Cirrus SR2x

Recommendations

Info

AUTOMATIC FLIGHT CONTROL SYSTEM SYSTEM OVERVIEW FLIGHT INSTRUMENTS AFCS ANNUNCIATIONS AND ALERTS AFCS STATUS ALERTS The annunciations in Table 7-5 (listed in order of increasing priority) can appear on the PFD above the Airspeed and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by criticality. AFCS Status Annunciation AUDIO PANEL & CNS EIS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS Figure 7-41 AFCS Status Annunciation Alert Condition Annunciation Description Rudder Mistrim Right Rudder Mistrim Left Aileron Mistrim Right Aileron Mistrim Left Elevator Mistrim Down Elevator Mistrim Up Pitch Trim Failure Yaw Damper Failure Yaw servo providing sustained force in the indicated direction Roll servo providing sustained force in the indicated direction Pitch servo providing sustained force in the indicated direction If AP engaged, take control of the aircraft and disengage AP If AP disengaged, move MET switch to unstick YD control failure ADDITIONAL FEATURES APPENDICES INDEX Roll Failure Pitch Failure System Failure Preflight Test Hypoxia Recognition System is activated Roll axis control failure; AP inoperative Pitch axis control failure AP and MET are unavailable; FD may still be available Performing preflight system test. Do not press the AP DISC Button during servo power-up and preflight system tests as this may cause the preflight system test to fail or never to start (if servos fail their power-up tests). Power must be cycled to the servos to remedy the situation. Preflight system test failed; aural alert sounds at failure Activated only by the Hypoxia Recognition System Table 7-5 AFCS Status Alerts 540 Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin 190-00820-11 Rev. A
AUTOMATIC FLIGHT CONTROL SYSTEM OVERSPEED PROTECTION NOTE: Overspeed protection is not active in ALT, GS or GP Modes. While Pitch Hold, Vertical Speed, Indicated Airspeed, Vertical Path Tracking, or an altitude capture mode is active, airspeed is monitored by the flight director. Pitch commands are not changed until overspeed protection becomes active. Overspeed protection is provided in situations where the flight director cannot acquire and maintain the mode reference for the selected vertical mode without exceeding the certified maximum autopilot airspeed. When an autopilot overspeed condition occurs, the Airspeed Reference appears in a box above the Airspeed Indicator, flashing a yellow ‘MAXSPD’ annunciation. The autopilot, if engaged, will follow the pitch up command from the flight director. Engine power should be reduced and/or the pitch reference adjusted to slow the aircraft. The annunciation disappears when the overspeed condition is resolved. NOTE: When the autopilot is outside normal operating limits, it uses more aggressive commands to return to normal limits. SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Airspeed Indicator FLIGHT MANAGEMENT UNDERSPEED PROTECTION Figure 7-42 Overspeed Annunciation HAZARD AVOIDANCE NOTE: While underspeed protection is active, the aircraft will deviate from the selected reference. Underspeed Protection is designed to discourage aircraft operation below minimum established airspeeds and is available when the autopilot is on. When the aircraft reaches a predetermined airspeed (Table 7-6), a yellow MINSPD annunciation (Figure 7-43) will appear above the airspeed indicator. When the airspeed trend vector reaches a predetermined airspeed (Table 7-6), a single aural “AIRSPEED” will sound, alerting the pilot to the impending underspeed condition. TKS FIKI * Flaps MINSPD Annunciation Aural AIRSPEED Alert OFF ON 0% 80 kt 85 kt 50% 76 kt 80 kt 100% 70 kt 80 kt 0% 85 kt 90 kt 50% 81 kt 85 kt * The optional TKS Flight Into Known Icing (FIKI) Anti-Ice System is only available on SR22 Models Table 7-6 MINSPD Annunciation and AIRSPEED Alert AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-11 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective by Garmin 541
Page 1:
® Cirrus SR2x Integrated Avionics
Page 4 and 5:
Copyright © 2008-2015 Garmin Ltd.
Page 6 and 7:
Blank Page Pilot’s Guide for the
Page 8 and 9:
WARNINGS, CAUTIONS, AND NOTES WARNI
Page 10 and 11:
WARNINGS, CAUTIONS, AND NOTES that
Page 12 and 13:
REVISION INFORMATION Record of Rele
Page 14 and 15:
TABLE OF CONTENTS 4.5 Additional Au
Page 16 and 17:
TABLE OF CONTENTS Day/Night View...
Page 18 and 19:
SYSTEM OVERVIEW SYSTEM OVERVIEW FLI
Page 20 and 21:
SYSTEM OVERVIEW SYSTEM OVERVIEW •
Page 22 and 23:
SYSTEM OVERVIEW SYSTEM OVERVIEW •
Page 24 and 25:
Page 26 and 27:
SYSTEM OVERVIEW SYSTEM OVERVIEW PFD
Page 28 and 29:
SYSTEM OVERVIEW SYSTEM OVERVIEW GAR
Page 30 and 31:
SYSTEM OVERVIEW SYSTEM OVERVIEW 3 C
Page 32 and 33:
SYSTEM OVERVIEW SYSTEM OVERVIEW GMA
Page 34 and 35:
Page 36 and 37:
Page 38 and 39:
Page 40 and 41:
Page 42 and 43:
SYSTEM OVERVIEW SYSTEM OVERVIEW Lev
Page 44 and 45:
Page 46 and 47:
Page 48 and 49:
Page 50 and 51:
Page 52 and 53:
Page 54 and 55:
Page 56 and 57:
Page 58 and 59:
Page 60 and 61:
SYSTEM OVERVIEW AUDIO PANEL & CNS E
Page 62 and 63:
Page 64 and 65:
Page 66 and 67:
Page 68 and 69:
Page 70 and 71:
Page 72 and 73:
Page 74 and 75:
FLIGHT INSTRUMENTS SYSTEM OVERVIEW
Page 76 and 77:
Page 78 and 79:
Page 80 and 81:
Page 82 and 83:
Page 84 and 85:
Page 86 and 87:
Page 88 and 89:
Page 90 and 91:
Page 92 and 93:
Page 94 and 95:
Page 96 and 97:
Page 98 and 99:
Page 100 and 101:
Page 102 and 103:
Page 104 and 105:
Page 106 and 107:
Page 108 and 109:
ENGINE INDICATION SYSTEM SYSTEM OVE
Page 110 and 111:
ENGINE INDICATION SYSTEM FLIGHT INS
Page 112 and 113:
Page 114 and 115:
Page 116 and 117:
Page 118 and 119:
Page 120 and 121:
Page 122 and 123:
Page 124 and 125:
Page 126 and 127:
AUDIO PANEL AND CNS SYSTEM OVERVIEW
Page 128 and 129:
Page 130 and 131:
Page 132 and 133:
Page 134 and 135:
Page 136 and 137:
Page 138 and 139:
Page 140 and 141:
Page 142 and 143:
Page 144 and 145:
Page 146 and 147:
Page 148 and 149:
AUDIO PANEL AND CNS ADDITIONAL FEAT
Page 150 and 151:
Page 152 and 153:
Page 154 and 155:
Page 156 and 157:
Page 158 and 159:
Page 160 and 161:
Page 162 and 163:
Page 164 and 165:
Page 166 and 167:
Page 168 and 169:
Page 170 and 171:
Page 172 and 173:
Page 174 and 175:
Page 176 and 177:
Page 178 and 179:
FLIGHT MANAGEMENT SYSTEM OVERVIEW N
Page 180 and 181:
FLIGHT MANAGEMENT SYSTEM OVERVIEW F
Page 182 and 183:
Page 184 and 185:
Page 186 and 187:
FLIGHT MANAGEMENT SYSTEM OVERVIEW W
Page 188 and 189:
Page 190 and 191:
Page 192 and 193:
FLIGHT MANAGEMENT SYSTEM OVERVIEW I
Page 194 and 195:
Page 196 and 197:
FLIGHT MANAGEMENT SYSTEM OVERVIEW 8
Page 198 and 199:
Page 200 and 201:
Page 202 and 203:
FLIGHT MANAGEMENT FLIGHT INSTRUMENT
Page 204 and 205:
Page 206 and 207:
FLIGHT MANAGEMENT SYSTEM OVERVIEW S
Page 208 and 209:
Page 210 and 211:
Page 212 and 213:
Page 214 and 215:
FLIGHT MANAGEMENT SYSTEM OVERVIEW I
Page 216 and 217:
Page 218 and 219:
Page 220 and 221:
Page 222 and 223:
Page 224 and 225:
Page 226 and 227:
Page 228 and 229:
Page 230 and 231:
Page 232 and 233:
Page 234 and 235:
Page 236 and 237:
Page 238 and 239:
Page 240 and 241:
Page 242 and 243:
Page 244 and 245:
FLIGHT MANAGEMENT SYSTEM OVERVIEW P
Page 246 and 247:
Page 248 and 249:
Page 250 and 251:
Page 252 and 253:
Page 254 and 255:
Page 256 and 257:
Page 258 and 259:
Page 260 and 261:
Page 262 and 263:
Page 264 and 265:
Page 266 and 267:
Page 268 and 269:
Page 270 and 271:
Page 272 and 273:
Page 274 and 275:
Page 276 and 277:
FLIGHT MANAGEMENT FLIGHT INSTRUMENT
Page 278 and 279:
Page 280 and 281:
Page 282 and 283:
Page 284 and 285:
Page 286 and 287:
Page 288 and 289:
Page 290 and 291:
Page 292 and 293:
Page 294 and 295:
Page 296 and 297:
Page 298 and 299:
Page 300 and 301:
Page 302 and 303:
Page 304 and 305:
Page 306 and 307:
Page 308 and 309:
FLIGHT MANAGEMENT SYSTEM OVERVIEW b
Page 310 and 311:
FLIGHT MANAGEMENT SYSTEM OVERVIEW h
Page 312 and 313:
Page 314 and 315:
Page 316 and 317:
FLIGHT MANAGEMENT SYSTEM OVERVIEW d
Page 318 and 319:
FLIGHT MANAGEMENT SYSTEM OVERVIEW b
Page 320 and 321:
FLIGHT MANAGEMENT AUDIO PANEL & CNS
Page 322 and 323:
Page 324 and 325:
Page 326 and 327:
Page 328 and 329:
Page 330 and 331:
Page 332 and 333:
Page 334 and 335:
Page 336 and 337:
FLIGHT MANAGEMENT AUDIO PANEL & CNS
Page 338 and 339:
HAZARD AVOIDANCE SYSTEM OVERVIEW FL
Page 340 and 341:
Page 342 and 343:
Page 344 and 345:
HAZARD AVOIDANCE SYSTEM OVERVIEW So
Page 346 and 347:
Page 348 and 349:
Page 350 and 351:
Page 352 and 353:
Page 354 and 355:
Page 356 and 357:
Page 358 and 359:
Page 360 and 361:
Page 362 and 363:
Page 364 and 365:
HAZARD AVOIDANCE AUDIO PANEL & CNS
Page 366 and 367:
Page 368 and 369:
Page 370 and 371:
Page 372 and 373:
HAZARD AVOIDANCE SYSTEM OVERVIEW TF
Page 374 and 375:
Page 376 and 377:
HAZARD AVOIDANCE SYSTEM OVERVIEW 3)
Page 378 and 379:
HAZARD AVOIDANCE SYSTEM OVERVIEW NO
Page 380 and 381:
HAZARD AVOIDANCE SYSTEM OVERVIEW EN
Page 382 and 383:
HAZARD AVOIDANCE SYSTEM OVERVIEW If
Page 384 and 385:
HAZARD AVOIDANCE SYSTEM OVERVIEW In
Page 386 and 387:
HAZARD AVOIDANCE EIS FLIGHT INSTRUM
Page 388 and 389:
Page 390 and 391:
Page 392 and 393:
Page 394 and 395:
Page 396 and 397:
Page 398 and 399:
Page 400 and 401:
Page 402 and 403:
HAZARD AVOIDANCE SYSTEM OVERVIEW 4)
Page 404 and 405:
HAZARD AVOIDANCE SYSTEM OVERVIEW AB
Page 406 and 407:
Page 408 and 409:
HAZARD AVOIDANCE SYSTEM OVERVIEW FI
Page 410 and 411:
Page 412 and 413:
HAZARD AVOIDANCE SYSTEM OVERVIEW If
Page 414 and 415:
Page 416 and 417:
Page 418 and 419:
Page 420 and 421:
Page 422 and 423:
HAZARD AVOIDANCE SYSTEM OVERVIEW He
Page 424 and 425:
Page 426 and 427:
HAZARD AVOIDANCE SYSTEM OVERVIEW TF
Page 428 and 429:
Page 430 and 431:
Page 432 and 433:
Page 434 and 435:
Page 436 and 437:
Page 438 and 439:
HAZARD AVOIDANCE SYSTEM OVERVIEW Sh
Page 440 and 441:
Page 442 and 443:
Page 444 and 445:
Page 446 and 447:
HAZARD AVOIDANCE SYSTEM OVERVIEW 80
Page 448 and 449:
Page 450 and 451:
Page 452 and 453:
HAZARD AVOIDANCE SYSTEM OVERVIEW Sh
Page 454 and 455:
Page 456 and 457:
HAZARD AVOIDANCE SYSTEM OVERVIEW 80
Page 458 and 459:
HAZARD AVOIDANCE SYSTEM OVERVIEW Fi
Page 460 and 461:
HAZARD AVOIDANCE SYSTEM OVERVIEW Al
Page 462 and 463:
Page 464 and 465:
Page 466 and 467:
Page 468 and 469:
Page 470 and 471:
Page 472 and 473:
Page 474 and 475:
Page 476 and 477:
HAZARD AVOIDANCE FLIGHT INSTRUMENTS
Page 478 and 479:
HAZARD AVOIDANCE SYSTEM OVERVIEW SY
Page 480 and 481:
Page 482 and 483:
Page 484 and 485:
Page 486 and 487:
Page 488 and 489:
Page 490 and 491:
Page 492 and 493:
Page 494 and 495:
Page 496 and 497:
Page 498 and 499:
Page 500 and 501:
Page 502 and 503:
HAZARD AVOIDANCE SYSTEM OVERVIEW A
Page 504 and 505:
Page 506 and 507: HAZARD AVOIDANCE SYSTEM OVERVIEW FL
Page 508 and 509: HAZARD AVOIDANCE EIS FLIGHT INSTRUM
Page 510 and 511: HAZARD AVOIDANCE SYSTEM OVERVIEW FL
Page 512 and 513: HAZARD AVOIDANCE FLIGHT MANAGEMENT
Page 514 and 515: AUTOMATIC FLIGHT CONTROL SYSTEM SYS
Page 546 and 547: 6 AUTOMATIC FLIGHT CONTROL SYSTEM S
Page 562 and 563: ADDITIONAL FEATURES SYSTEM OVERVIEW
Page 606 and 607:
ADDITIONAL FEATURES SYSTEM OVERVIEW
Page 608 and 609:
Page 610 and 611:
Page 612 and 613:
Page 614 and 615:
Page 616 and 617:
Page 618 and 619:
Page 620 and 621:
Page 622 and 623:
Page 624 and 625:
Page 626 and 627:
Page 628 and 629:
Page 630 and 631:
Page 632 and 633:
Page 634 and 635:
Page 636 and 637:
Page 638 and 639:
Page 640 and 641:
Page 642 and 643:
Page 644 and 645:
Page 646 and 647:
Page 648 and 649:
Page 650 and 651:
Page 652 and 653:
Page 654 and 655:
Page 656 and 657:
Page 658 and 659:
Page 660 and 661:
Page 662 and 663:
Page 664 and 665:
Page 666 and 667:
Page 668 and 669:
Page 670 and 671:
Page 672 and 673:
Page 674 and 675:
Page 676 and 677:
Page 678 and 679:
Page 680 and 681:
Page 682 and 683:
Page 684 and 685:
ADDITIONAL FEATURES AUDIO PANEL & C
Page 686 and 687:
APPENDIX A SYSTEM OVERVIEW FLIGHT I
Page 688 and 689:
Page 690 and 691:
Page 692 and 693:
APPENDIX A SYSTEM OVERVIEW GTS 800
Page 694 and 695:
APPENDIX A SYSTEM OVERVIEW System A
Page 696 and 697:
Page 698 and 699:
Page 700 and 701:
Page 702 and 703:
Page 704 and 705:
Page 706 and 707:
Page 708 and 709:
APPENDIX A SYSTEM OVERVIEW GARMIN A
Page 710 and 711:
Page 712 and 713:
APPENDIX A SYSTEM OVERVIEW TAS SYST
Page 714 and 715:
APPENDIX A SYSTEM OVERVIEW CONNEXT
Page 716 and 717:
APPENDIX B SYSTEM OVERVIEW 2) Apply
Page 718 and 719:
APPENDIX B EIS AUDIO PANEL & CNS FL
Page 720 and 721:
APPENDIX B SYSTEM OVERVIEW FLIGHT I
Page 722 and 723:
Page 724 and 725:
Page 726 and 727:
APPENDIX B AUDIO PANEL & CNS EIS FL
Page 728 and 729:
APPENDIX C SYSTEM OVERVIEW CHT CHKL
Page 730 and 731:
APPENDIX C SYSTEM OVERVIEW GCS GDC
Page 732 and 733:
APPENDIX C SYSTEM OVERVIEW FLIGHT I
Page 734 and 735:
APPENDIX C SYSTEM OVERVIEW FLIGHT I
Page 736 and 737:
APPENDIX C AUDIO PANEL & CNS EIS FL
Page 738 and 739:
APPENDIX D SYSTEM OVERVIEW FLIGHT I
Page 740 and 741:
APPENDIX D SYSTEM OVERVIEW FLIGHT I
Page 742 and 743:
APPENDIX E SYSTEM OVERVIEW HAZARD A
Page 744 and 745:
APPENDIX E SYSTEM OVERVIEW FLIGHT I
Page 746 and 747:
INDEX SYSTEM OVERVIEW FLIGHT INSTRU
Page 748 and 749:
INDEX SYSTEM OVERVIEW FLIGHT INSTRU
Page 750:
INDEX AUDIO PANEL & CNS EIS FLIGHT
show all

Cirrus SR2x

Create successful ePaper yourself

Delete template?

Save as template?