Instrumentation

Recommendations

Info

31 AFCS Revision Questions 31 AFCS Revision Questions 7. Consider the following statements regarding flight envelope protection: A B High speed protection prevents the airspeed from exceeding V MO /M MO High angle of attack protection comes in when the aircraft reaches the stalling AoA a. Only statement A is correct b. Only statement B is correct c. Both statements are correct d. Neither statement is correct 8. The control laws for an autopilot are known as: a. normal law and emergency law b. alternate law and direct law c. normal, alternate and emergency laws d. normal, alternate and direct laws 9. An autoland system that, in the event of an autopilot failure, continues to function without degradation of performance beyond the limits required automatic, would be one with the status: a. fail-passive b. fail-safe c. fail-operational d. duplex 10. The autoland sequence is considered to be complete when: a. reverse thrust is engaged b. the autopilot is manually disengaged by the pilot c. the aircraft touches down d. the aircraft reaches the end of the runway 11. The autothrottle will come on automatically even with the A/T switch OFF when: a. in a FBW aircraft the AoA reaches a critical value called floor b. the AoA reaches the stalling angle c. TOGA button is pressed d. reverse thrust is selected in flight 12. An aircraft on autopilot is engaged in the VOR mode and loses the VOR signals as it flies through the VOR cone of silence. The autopilot: a. automatically switches to Heading mode b. decouples from the VOR and disconnects c. tunes to the next VOR on the route d. decouples from the VOR and flies the last heading for a fixed period 428
AFCS Revision Questions 31 13. For an aircraft with a non-synchronized autopilot system, ‘snatching’ of the controls by the autopilot when engaging or disengaging can be prevented by: a. the pilot ensuring that the aircraft is trimmed out before selecting or disengaging the autopilot b. being in a straight and level position c. disengaging the auto-trim d. switching on the yaw dampers 14. With the autopilot in CWS the pilot manoeuvres the aircraft and releases control. The aircraft will maintain: AFCS Revision Questions 31 a. heading and altitude b. heading, speed and attitude c. altitude and attitude d. attitude at the time of release 15. Autopilot corrections affecting pitch are carried out by: a. auto-trim only b. auto-trim and elevators c. elevators only d. autothrottle 16. For a commercial aircraft operating with a single pilot in IFR the minimum requirement is that the autopilot should have control in: a. three axes b. Heading mode c. Altitude Hold and Heading mode d. Altitude Hold, Heading mode and Speed 429
Page 1 and 2:
10 INSTRUMENTATION ATPL GROUND TRAI
Page 3 and 4:
Introduction I Textbook Series Book
Page 5 and 6:
Introduction I Contents ATPL Book 5
Page 7 and 8:
Chapter 1 Characteristics and Gener
Page 9 and 10:
Characteristics and General Definit
Page 11 and 12:
Page 13 and 14:
Page 15 and 16:
Page 17 and 18:
Chapter 2 Pitot and Static Sources
Page 19 and 20:
Pitot and Static Sources 2 Introduc
Page 21 and 22:
Pitot and Static Sources 2 Requirem
Page 23 and 24:
Pitot and Static Sources 2 This par
Page 25 and 26:
Questions 2 Questions 1. A pitot he
Page 27 and 28:
Questions 2 Questions 2 21
Page 29 and 30:
Chapter 3 Air Temperature Measureme
Page 31 and 32:
Air Temperature Measurement 3 Intro
Page 33 and 34:
Air Temperature Measurement 3 Air T
Page 35 and 36:
Air Temperature Measurement 3 In or
Page 37 and 38:
Air Temperature Measurement 3 • T
Page 39 and 40:
Air Temperature Measurement 3 Accur
Page 41 and 42:
Air Temperature Measurement 3 Air T
Page 43 and 44:
Questions 3 8. Which of these formu
Page 45 and 46:
Chapter 4 The Airspeed Indicator (A
Page 47 and 48:
The Airspeed Indicator (ASI) 4 Prin
Page 49 and 50:
The Airspeed Indicator (ASI) 4 pilo
Page 51 and 52:
The Airspeed Indicator (ASI) 4 The
Page 53 and 54:
Questions 4 Questions 1. A leak in
Page 55 and 56:
Page 57 and 58:
Chapter 5 The Pressure Altimeter Pr
Page 59 and 60:
The Pressure Altimeter 5 Principle
Page 61 and 62:
The Pressure Altimeter 5 Simple Alt
Page 63 and 64:
The Pressure Altimeter 5 Reading Ac
Page 65 and 66:
The Pressure Altimeter 5 Servo-assi
Page 67 and 68:
The Pressure Altimeter 5 Altimeter
Page 69 and 70:
The Pressure Altimeter 5 Temperatur
Page 71 and 72:
The Pressure Altimeter 5 Blockages
Page 73 and 74:
Questions 5 Questions 1. The diagra
Page 75 and 76:
Page 77 and 78:
Chapter 6 The Vertical Speed Indica
Page 79 and 80:
The Vertical Speed Indicator 6 Intr
Page 81 and 82:
The Vertical Speed Indicator 6 Any
Page 83 and 84:
The Vertical Speed Indicator 6 The
Page 85 and 86:
Questions 6 8. Change of temperatur
Page 87 and 88:
Chapter 7 The Machmeter High Speed
Page 89 and 90:
The Machmeter 7 High Speed Flight I
Page 91 and 92:
The Machmeter 7 Machmeter Construct
Page 93 and 94:
The Machmeter 7 Climb at a Constant
Page 95 and 96:
The Machmeter 7 Example Problems As
Page 97 and 98:
The Machmeter 7 If the aircraft is
Page 99 and 100:
Questions 7 7. The relationships be
Page 101 and 102:
Chapter 8 Air Data Computer Introdu
Page 103 and 104:
Air Data Computer 8 Introduction In
Page 105 and 106:
Air Data Computer 8 The relationshi
Page 107 and 108:
Air Data Computer 8 Figure 8.4 Comb
Page 109 and 110:
Chapter 9 Terrestrial Magnetism The
Page 111 and 112:
Terrestrial Magnetism 9 The Magnet
Page 113 and 114:
Terrestrial Magnetism 9 Methods of
Page 115 and 116:
Terrestrial Magnetism 9 Hard Iron a
Page 117 and 118:
Terrestrial Magnetism 9 Variation c
Page 119 and 120:
Terrestrial Magnetism 9 In the UK t
Page 121 and 122:
Page 123 and 124:
Chapter 10 The Direct Indicating Co
Page 125 and 126:
The Direct Indicating Compass 10 Th
Page 127 and 128:
The Direct Indicating Compass 10 Fo
Page 129 and 130:
The Direct Indicating Compass 10 Ac
Page 131 and 132:
The Direct Indicating Compass 10 De
Page 133 and 134:
The Direct Indicating Compass 10 Tu
Page 135 and 136:
The Direct Indicating Compass 10 Th
Page 137 and 138:
The Direct Indicating Compass 10 At
Page 139 and 140:
Questions 10 7. The magnitude, and
Page 141 and 142:
Chapter 11 Gyroscopes Gyroscopes .
Page 143 and 144:
Gyroscopes 11 Gyroscopes The simple
Page 145 and 146:
Gyroscopes 11 Precession In Figure
Page 147 and 148:
Gyroscopes 11 Wander Figure 11.7 Ho
Page 149 and 150:
Gyroscopes 11 However, at a pole: A
Page 151 and 152:
Gyroscopes 11 An earth gyro is one
Page 153 and 154:
Gyroscopes 11 As well as a directio
Page 155 and 156:
Questions 11 8. The main advantage
Page 157 and 158:
Chapter 12 Directional Gyro Indicat
Page 159 and 160:
Directional Gyro Indicator (DGI) 12
Page 161 and 162:
Page 163 and 164:
Page 165 and 166:
Page 167 and 168:
Page 169 and 170:
Page 171 and 172:
Questions 12 7. The purpose of the
Page 173 and 174:
Chapter 13 The Artificial Horizon T
Page 175 and 176:
The Artificial Horizon 13 The Artif
Page 177 and 178:
The Artificial Horizon 13 Figure 13
Page 179 and 180:
The Artificial Horizon 13 Figure 13
Page 181 and 182:
The Artificial Horizon 13 • Roll
Page 183 and 184:
The Artificial Horizon 13 The Elect
Page 185 and 186:
The Artificial Horizon 13 Instead o
Page 187 and 188:
Questions 13 7. Inside an artificia
Page 189 and 190:
Chapter 14 The Turn and Slip Indica
Page 191 and 192:
The Turn and Slip Indicator 14 The
Page 193 and 194:
The Turn and Slip Indicator 14 The
Page 195 and 196:
The Turn and Slip Indicator 14 Figu
Page 197 and 198:
Questions 14 Questions 1. The rate
Page 199 and 200:
Chapter 15 The Turn Co-ordinator Tu
Page 201 and 202:
The Turn Co-ordinator 15 Turn Co-or
Page 203 and 204:
Page 205 and 206:
Chapter 16 Aircraft Magnetism Devia
Page 207 and 208:
PUSH PUSH Aircraft Magnetism 16 Dev
Page 209 and 210:
Aircraft Magnetism 16 Heading north
Page 211 and 212:
Aircraft Magnetism 16 Occasions for
Page 213 and 214:
Questions 16 7. In the diagram belo
Page 215 and 216:
Chapter 17 Remote Indicating Magnet
Page 217 and 218:
Remote Indicating Magnetic Compass
Page 219 and 220:
Page 221 and 222:
Page 223 and 224:
Page 225 and 226:
Page 227 and 228:
Page 229 and 230:
Questions 17 6. A flux valve senses
Page 231 and 232:
Chapter 18 Inertial Navigation Syst
Page 233 and 234:
Inertial Navigation Systems 18 Intr
Page 235 and 236:
Inertial Navigation Systems 18 Acce
Page 237 and 238:
Inertial Navigation Systems 18 The
Page 239 and 240:
Page 241 and 242:
Inertial Navigation Systems 18 Eart
Page 243 and 244:
Page 245 and 246:
Inertial Navigation Systems 18 Inhe
Page 247 and 248:
Inertial Navigation Systems 18 As a
Page 249 and 250:
Inertial Navigation Systems 18 Head
Page 251 and 252:
Inertial Navigation Systems 18 Dist
Page 253 and 254:
Questions 18 Questions 1. INS error
Page 255 and 256:
Page 257 and 258:
Chapter 19 Inertial Reference Syste
Page 259 and 260:
Inertial Reference System 19 Inerti
Page 261 and 262:
Inertial Reference System 19 The La
Page 263 and 264:
Inertial Reference System 19 Accura
Page 265 and 266:
Questions 19 Question 1. Dither is
Page 267 and 268:
Chapter 20 Radio Altimeter Introduc
Page 269 and 270:
Radio Altimeter 20 Introduction The
Page 271 and 272:
Radio Altimeter 20 Height Scale The
Page 273 and 274:
Radio Altimeter 20 Range and Accura
Page 275 and 276:
Chapter 21 Flight Management System
Page 277 and 278:
Flight Management System 21 Princip
Page 279 and 280:
Flight Management System 21 The pur
Page 281 and 282:
Flight Management System 21 Notes:
Page 283 and 284:
Flight Management System 21 DIR INT
Page 285 and 286:
Chapter 22 Electronic Flight Inform
Page 287 and 288:
Electronic Flight Information Syste
Page 289 and 290:
Page 291 and 292:
Page 293 and 294:
Page 295 and 296:
Page 297 and 298:
Page 299 and 300:
Page 301 and 302:
Page 303 and 304:
Page 305 and 306:
Page 307 and 308:
Questions 22 6. The following yello
Page 309 and 310:
Questions 22 Annex A Questions 22 3
Page 311 and 312:
Chapter 23 Basic Computers Computer
Page 313 and 314:
Basic Computers 23 Computers A comp
Page 315 and 316:
Basic Computers 23 BIOS (Basic Inpu
Page 317 and 318:
Basic Computers 23 Aircraft Systems
Page 319 and 320:
Questions 23 6. In computer termino
Page 321 and 322:
Chapter 24 Future Air Navigation Sy
Page 323 and 324:
Future Air Navigation Systems (FANS
Page 325 and 326:
Page 327 and 328:
Page 329 and 330:
Page 331 and 332:
Page 333 and 334:
Page 335 and 336:
Page 337 and 338:
10 AUTOMATIC FLIGHT AND CONTROL SYS
Page 339 and 340:
Chapter 25 Flight Director Systems
Page 341 and 342:
Flight Director Systems 25 Glossary
Page 343 and 344:
Flight Director Systems 25 Introduc
Page 345 and 346:
Flight Director Systems 25 Primary
Page 347 and 348:
Flight Director Systems 25 Flight D
Page 349 and 350:
Flight Director Systems 25 Poor rec
Page 351 and 352:
Flight Director Systems 25 Navigati
Page 353 and 354:
Flight Director Systems 25 Flight D
Page 355 and 356:
Chapter 26 Autopilot Introduction .
Page 357 and 358:
Autopilot 26 Introduction The main
Page 359 and 360:
Autopilot 26 Control Loops An autop
Page 361 and 362:
Autopilot 26 TRANSDUCER ATTITUDE SE
Page 363 and 364:
Autopilot 26 EU-OPS Requirements Si
Page 365 and 366:
Autopilot 26 Such safeguards are im
Page 367 and 368:
Autopilot 26 Trim Manual Systems Th
Page 369 and 370:
Autopilot 26 Figure 26.9 Auto-trim
Page 371 and 372:
Autopilot 26 Autoland Roll Channel
Page 373 and 374:
Autopilot 26 Radio Navigation To al
Page 375 and 376:
Autopilot 26 The HDG SEL mode autom
Page 377 and 378:
Autopilot 26 Pressing the V/S switc
Page 379 and 380:
Autopilot 26 With CWS engaged, the
Page 381 and 382:
Autopilot 26 Flight Management Syst
Page 383 and 384: Chapter 27 Autoland Introduction .
Page 385 and 386: Autoland 27 Introduction The approa
Page 387 and 388: Autoland 27 With a radio altimeter
Page 389 and 390: Autoland 27 When reverse thrust is
Page 391 and 392: Autoland 27 Figure 27.1 Autoland Se
Page 393 and 394: Autoland 27 Category 2 A precision
Page 395 and 396: Chapter 28 Autothrottle Introductio
Page 397 and 398: Autothrottle 28 Introduction An aut
Page 399 and 400: Autothrottle 28 Power Management Co
Page 401 and 402: Autothrottle 28 FMC Speed Mode The
Page 403 and 404: Autothrottle 28 Flexible Take-off I
Page 405 and 406: Autothrottle 28 When the thrust lev
Page 407 and 408: Chapter 29 Yaw Dampers Dutch Roll .
Page 409 and 410: Yaw Dampers 29 Dutch Roll Dutch rol
Page 411 and 412: Yaw Dampers 29 The Yaw Damper Typic
Page 413 and 414: Yaw Dampers 29 On aircraft with a s
Page 415 and 416: Yaw Dampers 29 29 Yaw Dampers Figur
Page 417 and 418: Chapter 30 Control Laws Introductio
Page 419 and 420: Control Laws 30 Introduction The au
Page 421 and 422: Control Laws 30 Flight Envelope Pro
Page 423 and 424: Control Laws 30 Autopilot Gain Adap
Page 425 and 426: Chapter 31 AFCS Revision Questions
Page 427 and 428: AFCS Revision Questions 31 Question
Page 429 and 430: AFCS Revision Questions 31 15. Duri
Page 431 and 432: AFCS Revision Questions 31 29. Head
Page 433: AFCS Revision Questions 31 Question
Page 437 and 438: Chapter 32 Flight Warning Systems I
Page 439 and 440: Flight Warning Systems 32 Introduct
Page 441 and 442: Figure 1.1 shows the cockpit displa
Page 443 and 444: Chapter 33 Aerodynamic Warnings Int
Page 445 and 446: Aerodynamic Warnings 33 Introductio
Page 447 and 448: Aerodynamic Warnings 33 Regulatory
Page 449 and 450: Aerodynamic Warnings 33 Stall Warni
Page 451 and 452: Aerodynamic Warnings 33 condition,
Page 453 and 454: Chapter 34 Ground Proximity Warning
Page 455 and 456: Ground Proximity Warning System 34
Page 479 and 480: Questions 34 6. An aircraft ‘goes
Page 481 and 482: Questions 34 Questions 34 475
Page 483 and 484: Chapter 35 Airborne Collision and A
Page 485 and 486:
Airborne Collision and Avoidance Sy
Page 487 and 488:
Page 489 and 490:
Page 491 and 492:
Page 493 and 494:
Page 495 and 496:
Page 497 and 498:
Page 499 and 500:
Questions 35 Questions 1. On receip
Page 501 and 502:
Chapter 36 Flight Data Recorder Int
Page 503 and 504:
Flight Data Recorder 36 Introductio
Page 505 and 506:
Flight Data Recorder 36 Flight Data
Page 507 and 508:
Flight Data Recorder 36 Other Requi
Page 509 and 510:
Chapter 37 Cockpit Voice Recorder I
Page 511 and 512:
Cockpit Voice Recorder 37 Introduct
Page 513 and 514:
Cockpit Voice Recorder 37 CVR TEST
Page 515 and 516:
Questions 37 5. GPWS may indicate:
Page 517 and 518:
10 POWERPLANT & SYSTEMS MONITORING
Page 519 and 520:
Chapter 38 Engine Instrumentation A
Page 521 and 522:
Engine Instrumentation 38 An Introd
Page 523 and 524:
Engine Instrumentation 38 The engin
Page 525 and 526:
Engine Instrumentation 38 - Engine
Page 527 and 528:
Engine Instrumentation 38 The Elect
Page 529 and 530:
Engine Instrumentation 38 The tacho
Page 531 and 532:
Engine Instrumentation 38 The gas t
Page 533 and 534:
Engine Instrumentation 38 Air tempe
Page 535 and 536:
Engine Instrumentation 38 indicates
Page 537 and 538:
Engine Instrumentation 38 Engine In
Page 539 and 540:
Engine Instrumentation 38 The princ
Page 541 and 542:
Engine Instrumentation 38 As well a
Page 543 and 544:
Chapter 39 Electronic Instrumentati
Page 545 and 546:
Electronic Instrumentation 39 Elect
Page 547 and 548:
Electronic Instrumentation 39 Seven
Page 549 and 550:
Electronic Instrumentation 39 Displ
Page 551 and 552:
Electronic Instrumentation 39 In or
Page 553 and 554:
Electronic Instrumentation 39 As fa
Page 555 and 556:
Electronic Instrumentation 39 Failu
Page 557 and 558:
Electronic Instrumentation 39 Elect
Page 559 and 560:
Questions 39 7. The electronic engi
Page 561 and 562:
10 REVISION QUESTIONS ATPL GROUND T
Page 563 and 564:
Chapter 40 Revision Questions Fligh
Page 565 and 566:
Revision Questions 40 Flight Instru
Page 567 and 568:
Revision Questions 40 14. The verti
Page 569 and 570:
Revision Questions 40 27. V FE is t
Page 571 and 572:
Revision Questions 40 39. The prope
Page 573 and 574:
Revision Questions 40 53. In a righ
Page 575 and 576:
Revision Questions 40 68. If a pito
Page 577 and 578:
Revision Questions 40 82. What is t
Page 579 and 580:
Revision Questions 40 96. V NE is d
Page 581 and 582:
Revision Questions 40 109. The sing
Page 583 and 584:
Revision Questions 40 123. What doe
Page 585 and 586:
Revision Questions 40 138. When des
Page 587 and 588:
Revision Questions 40 152. What is
Page 589 and 590:
Answers 40 Answers to Flight Instru
Page 591 and 592:
Revision Questions 40 7. A yaw damp
Page 593 and 594:
Revision Questions 40 21. At the mi
Page 595 and 596:
Revision Questions 40 33. In an aut
Page 597 and 598:
Revision Questions 40 44. Regarding
Page 599 and 600:
Revision Questions 40 56. The autos
Page 601 and 602:
Revision Questions 40 Warning & Rec
Page 603 and 604:
Revision Questions 40 13. A stall w
Page 605 and 606:
Revision Questions 40 25. What corr
Page 607 and 608:
Answers 40 Answers to Warning & Rec
Page 609 and 610:
Revision Questions 40 7. If the int
Page 611 and 612:
Revision Questions 40 19. Total Air
Page 613 and 614:
Revision Questions 40 30. In a thre
Page 615 and 616:
Revision Questions 40 43. What does
Page 617 and 618:
Answers 40 Answers to Engine Instru
Page 619 and 620:
Revision Questions 40 8. Which of t
Page 621 and 622:
Revision Questions 40 20. What is u
Page 623 and 624:
Revision Questions 40 34. An IRS di
Page 625 and 626:
Revision Questions 40 45. Sound is
Page 627 and 628:
Revision Questions 40 59. The EADI
Page 629 and 630:
Answers 40 Explanations to Specimen
Page 631 and 632:
Answers 40 10. To calculate the rat
Page 633 and 634:
Answers 40 22. Answer B 23. Answer
Page 635 and 636:
Answers 40 47. C ± D = M ± V = T
Page 637 and 638:
Revision Questions 40 Specimen Exam
Page 639 and 640:
Revision Questions 40 12. Which of
Page 641 and 642:
Revision Questions 40 22. What erro
Page 643 and 644:
Revision Questions 40 32. During an
Page 645 and 646:
Revision Questions 40 42. What are
Page 647 and 648:
Revision Questions 40 50. EPR is th
Page 649 and 650:
Revision Questions 40 Revision Ques
Page 651 and 652:
Chapter 41 Index 645
Page 653 and 654:
Index 41 Symbols 400 - 330 feet RA
Page 655 and 656:
Index 41 Carrier Frequency ........
Page 657 and 658:
Index 41 Electrics and Electronics
Page 659 and 660:
Index 41 Independent Mode .........
Page 661 and 662:
Index 41 Off Route Waypoints ......
Page 663 and 664:
Index 41 Serviceability Checks ....
Page 665 and 666:
Index 41 Wedge Plate ..............
show all

Instrumentation

Create successful ePaper yourself

Delete template?

Save as template?