OPERATIONS MANUAL

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Fire Protection Fire Warnings: When a fire is detected, the fire bell on the flight deck rings every five seconds. The first ring is louder than the subsequent rings. In case of an APU fire, the APU fire warning horn sounds also; the horn is installed in the right body gear wheel well. Both the bell and the horn can be silenced by extinguishing the APU fire, or by pulling the APU fire switch. In any case of a fire—in the APU, engine, cargo, or wheel well—, pushing a master warning reset switch silences the flight deck fire bell and turns off the master warning lights. Fire warnings are entirely reset when the respective fire is extinguished. Fire warnings are inhibited during part of the takeoff: the inhibit starts at V1 if the FMC provides a valid V1 speed, else when the aircraft pitch rises through 5°. The inhibit ends after 25 seconds or when climbing through 400 ft. Squibs and Fire Extinguisher Bottles: Squibs are small, electrically triggered explosive devices mounted on the sealed outlets of the fire extinguisher bottles. When a squib detonates, it tears the outlet open, and pressurized halon gas in the bottle will discharge through a duct system into the area where the fire is located. The main hot battery bus provides the trigger power; the power may be routed to a squib using the respective fire switch. Using a test switch on the maintenance panel, the power can be routed to the squib through a test lamp; the lamp acts as a resistor and reduces the current so that the squib will not explode during the test. Lights that do not illuminate during the test will indicate the respective power line to the squib is broken, or not powered, or the squib has been fired. Each test switch refers to the squibs on the A or B engine bottles and the APU bottle,—or to cargo bottle squibs,—or to both. For example, on a non-ER passenger aircraft, test switch 1 refers to all A bottle squibs and all cargo bottle forward squibs; and test switch 2 refers to all B bottle squibs and all cargo bottle aft squibs. Other aircraft include two more test switches that refer to the cargo bottle squibs only. The test light itself incorporates another switch; when that switch is pushed and the light does not illuminate, the test lamp is broken, or power is removed. That is a plain lamp test and cannot be influenced by a failed squib. — Page 240 — For preview only. Not for sale. Many pages are intentionally removed.
Fire Protection Maintenance Panel: Squib systems are aircraft specific. Squib test switch Push (momentary action) Checks if the squibs in the respective test group are operative, and if trigger power is available. Do not push switches 1 and 2 (or 3 and 4) at the same time; it will invalidate the test. Freighter & all ER aircraft Squib test light & lamp test switch Push (momentary action) Checks if the test lamp is intact, and if trigger power is available. GREEN LIGHT During lamp test: indicates the test lamp is intact. During squib test: indicates the squib system is intact. Non-ER passenger aircraft Combi aircraft — Page 241 — For preview only. Not for sale. Many pages are intentionally removed.
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® OPERATIONS MANUAL VERSION 10 For
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Simulator Handling Introduction: Pr
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Simulator Handling End User License
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Simulator Handling Starting the Sim
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Simulator Handling Java Look & Feel
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Simulator Handling User Files - Ove
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Simulator Handling Mouse - How to D
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Simulator Handling Mouse - How to Z
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Simulator Handling Mouse - How to A
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Simulator Handling Mouse - How to T
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Simulator Handling Keyboard - Impor
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Simulator Handling Keyboard - Summa
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Simulator Handling Instructor > Sit
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Simulator Handling Instructor > Lay
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Simulator Handling Instructor > Lay
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Simulator Handling Instructor > Net
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Simulator Handling Network Examples
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Simulator Handling Boost Server: Th
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Simulator Handling Instructor > Pre
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Simulator Handling Instructor > Abo
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Aircraft General Aircraft General
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Aircraft General Main Panel Lightin
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Aircraft General Glareshield Panel
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Air Systems Air Conditioning Contro
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Air Systems Air Conditioning Contro
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Automatic Flight System Overview: A
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Automatic Flight MCP: Vertical navi
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Automatic Flight MCP: Bank limit se
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Automatic Flight MCP: Altitude wind
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Automatic Flight Takeoff Operation:
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Auxiliary Power APU Control: Batter
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Page 123 and 124: Communications ACP: (continued) Pus
Page 127 and 128: Communications RTP: (continued) HF
Page 129 and 130: Communications Cockpit Voice Record
Page 131 and 132: Communications Cabin Interphone Sys
Page 133 and 134: Communications ACARS - Basics: The
Page 135 and 136: Communications ACARS - Flight Plan
Page 137 and 138: Communications ACARS - OOOI Status
Page 139 and 140: Electrical Bus Tie System: (continu
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Page 143 and 144: Electrical Main Instrument Panel: A
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Page 157 and 158: Electrical Main Hot Battery Bus - E
Page 159 and 160: Electrical Main Standby Bus - Equip
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Page 163 and 164: Electrical EICAS Messages: CAUTION
Page 167 and 168: Emergency Equipment Overhead Panel:
Page 171: Fire Protection Dual Loop Detectors
Page 177 and 178: Fire Protection Fire and Overheat T
Page 181 and 182: Flight Controls Maintenance Panel:
Page 183 and 184: Flight Controls Aisle Stand: (In th
Page 187 and 188: Flight Controls Surface Position In
Page 189 and 190: Flight Controls Stabilizer Trim: Th
Page 191 and 192: Flight Controls Rudder Control: Fla
Page 193 and 194: Flight Controls EICAS Messages: AIL
Page 195 and 196: Flight Instruments Integrated Displ
Page 197 and 198: Flight Instruments IDU Controls: Se
Page 199 and 200: Flight Instruments IDU Switching: (
Page 201 and 202: Flight Instruments Instrument Sourc
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Page 207 and 208: Flight Instruments Altitude Indicat
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Page 215 and 216: Flight Instruments ND VOR Mode: In
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Flight Instruments Standby Attitude
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Flight Instruments Integrated Stand
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Flight Instruments Clock: Chronogra
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FMS IRS LEGS Page: 1L 2L 3L 4L 5L 6
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FMS ALTN NAV RADIO Page: 1L 2L 3L A
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FMS SELECT DESIRED WPT Page: 1L 2L
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FMS PROGRESS 2/3 Page: 1L 2L 3L 4L
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FMS NAV RADIO Page: 1L 2L 3L 1R 2R
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FMS FIX INFO Page: 1L 2L 3L 4L 5L 6
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FMS TAKEOFF REF Page: 1L 2L 3L 4L A
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FMS APPROACH REF Page: 1L 3L 4L 6L
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FMS MAINTENANCE INDEX Page: 1L 2L 3
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FMS RTE Page: 1L 3L 6L 1R 2R 3R 6R
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FMS RTE Page: (continued) 1L 2L 3L
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FMS RTE Page: (continued) 2L 3L 3R
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FMS DEP/ARR INDEX Page: 1L 3L 6L 1R
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FMS ARRIVALS Page (Active Route): 1
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FMS ARRIVALS Page (Active Route): (
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FMS LEGS Page: (continued) 6L Valid
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FMS LEGS Page: (continued) Single l
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FMS LEGS Page: (continued) Map view
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FMS LEGS Page: (continued) Direct-t
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FMS RTE DATA Page: 1L 2L 3L 4L 5L 6
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FMS VNAV CLB Page: (continued) 3R 4
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FMS VNAV CRZ Page: (continued) 2L 3
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FMS VNAV DES Page: Page title 1L 2L
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FMS DESCENT FORECAST Page: 1L 2L 3L
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FMS OFFPATH DES Page: 1L 2L 3L 4L 5
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FMS INDEX Page: 1L 2L 3L 4L 5L 6L I
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FMS LOG Page: 1L 2L 3L 4L 5L 6L 1R
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FMS Sent REPORT Page (Message to Co
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FMS EMERGENCY REPORT Page: 1L 2L 3L
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FMS VERIFY EMERGENCY Page: Access:
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FMS ALT REQUEST Page (Message to Co
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FMS OFFSET REQUEST Page (Message to
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FMS VERIFY REQUEST Page for Navigat
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FMS WHEN CAN WE EXPECT Page (Messag
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Fuel System Transfer and Jettison P
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Fuel System EICAS Fuel Synoptics: F
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Fuel System Fuel Pumps: Main boost
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Fuel System EICAS Interface: The fu
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Fuel System Stabilizer Tank Operati
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Fuel System EICAS Messages: >FUEL A
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Hydraulics EICAS Hydraulic Synoptic
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Hydraulics EICAS Messages: CAUTION
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Ice & Rain Protection System Overvi
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Ice & Rain Protection Anti-Ice with
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Ice & Rain Protection EICAS Message
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Landing Gear Landing Gear — Page
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Landing Gear System Overview: (cont
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Landing Gear Autobrakes: The select
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Landing Gear Primary EICAS Gear Ind
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Navigation Systems Inertial Referen
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Navigation Systems Inertial Referen
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Navigation Systems Weather Radar Sy
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Navigation Systems ATC Transponder
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Navigation Systems DME System: Two
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Navigation Systems VOR and Marker B
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Navigation Systems EICAS Messages:
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Power Plant Power Plant — Page 49
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Power Plant Forward Thrust Levers a
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Power Plant Electronic Engine Contr
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Power Plant Electronic Engine Contr
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Power Plant Ignition Control - GE M
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Power Plant Ignition Control - RR M
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Power Plant Primary EICAS Display -
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Power Plant Primary EICAS Display -
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Power Plant Secondary Engine Displa
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Power Plant Compact Engine Indicati
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Warning Systems EICAS Messages: (co
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Warning Systems EICAS Messages: (co
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Warning Systems EGPWS: The aircraft
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Warning Systems EGPWS - Mode 2: 245
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Warning Systems EGPWS - Terrain Cle
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Warning Systems EGPWS - Terrain Ale
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Warning Systems EGPWS - Aural Messa
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Limitations Approved low visibility
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Procedures Two Engines Inoperative
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Procedures Normal Procedures (Examp
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Procedures First Officer - Cockpit
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Abnormal Lists Air Systems: — Pag
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OPERATIONS MANUAL

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