer...
  • Page 39 777 TRAINING MANUAL CENTER CONTROL ENGINE FIRE DISPLAY UNIT PANEL RADIO TUNING PANEL (3) AUDIO CONTROL PANEL (3) TRANSPONDER PANEL WEATHER +BRT- INIT (TYPICAL) ALTN VNAV RADAR PANEL HOLD LEGS PROG EXEC (TYPICAL) MENU PREV NEXT PAGE PAGE AILERON/RUDDER TRIM PANEL EMERGENCY EVACUATION PANEL...
  • Page 40 777 TRAINING MANUAL 777 GENERAL -- P5 OVERHEAD PANEL General Forward cargo air conditioning system. Air cleaner system. The P5 overhead panel has controls for these functions Cabin telephone system. (reference numbers on graphic): 1 Air data inertial reference system (ADIRS) 2 Primary flight computers 3 Electrical system/APU 4 Wiper control and landscape cameras...
  • Page 41 777 TRAINING MANUAL CARGO FIRE APU BTL DISCH ARMED ARMED DISCH DISCH AIR CONDITIONING FIRE/ EQUIP OVHT COOLING GASPER TEST AUTO DISCH RECIRC FANS OVRD UPPER LOWER EMER SERV PASS FLT DECK CABIN ENGINE LIGHTS INTPH OXYGEN TEMP TEMP EEC MODE ADIRU AUTO NORM...
  • Page 42 777 TRAINING MANUAL 777 GENERAL -- P61 OVERHEAD MAINTENANCE PANEL General The P61 overhead maintenance panel has control functions used normally only by maintenance personnel. The P61 overhead maintenance panel has these controls: Backup window heat switches Standby power switch Flight control shutoff switches APU and EEC maintenance panel Cargo temperature select panel...
  • Page 43 777 TRAINING MANUAL STANDBY APU AND EEC POWER SWITCH MAINTENANCE PANEL BACKUP WINDOW HEAT PANEL CARGO TEMPERATURE SELECT PANEL FLIGHT CONTROL HYDRAULIC POWER GROUND TEST AND PANEL TOWING POWER PANEL COCKPIT VOICE RECORDER PANEL CARD FILE CARD FILE P61 OVERHEAD MAINTENANCE PANEL 777 GENERAL - P61 OVERHEAD MAINTENANCE PANEL 00-00-00 - 35 -...
  • Page 44 777 TRAINING MANUAL 777 GENERAL -- P13 AND P14 SIDEWALL PANELS General The sidewall panels have these controls: Shoulder heater (2) Foot heater (2) Outboard display brightness (2) Inboard display weather radar brightness (2) Panel flood light brightness (2). 00-00-00 - 36 - ALTEON PROPRIETARY.
  • Page 45 777 TRAINING MANUAL HEATERS HEATERS SHOULDER FOOT FOOT SHOULDER HIGH HIGH HIGH HIGH FWD PANEL BRIGHTNESS FWD PANEL BRIGHTNESS OUTBD INBD DSPL/ PNL/ PNL/ INBD DSPL/ OUTBD DSPL FLOOD FLOOD DSPL P13 LEFT SIDEWALL PANEL P14 RIGHT SIDEWALL PANEL 777 GENERAL - P13 AND P14 SIDEWALL PANELS 00-00-00 - 37 - ALTEON PROPRIETARY.
  • Page 46 777 TRAINING MANUAL 777 GENERAL -- P18 MAT/SECOND OBSERVER PANEL General The MAT/second observer panel has these maintenance access terminal (MAT) items: MAT display MAT cursor control device (CCD) MAT keyboard Portable MAT (PMAT) receptacle. These components are located behind an access door at the bottom of the MAT chassis: MAT floppy disk drive MAT hard disk drive...
  • Page 47 777 TRAINING MANUAL MAT DISPLAY SECOND OBSERVER MAT CURSOR MAP LIGHT CONTROL CONTROL DEVICE MAT KEYBOARD MAT FLOPPY DISK DRIVE MAT HARD DISK DRIVE MAT FLASH MEMORY MODULE MAT CD-ROM DRIVE (BEHIND ACCESS DOOR) PMAT RECEPTACLE 777 GENERAL - P18 MAT/SECOND OBSERVER PANEL 00-00-00 - 39 - ALTEON PROPRIETARY.
  • Page 48 777 TRAINING MANUAL 777 GENERAL -- EQUIPMENT CENTER AND RACKS - INTRODUCTION Equipment Centers The airplane has these equipment centers: Forward equipment center (FEC) Main equipment center (MEC). The forward and main equipment centers are in the lower lobe area. The FEC is forward of the nose wheel well, and the MEC is aft of the nose wheel well.
  • Page 49 777 TRAINING MANUAL E7 RACK E11 RACK E12 RACK E10 RACK E6 RACK E17 RACK FORWARD EQUIPMENT E5 RACK CENTER E16 RACK MAIN EQUIPMENT CENTER 777 GENERAL - EQUIPMENT CENTER AND RACKS - INTRODUCTION 00-00-00 - 41 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 50 777 TRAINING MANUAL 777 GENERAL -- MAIN EQUIPMENT CENTER - 1 Main Equipment Center Electronics Access to the Main Equipment Center The main equipment center (MEC) contains most of the Access to the MEC is through these: electronics equipment on the airplane. The electronics equipment in the MEC is on the E1, E2, E3, and E4 racks.
  • Page 51 777 TRAINING MANUAL E2 RACK E1 RACK P210 RIGHT POWER MANAGEMENT PANEL P310 STANDBY POWER MANAGEMENT PANEL P300 AUXILIARY POWER PANEL P110 LEFT POWER MANAGEMENT PANEL ACCESS HATCH LOOKING AFT E4 RACK LADDER TO ACCESS E3 RACK DOOR FROM CABIN P200 RIGHT POWER PANEL P100 LEFT...
  • Page 52 777 TRAINING MANUAL 777 GENERAL -- MAIN EQUIPMENT CENTER - 2 General Right engine fire/overheat detection ARINC 629 signal gateway (ASG) The systems card files hold interface cards for systems Environmental control system (ECS) that use ARINC 429 buses. Weight on wheels (WOW). These are the two systems card files in the main equipment center: P85 left systems card file (LSCF)
  • Page 53 777 TRAINING MANUAL P84 RIGHT P85 LEFT SYSTEMS SYSTEMS CARD FILE CARD FILE MAIN EQUIPMENT CENTER MAIN EQUIPMENT CENTER (LEFT SIDE, LOOKING FORWARD) (RIGHT SIDE, LOOKING FORWARD) 777 GENERAL - MAIN EQUIPMENT CENTER - 2 00-00-00 - 45 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 54 777 TRAINING MANUAL 777 GENERAL -- FORWARD EQUIPMENT CENTER Forward Equipment Center Electronics The forward equipment center contains the two weather radar receiver/transmitters (WXR/RTs) and the forward and down looking video camera equipment. Access to the Forward Equipment Center Access to the forward equipment center is through the access door forward of the nose landing gear.
  • Page 55 777 TRAINING MANUAL LEFT WXR RT RIGHT WXR RT DOWN CAMERA CAMERA INTERFACE UNIT FORWARD CAMERA FORWARD EQUIPMENT CENTER DOOR (REF) CAMERA WINDOW FORWARD EQUIPMENT CENTER (LOOKING FORWARD) 777 GENERAL - FORWARD EQUIPMENT CENTER 00-00-00 - 47 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 56 777 TRAINING MANUAL 777 GENERAL -- CARGO DOOR EQUIPMENT RACKS General E6 Rack These four equipment racks are adjacent to the cargo The E6 rack is at the aft cargo door at station 1754. It doors: contains components for these functions: E16 rack and E5 rack (forward cargo door) HF communication E17 rack and E6 rack (aft cargo door).
  • Page 57 777 TRAINING MANUAL E5 RACK E16 RACK FWD CARGO DOOR (LOOKING AFT) FWD CARGO DOOR (LOOKING FORWARD) E6 RACK E17 RACK AFT CARGO DOOR AFT CARGO DOOR (LOOKING AFT) (LOOKING FORWARD) 777 GENERAL - CARGO DOOR EQUIPMENT RACKS 00-00-00 - 49 - ALTEON PROPRIETARY.
  • Page 58 777 TRAINING MANUAL 777 GENERAL -- OTHER EQUIPMENT RACKS General E10 Rack In addition to the equipment racks in the main The E10 rack is aft of the bulk cargo door on the right equipment center and at the forward and aft cargo side of the lower lobe at station 1937.
  • Page 59 777 TRAINING MANUAL E12 RACK E11 RACK E10 RACK BULK CARGO DOOR OVERHEAD PASSENGER COMPARTMENT BULK CARGO COMPARTMENT (LEFT SIDE LOOKING INBOARD) (RIGHT SIDE LOOKING OUTBOARD) E7 RACK OVERHEAD PASSENGER COMPARTMENT (RIGHT SIDE LOOKING OUTBOARD) 777 GENERAL - OTHER EQUIPMENT RACKS 00-00-00 - 51 - ALTEON PROPRIETARY.
  • Page 60 777 TRAINING MANUAL 777 GENERAL -- CREW REST MODULE Overhead Flight Crew Rest (OFCR) Lighting Attendant call The OFCR contains two seats and two bunks for two crew Supplemental oxygen. members and a storage compartment (not shown). The OFCR module can have these functions (not shown): Access to Flight Attendant Rest Module Ventilation and heating Access to the flight attendant rest module is in the...
  • Page 61 777 TRAINING MANUAL FLIGHT ATTENDANT REST (OFAR) DOOR 5 OFCR ENTRANCE ENCLOSURE FLIGHT CREW REST MODULE OFAR ENTRANCE ENCLOSURE DOOR 5 777 GENERAL - CREW REST MODULE 00-00-00 - 53 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 62 777 TRAINING MANUAL 777 GENERAL -- PASSENGER DOORS - INTRODUCTION Purpose Passenger entry doors give access to the passenger compartment. General Description There are five passenger entry doors on each side of the airplane. Physical Description Handles to open and close the door are on the inner side and outer side of the door.

  • Page 63: Inside View

    777 TRAINING MANUAL PASSENGER ENTRY DOOR DOOR (10) OPEN FUSELAGE DOOR CLOSED SKIN LINE (REF) TOP VIEW MODE SELECT LEVER DOOR HINGE DOOR DOOR HANDLE LINING DOOR HANDLE ESCAPE SLIDE/RAFT INBD INSIDE VIEW OUTSIDE VIEW 777 GENERAL - PASSENGER DOORS - INTRODUCTION 00-00-00 - 55 - ALTEON PROPRIETARY.
  • Page 64 777 TRAINING MANUAL 777 GENERAL -- PASSENGER DOORS - OPERATION THIS PAGE INTENTIONALLY LEFT BLANK 00-00-00 - 56 - ALTEON PROPRIETARY. Copyright. See title page for details...

  • Page 65: Training Manual

    777 TRAINING MANUAL 777 GENERAL -- PASSENGER DOORS - OPERATION General If the external handle is not in the extended position, pull it outboard and rotate it 180 degrees. It will The general information that follows is for all of the stay extended outboard.
  • Page 66 777 TRAINING MANUAL 777 GENERAL -- PASSENGER DOORS - OPERATION If either flag shows, do not use the door. Do a system check. Move the internal handle to the open position. Push outboard and forward on the door. When the door stops, do a check to see that the hold-open hook has engaged the hold-open catch.
  • Page 67 777 TRAINING MANUAL MODE SELECT HANDLE VENT DOOR HINGE COVER EXTERNAL HANDLE WINDOW (REF) HOLD-OPEN HANDLE INTERNAL HANDLE EPAS BATTERY SAFETY SWITCH (UNDER HINGE COVER) WITNESS PORT EXTERNAL VIEW INTERNAL VIEW 777 GENERAL - PASSENGER DOORS - OPERATION 00-00-00 - 59 - ALTEON PROPRIETARY.
  • Page 68 777 TRAINING MANUAL 777 GENERAL -- FLIGHT DECK LIGHTS General glareshield light control is on the passenger signs/lighting panel on the P5 overhead panel. These are the lights used for general flight deck lighting: Storm Light Switch Dome lights The storm light switch (STORM) is on the passenger Center aisle stand flood light signs/lighting panel on the P5 overhead panel.
  • Page 69 777 TRAINING MANUAL DOME LIGHTS PASS SIGNS NO SMOKING SEAT BELTS AUTO AUTO CENTER AISLE STAND FLOOD LIGHT GLARESHIELD FLOOD LIGHTS LEFT FORWARD PANEL FLOOD RIGHT FORWARD LIGHT OVHD/ MASTER PANEL FLOOD STORM BRIGHT DOME LIGHT PUSH ON/OFF GLARESHIELD PNL/FLOOD LANDING LEFT RIGHT...
  • Page 70 777 TRAINING MANUAL 777 GENERAL -- PASSENGER COMPARTMENT LIGHTS Purpose Use the up and down arrows to select the differnt lighting scenes. The shaded area shows the selected The passenger compartment lights supply these types of scene. lights for the passenger compartment: Use the selections below the cabin area description to Passenger loading ceiling lights (not shown) control the lighting level.
  • Page 71 777 TRAINING MANUAL PANEL EXIT CABIN CONTROLS MAIN MENU OVERRIDE NIGHT LIGHTING SEAT CONTROL AND AUDIO MONITOR LIGHT PASSENGER SERVICE CALL/CHIME CONTROL PASSENGER ADDRESS COMPARTMENT CEILING LIGHT CABIN TEMPERATURE CABIN DOOR STATUS WATER/WASTE TANK STATUS DISPLAY CONTROLS BOARDING MUSIC SMOKING ASSIGNMENTS SPECIAL FUNCTIONS CSCP/CACP MAIN...
  • Page 72 777 TRAINING MANUAL 777 GENERAL -- ELECTRICAL CONTROL Power Sources Battery IFE/Pass Seats The electrical power system has five main power Cabin/Utility sources, two backup power sources, and two standby APU generator power sources. These are the main power sources and Bus tie (2) their continuous supply capacity: Generator control (2)
  • Page 73 777 TRAINING MANUAL 777 GENERAL -- ELECTRICAL CONTROL position. OFF is an amber light that shows when the EPC. The available (AVAIL) light goes off when the EPC switch is out and the airplane has ac power. closes. APU Generator Switch Generator Control Switches The APU generator switch arms the APU GCU to Each generator control switch arms its GCU to control...
  • Page 74 777 TRAINING MANUAL 777 GENERAL -- ELECTRICAL CONTROL pressure. Plastic guards cover the drive disconnect the switch moves it to OFF. The switch is normally in switches to prevent accidental operation. the OFF position. Standby Power Switch The standby power switch has these three positions: AUTO BAT (momentary).
  • Page 75 777 TRAINING MANUAL ELECTRICAL STANDBY TOWING POWER POWER BATTERY START IFE/PASS CABIN/ SEATS UTILITY AUTO ON BAT APU GEN FAULT GROUND TEST PANEL (P61) BACKUP WINDOW HEAT L BUS TIE R BUS TIE PANEL (P61) AUTO AUTO SECONDARY PRIMARY ISLN ISLN EXT PWR EXT PWR...
  • Page 76 777 TRAINING MANUAL 777 GENERAL -- EXTERNAL POWER OPERATION THIS PAGE INTENTIONALLY LEFT BLANK 00-00-00 - 68 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 77 777 TRAINING MANUAL 777 GENERAL -- EXTERNAL POWER OPERATION General Observe Indications To connect external power to the airplane electrical When you put power on at the power source, the lights system, you do these steps: above the power receptacle come on. If the lights do not come on, there is a problem with the power quality.
  • Page 78 777 TRAINING MANUAL 777 GENERAL -- EXTERNAL POWER OPERATION loads it controls, or the BPCU will open the external power contactors. See the electrical load management section for more information on load shed by the ELMS. 00-00-00 - 70 - ALTEON PROPRIETARY.
  • Page 79 777 TRAINING MANUAL ELECTRICAL BATTERY START IFE/PASS CABIN/ SEATS UTILITY SECONDARY POWER PRIMARY POWER L24021 L24020 L24019 L24018 APU GEN CONNECTED NOT IN USE CONNECTED NOT IN FAULT L BUS TIE R BUS TIE AUTO AUTO SECONDARY PRIMARY ISLN ISLN EXT PWR EXT PWR AVAIL...
  • Page 80 777 TRAINING MANUAL 777 GENERAL -- ELECTRICAL SYNOPTIC General The electrical synoptic supplies the information necessary to make sure electric power is available and to see the status of the electrical buses. Information The electrical synoptic shows this data: Bus data Bus tie breakers status Generator drive status and control Backup generator status...
  • Page 81 777 TRAINING MANUAL ISLN L BUS TIE R BUS TIE EXT PWR EXT PWR L MAIN R MAIN L UTIL R UTIL L XFR R XFR L GEN R GEN CTRL CTRL DRIVE BACKUP L DRIVE R DRIVE MAIN BAT APU BAT VOLTS VOLTS...
  • Page 82 777 TRAINING MANUAL 777 GENERAL -- AUXILIARY POWER SYSTEM OPERATION THIS PAGE INTENTIONALLY LEFT BLANK 00-00-00 - 74 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 83 777 TRAINING MANUAL 777 GENERAL -- AUXILIARY POWER SYSTEM OPERATION General memo message APU COOLDOWN shows during this period. After the cool down, the APU stops. The APU controls include: Non-Normal Shutdown APU selector on the electrical panel (P5) APU fire switch on the cargo fire/engine control You can also stop the APU with the APU fire switch.
  • Page 84 777 TRAINING MANUAL 777 GENERAL -- AUXILIARY POWER SYSTEM OPERATION Training Information Point To start and operate the APU for one hour, there must be a minimum of 950 lbs (430 kgs) of fuel in the left main tank. 00-00-00 - 76 - ALTEON PROPRIETARY.
  • Page 85 777 TRAINING MANUAL ELECTRICAL APU BTL DISCH START APU GEN FAULT DISCH ELECTRICAL PANEL (P5) APU RUNNING APU FIRE WARNING HORN EICAS DISPLAY CARGO FIRE/ENGINE CONTROL PANEL (P5) APU FIRE FIRE BOTTLE ARMED RESET: FIRE/OVHT TEST SW (P5) BOTTLE DISCHARGED APU MAINT EEC MAINT APU FIRE...
  • Page 86 777 TRAINING MANUAL 777 GENERAL -- AIR CONDITIONING CONTROL General These are the panels that give control of the air conditioning and equipment cooling systems: Air conditioning panel Bleed air/pressurization panel. Both panels are on the P5 overhead panel in the flight deck.
  • Page 87 777 TRAINING MANUAL AIR CONDITIONING EQUIP COOLING GASPER AUTO RECIRC FANS UPPER LOWER FLT DECK CABIN TEMP TEMP AUTO AIR COND RESET BLEED AIR L PACK R PACK ISLN ISLN AUTO AUTO L TRIM AIR R AUTO AUTO AUTO L ENG R ENG AIR CONDITIONING PANEL (P5) AUTO...
  • Page 88 777 TRAINING MANUAL 777 GENERAL -- AIR SYNOPTIC General The air synoptic supplies the information necessary to make sure air is available and to see the various temperatures on the aircraft. Information The MASTER temperature shows the temperature set with the cabin temperature control on the air conditioning panel.
  • Page 89 777 TRAINING MANUAL MASTER BULK F/D TRIM L PACK TRIM R PACK DUCT PRESS DUCT PRESS ISLN ISLN AIR 1 AIR 2 START L ENG R ENG START START AIR SYNOPTIC 777 GENERAL - AIR SYNOPTIC 00-00-00 - 81 - ALTEON PROPRIETARY.
  • Page 90 777 TRAINING MANUAL 777 GENERAL -- HYDRAULIC CONTROL General When the systems are unpressurized, the pump fault lights are on. The hydraulic system has nine pumps. Four are primary pumps and four are demand pumps. The left and right Parking Brake Operation systems have engine driven pumps (EDPs) for primary and electric pumps for demand.
  • Page 91 777 TRAINING MANUAL RAM AIR TURBINE HYDRAULIC ELEC L ENG R ENG FAULT FAULT FAULT FAULT PUMP FAULT L ELEC AUTO AUTO R ELEC LIGHTS (TYP) AUTO AUTO FAULT FAULT FAULT FAULT HYDRAULIC/RAT PANEL (P5) 777 GENERAL - HYDRAULIC CONTROL 00-00-00 - 83 - ALTEON PROPRIETARY.
  • Page 92 777 TRAINING MANUAL 777 GENERAL -- HYDRAULIC SYNOPTIC General The hydraulic synoptic supplies the information necessary to make sure hydraulic power is available and to see the status of the hydraulic systems. Information The hydraulic synoptic shows: User systems Pump status Valve information Reservoir quantity and status System pressure.
  • Page 93 777 TRAINING MANUAL NORM BRKS FLAPS L REV R REV USER SYSTEMS NOSE GEAR ALTN/RSV MAIN GEAR & STEERING BRAKES & STEERING FLT CTRL FLT CTRL FLT CTRL ISLN ISLN PUMP (TYP) ELEC ELEC ELEC ELEC SYSTEM QUANTITY 0.90 0.90 0.68 SYSTEM PRESSURE 2990...
  • Page 94 777 TRAINING MANUAL 777 GENERAL -- FIRE PROTECTION THIS PAGE INTENTIONALLY LEFT BLANK 00-00-00 - 86 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 95 777 TRAINING MANUAL 777 GENERAL -- FIRE PROTECTION Engine Fire Indications Master warning lights Fire warning light in the APU fire switch These are the engine fire indications: Fire bell APU fire light on the P40 nose gear electrical EICAS message service panel (not shown) Master warning lights APU fire horn on the P40 panel (not shown).
  • Page 96 777 TRAINING MANUAL 777 GENERAL -- FIRE PROTECTION Cargo Compartment Fire Extinguishing Two fire extinguishing bottles discharge when you push one of the cargo fire arm switches and the cargo fire discharge switch. If on the ground, one of the remaining fire extinguishing bottles discharges after 20 minutes.
  • Page 97 777 TRAINING MANUAL APU BOTTLE DISCHARGE LIGHT CARGO FIRE ARM SWITCHES CARGO FIRE APU BTL DISCH APU FIRE ARMED ARMED SWITCH DISCH DISCH CARGO FIRE FIRE/ OVHT WARNING LIGHTS TEST DISCH CARGO FIRE DISCHARGE SWITCH CARGO FIRE/ENGINE CONTROL PANEL (P5) ENGINE BOTTLE DISCHARGE LIGHTS ENGINE FIRE...
  • Page 98 777 TRAINING MANUAL 777 GENERAL -- ENGINE HAZARD AREAS General Noise The hazards around jet engines in operation include: Engine noise can cause hearing loss. You must wear cup- type ear protection near an engine in operation. Inlet suction Heat Engine Entry Corridors Thrust Noise.
  • Page 99 777 TRAINING MANUAL INLET HAZARD AREAS EXHAUST HAZARD AREAS 4 FEET (1.2 M) 15-FOOT RADIUS (4.6 M) DISTANCE FROM TAIL ENGINE ENTRY CORRIDOR 175 FT IDLE POWER (53 M) IDLE POWER INLET HAZARD RADIUS IS 28.5 FEET (8.7 M) EXTENDS 11 FEET BACK ON INLET 670 FT BREAKAWAY POWER (205 M)
  • Page 100 777 TRAINING MANUAL 777 GENERAL -- AIRPLANE TOWING General You can push or tow the airplane from the nose or main landing gear. There is a forward tow fitting for a tow bar on the nose gear. There is a forward and an aft (not shown) tow bar fitting on each main gear truck.
  • Page 101 777 TRAINING MANUAL PUSHBACK CAUTION ZONE VEHICLE PUSHBACK HAZARD ZONE MAIN LANDING GEAR FORWARD TOW FITTING FORWARD TOW FITTING TOWING HAZARD ZONES NOSE GEAR TOW FITTINGS (TOP VIEW) 777 GENERAL - AIRPLANE TOWING 00-00-00 - 93 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 102 777 TRAINING MANUAL 777 GENERAL -- AIRPLANE LEVELING General For some maintenance procedures, the airplane must be level. To do a check of the airplane attitude, the airplane has these components: Longitudinal inclinometer Lateral inclinometer Plumb bob fitting Plumb bob scale. You can use either the inclinometers or the plumb bob scale to find the airplane pitch and roll attitudes.
  • Page 103 777 TRAINING MANUAL PLUMB BOB FITTING RIGHT MAIN WHEEL WELL NOSE WHEEL WELL INBD LONGITUDINAL INCLINOMETER LATERAL INCLINOMETER PLUMB BOB SCALE 777 GENERAL - AIRPLANE LEVELING 00-00-00 - 95 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 104 777 TRAINING MANUAL 777 GENERAL -- AIRPLANE JACKING THIS PAGE INTENTIONALLY LEFT BLANK 00-00-00 - 96 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 105 777 TRAINING MANUAL 777 GENERAL -- AIRPLANE JACKING General When you jack the airplane, the airplane must remain level within specified limits. One person must stay in You can lift all of the airplane on jacks, or lift only the nose wheel well to monitor the airplane the airplane nose.
  • Page 106 777 TRAINING MANUAL 777 GENERAL -- AIRPLANE JACKING Training Information Point If you supply electrical power to the airplane while it is on jacks, obey this warning: WARNING: DO THE DEACTIVATION PROCEDURE FOR THE AIR MODE SIMULATION (AMM 32-09-01) BEFORE YOU LIFT THE AIRPLANE.
  • Page 107 777 TRAINING MANUAL AIRPLANE JACKING AXLE JACKING POINT H POINT F POINT B POINT C INNER WING JACK ADAPTER (POINTS E AND F) BODY INTEGRAL JACK PAD (POINTS A AND B) POINT D POINT A POINT E POINT G OUTER WING JACK ADAPTER AFT FUSELAGE INTEGRAL JACK PAD JACK ADAPTER (POINTS G AND H)
  • Page 108 777 TRAINING MANUAL 777 GENERAL -- GROUND CREW CALL SYSTEM Purpose Use the FLIGHT DECK CALL switch to send a signal to the flight compartment. It is on the P40 Service and APU Shutdown panel. This gives an indication to the flight crew to use the flight interphone system to speak to the ground crew.

  • Page 109: Call Light

    777 TRAINING MANUAL CALL LIGHT (GREEN) CALL FLIGHT DECK FLIGHT FLIGHT DECK CALL INPH NLG DOORS CLOSE CALL SWITCH SPKR SERVICE INPH EMER EXIT WHEELWELL LT TEST LIGHTS TEST NORM AUDIO CONTROL PANEL (TYP) P40 SERVICE AND APU SHUTDOWN PANEL 777 GENERAL - GROUND CREW CALL SYSTEM 00-00-00 - 101 -...
  • Page 110 777 TRAINING MANUAL 777 GENERAL -- SERVICE INTERPHONE SYSTEM - GENERAL DESCRIPTION Purpose The ground crew uses the service interphone system to talk to each other and to the flight crew. General Description There are service interphone jacks at different places on the airplane.
  • Page 111 777 TRAINING MANUAL SERV INTPH GROUP 1 SEATTLE, WASHINGTON USA SERVICE INT HEADSET SERVICE INTERPHONE JACK (6) SERVICE INTERPHONE SWITCH CAUTION _______ GROUP 2 FLIGHT THIS ASSEMBLY CONTAINS INTERPHONE ELECTROSTATIC SENSITIVE FLIGHT DECK DEVICES SERVICE INT HEADSETS/ HEADPHONES SERVICE HEADSET INTERPHONE JACK (2) FLIGHT...
  • Page 112 777 TRAINING MANUAL 777 GENERAL -- SERVICE INTERPHONE SYSTEM - COMPONENT LOCATIONS Jack Locations The service interphone jacks are in these locations: Adjacent to the weather radar transceiver (location A) P40 service and APU shutdown panel (location B) E3 rack in the main equipment center (location C) P35 forward cargo handling accessory panel (location D) L and R engine nacelle (location E)
  • Page 113 777 TRAINING MANUAL EMER SERV PASS LIGHTS INTPH OXYGEN ARMED WINDOW HEAT SIDE SIDE INOP INOP INOP INOP P5 OVERHEAD PANEL SERV INTPH JACK LOCATIONS SERVICE INTERPHONE SWITCH 777 GENERAL - SERVICE INTERPHONE SYSTEM - COMPONENT LOCATIONS 00-00-00 - 105 - ALTEON PROPRIETARY.
  • Page 114 777 TRAINING MANUAL 777 GENERAL -- FLIGHT INTERPHONE SYSTEM - GENERAL DESCRIPTION THIS PAGE INTENTIONALLY LEFT BLANK 00-00-00 - 106 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 115 777 TRAINING MANUAL 777 GENERAL -- FLIGHT INTERPHONE SYSTEM - GENERAL DESCRIPTION General Hand microphone. The flight interphone systems permit communication The AMU sends audio signals to the headsets or to the between the flight crew and the cabin crew. Audio cockpit speakers.
  • Page 116 777 TRAINING MANUAL 777 GENERAL -- FLIGHT INTERPHONE SYSTEM - GENERAL DESCRIPTION Satellite data unit Passenger address cabin interphone controller. These discretes control the call lights on the ACPs. 00-00-00 - 108 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 117 777 TRAINING MANUAL OBS AUDIO OBSERVER NORM CAPT AUDIO CAPT GLARESHIELD SELECTOR MIC SWITCH SEATTLE, WASHINGTON SPKR SERV INTPH SERVICE CAPT AUDIO CONTROL PANEL INTERPHONE CAPT CONTROL SWITCH COLUMN MIC SWITCH MAIN EQUIPMENT CENTER JACK SERVICE AND APU CAUTION SHUTDOWN PANEL JACK THIS ASSEMBLY FLT DECK CONTAINS...
  • Page 118 777 TRAINING MANUAL 777 GENERAL -- FLIGHT INTERPHONE SYSTEM - FLIGHT DECK COMPONENT LOCATIONS - 1 Flight Interphone Component Locations These are the flight interphone system components on the flight deck: Captain's audio control panel (ACP) First officer's ACP First observer's ACP First observer's jack panel Second observer's jack panel Control column mic switches...
  • Page 119 777 TRAINING MANUAL P5 OVERHEAD PANEL P7 GLARESHIELD PANEL Ñ SERVICE INTERPHONE Ñ MIC SWITCHES SWITCH Ñ Ñ P18 SECOND OBSERVER'S PANEL Ñ SECOND OBSERVER'S JACK PANEL STOWAGE BOX (MASK MIC) Ñ SECOND OBSERVER'S OXYGEN MASK CONTROL COLUMN MIC SWITCHES P8 AFT AISLE STAND PANEL Ñ...
  • Page 120 777 TRAINING MANUAL 777 GENERAL -- FLIGHT INTERPHONE SYSTEM - FLIGHT DECK COMPONENT LOCATIONS - 2 Flight Interphone Component Locations The flight interphone system components on the left side of the flight deck include: Captain's jack panel Captain's cockpit speaker Captain's hand microphone jack.
  • Page 121 777 TRAINING MANUAL P13-3 FORWARD LEFT AUX PANEL - CAPT JACK PANEL P15 LEFT AUX PANEL - CAPT OXYGEN MASK STOWAGE BOX (MASK MICROPHONE) P13 FORWARD LEFT AUX PANEL - CAPT COCKPIT SPEAKER - CAPT HAND MICROPHONE JACK 777 GENERAL - FLIGHT INTERPHONE SYSTEM - FLIGHT DECK COMPONENT LOCATIONS - 2 00-00-00 - 113 - ALTEON PROPRIETARY.
  • Page 122 777 TRAINING MANUAL 777 GENERAL -- FLIGHT INTERPHONE SYSTEM - OPERATION THIS PAGE INTENTIONALLY LEFT BLANK 00-00-00 - 114 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 123 777 TRAINING MANUAL 777 GENERAL -- FLIGHT INTERPHONE SYSTEM - OPERATION General White MIC light on the upper half of the switch comes on You use controls on these panels to operate the flight Receive audio of the selected system comes on at interphone system: the volume set on the receiver control.
  • Page 124 777 TRAINING MANUAL 777 GENERAL -- FLIGHT INTERPHONE SYSTEM - OPERATION receive light comes on to show that the related The selector lets the captain or first officer use the receiver control is on. first observer audio control panel (ACP) to control their audio if their AMU audio station card or ACP has Mic/Interphone Switch a failure.
  • Page 125 777 TRAINING MANUAL CALL RTP (TYP) LIGHT LIGHT RECEIVER TRANSMIT LIGHT SWITCH ACP (TYP) RECEIVER CALL VOLUME CONTROL INIT ALTN VNAV LEGS HOLD PROG COMM EXEC MENU MIC/INT PREV NEXT PAGE PAGE SWITCH SPEAKER SPKR VOLUME CONTROL ACP (TYPICAL) FLIGHT INTERPHONE JACK FLIGHT DECK...
  • Page 126 777 TRAINING MANUAL 777 GENERAL -- CABIN INTERPHONE SYSTEM THIS PAGE INTENTIONALLY LEFT BLANK 00-00-00 - 118 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 127 777 TRAINING MANUAL 777 GENERAL -- CABIN INTERPHONE SYSTEM Purpose When you make a two-way connection, you can add a third. To add the third, use the dial to put in the Flight attendants use the cabin interphone system (CIS) other station number.
  • Page 128 777 TRAINING MANUAL 777 GENERAL -- CABIN INTERPHONE SYSTEM The CAB - CALL light on all three audio control panels (ACPs). To receive the call, push the CAB transmitter select switch. This also causes the CALL light to go off. The CAB receiver control sets the volume.
  • Page 129 777 TRAINING MANUAL STATION DIAL CODE (TYP) CABIN INTERPHONE MENU < < TRANSMITTER SELECT SWITCH < - - - - - - - - - - - - - - - - - - - - - - - - RECEIVER >...
  • Page 130 777 TRAINING MANUAL 777 GENERAL -- VHF COMMUNICATION SYSTEM General After you set the RTP, you use these ACP controls to operate the system: The very high frequency (VHF) communication system permits voice and data communication over line-of-sight Receiver volume control - push to listen to a VHF distances.
  • Page 131 777 TRAINING MANUAL ACTIVE FREQUENCY STANDBY RTP (TYP) FREQUENCY TRANSFER FREQUENCY WINDOW SWITCH WINDOW RADIO SWITCH ACP (TYP) (TYP) ACTIVE STANDBY INIT ALTN VNAV LEGS HOLD PROG COMM EXEC VHF L VHF C VHF R MENU PREV NEXT PAGE PAGE HF SENS HF L HF R...
  • Page 132 777 TRAINING MANUAL 777 GENERAL -- ELECTROSTATIC DISCHARGE SENSITIVE (ESDS) DEVICES General Training Information Point Many electronic line replaceable units (LRUs) contain When you remove a unit, do not touch the pins in the micro-circuits and other devices that electrostatic electrical connectors.
  • Page 133 777 TRAINING MANUAL WRIST STRAP LOCATION P84 RIGHT SYSTEMS CARD FILE (TYPICAL) MAIN EQUIPMENT CENTER (LOOKING FORWARD) E1 AND E2 RACKS (LOOKING AFT) EXTRACTORS CAUTION OBSERVE PRECAUTIONS FOR HANDLING ELECTROSTATIC SENSITIVE DEVICES STATIC SENSITIVE PLACARD ESDS SYMBOL AND PLACARD (TYPICAL) ESDS PRINTED CIRCUIT BOARD (TYPICAL) 777 GENERAL - ELECTROSTATIC DISCHARGE SENSITIVE (ESDS) DEVICES...
  • Page 134 777 TRAINING MANUAL 777 GENERAL -- DATA BUSES General at the same time. Some LRU/LRMs only receive ARINC 629 data. The 777 line replaceable units (LRUs) and line replaceable modules (LRMs) use different data buses. An ARINC 629 LRU/LRM sends and receives data on the ARINC 629 data bus at 2 megabits per second (Mbps).
  • Page 135 777 TRAINING MANUAL 777 GENERAL -- DATA BUSES RS-232 A 10/100 base T LRU/LRM sends and receives data at 10 Mbps on a 10 base T data bus or 100Mbps on a 100 base T The RS-232 data bus is a one-way bus that sends data on data bus.
  • Page 136 777 TRAINING MANUAL 777 GENERAL -- DATA BUSES A 1000 base F LRU/LRM sends and receives data at 1000 Mbps on the ARINC 636 data bus. 00-00-00 - 128 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 137 777 TRAINING MANUAL LRU X TRANSMIT/RECEIVE LRU X LRU Y LRU X LRU Y OTHER LRU Y LRUS RECEIVE ONLY ONE-WAY DATA BUSES TWO-WAY DATA BUSES ARINC 429 10 BASE T ARINC 453 10/100 BASE T ARINC 717 RS-485 ARINC 618 LRU Z XXX ARINC 629 BUS RS-422...
  • Page 138 777 TRAINING MANUAL 777 GENERAL -- ARINC 629 - GENERAL DESCRIPTION THIS PAGE INTENTIONALLY LEFT BLANK 00-00-00 - 130 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 139 777 TRAINING MANUAL 777 GENERAL -- ARINC 629 - GENERAL DESCRIPTION General All data on the bus is available to all the LRUs on that bus. An ARINC 629 data bus is a twisted-pair of wires with termination resistors at each end. As many as 120 LRUs ARINC 629 Data Bus Configuration can use one ARINC 629 data bus.
  • Page 140 777 TRAINING MANUAL 777 GENERAL -- ARINC 629 - GENERAL DESCRIPTION transmit until there is a stop in data movement (Bus Quiet) on the bus from other LRUs. 00-00-00 - 132 - ALTEON PROPRIETARY. Copyright. See title page for details...

  • Page 141: Termination Resistors

    777 TRAINING MANUAL LRU N-2 LRU N-1 TERMINATION RESISTORS DATA BUS CABLE CURRENT-MODE COUPLER N-1 CURRENT-MODE COUPLER 1 STUB CABLE TERMINAL CONTROLLER LRU 1 SERIAL SERIAL CURRENT-MODE INTERFACE INTERFACE COUPLER N-2 MODULE MODULE (46 MAXIMUM) TERMINATION RESISTORS 777 GENERAL - ARINC 629 - GENERAL DESCRIPTION 00-00-00 - 133 - ALTEON PROPRIETARY.
  • Page 142 777 TRAINING MANUAL 777 GENERAL -- ARINC 629 - MEC COMPONENT LOCATIONS General There are seven bus panels in the forward section on the left and right sides of the nose wheel well. Each panel has the current-mode couplers and ARINC 629 buses.
  • Page 143 777 TRAINING MANUAL P112 BUS PANEL - LEFT FLIGHT CONTROLS BUS SECTION 41 P312 BUS PANEL - CENTER FLIGHT CONTROLS BUS P211 BUS PANEL - FWD RIGHT SYSTEMS P111 BUS PANEL - FWD LEFT SYSTEMS BUS P311 BUS PANEL - CENTER 1 SYSTEMS BUS P313 BUS PANEL P212 BUS PANEL - CENTER 2 SYSTEMS BUS...
  • Page 144 777 TRAINING MANUAL 777 GENERAL -- ARINC 629 - BULK CARGO COMPARTMENT COMPONENT LOCATIONS General There are two bus panels in the aft section of the airplane. Each panel contains current-mode couplers and ARINC 629 buses. Bus Panels These are the bus panels in the aft section: P115 has the aft section of the left systems bus P215 has the aft section of the right systems bus.
  • Page 145 777 TRAINING MANUAL BULK CARGO DOOR P215 BUS PANEL P115 BUS PANEL - AFT RIGHT - AFT LEFT SYSTEMS BUS SYSTEMS BUS SECTION 47 SECTION 47 (OPPOSITE BULK CARGO DOOR) 777 GENERAL - ARINC 629 - BULK CARGO COMPARTMENT COMPONENT LOCATIONS 00-00-00 - 137 - ALTEON PROPRIETARY.
  • Page 146 777 TRAINING MANUAL 777 GENERAL -- ARINC 629 - CURRENT MODE COUPLER Purpose Location The current-mode coupler connects the bus cable to the All the current-mode couplers are on the bus panels. stub cable. Training Information Point Physical Description Couplers are interchangeable units. Covers and bases There are different suppliers for current-mode from different suppliers are not interchangeable.
  • Page 147 777 TRAINING MANUAL QUARTER-TURN FASTENER QUARTER-TURN FASTENER COUPLER COVER COUPLER COVER COUPLERS WIRE RECEPTACLE GUIDES COUPLING WIRE LATCH GUIDES RECEPTACLE CAPTIVE SCREWS COUPLER BASE E-CORE E-CORE COUPLING COUPLING CAPTIVE SCREWS SLOT COUPLER BASE LATCH COUPLER-AMPHENOL (DUAL PIECE) COUPLER-SCI (DUAL PIECE) PANEL BUS PANEL (COVER REMOVED) (TYPICAL)
  • Page 148 777 TRAINING MANUAL 777 GENERAL -- ARINC 629 - DATA BUS CABLE Purpose bus panel (P215) with a production break in the aft cargo compartment at station 1465. The bus cable moves data between LRUs. A current-mode coupler and a stub cable attach each LRU terminal to Training Information Point the data bus cable.

  • Page 149: Termination Resistor

    777 TRAINING MANUAL INDIVIDUAL WIRE TEFLON SKIN CONDUCTOR FOAM TERMINATION RESISTOR CROSS-SECTION OF A WIRE OF A DATA BUS CABLE (TYPICAL) TERMINATION RESISTORS PANEL BUS CABLE (TYPICAL) PRODUCTION SHIELDED DATA BREAK BUS CABLE CABLE CONNECTOR COUPLER PANEL MOUNTING PANEL BUS CABLE TERMINATION CONNECTOR...
  • Page 150 777 TRAINING MANUAL 777 GENERAL -- ARINC 629 - STUB CABLE Purpose The stub cables are for bi-directional data movement between the LRU and the current-mode coupler. The stub cables also supply power from the LRUs to the current- mode couplers. Physical Description A stub cable has four wires.
  • Page 151 777 TRAINING MANUAL ARINC 600 CONNECTOR (TYPICAL) STUB CABLES (TWO SHIELDED TWISTED PAIRS) STANCHION DISCONNECT LRU TRAY STUB CABLE (FOUR CONDUCTORS SHIELDED WITH OVERALL SHIELD) ARINC 629 CURRENT-MODE COUPLER 777 GENERAL - ARINC 629 - STUB CABLE 00-00-00 - 143 - ALTEON PROPRIETARY.
  • Page 152 777 TRAINING MANUAL 777 GENERAL -- OVERHEAD PANEL ARINC 629 SYSTEM (OPAS) General Physical Description The overhead panel ARINC 629 system (OPAS) moves data The OPAS has six parts: between many flight deck switches and lights and the ARINC 629 systems buses. Left and right OPCFs Left and right PDCUs The OPAS moves data through overhead panel card files...
  • Page 153 777 TRAINING MANUAL SWITCHES AND LIGHTS ON PANELS: LEFT SYSTEMS Ñ P5 ARINC 629 BUS Ñ P61 OPCF (2) SWITCHES AND LIGHTS ON PANELS: Ñ P1 Ñ P3 RIGHT SYSTEMS Ñ P7 ARINC 629 BUS Ñ P8 OPBC (2) Ñ P9 Ñ...
  • Page 154 777 TRAINING MANUAL 777 GENERAL -- ARINC 629 SIGNAL GATEWAY (ASG) CARDS General The ARINC 629 signal gateway (ASG) cards change data format from ARINC 429 to ARINC 629, and from ARINC 629 to ARINC 429. The cards move data between the interface cards in the systems card files and ARINC 629 system buses.
  • Page 155 777 TRAINING MANUAL LEFT SYSTEMS ARINC 629 BUS Ñ INTERFACE LEFT ASG CARD (2) CARDS IN LEFT AND RIGHT SYSTEM CARD FILES Ñ FWD AND AFT CARGO SMOKE DETECTORS RIGHT SYSTEMS ARINC 629 BUS RIGHT ASG CARD (2) 777 GENERAL - ARINC 629 SIGNAL GATEWAY (ASG) CARDS 00-00-00 - 147 - ALTEON PROPRIETARY.
  • Page 156 777 TRAINING MANUAL STRUCTURES -- INTRODUCTION General These chapters give an overview of these parts of the airplane: Nose Radome (chapter 53) Fuselage (53) Wings (57) Vertical stabilizer (55) Horizontal stabilizer (55) Wing-to-body fairing (53) Pylon (54). Abbreviations and Acronyms - air drive unit - buttock line - environmental control system...
  • Page 157 777 TRAINING MANUAL VERTICAL STABILIZER WING HORIZONTAL STABILIZER WING-TO-BODY FAIRING FUSELAGE PYLON NOSE RADOME STRUCTURES - INTRODUCTION 51-00-00 - 149 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 158 777 TRAINING MANUAL STRUCTURES -- COMPOSITE MATERIALS General Some airplane structure and parts are made of composite materials instead of aluminum. Composite materials are lighter and more resistant to corrosion than aluminum. Composite materials are layers (plies) of carbon or fiberglass in a mixture of plastic resin.
  • Page 159 777 TRAINING MANUAL VERTICAL STABILIZER AILERON TORQUE BOX STABILIZER WING FIXED TORQUE BOX RUDDER LEADING EDGE ELEVATOR FLOOR BEAMS OUTBOARD FLAP TRAILING EDGE PANELS PYLON FWD AND LEADING AND TRAILING AFT FAIRINGS EDGE PANELS WING-TO-BODY FAIRING FLAPS FLAPERON NOSE GEAR INBOARD AND DOORS OUTBOARD SPOILERS...
  • Page 160 777 TRAINING MANUAL STRUCTURES -- STATION NUMBERS, WATER LINES, AND BUTTOCK LINES General These designated numbers help you find areas of the airplane: Water line (WL) Buttock line (BL) Station (Sta). The water line is a height measurement in inches from a reference plane below the airplane.
  • Page 161 777 TRAINING MANUAL WL 343.14 RBL 381 LBL 381 WL 200.5 WL 122.5 WL 700 RBL 82 BL 0 LBL 82 WL 13.5 STA 867 STA 92.5 STA 1643 STA 2042.5 STA 2562 STRUCTURES - STATION NUMBERS, WATER LINES, AND BUTTOCK LINES 51-00-00 - 153 - ALTEON PROPRIETARY.
  • Page 162 777 TRAINING MANUAL FUSELAGE -- INTRODUCTION General The sections attach to each other with rivets in all places except the floor and the aft cargo door (not The fuselage is a semi-monocoque structure. This means shown). At those places the sections attach with hi- that the skin gives structural support to the fuselage.
  • Page 163 777 TRAINING MANUAL SEC 48 SEC 47 TAILCONE SEC 46 AFT PRESSURE SEC 44 BULKHEAD SEC 45 SEC 43 FLOOR BEAMS SEC 41 WING-TO-BODY FAIRING KEEL BEAM FRAMES NOSE STRINGERS RADOME FWD PRESSURE BULKHEAD FUSELAGE - INTRODUCTION 53-00-00 - 155 - ALTEON PROPRIETARY.
  • Page 164 777 TRAINING MANUAL FUSELAGE -- NOSE RADOME General The nose radome is a fairing on the nose of the airplane. You open it to get access to these antennas: Instrument landing system (ILS) localizer antennas ILS glideslope capture antennas Weather radar antenna. Nose Radome Parts The nose radome has these parts: Snubbers (2)
  • Page 165 777 TRAINING MANUAL SNUBBER LEFT AND RIGHT HINGE LOCALIZER ANTENNA HOLD OPEN FITTING (2) WEATHER RADAR ANTENNA CENTER LOCALIZER ANTENNA LEFT AND RIGHT GLIDESLOPE CAPTURE ANTENNA LIGHTNING DIVERTER STRIP (6) LATCH (6) CENTER GLIDESLOPE CAPTURE ANTENNA FUSELAGE - NOSE RADOME 53-00-00 - 157 - ALTEON PROPRIETARY.
  • Page 166 777 TRAINING MANUAL FUSELAGE -- WING-TO-BODY FAIRING General RAT service door RAT door The wing-to-body fairing is made of composite panels Main wheel well electrical service panel. with a honeycomb core. It has many panels and doors for inspection and servicing. Panels and Doors These panels and doors are on each side of the wing-to- body fairing:...
  • Page 167 777 TRAINING MANUAL JACK PAD COVER ECS RAM AIR INLET HEAT EXCHANGER DOOR HIGH PRESSURE ECS RAM AIR PNEUMATIC OUTLET PANEL CONNECTION DOOR HEAT EXCHANGER BLOWOUT DOOR TRAILING EDGE FLAP DOOR ADU FILTER ACCESS DOOR ADU ACCESS LOW PRESSURE DOOR PNEUMATIC CONNECTION DOOR ADU PRESSURE...
  • Page 168 777 TRAINING MANUAL WINGS -- TOP General The wing has an aluminum structure and is covered by aluminum skin panels. These components attach to the wing structure: Engine pylon Flight control surfaces Wing tip. 57-00-00 - 160 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 169 777 TRAINING MANUAL ENGINE PYLON LEADING EDGE SLAT (7) INBOARD AFT FLAP FLAPERON INBOARD MAIN FLAP SPOILER (7) OUTBOARD FLAP WING TIP AILERON WINGS - TOP 57-00-00 - 161 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 170 777 TRAINING MANUAL WINGS -- BOTTOM General The wing has an aluminum structure and is covered by aluminum skin panels. These components attach to the wing structure: Engine pylon Landing gear strut (not shown) Flight control surfaces Fairings. The fairings cover the flap drive units and the wing tip.
  • Page 171 777 TRAINING MANUAL DRY BAY ACCESS DOOR CENTER FUEL TANK ACCESS DOOR (3) ENGINE PYLON LEADING EDGE SLATS (7) WING LANDING GEAR DOOR WING FUEL TANK ACCESS DOOR (40) INBOARD AFT FLAP SURGE TANK ACCESS DOOR (2) WING TIP INBOARD FLAPERON ACCESS DOOR (13) MAIN FLAP...
  • Page 172 777 TRAINING MANUAL PYLON -- GENERAL DESCRIPTION General The pylon attaches to the wing and contains the strut (not shown). The strut supports the engine with forward and aft engine mounts. The pylon also contains these parts: Electrical lines Fuel lines Hydraulic lines Pneumatic lines Fairings.
  • Page 173 777 TRAINING MANUAL FUSE PIN PRESSURE RELIEF DOOR ACCESS DOOR STRUT ACCESS DOORS PYLON PYLON - GENERAL DESCRIPTION 54-00-00 - 165 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 174 777 TRAINING MANUAL STABILIZERS -- HORIZONTAL STABILIZER General The horizontal stabilizer is made of solid laminate carbon fiber reinforced plastic. Separate skin panels cover these areas: Auxiliary spar-to-front spar Front spar-to-rear spar Rear spar-to-trailing edge. The auxiliary box structure is aluminum. The horizontal stabilizer also has secondary structures attached to it.
  • Page 175 777 TRAINING MANUAL LEADING EDGE AUXILIARY SPAR-TO-FRONT SPAR PANEL VERTICAL STABILIZER (REF) FRONT SPAR-TO-REAR SPAR PANEL TIP FAIRING ELEVATOR REAR SPAR-TO-TRAILING EDGE PANEL NOTE: LEFT HALF OF HORIZONTAL STABILIZER IS SHOWN STABILIZERS - HORIZONTAL STABILIZER 55-00-00 - 167 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 176 777 TRAINING MANUAL STABILIZERS -- VERTICAL STABILIZER General The vertical stabilizer is made of solid laminate carbon fiber reinforced plastic. Separate skin panels cover these areas: Auxiliary spar-to-front spar Front spar-to-rear spar Rear spar-to-trailing edge. The auxiliary box structure is aluminum. These secondary structures attach to the vertical stabilizer: Leading edge...
  • Page 177 777 TRAINING MANUAL TIP FAIRING REAR FRONT SPAR-TO- SPAR-TO-TRAILING REAR SPAR PANEL EDGE PANEL AUXILIARY RUDDER HINGE SPAR-TO-FRONT SPAR PANEL RUDDER LEADING EDGE RUDDER TAB SECTION 48 (REF) STABILIZERS - VERTICAL STABILIZER 55-00-00 - 169 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 178 777 TRAINING MANUAL ARINC 629 -- INTRODUCTION General - read only memory - receive personality PROM An ARINC 629 data bus is an electronic data movement - receive input line 1 system. It connects multiple line replaceable units - receive input line 2 (LRUs) in one communication loop.
  • Page 179 777 TRAINING MANUAL ARINC 629 DATA BUS TYPICAL TYPICAL TYPICAL ARINC 629 - INTRODUCTION 23-91-00 - 171 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 180 777 TRAINING MANUAL ARINC 629 -- GENERAL DESCRIPTION THIS PAGE INTENTIONALLY LEFT BLANK 23-91-00 - 172 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 181 777 TRAINING MANUAL ARINC 629 -- GENERAL DESCRIPTION General All data on the bus is available to all the LRUs on that bus. An ARINC 629 data bus is a twisted-pair of wires with termination resistors at each end. As many as 120 LRUs ARINC 629 Data Bus Configuration can use one ARINC 629 data bus.
  • Page 182 777 TRAINING MANUAL ARINC 629 -- GENERAL DESCRIPTION transmit until there is a stop in data movement (Bus Quiet) on the bus from other LRUs. 23-91-00 - 174 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 183 777 TRAINING MANUAL LRU N-2 LRU N-1 TERMINATION RESISTORS DATA BUS CABLE CURRENT-MODE COUPLER N-1 CURRENT-MODE COUPLER 1 STUB CABLE CURRENT-MODE COUPLER N-2 TERMINAL CONTROLLER LRU 1 SERIAL CURRENT-MODE INTERFACE COUPLER N-2 MODULE (46 MAXIMUM) TERMINATION RESISTORS ARINC 629 - GENERAL DESCRIPTION 23-91-00 - 175 - ALTEON PROPRIETARY.
  • Page 184 777 TRAINING MANUAL ARINC 629 -- FORWARD COMPONENT LOCATIONS General There are seven bus panels in the forward section on the left and right sides of the nose wheel well. Each panel has the current-mode couplers and ARINC 629 buses. Bus Panels These are the seven bus panels in the forward section: P111 - Forward section of left systems ARINC 629...
  • Page 185 777 TRAINING MANUAL P112 BUS PANEL - LEFT FLIGHT CONTROLS BUS SECTION 41 P312 BUS PANEL - CENTER FLIGHT CONTROLS BUS P211 BUS PANEL - FWD RIGHT SYSTEMS P111 BUS PANEL - FWD LEFT SYSTEMS BUS P311 BUS PANEL - CENTER 1 SYSTEMS BUS P313 BUS PANEL P212 BUS PANEL - CENTER 2 SYSTEMS BUS...
  • Page 186 777 TRAINING MANUAL ARINC 629 -- AFT COMPONENT LOCATIONS General There are two bus panels in the aft section of the airplane. Each panel contains current-mode couplers and ARINC 629 buses. Bus Panels These are the bus panels in the aft section: P115 has the aft section of the left systems bus P215 has the aft section of the right systems bus.
  • Page 187 777 TRAINING MANUAL P215 BUS PANEL BULK CARGO DOOR Ñ AFT RIGHT SYSTEMS BUS P115 BUS PANEL Ñ AFT LEFT SYSTEMS BUS SECTION 47 SECTION 47 (OPPOSITE BULK CARGO DOOR) ARINC 629 - AFT COMPONENT LOCATIONS 23-91-00 - 179 - ALTEON PROPRIETARY.
  • Page 188 777 TRAINING MANUAL ARINC 629 -- SYSTEMS BUS PRODUCTION BREAKS General There is a production break in the left systems ARINC 629 bus and in the right systems ARINC 629 bus. The break divides the bus in two parts to help in removal and installation.
  • Page 189 777 TRAINING MANUAL STATION 1465 STATION 1465 AFT CARGO AREA CEILING PANEL FORWARD BULKHEAD OF AFT CARGO AREA LEFT SYSTEMS BUS PRODUCTION BREAK RIGHT SYSTEMS BUS PRODUCTION BREAK SYSTEMS ARINC 629 BUSES ARINC 629 - SYSTEMS BUS PRODUCTION BREAKS 23-91-00 - 181 - ALTEON PROPRIETARY.
  • Page 190 777 TRAINING MANUAL ARINC 629 -- SYSTEMS BUS INTERFACES THIS PAGE INTENTIONALLY LEFT BLANK 23-91-00 - 182 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 191 777 TRAINING MANUAL ARINC 629 -- SYSTEMS BUS INTERFACES General Warning electronic system - WES-L CH 1 Autopilot flight director computer-left (AFDC) These are the four systems ARINC 629 buses: Engine data interface unit - EDIU-L CH A & CH B Passenger address/cabin interphone (PA/CI) Left systems bus controller...
  • Page 192 777 TRAINING MANUAL ARINC 629 -- SYSTEMS BUS INTERFACES Center 2 Systems ARINC 629 Bus Cabin system management unit (CSMU) Control display units (CDU) These LRUs/systems transmit and receive on the center 2 Airplane information management system (AIMS). systems bus: These LRUs also have a receive-only connection to the Engine data interface unit - EDIU-L CH B &...
  • Page 193 777 TRAINING MANUAL RIGHT LEFT CENTER 1 CENTER 2 BPCU GCU-L BPCU GCU-APU GCU-L GCU-R GCU-APU BU CONVERTER EDIU-R CH C GCU-R LSCF EDIU-R CH A BU CONVERTER RSCF FSEU-1 EDIU-L CH C LSCF P110 FSEU-2 EDIU-L CH B RSCF P210 WES-R CH 1 AIMS-R...
  • Page 194 777 TRAINING MANUAL ARINC 629 -- FLIGHT CONTROLS BUS INTERFACES THIS PAGE INTENTIONALLY LEFT BLANK 23-91-00 - 186 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 195 777 TRAINING MANUAL ARINC 629 -- FLIGHT CONTROLS BUS INTERFACES General Center Flight Controls ARINC 629 Bus These are the three flight controls ARINC 629 buses: These LRUs transmit and receive on the center flight controls bus. They are: Left flight controls bus Center flight controls bus Secondary attitude air data reference unit (SAARU) Right flight controls bus.
  • Page 196 777 TRAINING MANUAL ARINC 629 -- FLIGHT CONTROLS BUS INTERFACES Primary flight computer - R (PFC) Actuator control electronics - R (ACE). These LRUs also have a receive only connection to the right flight controls bus. They are: Secondary attitude air data reference unit (SAARU) Airplane information management system (AIMS) Control display unit - R (CDU) Autopilot flight director computers - L &...
  • Page 197 777 TRAINING MANUAL RIGHT LEFT CENTER ADIRU-1 ADIRU-1 ADIRU-2 SAARU ADIRU-2 AIMS-L1 ADM TP-C AIMS-R3 AIMS-L2 ADM SP-C AIMS-R4 AIMS-R1 AFDC-C AIMS-L3 ADM TP-L PSA-C ADM TP-R ADM SP-L PFC-C1 ADM SP-R AFDC-L PFC-C2 AFDC-R PSA-L PFC-C3 PSA-R PFC-L1 ACE-C PFC-R1 PFC-L2 SAARU...
  • Page 198 777 TRAINING MANUAL ARINC 629 -- CURRENT-MODE COUPLER Purpose Location The current-mode coupler connects the bus cable to the All the current-mode couplers are on the bus panels. stub cable. Training Information Point Physical Description Couplers are interchangeable units. Covers and bases There are different suppliers for current-mode from different suppliers are not interchangeable.
  • Page 199 777 TRAINING MANUAL QUARTER-TURN FASTENER QUARTER-TURN FASTENER COUPLER COVER COUPLER COVER COUPLERS WIRE GUIDES RECEPTACLE COUPLING WIRE LATCH RECEPTACLE GUIDES CAPTIVE SCREWS (FOUR PLACES) COUPLER BASE E-CORE E-CORE COUPLING COUPLING CAPTIVE SCREWS SLOT LATCH (FOUR PLACES) COUPLER BASE COUPLER-AMPHENOL (DUAL PIECE) COUPLER-SCI (DUAL PIECE) PANEL BUS PANEL (COVER REMOVED)
  • Page 200 777 TRAINING MANUAL ARINC 629 -- BUS CABLE AND BUS PANEL Purpose to the aft bus panel (P215). There is a production break in the aft cargo compartment at station 1465. The bus cable moves data between LRUs. A current-mode coupler and a stub cable attach each LRU terminal to Training Information Point the data bus cable.
  • Page 201 777 TRAINING MANUAL TEFLON SKIN INDIVIDUAL WIRE CONDUCTOR FOAM TERMINATION RESISTOR TERMINATION RESISTORS CROSS-SECTION OF A WIRE OF A DATA BUS CABLE (TYPICAL) PANEL BUS CABLE (TYPICAL) SHIELDED DATA BUS CABLE BUS CABLE CONNECTOR PANEL BUS CABLE PRODUCTION TERMINATION BREAK CONNECTOR RESISTOR COUPLER PANEL MOUNTING...
  • Page 202 777 TRAINING MANUAL ARINC 629 -- STUB CABLE Purpose The stub cables are for bi-directional data movement between the LRU and the current-mode coupler. The stub cables also supply power from the LRUs to the current- mode couplers. Physical Description A stub cable has four wires.
  • Page 203 777 TRAINING MANUAL ARINC 600 CONNECTOR (TYPICAL) STUB CABLES (TWO SHIELDED TWISTED PAIRS) STANCHION LRU TRAY DISCONNECT STUB CABLE (FOUR CONDUCTORS SHIELDED WITH OVERALL SHIELD) ARINC 629 CURRENT-MODE COUPLER ARINC 629 - STUB CABLE 23-91-00 - 195 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 204 777 TRAINING MANUAL ARINC 629 -- CURRENT-MODE COUPLER FUNCTIONAL DESCRIPTION THIS PAGE INTENTIONALLY LEFT BLANK 23-91-00 - 196 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 205 777 TRAINING MANUAL ARINC 629 -- CURRENT-MODE COUPLER FUNCTIONAL DESCRIPTION General Power A current mode coupler (CMC), together with a serial The coupler rectifier receives power from the SIM interface module (SIM) supplies the interface between through the transmit and receive stub cables. The the ARINC 629 data bus cable and an ARINC 629 terminal voltage is a nominal 30v dc derived from the LRU controller in the LRU.
  • Page 206 777 TRAINING MANUAL ARINC 629 -- CURRENT-MODE COUPLER FUNCTIONAL DESCRIPTION Shutdown Operation The SIM will shut off all power to the CMC if the overcurrent protection function senses excessive current draw over the transmit/receive stubs. The terminal controller in the LRU can also command the SIM to shut off power to the CMC.
  • Page 207 777 TRAINING MANUAL 629 DATA BUS TRANSMIT TRANSMIT STUB CABLE DRIVER 1 TRANSMIT TRANSMIT INTERFACE DRIVER 2 CHANNEL SELECT LOGIC RECTIFIER RECEIVE STUB CABLE RECEIVE RECEIVER 1 INTERFACE RECEIVER 2 ARINC 629 LRU CURRENT MODE COUPLER (TYPICAL) ARINC 629 - CURRENT-MODE COUPLER FUNCTIONAL DESCRIPTION 23-91-00 - 199 - ALTEON PROPRIETARY.
  • Page 208 777 TRAINING MANUAL ARINC 629 -- LRU FUNCTIONAL DESCRIPTION General SIM Monitor Functions An ARINC 629 LRU contains a serial interface module The SIM monitors the waveform quality of its own (SIM) and a terminal controller. These two components transmitted signals as well as signals received from control the transfer of data between the LRU and the other LRUs.
  • Page 209 777 TRAINING MANUAL ARINC 629 -- LRU FUNCTIONAL DESCRIPTION Each LRU has a time period in which it may transmit. The receiver circuit monitors all signals on the data bus. After a LRU transmits, the control function measures the time and makes sure that it does not transmit again When it finds a message label on the bus, it knows if until all the other LRUs on the bus have transmitted the message is good or not based on the message...
  • Page 210 777 TRAINING MANUAL ARINC 629 -- LRU FUNCTIONAL DESCRIPTION The transmit function stops operation if there are repeated transmit signal errors. Power to the LRU must be reset to continue transmit operation. If the monitor function does not operate, all data transmission from the LRU will stop.
  • Page 211 777 TRAINING MANUAL MICROPROCESSOR MODULATION TRANSMITTER FAULT MONITOR SUBSYSTEM SUBSYSTEM AND CONTROL MEMORY INTERFACE DEMODULATION RECEIVER TRANSMIT SERIAL INTERFACE MODULE CURRENT MODE PERSONALITY COUPLER PROM CONTROL RECEIVE PERSONALITY PROM TERMINAL CONTROLLER ARINC 629 LRU ARINC 629 - LRU FUNCTIONAL DESCRIPTION 23-91-00 - 203 - ALTEON PROPRIETARY.
  • Page 212 777 TRAINING MANUAL ARINC 629 -- MESSAGE STRUCTURE FUNCTIONAL DESCRIPTION General A pulse of one half-bit time, called the pre-sync sync pulse (PSSP), comes before the first label word of a Data in the ARINC 629 system moves through the data bus message.
  • Page 213 777 TRAINING MANUAL SET OF MESSAGES ON DATA BUS MESSAGE MESSAGE MESSAGE ONE MESSAGE Ñ Ñ Ñ WORD STRING 1 N( 31) WORD STRING 2 TERMINAL GAP 4 BIT GAP ONE WORD STRING LABEL WORD DATA WORD DATA WORD DATA WORD M( 256) .
  • Page 214 777 TRAINING MANUAL ARINC 629 -- TIMING FUNCTIONAL DESCRIPTION THIS PAGE INTENTIONALLY LEFT BLANK 23-91-00 - 206 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 215 777 TRAINING MANUAL ARINC 629 -- TIMING FUNCTIONAL DESCRIPTION General Synchronization Gap (SG) Because an ARINC 629 bus has many LRUs connected to it The SG is used to maintain synchronization on the bus. so there must be a method to control when the LRUs can All LRUs on a specific bus have the same SG.
  • Page 216 777 TRAINING MANUAL ARINC 629 -- TIMING FUNCTIONAL DESCRIPTION Summary After an LRU has transmitted to the bus, it can only transmit again if the bus is quiet and the following three conditions are met: TI has expired The bus has been quiet for a period longer than the The bus has been quiet for a period equal to or greater than the TG after the SG has elapsed.
  • Page 217 777 TRAINING MANUAL LRU A LRU A TRANSMITS LRU B TRANSMITS AGAIN LRU B TRANSMITS TRANSMITS AGAIN SG(A) LRU A TIMERS TI(A) SG(B) LRU B TIMERS TI(B) SG(C) LRU C TIMERS TI(C) ARINC 629 - TIMING FUNCTIONAL DESCRIPTION 23-91-00 - 209 - ALTEON PROPRIETARY.
  • Page 218 777 TRAINING MANUAL ARINC 629 -- PERIODIC MODE TIMING FUNCTIONAL DESCRIPTION THIS PAGE INTENTIONALLY LEFT BLANK 23-91-00 - 210 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 219 777 TRAINING MANUAL ARINC 629 -- PERIODIC MODE TIMING FUNCTIONAL DESCRIPTION General Data base loads Maintenance BITE. An ARINC 629 data bus uses these three timers: In aperiodic operation, the LRUs transmit in order of Transmit interval (TI) shortest TG to longest TG. Synchronization gap (SG) Terminal gap (TG).
  • Page 220 777 TRAINING MANUAL ARINC 629 -- PERIODIC MODE TIMING FUNCTIONAL DESCRIPTION At event 8, all three SG timers are complete and the TG At event 6, LRU 2 no longer transmits and all three timers start. LRUs start their SG timers. At event 9, the TG for LRU 1 completes but its TI At event 7, all three SG timers are complete and the TG continues, so it does not transmit.
  • Page 221 777 TRAINING MANUAL EVENT 8 9 10 11 8 9 10 11 LRU 1 LRU 2 LRU 3 PERIODIC MODE EVENT LRU 1 LRU 2 LRU 3 APERIODIC MODE NOTE: ONLY ELAPSED TIMERS ARE SHOWN. ARINC 629 - PERIODIC MODE TIMING FUNCTIONAL DESCRIPTION 23-91-00 - 213 - ALTEON PROPRIETARY.
  • Page 222 777 TRAINING MANUAL ARINC 629 -- TEST Tests The maintenance access terminal (MAT) on the P18 panel is used to do the ARINC 629 Multi Transmitter Data Bus - Operational Test. The central maintenance computing function (CMCF) does not have a specified ARINC 629 system test to check the entire system.

  • Page 223: System Configuration

    777 TRAINING MANUAL LINE SYSTEM CONFIGURATION EXTENDED MAINTENANCE MAINTENANCE Select ATA System (27) INBOUND FLIGHT XX Aaaaaaaaaaaaaaaaaaaaa DECK EFFECTS XX Bbbbbbbbbbbbbbbbbbbbb EXISTING FLIGHT XX Ccccccccccccccccccccc DECK EFFECTS XX Ddddddddddddddddddddd XX Eeeeeeeeeeeeeeeeeeeee GROUND TESTS XX Fffffffffffffffffffff 22 Autopilot Flight Director System SYSTEM CONFIGURATION XX Ggggggggggggggggggggg...
  • Page 224 777 TRAINING MANUAL ARINC 629 -- OVERALL INTERFACE DIAGRAM Interface This page is for reference only. 23-91-00 - 216 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 225 777 TRAINING MANUAL ARINC 629 SYSTEM BUSES ELMS ELMS ELMS BPCU GCU-L GCU-APU GCU-R SCF-L SCF-R PSEU-1 PSEU-2 BU CONV FQIS PWP-L PWP-STBY PWP-R ARINC 629 FLIGHT CONTROL ARINC 629 BUSES FLIGHT CONTROL BUSES APUC ADIRU ACE-L1 AVM-L SAARU ACE-L2 AVM-R AIMS-L ACE-C...
  • Page 226 777 TRAINING MANUAL ARINC 629 -- OVERALL FUNCTIONAL DESCRIPTION DIAGRAM Functional Description THIS PAGE INTENTIONALLY LEFT BLANK. 23-91-00 - 218 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 227 777 TRAINING MANUAL 629 DATA BUS TRANSMIT DRIVER 1 TRANSMIT MICRO- MODULATION TRANSMITTER TRANSMIT INTERFACE PROCESSOR DRIVER 2 CHANNEL SUBSYSTEM FAULT MONITOR SUBSYSTEM SELECT MEMORY INTERFACE AND CONTROL LOGIC RECEIVER DEMODULATION RECTIFIER TRANSMIT PERSONALITY PROM RECEIVE RECEIVE CONTROL DRIVER 1 INTERFACE RECEIVE PERSONALITY...
  • Page 228 777 TRAINING MANUAL OVERHEAD PANEL ARINC 629 SYSTEM -- INTRODUCTION General OPIC - overhead panel interface card PDCU - panel data concentrator unit The overhead panel ARINC 629 system (OPAS) sends flight deck switch position data to the ARINC 629 systems buses.
  • Page 229 777 TRAINING MANUAL ARINC 629 DATA BUS OPAS SWITCHES LIGHTS OVERHEAD PANEL ARINC 629 SYSTEM - INTRODUCTION 23-93-00 - 221 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 230 777 TRAINING MANUAL OPAS -- GENERAL DESCRIPTION General The OPAS gets flight deck switch position and indicator data from flight deck equipment. It moves this data through the overhead panel card files (OPCFs) and panel data concentrator units (PDCUs). The overhead panel bus controllers (OPBCs) are the interface units for the ARINC 629 buses.
  • Page 231 777 TRAINING MANUAL SWITCHES AND LIGHTS ON PANELS: - P5 - P61 LEFT SYSTEMS ARINC 629 BUS OPCF (2) SWITCHES AND LIGHTS ON PANELS: - P1 - P3 - P7 - P8 - P9 RIGHT SYSTEMS - P10 PDCU (2) OPBC (2) ARINC 629 BUS - P55...
  • Page 232 777 TRAINING MANUAL OPAS -- COMPONENT LOCATIONS General These are the OPAS components in the flight deck: Left and right overhead panel card files (OPCFs) Left and right panel data concentrator units (PDCUs) Left and right overhead panel bus controllers (OPBCs).
  • Page 233 777 TRAINING MANUAL LEFT OPCF RIGHT OPCF LEFT OPBC LEFT PDCU RIGHT PDCU RIGHT OPBC OPAS - COMPONENT LOCATIONS 23-93-00 - 225 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 234 777 TRAINING MANUAL OPAS -- OVERHEAD PANEL CARD FILES INTERFACES General There are two overhead panel card files (OPCFs). Each OPCF has two interchangeable overhead panel interface cards (OPICs). These are cards A1 and A2. The OPICs send data to the right and left overhead panel bus controllers (OPBCs) on RS 485 buses.
  • Page 235 777 TRAINING MANUAL 28V DC RIGHT BUS OPAS 2 P11 OVERHEAD CIRCUIT BREAKER PANEL OPIC A2 OPIC A1 RIGHT OPCF P5 AND P61 PANELS RIGHT OPBC OPIC A2 28V DC CAPT FLT INST BUS OPAS 1 OPIC A1 P11 OVERHEAD CIRCUIT LEFT OPCF BREAKER PANEL ARINC 629...
  • Page 236 777 TRAINING MANUAL OPAS -- PANEL DATA CONCENTRATOR UNITS INTERFACES General Switches and lights in the flight deck connect to the right and left panel data concentrator units (PDCUs). The PDCUs connect to the right and left overhead panel bus controllers (OPBCs). The OPBCs connect to the left and right systems ARINC 629 buses.
  • Page 237 777 TRAINING MANUAL 28V DC CAPT BUS OPAS 3 P11 OVERHEAD CIRCUIT BREAKER PANEL RIGHT PDCU RIGHT OPBC P1, P3, P7, P8, P9, P10 AND P55 PANELS 28V DC CAPT FLT INST BUS RS 485 (TYP) OPAS 1 P11 OVERHEAD CIRCUIT LEFT PDCU LEFT OPBC ARINC 629...
  • Page 238 777 TRAINING MANUAL OPAS -- OVERHEAD PANEL CARD FILES Purpose The overhead panel card files (OPCFs) send switch position data from the P5 and P61 panels to the overhead panel bus controllers (OPBCs). They also get data from the OPBCs to control some lights in the P5 and P61 panels.
  • Page 239 777 TRAINING MANUAL OPCF CHASSIS ELECTRICAL CONNECTOR COVER ELECTRICAL CONNECTOR OVERHEAD PANEL INTERFACE CARD A2 OVERHEAD PANEL INTERFACE CARD A1 OPAS - OVERHEAD PANEL CARD FILES 23-93-00 - 231 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 240 777 TRAINING MANUAL OPAS -- OVERHEAD PANEL CARD FILES FUNCTIONAL DESCRIPTION General OPIC Operation Each overhead panel card file (OPCF) has two overhead The multiplexer receives inputs from the panel panel interface cards (OPICs), A1 and A2. The positions switches. It selects a signal from one switch at a time of many switches in the P5 and P61 panels go to the and sends it to the microprocessor.
  • Page 241 777 TRAINING MANUAL FAULT MONITOR MULTIPLEXER RS485 RIGHT OPBC PANEL SWITCH (TYPICAL) SERIAL PORT RS485 LEFT MASTER OPBC DIM AND MICROPROCESSOR TEST DEMULTIPLEXER CHANNEL PROGRAM PANEL LIGHT (TYPICAL) PINS 36 CIRCUITS OPIC A2 LEFT OPBC RIGHT SAME AS OPIC A2 OPBC OPIC A1 RIGHT OPCF...
  • Page 242 777 TRAINING MANUAL OPAS -- PANEL DATA CONCENTRATOR UNIT Purpose The panel data concentrator units (PDCUs) send switch position data from some flight deck panels to the overhead panel bus controllers (OPBCs). They also get data from the OPBCs to turn on and off some panel lights.
  • Page 243 777 TRAINING MANUAL ELECTRICAL CONNECTOR PDCU (TYPICAL) OPAS - PANEL DATA CONCENTRATOR UNIT 23-93-00 - 235 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 244 777 TRAINING MANUAL OPAS -- PANEL DATA CONCENTRATOR UNIT INSTALLATION General The left panel data concentrator unit (PDCU) is in the flight deck. It is near the floor between the captains rudder pedals. The right PDCU is in the same location between the first officers rudder pedals.
  • Page 245 777 TRAINING MANUAL LEFT PDCU CAPTAIN'S RUDDER PEDAL AREA OPAS - PANEL DATA CONCENTRATOR UNIT INSTALLATION 23-93-00 - 237 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 246 777 TRAINING MANUAL OPAS -- PANEL DATA CONCENTRATOR UNITS FUNCTIONAL DESCRIPTION General the serial ports to control lights. It also sends data to the demultiplexer. The panel data concentrator units (PDCUs) send RS485 serial switch position data to the overhead panel bus The demultiplexer controls the output to the lights.
  • Page 247 777 TRAINING MANUAL FAULT 80 CHANNELS MONITOR MULTIPLEXER RS485 SERIAL RIGHT OPBC PORT MICROPROCESSOR PANEL SWITCH (TYPICAL) LEFT DEMULTIPLEXER SERIAL OPBC PORT 18 CIRCUITS RIGHT PDCU RIGHT OPBC MASTER DIM AND SAME AS RIGHT PDCU TEST LEFT PANEL LIGHT OPBC (TYPICAL) LEFT PDCU OPAS - PANEL DATA CONCENTRATOR UNITS FUNCTIONAL DESCRIPTION...
  • Page 248 777 TRAINING MANUAL OPAS -- OVERHEAD PANEL BUS CONTROLLERS Purpose Two overhead panel bus controllers (OPBCs) are the OPAS interface with the ARINC 629 system buses. Physical Description An OPBC weighs 6.6 pounds. The dimensions are: Length - 10 inches Width - 7.6 inches Height - 4.9 inches.
  • Page 249 777 TRAINING MANUAL LEFT OPBC RIGHT OPBC OPAS - OVERHEAD PANEL BUS CONTROLLERS 23-93-00 - 241 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 250 777 TRAINING MANUAL OPAS -- OVERHEAD PANEL BUS CONTROLLER INSTALLATION Left OPBC The left overhead panel bus controller (OPBC) is behind a panel at the back of the captain storage cabinet. Right OPBC The right OPBC is under a panel in the storage cabinet adjacent to the MAT.
  • Page 251 777 TRAINING MANUAL RIGHT LEFT OPBC OPBC FLIGHT DECK FLIGHT DECK (LEFT SIDE, LOOKING OUTBOARD) (RIGHT SIDE, LOOKING OUTBOARD) OPAS - OVERHEAD PANEL BUS CONTROLLER INSTALLATION 23-93-00 - 243 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 252 777 TRAINING MANUAL OPAS -- OVERHEAD PANEL BUS CONTROLLER FUNCTIONAL DESCRIPTION General Fault Monitor There are two overhead panel bus controllers (OPBCs), The fault monitor circuit identifies OPAS faults to the one on each side of the flight deck. Each OPBC has microprocessor.
  • Page 253 777 TRAINING MANUAL FAULT MONITOR RS485 OPIC A2 IN SERIAL RIGHT OPCF INTERFACE CONTROLLER ARINC 629 TERMINAL CONTROLLER SERIAL RIGHT PDCU INTERFACE CONTROLLER MICROPROCESSOR ARINC 629 TERMINAL SERIAL LEFT PDCU INTERFACE CONTROLLER CONTROLLER OPIC A2 IN SERIAL CHANNEL PROGRAM LEFT OPCF INTERFACE PINS CONTROLLER...
  • Page 254 777 TRAINING MANUAL OPAS -- TEST General These are the system tests for the OPAS: Left overhead panel ARINC 629 system Right overhead panel ARINC 629 system OPAS System Test Each system test makes sure the operation of that channel is fully functional. Both system tests should be complied with in order to ensure the correct operation of OPAS is.

  • Page 255: Ground Tests

    777 TRAINING MANUAL LINE EXTENDED GROUND TESTS MAINTENANCE MAINTENANCE SELECT ATA SYSTEM (55) INBOUND FLIGHT DECK EFFECTS Select Test Type 23 VHF Communication System 23 Satellite Communications (SATCOM) System SYSTEM EXISTING FLIGHT TEST 23 Digital Control Audio System DECK EFFECTS 23 Overhead Panel ARINC 629 System OPERATIONAL 24 ELMS P210 Power Management Panel...
  • Page 256 777 TRAINING MANUAL OPAS -- OVERALL INTERFACES Interfaces THIS PAGE INTENTIONALLY LEFT BLANK. 23-93-00 - 248 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 257 777 TRAINING MANUAL 28V DC RIGHT BUS OPAS 2 OPIC A2 P11 OVERHEAD CB PANEL SWITCHES IN P5, P61 PANELS LIGHTS IN P5 & OPIC A1 P61 PANELS RIGHT OPCF SWITCHES IN P5, P61 PANELS LIGHTS IN P5, OPIC A2 P61 PANELS 28V DC RIGHT OPBC...
  • Page 258 777 TRAINING MANUAL OPAS -- OVERALL FUNCTIONAL DESCRIPTION Functional Description THIS PAGE INTENTIONALLY LEFT BLANK. 23-93-00 - 250 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 259 777 TRAINING MANUAL FAULT MONITOR FAULT MONITOR SERIAL ARINC 160 CIRCUITS SERIAL SWITCHES IN P5, INTERFACE MULTIPLEXER PORT P61 PANELS CONTROL 36 CIRCUITS TERM MICROPROCESSOR CHANNEL DEMULTIPLEXER SERIAL INTERFACE CONTROL OPIC A2 ARINC MICRO- PROCESSOR TERM LIGHTS IN P5, SERIAL P61 PANELS SAME AS RIGHT OPIC INTERFACE...
  • Page 260 777 TRAINING MANUAL SYSTEMS CARD FILES -- INTRODUCTION Purpose - power supply unit rcvr - receiver The systems card files hold the ARINC 429 bus interface - right hand cards for essential systems. RSCF - right systems card file - weight-on-wheels They also hold the ARINC signal gateway (ASG) cards.
  • Page 261 777 TRAINING MANUAL ARINC 629 DATA BUS ASG CARD CARD WITH CARD WITH CARD WITH ARINC 429 ARINC 429 ARINC 429 DATA DATA DATA (TYPICAL) (TYPICAL) (TYPICAL) CARD FILE (TYPICAL) ARINC 429 DATA BUS SYSTEMS SYSTEMS CARD FILES - INTRODUCTION 31-09-00 - 253 - ALTEON PROPRIETARY.
  • Page 262 777 TRAINING MANUAL SYSTEMS CARD FILES -- GENERAL DESCRIPTION General The left and right ASG cards in each card file connect to the left and right systems ARINC 629 buses. The systems card files hold cards for ARINC 429 systems. These cards calculate data for their systems. Data moves between the cards in the card files and the left and right ARINC 629 systems buses.

  • Page 263: General Description

    777 TRAINING MANUAL POWER SUPPLY CARDS (4) ARINC 429 CARDS (8) ASG CARDS (2) LEFT SYSTEMS ARINC 629 BUS AIRPLANE SYSTEMS FORWARD CARGO SMOKE DETECTOR LEFT SYSTEMS CARD FILE AFT CARGO RIGHT SYSTEMS SMOKE DETECTOR ARINC 629 BUS AIRPLANE SYSTEMS POWER SUPPLY CARDS (4) ARINC 429 CARDS (9) ASG CARDS (2)
  • Page 264 777 TRAINING MANUAL SYSTEMS CARD FILES -- COMPONENT LOCATION - MAIN EQUIPMENT CENTER General These two systems card files are in the main equipment center: P85 Left systems card file (LSCF) P84 Right systems card file (RSCF). 31-09-00 - 256 - ALTEON PROPRIETARY.
  • Page 265 777 TRAINING MANUAL P85 LEFT SYSTEMS P84 RIGHT SYSTEMS CARD FILE CARD FILE MAIN EQUIPMENT CENTER MAIN EQUIPMENT CENTER (LEFT SIDE, LOOKING FORWARD) (RIGHT SIDE, LOOKING FORWARD) SYSTEMS CARD FILES - COMPONENT LOCATION - MAIN EQUIPMENT CENTER 31-09-00 - 257 - ALTEON PROPRIETARY.
  • Page 266 777 TRAINING MANUAL SYSTEMS CARD FILES -- COMPONENT LOCATION - LSCF CARDS General The left systems card file (LSCF) in the P85 panel has 18 slots. They are slots A2 through A19. The LSCF contains these interface cards: A2 - PSU - preregulator card A3 - PSU - linear/monitor card A4 - center hydraulic interface module (HYDIM) card CH2...
  • Page 267 777 TRAINING MANUAL LEFT SYSTEMS CARD FILE (P85) SYSTEMS CARD FILES - COMPONENT LOCATION - LSCF CARDS 31-09-00 - 259 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 268 777 TRAINING MANUAL SYSTEMS CARD FILES -- COMPONENT LOCATION - RSCF CARDS General The right systems card file (RSCF) in the P84 panel has 18 slots. They are slots A2 through A19. The RSCF contains these interface cards: A2 - PSU - preregulator card A3 - PSU - linear/monitor card A4 - center hydraulic interface module (HYDIM) card CH1...
  • Page 269 777 TRAINING MANUAL RIGHT SYSTEMS CARD FILE (P84) SYSTEMS CARD FILES - COMPONENT LOCATION - RSCF CARDS 31-09-00 - 261 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 270 777 TRAINING MANUAL SYSTEMS CARD FILES -- POWER INTERFACES General The LSCF PS1 circuit breaker in the P310 standby power management panel connects 28v dc to the preregulator 1 card in the LSCF. The LSCF PS2 circuit breaker connects 28v dc to the preregulator 2 card in the LSCF. The RSCF PS1 circuit breaker in the P310 standby power management panel connects 28v dc to the preregulator 1 card in the RSCF.
  • Page 271 777 TRAINING MANUAL 28V DC HOT BAT +28V DC LSCF PS1 PREREGULATOR 1 28V DC BAT BUS +28V DC SEC 2 LSCF PS2 PREREGULATOR 2 28V DC HOT BAT LEFT SYSTEMS CARD FILE RSCF PS1 28V DC HOT BAT +28V DC ELMS PWR P310 CF POWER...
  • Page 272 777 TRAINING MANUAL SYSTEMS CARD FILES -- LSCF POWER INTERFACES General card file assembly. These switch inputs allow maintenance personnel to remove power from the The left system card file (LSCF) has two power individual cards. supplies. Each power supply has these two cards: Preregulator Linear monitor.
  • Page 273 777 TRAINING MANUAL A4 C HYDIM LIN REG 1 +6V DC +17V DC POWER A5 L DLODS CONTROL LIN REG 2 COMBINING +30V DC +5V DC A6 L ACIPS LIN REG 3 PREREGULATOR 1 A7 SPARE LIN REG 4 POWER CONTROL ARINC 429 TO SW (7)
  • Page 274 777 TRAINING MANUAL SYSTEMS CARD FILES -- RSCF POWER INTERFACES General card file assembly. These switch inputs allow maintenance personnel to remove power from the The right system card file (RSCF) has two power individual cards. supplies. Each power supply has these two cards: Preregulator Linear monitor.
  • Page 275 777 TRAINING MANUAL LIN REG 1 A4 C HYDIM +6V DC +17V DC POWER CONTROL LIN REG 2 A5 R DLODS COMBINING +30V DC +5V DC LIN REG 3 A6 R ACIPS PREREGULATOR 1 LIN REG 4 A7 C ACIPS POWER CONTROL ARINC 429 TO...
  • Page 276 777 TRAINING MANUAL SYSTEMS CARD FILES -- ARINC 429 AND 629 INTERFACES General The individual cards in the system card files interface with their specific systems. They send and receive this type of information: ARINC 429 digital data Analog signals Analog discretes.
  • Page 277 777 TRAINING MANUAL STATUS LINEAR/ MONITOR ARINC 429 ANALOG SIGNALS ARINC 429 A429 DATA RCV A LEFT ASG (A12) ANALOG DISCRETES ARINC 429 RCV B LRU INTERFACE CARD (TYP) ARINC 429 RCV - CH1 ARINC 429 RCV - CH2 ARINC 429 XMT - CH1 ARINC 429 XMT - CH2...
  • Page 278 777 TRAINING MANUAL SYSTEMS CARD FILES -- CHASSIS Purpose Training Information Point The left systems card file (LSCF) and right systems The RSCF chassis is the same as the LSCF chassis except card file (RSCF) hold interface cards for the member that it holds right airplane electrical systems or one systems LRUs.
  • Page 279 777 TRAINING MANUAL DRIP SHIELD ESDS JACK CARD FILE CHASSIS A18 LINEAR MONITOR CARD W/POWER SWITCHES ARINC 429, ANALOG, ANALOG DISCRETE INTERFACES ARINC 629 INTERFACES A3 LINEAR MONITOR CARD W/POWER SWITCHES SYSTEMS CARD FILE (TYPICAL) CARD FILE COVER (SHOWN OPEN) SYSTEMS CARD FILE WITH COVER OPEN (TYPICAL) SYSTEMS CARD FILES - CHASSIS 31-09-00...
  • Page 280 777 TRAINING MANUAL SYSTEMS CARD FILES -- ASG CARDS Purpose ARINC 629 signal gateway (ASG) cards change data format between ARINC 429 and ARINC 629. The ASG cards move data between the LRU interface cards in the systems card files and systems ARINC 629 buses. The ASG cards also move data between the forward and aft cargo smoke detectors and the systems ARINC 629 buses.
  • Page 281 777 TRAINING MANUAL ARINC 629 SIGNAL GATEWAY (ASG) CARD SYSTEMS CARD FILES - ASG CARDS 31-09-00 - 273 - ALTEON PROPRIETARY. Copyright. See title page for details...
  • Page 282 777 TRAINING MANUAL SYSTEMS CARD FILES -- ASG CARD FUNCTIONAL DESCRIPTION General ARINC 629 Terminal An ARINC 629 signal gateway (ASG) card changes ARINC The ARINC 629 terminal transmits the data to an ARINC 429 data from LRU interface cards and cargo smoke 629 systems bus.
  • Page 283 777 TRAINING MANUAL ARINC 429 ARINC 429 TO ARINC 629 RECEIVER CONVERTER LRU INTERFACE CARDS AND ARINC 629 CARGO SMOKE TERMINAL DETECTORS ARINC 629 ARINC 429 TO ARINC 429 TRANSMITTER CONVERTER ARINC 629 ASG CARD SYSTEM BUS SYSTEMS CARD FILES - ASG CARD FUNCTIONAL DESCRIPTION 31-09-00 - 275 - ALTEON PROPRIETARY.

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