OPERATIONS MANUAL

More documents

Recommendations

Info

Power Plant Electronic Engine Control: The NORM function may be in the upper or lower position. EEC maintenance power switch (guarded) NORM Power to the EEC is selected by normal system logic. TEST The EEC is directly connected to the associated DC bus. GE & PW models RR models EEC maintenance channel select switch NORM EEC controlling channel A or B is selected by system logic. CH B EEC controlling channel B is selected for testing. — Page 504 — For preview only. Not for sale. Many pages are intentionally removed.
Power Plant Electronic Engine Control: Engine autostart switch (engines 1, 2, 3, 4) OFF Disables the autostart system on the associated engine. The fuel control switch must not be set to RUN before the N2 (or N3) RPM is spooled up to the fuel-on minimum. ON Enables the autostart system on the associated engine. The fuel control switch must be set to RUN to initiate the autostart program. EEC switch (engines 1, 2, 3, 4) NORM Enables the EEC to operate in normal mode. On PW & RR models, EPR is used as the controlling parameter. ALTN Commands the EEC to operate in alternate mode. N1 is used as the controlling parameter. EEC operates in alternate mode. ALTN LIGHT On GE models, autothrottle operation is possible when all four EECs are in the same mode. On PW & RR models, autothrottle operation is possible when all four EECs are in normal mode. — Page 505 — For preview only. Not for sale. Many pages are intentionally removed.
Page 1 and 2:
® OPERATIONS MANUAL VERSION 10 For
Page 3 and 4:
Simulator Handling Introduction: Pr
Page 5 and 6:
Simulator Handling End User License
Page 7 and 8:
Simulator Handling Starting the Sim
Page 9 and 10:
Simulator Handling Java Look & Feel
Page 11 and 12:
Simulator Handling User Files - Ove
Page 13 and 14:
Simulator Handling Mouse - How to D
Page 15 and 16:
Simulator Handling Mouse - How to Z
Page 17 and 18:
Simulator Handling Mouse - How to A
Page 19 and 20:
Simulator Handling Mouse - How to M
Page 21 and 22:
Simulator Handling Mouse - How to T
Page 23 and 24:
Simulator Handling Keyboard - Impor
Page 25 and 26:
Simulator Handling Keyboard - Summa
Page 27 and 28:
Page 29 and 30:
Page 31 and 32:
Simulator Handling Instructor > Sit
Page 33 and 34:
Page 35 and 36:
Page 37 and 38:
Page 39 and 40:
Page 41 and 42:
Page 43 and 44:
Page 45 and 46:
Page 47 and 48:
Page 49 and 50:
Page 51 and 52:
Page 53 and 54:
Simulator Handling Instructor > Mod
Page 55 and 56:
Simulator Handling Instructor > Mod
Page 57 and 58:
Simulator Handling Instructor > Ana
Page 59 and 60:
Page 61 and 62:
Page 63 and 64:
Simulator Handling Instructor > Lay
Page 65 and 66:
Simulator Handling Instructor > Lay
Page 67 and 68:
Simulator Handling Instructor > Net
Page 69 and 70:
Simulator Handling Network Examples
Page 71 and 72:
Page 73 and 74:
Page 75 and 76:
Page 77 and 78:
Page 79 and 80:
Simulator Handling Boost Server: Th
Page 81 and 82:
Simulator Handling Instructor > Pre
Page 83 and 84:
Page 85 and 86:
Page 87 and 88:
Page 89 and 90:
Simulator Handling Instructor > Abo
Page 91 and 92:
Aircraft General Aircraft General
Page 93 and 94:
Aircraft General Main Panel Lightin
Page 95 and 96:
Aircraft General Glareshield Panel
Page 97 and 98:
Some pages are intentionally remove
Page 99 and 100:
Air Systems Air Conditioning Contro
Page 101 and 102:
Air Systems Air Conditioning Contro
Page 103 and 104:
Page 105 and 106:
Automatic Flight System Overview: A
Page 107 and 108:
Page 109 and 110:
Automatic Flight MCP: Vertical navi
Page 111 and 112:
Automatic Flight MCP: Bank limit se
Page 113 and 114:
Automatic Flight MCP: Altitude wind
Page 115 and 116:
Automatic Flight Takeoff Operation:
Page 117 and 118:
Page 119 and 120:
Auxiliary Power APU Control: Batter
Page 121 and 122:
Page 123 and 124:
Communications ACP: (continued) Pus
Page 125 and 126:
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
Page 141 and 142:
Electrical Battery Busses and Hot B
Page 143 and 144:
Electrical Main Instrument Panel: A
Page 145 and 146:
Electrical Overhead Panel: Bus tie
Page 147 and 148:
Page 149 and 150:
Electrical APU Standby Bus System w
Page 151 and 152:
Page 153 and 154:
Electrical DC Bus 2 - Equipment Lis
Page 155 and 156:
Electrical DC Bus 3 - Equipment Lis
Page 157 and 158:
Electrical Main Hot Battery Bus - E
Page 159 and 160:
Electrical Main Standby Bus - Equip
Page 161 and 162:
Electrical Ground Service Bus - Equ
Page 163 and 164:
Electrical EICAS Messages: CAUTION
Page 165 and 166:
Page 167 and 168:
Emergency Equipment Overhead Panel:
Page 169 and 170:
Page 171 and 172:
Fire Protection Dual Loop Detectors
Page 173 and 174:
Fire Protection Maintenance Panel:
Page 175 and 176:
Page 177 and 178:
Fire Protection Fire and Overheat T
Page 179 and 180:
Page 181 and 182:
Flight Controls Maintenance Panel:
Page 183 and 184:
Flight Controls Aisle Stand: (In th
Page 185 and 186:
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
Page 203 and 204:
Flight Instruments Instrument Sourc
Page 205 and 206:
Page 207 and 208:
Flight Instruments Altitude Indicat
Page 209 and 210:
Page 211 and 212:
Flight Instruments ND Symbology: (c
Page 213 and 214:
Flight Instruments ND Symbology: (c
Page 215 and 216:
Flight Instruments ND VOR Mode: In
Page 217 and 218:
Flight Instruments ND Plan Mode - V
Page 219 and 220:
Flight Instruments ND Position Chec
Page 221 and 222:
Flight Instruments ND Test & Failur
Page 223 and 224:
Flight Instruments Standby Attitude
Page 225 and 226:
Flight Instruments Integrated Stand
Page 227 and 228:
Flight Instruments Clock: Chronogra
Page 229 and 230:
FMS IRS LEGS Page: 1L 2L 3L 4L 5L 6
Page 231 and 232:
FMS ALTN NAV RADIO Page: 1L 2L 3L A
Page 233 and 234:
FMS SELECT DESIRED WPT Page: 1L 2L
Page 235 and 236:
FMS PROGRESS 2/3 Page: 1L 2L 3L 4L
Page 237 and 238:
FMS NAV RADIO Page: 1L 2L 3L 1R 2R
Page 239 and 240:
FMS FIX INFO Page: 1L 2L 3L 4L 5L 6
Page 241 and 242:
FMS TAKEOFF REF Page: 1L 2L 3L 4L A
Page 243 and 244:
FMS APPROACH REF Page: 1L 3L 4L 6L
Page 245 and 246:
FMS MAINTENANCE INDEX Page: 1L 2L 3
Page 247 and 248:
FMS RTE Page: 1L 3L 6L 1R 2R 3R 6R
Page 249 and 250:
FMS RTE Page: (continued) 1L 2L 3L
Page 251 and 252:
FMS RTE Page: (continued) 2L 3L 3R
Page 253 and 254:
FMS DEP/ARR INDEX Page: 1L 3L 6L 1R
Page 255 and 256:
FMS ARRIVALS Page (Active Route): 1
Page 257 and 258:
FMS ARRIVALS Page (Active Route): (
Page 259 and 260:
FMS LEGS Page: (continued) 6L Valid
Page 261 and 262:
FMS LEGS Page: (continued) Single l
Page 263 and 264:
FMS LEGS Page: (continued) Map view
Page 265 and 266:
FMS LEGS Page: (continued) Direct-t
Page 267 and 268:
FMS RTE DATA Page: 1L 2L 3L 4L 5L 6
Page 269 and 270:
Page 271 and 272:
FMS VNAV CLB Page: (continued) 3R 4
Page 273 and 274:
FMS VNAV CRZ Page: (continued) 2L 3
Page 275 and 276:
FMS VNAV DES Page: Page title 1L 2L
Page 277 and 278:
FMS DESCENT FORECAST Page: 1L 2L 3L
Page 279 and 280:
FMS OFFPATH DES Page: 1L 2L 3L 4L 5
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
Page 297 and 298:
FMS WHEN CAN WE EXPECT Page (Messag
Page 299 and 300:
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 313 and 314: Some pages are intentionally remove
Page 315 and 316: Hydraulics EICAS Hydraulic Synoptic
Page 317 and 318: Hydraulics EICAS Messages: CAUTION
Page 319 and 320: Ice & Rain Protection System Overvi
Page 321 and 322: Ice & Rain Protection Anti-Ice with
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
Page 337 and 338: Navigation Systems Inertial Referen
Page 339 and 340: Navigation Systems Weather Radar Sy
Page 341 and 342: Navigation Systems ATC Transponder
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:
Page 349 and 350: Power Plant Power Plant — Page 49
Page 351 and 352: Power Plant Forward Thrust Levers a
Page 353: Power Plant Electronic Engine Contr
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 -
Page 363 and 364: Power Plant Primary EICAS Display -
Page 365 and 366: Power Plant Secondary Engine Displa
Page 367 and 368: Power Plant Compact Engine Indicati
Page 369 and 370: Warning Systems EICAS Messages: (co
Page 371 and 372: Warning Systems EICAS Messages: (co
Page 373 and 374: Warning Systems EGPWS: The aircraft
Page 375 and 376: Warning Systems EGPWS - Mode 2: 245
Page 377 and 378: Warning Systems EGPWS - Terrain Cle
Page 379 and 380: Warning Systems EGPWS - Terrain Ale
Page 381 and 382: Warning Systems EGPWS - Aural Messa
Page 385 and 386: Limitations Approved low visibility
Page 387 and 388: Procedures Two Engines Inoperative
Page 389 and 390: Procedures Normal Procedures (Examp
Page 391 and 392: Procedures First Officer - Cockpit
Page 395 and 396: Abnormal Lists Air Systems: — Pag
Page 397: Some pages are intentionally remove
show all

OPERATIONS MANUAL

Create successful ePaper yourself

Delete template?

Save as template?