OPERATIONS MANUAL

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Ice & Rain Protection Ice & Rain Protection — Page 461 — For preview only. Not for sale. Many pages are intentionally removed.
Ice & Rain Protection System Overview: Ice detection (Normally, installed on just some aircraft; and if installed, it is either a single or a dual probe system. In the simulator, all aircraft are equipped with a dual probe system.) Two ice detector probes are installed externally on the forward fuselage; one on the left, and one on the right side. The tip of each probe vibrates at 40 kHz by magnetostrictive effects, driven by an electric coil. When ice builds up on the tip, the frequency decreases. When the frequency has dropped to a certain limit, a heater activates and melts the ice. When the frequency has returned to 40 kHz, the heater deactivates and allows the tip to build up ice again. These cycles are repeated as long as icing conditions exist, and the system counts these cycles. In non-severe icing conditions, the heater will melt the ice in circa 10 seconds. In severe icing, the melting process will take more than 15 seconds; such long cycles will be counted as 2 cycles. Automatic anti-ice on the nacelles activates after 2 counted cycles, and that on the wings after 10, provided the respective automatic control is installed and enabled. When the tip has been vibrating at 40 kHz for 3 minutes, the counter is reset to zero, and all automatic antiice operation is terminated. When the aircraft is on the ground, the system will cycle also and melt the ice on the tip, but the counter will be locked at zero to prevent automatic anti-ice activation on the ground. Probe heat The aircraft is equipped with 2 total air temperature (TAT), 4 pitot-static (P/S), and 2 angle of attack (AOA) probes; engine specific probes are installed in the nacelles. All probes are electrically heated to prevent ice formation. There are no flight deck controls for probe heat aside from circuit breakers. Heat for the TAT probe is automatically activated when in flight. Heat for P/S, AOA, and engine internal probes is automatically activated when any engine is running in flight or on the ground. Water line and waste drain heat Electric heaters powered by 115 V AC protect all water systems on the aircraft against icing. Windows All flight deck windows are fitted with interior anti-fog systems. The forward windows also include exterior anti-fog and anti-ice systems. All systems use electric heat which is automatically modulated. The side window systems are powered whenever AC power is available; the front window systems require the WINDOW HEAT switches on the overhead panel to be set to ON.—The pilots can activate windshield defogging air by switches on the auxiliary panels (in the simulator not shown).—Controls for windshield wipers and washers are available on the overhead panel. (continued next page) — Page 462 — 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 M
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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 > Mod
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Simulator Handling Instructor > Mod
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Simulator Handling Instructor > Ana
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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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Communications ACP: (continued) Pus
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Communications RTP: (continued) HF
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Communications Cockpit Voice Record
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Communications Cabin Interphone Sys
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Communications ACARS - Basics: The
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Communications ACARS - Flight Plan
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Communications ACARS - OOOI Status
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Electrical Bus Tie System: (continu
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Electrical Battery Busses and Hot B
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Electrical Main Instrument Panel: A
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Electrical Overhead Panel: Bus tie
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Electrical APU Standby Bus System w
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Electrical DC Bus 2 - Equipment Lis
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Electrical DC Bus 3 - Equipment Lis
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Electrical Main Hot Battery Bus - E
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Electrical Main Standby Bus - Equip
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Electrical Ground Service Bus - Equ
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Electrical EICAS Messages: CAUTION
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Emergency Equipment Overhead Panel:
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Fire Protection Dual Loop Detectors
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Fire Protection Maintenance Panel:
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Fire Protection Fire and Overheat T
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Flight Controls Maintenance Panel:
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Flight Controls Aisle Stand: (In th
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Flight Controls Surface Position In
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Flight Controls Stabilizer Trim: Th
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Flight Controls Rudder Control: Fla
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Flight Controls EICAS Messages: AIL
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Flight Instruments Integrated Displ
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Flight Instruments IDU Controls: Se
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Flight Instruments IDU Switching: (
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Flight Instruments Instrument Sourc
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Flight Instruments Instrument Sourc
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Flight Instruments Altitude Indicat
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Flight Instruments ND Symbology: (c
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Flight Instruments ND Symbology: (c
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Flight Instruments ND VOR Mode: In
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Flight Instruments ND Plan Mode - V
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Flight Instruments ND Position Chec
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Flight Instruments ND Test & Failur
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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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Page 281 and 282: FMS INDEX Page: 1L 2L 3L 4L 5L 6L I
Page 283 and 284: FMS LOG Page: 1L 2L 3L 4L 5L 6L 1R
Page 285 and 286: FMS Sent REPORT Page (Message to Co
Page 287 and 288: FMS EMERGENCY REPORT Page: 1L 2L 3L
Page 289 and 290: FMS VERIFY EMERGENCY Page: Access:
Page 291 and 292: FMS ALT REQUEST Page (Message to Co
Page 293 and 294: FMS OFFSET REQUEST Page (Message to
Page 295 and 296: FMS VERIFY REQUEST Page for Navigat
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Page 301 and 302: Fuel System Transfer and Jettison P
Page 303 and 304: Fuel System EICAS Fuel Synoptics: F
Page 305 and 306: Fuel System Fuel Pumps: Main boost
Page 307 and 308: Fuel System EICAS Interface: The fu
Page 309 and 310: Fuel System Stabilizer Tank Operati
Page 311 and 312: Fuel System EICAS Messages: >FUEL A
Page 315 and 316: Hydraulics EICAS Hydraulic Synoptic
Page 317: Hydraulics EICAS Messages: CAUTION
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Page 323 and 324: Ice & Rain Protection EICAS Message
Page 325 and 326: Landing Gear Landing Gear — Page
Page 327 and 328: Landing Gear System Overview: (cont
Page 329 and 330: Landing Gear Autobrakes: The select
Page 331 and 332: Landing Gear Primary EICAS Gear Ind
Page 335 and 336: Navigation Systems Inertial Referen
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Page 339 and 340: Navigation Systems Weather Radar Sy
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Page 343 and 344: Navigation Systems DME System: Two
Page 345 and 346: Navigation Systems VOR and Marker B
Page 347 and 348: Navigation Systems EICAS Messages:
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Page 351 and 352: Power Plant Forward Thrust Levers a
Page 353 and 354: Power Plant Electronic Engine Contr
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Page 357 and 358: Power Plant Ignition Control - GE M
Page 359 and 360: Power Plant Ignition Control - RR M
Page 361 and 362: Power Plant Primary EICAS Display -
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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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