HIGHLIGHTS __________

REVISION NO. 52 Mar 01/07

Pages which have been revised are outlined below, together with the Highlights of theRevision

--------------------------------------------------------------------------------------CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES--------------------------------------------------------------------------------------

CHAPTER 22__________

L.E.P. 1- 7 Revised to Reflect this revision indicating new,revised, and/or deleted pagesT. OF C. Revised to reflect this revision 10- 1322-10-00 Layout Improved or Effectivity Updated 501- 502, 505

22-12-28 Layout Improved or Effectivity Updated 417, 419

22-23-00 Effectivity updated 21, 23

22-23-00 Layout Improved or Effectivity Updated 501- 502, 506- 531

22-23-39 02 Effectivity updated 401- 404

22-HIGHLIGHTS REVISION NO. 52 Page 1 of 1 JAS Mar 01/07

CHAPTER 22 __________

AUTO FLIGHT

LIST OF EFFECTIVE PAGES _______________________ N, R or D indicates pages which are New, Revised or Deleted respectively Remove and insert the affected pages and complete the Record of Revisions and the Record of Temporary Revisions as necessary

CH/SE/SU C PAGE DATE CH/SE/SU C PAGE DATE CH/SE/SU C PAGE DATE

RECORD 22-00-00 24 Mar01/03 22-10-00 507 Mar01/06OF TEMP. 22-00-00 301 Oct30/81 22-10-00 508 Mar01/06REVISION 22-00-00 401 Mar01/99 22-10-00 509 Mar01/06 22-00-00 402 Mar01/05 22-10-00 510 Mar01/06L.E.P. R 1- 7 Mar01/07 22-00-00 403 Mar01/99 22-10-00 511 Mar01/06T. of C. 1 Mar01/06 22-00-00 404 Mar01/99 22-10-00 512 Mar01/06T. of C. 2 Mar01/06 22-00-00 405 Mar01/06 22-10-00 513 Mar01/06T. of C. 3 Mar01/06 22-00-00 406 Mar01/99 22-10-00 514 Mar01/06T. of C. 4 Mar01/06 22-00-00 407 Mar01/99 22-10-00 515 Mar01/06T. of C. 5 Mar01/06 22-00-00 408 Mar01/99 22-10-00 516 Mar01/06T. of C. 6 Mar01/06 22-00-00 409 Mar01/99 22-10-00 517 Mar01/06T. of C. 7 Mar01/06 22-00-00 410 Mar01/99 22-10-00 518 Mar01/06T. of C. 8 Mar01/06 22-00-00 411 Mar01/06 22-10-00 519 Mar01/06T. of C. 9 Mar01/06 22-00-00 412 Mar01/06 22-10-00 520 Mar01/06T. of C. R 10 Mar01/07 22-00-00 501 Jul30/83 22-10-00 521 Mar01/06T. of C. R 11 Mar01/07 22-00-00 502 Jul30/83 22-10-00 522 Mar01/06T. of C. R 12 Mar01/07 22-00-00 503 Mar01/00 22-10-00 523 Mar01/06T. of C. R 13 Mar01/07 22-00-00 504 Mar01/00 22-10-00 524 Mar01/06 22-00-00 505 Mar01/00 22-10-00 525 Mar01/0622-00-00 1 Jan01/88 22-00-00 601 Oct30/8122-00-00 2 Oct30/79 22-00-00 602 Oct30/81 22-11-00 01 1 Mar01/0522-00-00 3 Oct30/81 22-11-00 01 2 Oct01/8922-00-00 4 Oct30/81 22-10-00 1 Mar01/05 22-11-00 01 3 Oct01/8922-00-00 5 Oct01/91 22-10-00 2 Oct30/79 22-11-00 01 4 Oct01/8722-00-00 6 Apr30/80 22-10-00 3 Oct01/89 22-11-00 01 5 Oct01/8922-00-00 7 Oct01/91 22-10-00 4 Oct01/89 22-11-00 01 6 Oct01/8922-00-00 8 Oct01/91 22-10-00 5 Oct01/91 22-11-00 01 7 Mar01/0522-00-00 9 Oct30/82 22-10-00 6 Oct01/91 22-11-00 01 8 Oct01/8922-00-00 10 Oct30/82 22-10-00 7 Oct01/89 22-11-00 01 9 Oct01/8922-00-00 11 Oct01/91 22-10-00 8 Oct01/89 22-11-00 01 10 Oct01/8922-00-00 12 Oct30/82 22-10-00 9 Oct01/89 22-11-00 01 11 Mar01/0522-00-00 13 Oct01/89 22-10-00 10 Oct01/89 22-11-00 01 12 Mar01/0522-00-00 14 Oct30/82 22-10-00 11 Oct01/89 22-11-00 01 13 Oct01/8922-00-00 15 Oct30/82 22-10-00 12 Mar01/05 22-11-00 01 14 Oct01/8922-00-00 16 Oct30/82 22-10-00 13 Oct01/89 22-11-00 01 15 Mar01/0522-00-00 17 Oct01/89 22-10-00 14 Oct01/89 22-11-00 01 16 Oct01/8922-00-00 18 Oct01/89 22-10-00 R 501 Mar01/07 22-11-00 01 17 Mar01/0022-00-00 19 Oct01/89 22-10-00 R 502 Mar01/07 22-11-00 01 18 Mar01/0022-00-00 20 Oct01/89 22-10-00 503 Mar01/06 22-11-00 01 19 Mar01/0022-00-00 21 Oct01/89 22-10-00 504 Mar01/06 22-11-00 01 20 Mar01/0022-00-00 22 Mar01/04 22-10-00 R 505 Mar01/07 22-11-00 01 21 Oct01/8922-00-00 23 Mar01/03 22-10-00 506 Mar01/06 22-11-00 01 22 Mar01/00

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22-11-00 01 23 Oct01/89 22-11-00 01 74 Mar01/05 22-11-00 02 524 Oct01/8922-11-00 01 24 Oct01/89 22-11-00 01 75 Mar01/05 22-11-00 02 525 Oct01/8922-11-00 01 25 Oct01/89 22-11-00 01 76 Mar01/05 22-11-00 02 526 Oct01/8922-11-00 01 26 Oct01/89 22-11-00 01 77 Mar01/05 22-11-00 02 527 Oct01/8922-11-00 01 27 Oct01/89 22-11-00 01 78 Mar01/05 22-11-00 02 528 Oct01/8922-11-00 01 28 Oct01/89 22-11-00 01 79 Mar01/05 22-11-00 02 529 Oct01/8922-11-00 01 29 Oct01/89 22-11-00 01 80 Mar01/05 22-11-00 02 530 Oct01/8922-11-00 01 30 Oct01/89 22-11-00 01 81 Mar01/05 22-11-00 02 531 Oct01/8922-11-00 01 31 Oct01/89 22-11-00 01 82 Mar01/05 22-11-00 02 532 Oct01/8922-11-00 01 32 Oct01/89 22-11-00 01 83 Mar01/05 22-11-00 02 533 Oct01/8922-11-00 01 33 Oct01/89 22-11-00 01 84 Mar01/05 22-11-00 02 534 Oct01/8922-11-00 01 34 Oct01/89 22-11-00 01 85 Mar01/05 22-11-12 401 Jul01/8822-11-00 01 35 Oct01/89 22-11-00 01 86 Mar01/05 22-11-12 402 Jul01/8822-11-00 01 36 Oct01/89 22-11-00 01 87 Mar01/05 22-11-12 403 Jul01/8822-11-00 01 37 Oct01/89 22-11-00 01 88 Mar01/05 22-11-12 404 Jul01/8822-11-00 01 38 Oct01/89 22-11-00 01 89 Mar01/05 22-11-12 405 Jan01/8822-11-00 01 39 Oct01/89 22-11-00 01 90 Oct01/89 22-11-13 401 Mar01/9922-11-00 01 40 Oct01/89 22-11-00 01 91 Mar01/05 22-11-13 402 Oct30/8122-11-00 01 41 Oct01/89 22-11-00 01 92 Mar01/05 22-11-13 403 Mar01/9922-11-00 01 42 Oct01/89 22-11-00 01 93 Mar01/05 22-11-13 404 Mar01/9922-11-00 01 43 Oct01/89 22-11-00 01 94 Mar01/05 22-11-14 401 Jul30/8122-11-00 01 44 Oct01/89 22-11-00 01 95 Mar01/05 22-11-14 402 Jul30/8122-11-00 01 45 Oct01/89 22-11-00 01 96 Mar01/05 22-11-14 403 Mar01/9922-11-00 01 46 Oct01/89 22-11-00 01 97 Mar01/05 22-11-14 404 Mar01/9922-11-00 01 47 Oct01/89 22-11-00 01 98 Mar01/05 22-11-14 405 Mar01/9922-11-00 01 48 Oct01/89 22-11-00 01 99 Mar01/05 22-11-17 401 Jan01/8822-11-00 01 49 Oct01/89 22-11-00 01 A 0 Mar01/05 22-11-17 402 Jul30/8122-11-00 01 50 Oct01/88 22-11-00 101 Jul30/82 22-11-17 403 Jan30/8222-11-00 01 51 Oct01/89 22-11-00 02 501 Oct01/89 22-11-17 404 Mar01/9922-11-00 01 52 Oct01/89 22-11-00 02 502 Oct01/89 22-11-17 405 Mar01/9922-11-00 01 53 Mar01/05 22-11-00 02 503 Oct01/89 22-11-17 406 Mar01/9922-11-00 01 54 Oct01/89 22-11-00 02 504 Mar01/05 22-11-17 407 Mar01/9922-11-00 01 55 Mar01/05 22-11-00 02 505 Oct01/89 22-11-17 408 Mar01/9922-11-00 01 56 Mar01/05 22-11-00 02 506 Oct01/89 22-11-21 401 Jan01/8822-11-00 01 57 Oct01/89 22-11-00 02 507 Oct01/89 22-11-21 402 Oct30/8122-11-00 01 58 Mar01/05 22-11-00 02 508 Oct01/89 22-11-21 403 Oct30/8322-11-00 01 59 Oct01/89 22-11-00 02 509 Oct01/89 22-11-21 404 Mar01/0522-11-00 01 60 Mar01/05 22-11-00 02 510 Oct01/89 22-11-21 405 Mar01/0522-11-00 01 61 Mar01/05 22-11-00 02 511 Oct01/89 22-11-26 401 Mar01/0022-11-00 01 62 Oct01/89 22-11-00 02 512 Oct01/89 22-11-26 402 Mar01/0022-11-00 01 63 Oct01/89 22-11-00 02 513 Oct01/89 22-11-26 403 Oct01/9422-11-00 01 64 Mar01/05 22-11-00 02 514 Oct01/89 22-11-26 404 Oct01/9422-11-00 01 65 Oct01/89 22-11-00 02 515 Oct01/89 22-11-26 405 Mar01/0022-11-00 01 66 Oct01/89 22-11-00 02 516 Oct01/90 22-11-26 406 Mar01/0022-11-00 01 67 Mar01/05 22-11-00 02 517 Oct01/89 22-11-26 407 Mar01/0022-11-00 01 68 Mar01/05 22-11-00 02 518 Oct01/89 22-11-26 408 Mar01/0022-11-00 01 69 Mar01/05 22-11-00 02 519 Oct01/91 22-11-26 409 Mar01/0022-11-00 01 70 Mar01/05 22-11-00 02 520 Oct01/89 22-11-26 410 Mar01/0022-11-00 01 71 Mar01/05 22-11-00 02 521 Oct01/89 22-11-26 411 Mar01/0022-11-00 01 72 Mar01/05 22-11-00 02 522 Oct01/89 22-11-26 412 Mar01/0022-11-00 01 73 Mar01/05 22-11-00 02 523 Oct01/89 22-11-26 413 Mar01/00

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22-11-26 414 Mar01/01 22-11-34 402 Apr30/83 22-12-00 01 42 Mar01/0422-11-26 415 Mar01/00 22-11-34 403 Apr01/89 22-12-00 01 43 Mar01/0522-11-26 416 Mar01/00 22-11-34 404 Apr01/89 22-12-00 01 44 Mar01/0422-11-26 417 Mar01/01 22-11-34 405 Apr01/89 22-12-00 01 45 Mar01/0522-11-26 418 Mar01/00 22-11-35 401 Oct30/81 22-12-00 01 46 Mar01/0422-11-26 419 Mar01/01 22-11-35 402 Oct30/81 22-12-00 01 47 Mar01/0522-11-26 420 Mar01/00 22-11-35 403 Oct30/81 22-12-00 01 48 Mar01/0522-11-26 421 Mar01/01 22-11-35 404 Jul01/88 22-12-00 01 49 Mar01/0522-11-26 422 Mar01/01 22-11-35 405 Jan01/88 22-12-00 01 50 Mar01/0522-11-26 423 Mar01/01 22-12-00 01 51 Mar01/0522-11-26 424 Mar01/01 22-12-00 01 1 Mar01/04 22-12-00 01 52 Mar01/0422-11-26 425 Mar01/01 22-12-00 01 2 Mar01/04 22-12-00 01 53 Mar01/0522-11-26 426 Mar01/01 22-12-00 01 3 Oct01/89 22-12-00 01 54 Mar01/0522-11-26 427 Mar01/01 22-12-00 01 4 Oct01/89 22-12-00 01 55 Mar01/0522-11-26 428 Mar01/01 22-12-00 01 5 Mar01/04 22-12-00 01 56 Mar01/0522-11-26 429 Mar01/01 22-12-00 01 6 Oct01/89 22-12-00 01 57 Mar01/0522-11-26 430 Mar01/01 22-12-00 01 7 Mar01/04 22-12-00 01 58 Mar01/0422-11-26 431 Mar01/01 22-12-00 01 8 Mar01/04 22-12-00 01 59 Mar01/0422-11-26 432 Mar01/01 22-12-00 01 9 Mar01/04 22-12-00 01 60 Mar01/0422-11-26 433 Mar01/01 22-12-00 01 10 Mar01/04 22-12-00 01 61 Mar01/0522-11-28 401 Mar01/05 22-12-00 01 11 Mar01/04 22-12-00 01 62 Mar01/0422-11-28 402 Oct01/95 22-12-00 01 12 Mar01/04 22-12-00 01 63 Mar01/0422-11-28 403 Mar01/05 22-12-00 01 13 Mar01/04 22-12-00 101 Jul30/8222-11-28 404 Mar01/05 22-12-00 01 14 Mar01/04 22-12-00 02 501 Oct01/8922-11-28 405 Mar01/05 22-12-00 01 15 Mar01/04 22-12-00 02 502 Oct01/8922-11-28 406 Mar01/05 22-12-00 01 16 Mar01/04 22-12-00 02 503 Mar01/0522-11-28 407 Mar01/05 22-12-00 01 17 Mar01/04 22-12-00 02 504 Oct01/8922-11-28 408 Mar01/05 22-12-00 01 18 Mar01/04 22-12-00 02 505 Oct01/8922-11-28 409 Mar01/05 22-12-00 01 19 Mar01/04 22-12-00 02 506 Oct01/8922-11-28 410 Mar01/05 22-12-00 01 20 Mar01/04 22-12-00 02 507 Oct01/8922-11-28 411 Mar01/05 22-12-00 01 21 Mar01/04 22-12-00 02 508 Mar01/0322-11-28 412 Mar01/05 22-12-00 01 22 Mar01/04 22-12-00 02 509 Oct01/8922-11-28 413 Mar01/05 22-12-00 01 23 Mar01/04 22-12-00 02 510 Oct01/8922-11-28 414 Mar01/05 22-12-00 01 24 Oct01/89 22-12-00 02 511 Oct01/8922-11-28 415 Mar01/05 22-12-00 01 25 Mar01/04 22-12-00 02 512 Oct01/8922-11-28 416 Mar01/05 22-12-00 01 26 Mar01/04 22-12-00 02 513 Oct01/8922-11-28 417 Mar01/05 22-12-00 01 27 Mar01/05 22-12-00 02 514 Oct01/8922-11-28 418 Mar01/05 22-12-00 01 28 Oct01/89 22-12-00 02 515 Oct01/8922-11-28 419 Mar01/05 22-12-00 01 29 Mar01/04 22-12-00 02 516 Oct01/8922-11-28 420 Mar01/05 22-12-00 01 30 Mar01/04 22-12-00 02 517 Oct01/8922-11-28 421 Mar01/05 22-12-00 01 31 Mar01/04 22-12-00 02 518 Oct01/8922-11-28 422 Mar01/05 22-12-00 01 32 Mar01/04 22-12-00 02 519 Oct01/8922-11-28 423 Mar01/05 22-12-00 01 33 Mar01/05 22-12-00 02 520 Oct01/8922-11-29 401 Mar01/05 22-12-00 01 34 Mar01/05 22-12-00 02 521 Oct01/8922-11-29 402 Oct01/95 22-12-00 01 35 Mar01/04 22-12-00 02 522 Oct01/8922-11-29 403 Oct01/95 22-12-00 01 36 Oct01/89 22-12-00 02 523 Oct01/8922-11-29 404 Mar01/05 22-12-00 01 37 Mar01/04 22-12-00 02 524 Oct01/8922-11-31 401 Oct01/89 22-12-00 01 38 Mar01/04 22-12-00 02 525 Oct01/8922-11-31 402 Oct01/89 22-12-00 01 39 Mar01/04 22-12-00 02 526 Oct01/8922-11-31 403 Oct01/89 22-12-00 01 40 Mar01/04 22-12-00 02 527 Oct01/9522-11-34 401 Dec30/84 22-12-00 01 41 Mar01/04 22-12-00 02 528 Oct01/89

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22-12-00 02 529 Oct01/89 22-13-00 02 11 Oct01/89 22-13-00 02 62 Oct01/8922-12-12 401 Jan01/88 22-13-00 02 12 Oct01/89 22-13-00 02 63 Mar01/0522-12-12 402 Apr30/80 22-13-00 02 13 Oct01/89 22-13-00 02 64 Oct01/8922-12-12 403 Mar01/05 22-13-00 02 14 Oct01/89 22-13-00 02 65 Mar01/0522-12-12 404 Jul01/85 22-13-00 02 15 Oct01/89 22-13-00 02 66 Mar01/0522-12-28 401 Mar01/04 22-13-00 02 16 Oct01/89 22-13-00 02 67 Oct01/8922-12-28 402 Mar01/04 22-13-00 02 17 Oct01/89 22-13-00 02 68 Mar01/0522-12-28 403 Apr01/86 22-13-00 02 18 Oct01/89 22-13-00 02 69 Mar01/0522-12-28 404 Mar01/04 22-13-00 02 19 Oct01/89 22-13-00 02 70 Mar01/0522-12-28 405 Mar01/04 22-13-00 02 20 Mar01/05 22-13-00 02 71 Oct01/8922-12-28 406 Mar01/04 22-13-00 02 21 Oct01/89 22-13-00 02 72 Oct01/8922-12-28 407 Mar01/04 22-13-00 02 22 Oct01/89 22-13-00 02 73 Mar01/0522-12-28 408 Mar01/04 22-13-00 02 23 Oct01/89 22-13-00 02 74 Mar01/0522-12-28 409 Mar01/04 22-13-00 02 24 Oct01/89 22-13-00 02 75 Mar01/0522-12-28 410 Mar01/04 22-13-00 02 25 Oct01/89 22-13-00 02 76 Mar01/0522-12-28 411 Mar01/04 22-13-00 02 26 Oct01/89 22-13-00 02 77 Mar01/0522-12-28 412 Mar01/04 22-13-00 02 27 Oct01/89 22-13-00 02 78 Mar01/0522-12-28 413 Mar01/04 22-13-00 02 28 Oct01/89 22-13-00 02 79 Mar01/0522-12-28 414 Mar01/04 22-13-00 02 29 Oct01/89 22-13-00 02 80 Mar01/0522-12-28 415 Mar01/04 22-13-00 02 30 Oct01/89 22-13-00 02 81 Mar01/0522-12-28 416 Mar01/04 22-13-00 02 31 Oct01/89 22-13-00 02 82 Mar01/0522-12-28 R 417 Mar01/07 22-13-00 02 32 Oct01/89 22-13-00 02 83 Mar01/0522-12-28 418 Mar01/04 22-13-00 02 33 Mar01/05 22-13-00 02 84 Mar01/0522-12-28 R 419 Mar01/07 22-13-00 02 34 Mar01/05 22-13-00 02 85 Mar01/0522-12-28 420 Mar01/04 22-13-00 02 35 Oct01/89 22-13-00 02 86 Mar01/0522-12-28 421 Mar01/04 22-13-00 02 36 Oct01/89 22-13-00 02 87 Mar01/0522-12-28 422 Mar01/04 22-13-00 02 37 Mar01/05 22-13-00 02 88 Mar01/0522-12-28 423 Mar01/04 22-13-00 02 38 Mar01/05 22-13-00 02 89 Mar01/0522-12-28 424 Mar01/04 22-13-00 02 39 Mar01/05 22-13-00 02 90 Mar01/0522-12-28 425 Mar01/04 22-13-00 02 40 Mar01/05 22-13-00 02 91 Mar01/0522-12-29 401 Oct01/97 22-13-00 02 41 Oct01/89 22-13-00 02 92 Mar01/0522-12-29 402 Oct01/97 22-13-00 02 42 Mar01/05 22-13-00 02 93 Mar01/0522-12-29 403 Oct01/97 22-13-00 02 43 Oct01/89 22-13-00 02 94 Mar01/0522-12-29 404 Oct01/97 22-13-00 02 44 Mar01/05 22-13-00 02 95 Mar01/0522-12-34 401 Mar01/05 22-13-00 02 45 Mar01/05 22-13-00 02 96 Mar01/0522-12-34 402 Apr30/83 22-13-00 02 46 Mar01/05 22-13-00 101 Jul30/8222-12-34 403 Mar01/05 22-13-00 02 47 Mar01/05 22-13-00 501 Dec30/8422-12-34 404 Mar01/05 22-13-00 02 48 Mar01/05 22-13-00 502 Jul01/8822-12-34 405 Mar01/05 22-13-00 02 49 Mar01/05 22-13-00 503 Jan01/8822-12-34 406 Mar01/05 22-13-00 02 50 Mar01/05 22-13-00 504 Jan01/88 22-13-00 02 51 Mar01/05 22-13-34 401 Mar01/0522-13-00 02 1 Oct01/89 22-13-00 02 52 Mar01/05 22-13-34 402 Oct30/8122-13-00 02 2 Oct01/89 22-13-00 02 53 Mar01/05 22-13-34 403 Oct01/9322-13-00 02 3 Oct01/91 22-13-00 02 54 Mar01/05 22-13-34 404 Mar01/0322-13-00 02 4 Jul01/88 22-13-00 02 55 Oct01/91 22-13-34 405 Mar01/0322-13-00 02 5 Oct01/89 22-13-00 02 56 Oct01/9122-13-00 02 6 Oct01/89 22-13-00 02 57 Oct01/89 22-14-00 1 Apr30/8022-13-00 02 7 Oct01/89 22-13-00 02 58 Oct01/89 22-14-00 2 Oct01/8922-13-00 02 8 Jul01/88 22-13-00 02 59 Oct01/89 22-14-00 3 Oct01/8922-13-00 02 9 Oct01/89 22-13-00 02 60 Oct01/89 22-14-00 4 Oct01/8922-13-00 02 10 Oct01/89 22-13-00 02 61 Oct01/89 22-14-00 5 Oct01/89

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22-14-00 6 Oct01/89 22-21-00 40 Jan01/88 22-23-00 1 Jan01/8822-14-00 7 Oct01/89 22-21-00 41 Jan01/88 22-23-00 2 Jan30/8122-14-00 8 Oct01/89 22-21-00 42 Jan01/88 22-23-00 3 Oct01/9622-14-00 9 Oct01/89 22-21-00 43 Jan01/88 22-23-00 4 Oct30/7922-14-00 10 Oct01/89 22-21-00 01 101 Jul30/82 22-23-00 5 Jan30/8122-14-00 501 Jul01/88 22-21-00 501 Jan01/88 22-23-00 6 Jan30/8122-14-00 502 Jan01/88 22-21-00 502 Jan30/81 22-23-00 7 Oct01/96 22-21-00 503 Jul01/85 22-23-00 8 Oct01/9622-20-00 1 Jul30/81 22-21-00 504 Mar01/05 22-23-00 9 Oct01/9622-20-00 2 Jul30/81 22-21-00 505 Jul01/89 22-23-00 10 Oct01/9622-20-00 3 Jul30/81 22-21-00 506 Jan30/81 22-23-00 11 Oct01/96 22-21-00 507 Jul01/88 22-23-00 12 Oct01/9622-21-00 1 Jan01/88 22-21-00 508 Jul01/88 22-23-00 13 Oct01/9622-21-00 2 Jul30/81 22-21-00 509 Jul01/88 22-23-00 14 Oct01/9622-21-00 3 Jul30/81 22-21-00 510 Jul01/88 22-23-00 15 Oct01/9622-21-00 4 Jul30/81 22-21-00 511 Mar01/05 22-23-00 16 Oct01/9622-21-00 5 Jul30/81 22-21-00 512 Jul01/88 22-23-00 17 Oct01/9622-21-00 6 Jul30/81 22-21-00 513 Mar01/05 22-23-00 18 Oct01/9622-21-00 7 Jul30/81 22-21-00 514 Mar01/04 22-23-00 19 Oct01/9622-21-00 8 Jul30/81 22-21-00 515 Mar01/04 22-23-00 20 Oct01/9622-21-00 9 Jul30/81 22-21-00 516 Jul01/88 22-23-00 R 21 Mar01/0722-21-00 10 Jul30/81 22-21-00 517 Jul01/89 22-23-00 22 Mar01/0022-21-00 11 Jul30/81 22-21-12 401 Oct30/81 22-23-00 R 23 Mar01/0722-21-00 12 Jul30/81 22-21-12 402 Oct30/81 22-23-00 24 Mar01/0022-21-00 13 Jul30/81 22-21-12 403 Oct30/81 22-23-00 25 Mar01/0022-21-00 14 Oct01/90 22-21-12 404 Oct30/81 22-23-00 26 Oct01/9622-21-00 15 Jul30/81 22-21-29 401 Oct01/97 22-23-00 27 Mar01/0022-21-00 16 Jul30/81 22-21-29 402 Oct01/97 22-23-00 28 Oct01/9622-21-00 17 Jul30/81 22-21-29 403 Jan01/89 22-23-00 29 Mar01/0022-21-00 18 Jul30/81 22-21-29 404 Oct01/97 22-23-00 30 Oct01/9622-21-00 19 Jul30/81 22-21-29 405 Oct01/97 22-23-00 31 Oct01/9622-21-00 20 Jan01/88 22-21-29 406 Oct01/97 22-23-00 32 Oct01/9622-21-00 21 Jan01/88 22-21-29 407 Oct01/97 22-23-00 33 Oct01/9622-21-00 22 Jan01/87 22-21-29 408 Oct01/97 22-23-00 34 Oct01/9622-21-00 23 Jan01/88 22-21-29 409 Oct01/97 22-23-00 35 Jul01/9822-21-00 24 Jan01/88 22-21-34 401 Jan01/88 22-23-00 36 Oct01/9622-21-00 25 Jan01/88 22-21-34 402 Jul30/82 22-23-00 37 Oct01/9622-21-00 26 Jan01/88 22-21-34 403 Jan30/84 22-23-00 38 Oct01/9622-21-00 27 Jan01/88 22-21-34 404 Jan30/84 22-23-00 39 Oct01/9622-21-00 28 Jan01/88 22-21-45 401 Jan01/88 22-23-00 40 Oct01/9622-21-00 29 Jan01/88 22-21-45 402 Apr30/80 22-23-00 41 Oct01/9622-21-00 30 Jan01/88 22-21-45 403 Apr30/80 22-23-00 42 Oct01/9622-21-00 31 Jan01/88 22-21-45 404 Jan30/82 22-23-00 43 Oct01/9622-21-00 32 Jan01/88 22-21-45 405 Oct01/91 22-23-00 44 Oct01/9622-21-00 33 Jan01/88 22-21-45 406 Oct01/91 22-23-00 45 Oct01/9622-21-00 34 Jan01/87 22-21-46 401 Jan01/88 22-23-00 101 Jul30/8222-21-00 35 Jan01/88 22-21-46 402 Oct30/81 22-23-00 R 501 Mar01/0722-21-00 36 Jan01/88 22-21-46 403 Oct30/81 22-23-00 R 502 Mar01/0722-21-00 37 Jan01/87 22-21-46 404 Jan01/87 22-23-00 503 Jan30/8122-21-00 38 Jan01/88 22-21-46 405 Oct30/81 22-23-00 504 Mar01/0622-21-00 39 Jan01/87 22-23-00 505 Mar01/06

22-L.E.P. Page 5 JAS Mar 01/07

CH/SE/SU C PAGE DATE CH/SE/SU C PAGE DATE CH/SE/SU C PAGE DATE

22-23-00 R 506 Mar01/07 22-24-00 3 Mar01/05 22-31-00 44 Mar01/0422-23-00 R 507 Mar01/07 22-24-15 401 Jan01/88 22-31-00 45 Mar01/0422-23-00 R 508 Mar01/07 22-24-15 402 Oct30/81 22-31-00 46 Mar01/0422-23-00 R 509 Mar01/07 22-24-15 403 Oct30/81 22-31-00 47 Mar01/0422-23-00 R 510 Mar01/07 22-24-21 401 Jan01/88 22-31-00 48 Mar01/0422-23-00 R 511 Mar01/07 22-24-21 402 Oct30/81 22-31-00 49 Mar01/0422-23-00 R 512 Mar01/07 22-24-21 403 Oct30/81 22-31-00 50 Mar01/0422-23-00 R 513 Mar01/07 22-31-00 51 Mar01/0422-23-00 R 514 Mar01/07 22-31-00 1 Jan01/88 22-31-00 52 Mar01/0422-23-00 R 515 Mar01/07 22-31-00 2 Oct30/80 22-31-00 53 Mar01/0422-23-00 R 516 Mar01/07 22-31-00 3 Jul01/89 22-31-00 54 Mar01/0422-23-00 R 517 Mar01/07 22-31-00 4 Oct30/79 22-31-00 55 Mar01/0422-23-00 R 518 Mar01/07 22-31-00 5 Apr30/80 22-31-00 56 Mar01/0422-23-00 R 519 Mar01/07 22-31-00 6 Apr30/80 22-31-00 101 Jan01/8822-23-00 R 520 Mar01/07 22-31-00 7 Apr30/81 22-31-00 401 Oct30/8122-23-00 R 521 Mar01/07 22-31-00 8 Apr30/81 22-31-00 402 Oct30/8122-23-00 R 522 Mar01/07 22-31-00 9 Oct01/87 22-31-00 403 Mar01/0522-23-00 R 523 Mar01/07 22-31-00 10 Oct01/89 22-31-00 404 Oct30/8122-23-00 R 524 Mar01/07 22-31-00 11 Jul01/89 22-31-00 501 Jan01/8822-23-00 R 525 Mar01/07 22-31-00 12 Oct01/89 22-31-00 502 Jul01/8922-23-00 R 526 Mar01/07 22-31-00 13 Oct01/89 22-31-00 503 Oct01/9322-23-00 R 527 Mar01/07 22-31-00 14 Oct01/89 22-31-00 504 Oct01/9322-23-00 N 528 Mar01/07 22-31-00 15 Oct01/89 22-31-00 505 Oct01/9322-23-00 N 529 Mar01/07 22-31-00 16 Oct01/89 22-31-00 506 Oct01/8722-23-00 N 530 Mar01/07 22-31-00 17 Oct01/89 22-31-00 507 Jul01/8922-23-00 N 531 Mar01/07 22-31-00 18 Oct01/89 22-31-00 508 Oct01/9022-23-12 401 Oct30/81 22-31-00 19 Oct01/89 22-31-00 509 Oct01/9022-23-12 402 Oct30/81 22-31-00 20 Oct01/89 22-31-00 510 Jul01/8922-23-12 403 Oct30/81 22-31-00 21 Oct01/89 22-31-00 511 Mar01/0522-23-29 401 Jan01/88 22-31-00 22 Oct01/89 22-31-00 512 Jul01/8922-23-29 402 Apr30/82 22-31-00 23 Mar01/04 22-31-00 513 Oct01/8722-23-29 403 Apr30/83 22-31-00 24 Mar01/04 22-31-00 514 Oct01/8722-23-29 404 Apr30/83 22-31-00 25 Mar01/04 22-31-00 515 Oct01/9222-23-29 405 Apr30/82 22-31-00 26 Mar01/04 22-31-00 516 Oct01/9022-23-34 401 Apr01/89 22-31-00 27 Mar01/04 22-31-00 517 Oct01/9222-23-34 402 Oct30/81 22-31-00 28 Mar01/04 22-31-00 518 Jul01/8922-23-34 403 Apr01/89 22-31-00 29 Mar01/04 22-31-00 519 Oct01/9022-23-37 401 Oct01/88 22-31-00 30 Mar01/04 22-31-00 520 Jul01/8922-23-37 402 Oct30/81 22-31-00 31 Mar01/04 22-31-00 521 Oct01/9222-23-37 403 Oct01/88 22-31-00 32 Mar01/04 22-31-00 522 Oct01/9222-23-39 01 401 Mar01/00 22-31-00 33 Mar01/04 22-31-00 523 Oct01/9222-23-39 01 402 Mar01/00 22-31-00 34 Mar01/04 22-31-00 524 Oct01/9222-23-39 01 403 Mar01/00 22-31-00 35 Mar01/04 22-31-00 525 Oct01/9222-23-39 01 404 Mar01/00 22-31-00 36 Mar01/04 22-31-00 526 Oct01/9222-23-39 02 R 401 Mar01/07 22-31-00 37 Mar01/04 22-31-00 527 Oct01/9222-23-39 02 R 402 Mar01/07 22-31-00 38 Mar01/04 22-31-00 528 Oct01/9222-23-39 02 R 403 Mar01/07 22-31-00 39 Mar01/04 22-31-00 529 Oct01/9222-23-39 02 R 404 Mar01/07 22-31-00 40 Mar01/04 22-31-00 530 Oct01/92 22-31-00 41 Mar01/04 22-31-00 531 Oct01/9222-24-00 1 Jan01/88 22-31-00 42 Mar01/04 22-31-00 532 Oct01/9222-24-00 2 Jan30/81 22-31-00 43 Mar01/04 22-31-00 533 Mar01/05

22-L.E.P. Page 6 JAS Mar 01/07

CH/SE/SU C PAGE DATE CH/SE/SU C PAGE DATE CH/SE/SU C PAGE DATE

22-31-00 534 Mar01/05 22-42-00 17 Jan01/8722-31-00 535 Oct01/92 22-42-00 18 Jan01/8822-31-00 536 Mar01/05 22-42-00 19 Jan01/8822-31-00 537 Oct01/92 22-42-00 20 Jan01/8822-31-00 538 Oct01/92 22-42-00 21 Jan01/8722-31-00 539 Oct01/92 22-42-00 22 Oct01/9022-31-00 540 Oct01/92 22-42-00 23 Oct01/9022-31-00 541 Oct01/92 22-42-00 24 Jan01/8722-31-00 542 Oct01/92 22-42-00 25 Jan01/8722-31-00 543 Oct01/92 22-42-00 26 Mar01/0522-31-00 544 Oct01/92 22-42-00 27 Jan01/8722-31-00 545 Oct01/92 22-42-00 28 Jan01/8722-31-00 546 Oct01/92 22-42-00 29 Jan01/8722-31-12 401 Mar01/05 22-42-00 30 Jan01/8722-31-12 402 Oct30/81 22-42-00 31 Jan01/8722-31-12 403 Oct01/88 22-42-00 32 Jan01/8722-31-27 401 Mar01/05 22-42-00 501 Jul01/8622-31-27 402 Oct30/81 22-42-00 502 Jul01/8622-31-27 403 Oct01/88 22-42-00 503 Jul01/8922-31-27 404 Oct01/88 22-42-00 504 Mar01/0522-31-27 405 Oct01/88 22-42-00 505 Mar01/0522-31-28 401 Oct01/88 22-42-00 506 Mar01/0522-31-28 402 Oct01/88 22-42-00 507 Oct01/9522-31-28 403 Oct01/88 22-42-00 508 Jul01/8922-31-28 404 Oct01/88 22-42-00 509 Jul01/8622-31-28 405 Oct01/88 22-42-00 510 Jul01/8722-31-28 406 Oct01/88 22-42-00 511 Jul01/8722-31-28 407 Oct01/88 22-42-00 512 Jul01/8922-31-28 408 Oct01/88 22-42-00 513 Oct01/9522-31-28 409 Oct01/88 22-42-00 514 Oct01/9522-31-34 401 Oct01/88 22-42-00 515 Jul01/8622-31-34 402 Jul30/81 22-42-21 401 Oct01/9222-31-34 403 Oct01/90 22-42-21 402 Jan01/8822-31-34 404 Oct01/88 22-42-21 403 Oct01/92 22-42-21 404 Oct01/9222-42-00 1 Apr30/80 22-42-21 405 Oct01/9222-42-00 2 Jan01/88 22-42-21 406 Oct01/9222-42-00 3 Apr30/80 22-42-34 401 Jan30/8122-42-00 4 Apr30/80 22-42-34 402 Jan30/8122-42-00 5 Jan01/88 22-42-34 403 Jan01/8722-42-00 6 Apr30/80 22-42-34 404 Mar01/0522-42-00 7 Jan01/8822-42-00 8 Apr30/8022-42-00 9 Oct01/9022-42-00 10 Oct30/7922-42-00 11 Apr30/8022-42-00 12 Apr30/8022-42-00 13 Apr30/8122-42-00 14 Jan01/8822-42-00 15 Apr30/8022-42-00 16 Apr30/80

22-L.E.P. Page 7 JAS Mar 01/07

CHAPTER 22 __________

AUTO FLIGHT

TABLE OF CONTENTS _________________

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________ AFCS 22-00-00 ____ Description and Operation 1 ALL Glossary of Terms and Abbreviations 22 ALL Servicing 301 ALL Deactivation/Reactivation 401 ALL MMEL Sect 1-22, Item 14. 401 ALL Deactivation 401 ALL Reactivation 402 ALL Deactivation/Reactivation 402 ALL MMEL Sect 1-22, 22-11-03 (FAA only) 402 ALL Deactivation 402 ALL Reactivation 404 ALL Deactivation/Reactivation 405 ALLR MMEL Sect 1-22, 22-11-06 (FAA only) 405 ALL Deactivation 405 ALL Reactivation 407 ALL Deactivation/Reactivation 408 ALL MMEL Sect 1-22, 22-31-01 (FAA only) 408 ALL Deactivation 408 ALL Reactivation 409 ALL Deactivation/Reactivation 410 ALL MMEL Sect 1-22, 22-23-02 (FAA only) 410 ALL Deactivation 410 ALL Reactivation 410 ALLR Deactivation/Reactivation 411 ALL Adjustment/Test 501 ALL Description 501 ALL Conditions for Cancellation 501 ALL Validation Conditions 501 ALL AFCS Components 501 ALL General 503 ALL Installation 503 ALL AFCS - Test Sets Operating 504 ALL Procedure Close-UP 505 ALL Inspection/Check 601 ALL AUTOPILOT/FLIGHT DIRECTOR 22-10-00 _________________________ Description and Operation 1 ALL General 1 ALL Description 1 ALL Piloting Integration 10 ALL Adjustment/Test 501 ALL Operational Check 501 ALL Pitch Mechanical Override 503 ALL Roll Mechanical Override 503 ALL Yaw Mechanical Override 504 ALL

22-CONTENTS Page 1 JAS Mar 01/06

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________R Automatic AP disengagement 505 ALL Functional Test : Automatic AP Cut- 507 ALL Off on the Ground Functional Test : LAND MODE 511 ALL LAND Mode with AP1 Engaged 513 ALL LAND Mode with AP2 Engaged 518 ALL LAND Mode with AP1 and AP2 519 ALL Engaged (LAND 3) AP/FD System Test 525 ALL

AP/FD ROLL/YAW CHANNEL 22-11-00 01 Description and Operation 1 001-101,103-999, General 1 001-101,103-999, Component Location 2 001-101,103-999, System Description 7 001-101,103-999, Component Description 7 001-101,103-999, Engage Module 56CA 7 001-101,103-999, Roll Module 55CA 12 001-101,103-999, Course Module (CRS) 53CA1 and 17 001-101,103-999, 53CA2 AFCS Mode Indicators 9CA1 and9CA2 18 001-101,103-999, FD Selection Box 11CA 20 001-101,103-999, Roll Servomotor 20CA 22 001-101,103-999, Yaw Servomotor 22CA 25 001-101,103-999, Torque Limiter Levers 25 001-101,103-999, Roll Dynamometric Rods 61CA 29 001-101,103-999, and 62CA Lateral Computer 3CA1, 3CA2 33 001-101,103-999, ADI 3FP1, 3FP2 48 001-101,103-999, Horizontal Situation Indicator 48 001-101,103-999, (HSI) 11FF1, 11FF2 Operation 48 001-101,103-999, Engagement/Disengagement 48 001-101,103-999, (Ref. 22-13-00) Computation Channels 48 001-101,103-999, Power Channel 55 001-101,103-999, Comparison of Peripherals 58 001-101,103-999, Attitude Comparisons 58 001-101,103-999, Heading Comparison 60 001-101,103-999, Course Comparison 61 001-101,103-999, Special Functions of YAW Axis 61 001-101,103-999, Mode Selection 61 001-101,103-999, Heading/Attitude Hold (ROLL) 64 001-101,103-999, Control Wheel Steering in 64 001-101,103-999, ROLL (ROLL CWS) 64 001-101,103-999, Heading Selection (HDG SEL) 68 001-101,103-999, VOR and VOR/DME mode 71 001-101,103-999, LOC Mode (V/L) 75 001-101,103-999, LOC Mode (APPR or LAND) 79 001-101,103-999, LAND Mode (ALIGN, ROLL OUT 79 001-101,103-999, Phases) GO-AROUND Mode (Lateral) 84 001-101,103-999,

22-CONTENTS Page 2 JAS Mar 01/06

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________ BACK BEAM Mode (B/B) 84 001-101,103-999, NAV Mode 89 ALL Interface 93 001-101,103-999, Air Data Computers (ADC) 1FL1 93 001-101,103-999, and/or 1FL2 Gyroscopic Units 1FP1 and/or 93 001-101,103-999, 1FP2, 1FP3 Compass Coupler 1FF1 and/or 1FF2 95 001-101,103-999, Radio Receivers 97 105-106,109-999, Radio Receivers 98 ALL Yaw Damper Computers 99 001-101,103-999, AFCS Test (Ref. 22-42-00) 99 001-101,103-999, Flight Controls A000 001-101,103-999, AP/FD ROLL/YAW CHANNEL 22-11-00 Fault Isolation Manual 101 ALL AP/FD ROLL/YAW CHANNEL 22-11-00 02 Adjustment/Test 501 ALL Operational Test 501 ALL Functional Test 503 ALL System Test 503 ALL FD Operation (without Hydraulic 507 ALL Power : Hydraulic Ground Power Supply Cart Depressurized) Engagement/Disengagement 507 ALL HDG SEL Mode 508 ALL VOR Mode 510 ALL BACK BEAM Mode 512 ALL NAV Mode 514 ALL APPROACH Mode 518 ALL Test of APPR Mode 518 ALL Check of Radio Altimeter 1000 ft. 521 ALL Contact and 2500 ft. Warning Flag AP Operation (with Hydraulic 523 ALL Power) Job Set-Up 523 ALL Engage Logic 523 ALL AP Engagement 523 ALL Check of Servomotor and 524 ALL Dynamometric Rod Adjustment Basic Mode and Control Wheel 525 ALL Steering (CWS) HDG SEL Mode 526 ALL Roll Attitude Comparison in 528 ALL Cruise Flight Roll Attitude Comparison 528 ALL during Landing Test with Both APs 531 ALL Check of Roll and Yaw Servomotor 531 ALL Co-ordination GO-AROUND Mode 532 ALL ENGAGE MODULE 22-11-12 Removal/Installation 401 ALL

22-CONTENTSR Page 3 JAS Mar 01/06

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________ ROLL MODULE 22-11-13 Removal/Installation 401 ALL COURSE Modules 53CA1 and 53CA2 22-11-14 Removal/Installation 401 ALL FLAP CONTROL MICROSWITCH UNIT 22-11-17 Removal/Installation 401 ALL AFCS MODE INDICATOR 9CA1 (9CA2) 22-11-21 Removal/Installation 401 ALL AUTOPILOT ROLL SERVOMOTOR 22-11-26 ROLL SERVOMOTOR 401 ALL Removal/Installation 401 ALL SERVO-VALVE 413 ALL Removal/Installation 413 ALL SOLENOIDS 419 ALL Removal/Installation 419 ALL FILTER 425 ALL Removal/Installation 425 ALL STRAINER 430 ALL Removal/Installation 430 ALL AUTOPILOT YAW SERVOMOTOR 22CA 22-11-28 YAW SERVOMOTOR 401 ALL Removal/Installation 401 ALL SERVO-VALVE 409 ALL Removal/Installation 409 ALL SOLENOIDS 412 ALL Removal/Instalation 412 ALL FILTERS 417 ALL Removal/Installation 417 ALL STRAINERS 421 ALL Removal/Installation 421 ALL YAW TORQUE LIMITER LEVER 23CA 22-11-29 Removal/Installation 401 ALL VOR SIGNAL CONDITIONER-95CA 22-11-31 Removal/Installation 401 ALL AP/FD LATERAL COMPUTER 3CA1 (3CA2) 22-11-34 Removal/Installation 401 ALL FD SELECTION BOX 22-11-35 Removal/Installation 401 ALL

AP/FD PITCH CHANNEL 22-12-00 01 Description and Operation 1 ALL General 1 ALL Component Location 1 ALL System Description 5 ALL Component Description 9 ALL Altitude Module 57CA 9 ALL Engage module 56CA 12 ALL Pitch Dynamometric Rods 69CA and 12 ALL 70CA Pitch Servomotor 18CA 16 ALL Pitch Torque Limiter Lever 19 ALL Longitudinal Computer 1CA1 (1CA2) 22 ALL

22-CONTENTSR Page 4 JAS Mar 01/06

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________ ADI 34 ALL Operation 35 ALL Engagement/Disengagement 35 ALL (Ref. 22-13-00) Computation Channels 35 ALL Power Channel 39 ALL Comparison of Peripherals 41 ALL Attitude Comparison 43 ALL Angle-of-Attack Comparison 43 ALL Mode Selection 43 ALL Attitude Hold (PITCH) and 43 ALL Turbulence (TURB) Attitude Hold in FD 45 ALL Control Wheel Steering in PITCH 48 ALL (PITCH CWS) Altitude Hold (ALT) 49 ALL Altitude Acquisition (ALT ACQ) 51 ALL Speed Hold (IAS) 51 ALL GLIDE mode (APPR or LAND) : GS 51 ALL FLARE Mode (LAND) 55 ALL GO-AROUND Mode (LONGITUDINAL) 55 ALL Autotrim (Ref. 22-23-00) 57 ALL Interface 58 ALL Air Data Computers (ADC) 58 ALL (1FL1, 1FL2) Gyroscopic Units 1FP1 and/or 1FP2 60 ALL and 1FP3 Radio Receivers 61 ALL Angle-of-Attack sensors (4FU1 62 ALL and FU2) Pitch Trim Computer 62 ALL AFCS Test Computer 63 ALL (Ref. 22-42-00) Flight Controls (Ref. 27-31-00) 63 ALL AP/FD PITCH CHANNEL 22-12-00 Fault Isolation Manual 101 ALL AP/FD PITCH CHANNEL 22-12-00 02 Adjustment/Test 501 ALL Operational Test 501 ALL FD Engagement Test 502 ALL Functional Test 502 ALL System Test 503 ALL FD Operation (Shut Down Hydraulic 507 ALL Power) Engagement/Disengagement 507 ALL FD Basic Mode 507 ALL IAS Mode 509 ALL ALT ACQ Mode and ALTITUDE ALERT 511 ALL Warning ALT Mode 513 ALL AP Operation (with Hydraulic 514 ALL Power)

22-CONTENTSR Page 5 JAS Mar 01/06

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________ Job Set-Up 514 ALL Engage Logic 514 ALL AP Engagement 515 ALL Check of Servomotor and 517 ALL Dynamometric Rod Adjustment 517 ALL Basic Mode and Control Wheel 518 ALL Steering (CWS) AP ALT Mode 519 ALL Test of AP Pitch Servomotor Tor- 521 ALL que Limiter Lever Autotrim Test 521 ALL LAND Mode (Mono-AP) 523 ALL Pitch Attitude Comparison During 523 ALL Landing Autotrim Test with AP1 and AP2 526 ALL Check of Autopilot Pitch Servo- 527 ALL Motor Connections ALTITUDE MODULE 22-12-12 Removal/Installation 401 ALL AUTOPILOT PITCH ACTUATOR 22-12-28 Autopilot Pitch Actuator R/I 401 ALL Autopilot Pitch Actuator, Servo- 411 ALL Valve R/I Autopilot Picth Actuator, 415 ALL Solenoid R/I Autopilot Pitch Actuator, Filter R/I 419 ALL Autopilot Pitch Actuator, 423 ALL Strainer R/I PITCH TORQUE LIMITER LEVER 22-12-29 Removal/Installation 401 ALL AP/FD LONGITUDINAL COMPUTER 1CA1 (1CA2) 22-12-34 Removal/Installation 401 ALL

AP/FD LOGIC/MONITOR CHANNEL 22-13-00 02 Description and Operation 1 ALL General 1 ALL Component Location 1 ALL System Description 7 ALL Component Description 11 ALL Engage Module 56CA 11 ALL Roll Module 55CA 11 ALL Altitude Module 57CA 11 ALL AFCS Mode Indicator 15 ALL Logic/Monitor Computer 15 ALL Clearing of ADI FD Bars 19 ALL AP Instinctive Disconnect 19 ALL GO-AROUND Tabs 20 ALL Flap Microswitch Unit 20 ALL Operation 22 ALL Engagement of AP 22 ALL Engage Logic Conditions 22 ALL Engagement of AP in CMD 24 ALL

22-CONTENTSR Page 6 JAS Mar 01/06

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________ Engagement of AP in MAN 24 ALL Disengagement 25 ALL Engagement of FD Function 27 ALL Engage Logic Conditions 27 ALL FD Engagement 27 ALL FD Disengagement 27 ALL AP/FD Engage Compatibility 29 ALL Mode Selection 30 ALL Special Mode Characteristics 30 ALL General Remarks on Mode Selection 30 ALL Basic LATERAL Mode : Heading/ 33 ALL Attitude (ROLL) Hold Heading Selection (HDG SEL) 33 ALL NOR/LOC Mode (V/L) 34 ALL BACK BEAM (B/B) Hold 34 ALL Navigation Mode 34 ALL Basic Longitudinal Mode (PITCH) 37 ALL Indicated Air speed (IAS) Hold 37 ALL Altitude (ALT) Hold 37 ALL Altitude Acquisition (ALT ACQ) 37 ALL Turbulence (TURB) 38 ALL Approach (APPR) 38 ALL Landing (LAND) 39 ALL Go-Around 40 ALL AFCS Operational Capability 47 ALL FD Selection and FD Flag 50 ALL Busbar and Compass Coupler 53 ALL Splitting Warnings - Monitors 59 ALL AP OFF Warning 59 ALL ALIGN Warning 63 ALL Warning Associated with AFCS 63 ALL Capability Change BEAM DEVN Warning Lights 65 ALL AUTOLAND Warning 68 ALL Altitude Alert 73 ALL Interface 78 ALL Air Data Computers (ADC) 78 ALL 1FL1 and/or 1FL2 Altimeters 2FL1 and/or 2FL2 78 ALL Gyroscopic Units 1FP1 and/or 78 ALL 1FP2, 1FP3 YAW DAMPER Computers 1CE1 and/ 79 ALL or 1CE2 Compass Couplers 1FF1 and/ 80 ALL or 1FF2 Pitch Trim Computers 1CC1 and/ 81 ALL or 1CC2 Autothrottle Computer 1CJ 82 ALL Radio Receivers (VOR, ILS, 82 ALL Radio Altimeter) Hydraulic System Low Pressure 91 ALL

22-CONTENTSR Page 7 JAS Mar 01/06

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________ Switches 26GR-28GR Lift Dumping Control Box 91 ALL Contactor 27XC 93 ALL AIDS 94 ALL AFCS Test (Ref. 22-42-00) 95 ALL Master Warning System 95 ALL AP/FD LOGIC/MONITOR CHANNEL 22-13-00 Fault Isolation Manual 101 ALL Adjustment/Test 501 ALL Operational Test 501 ALL Test of Altitude Alert 502 ALL AP OFF Warning 503 ALL AUTOLAND Warning 503 ALL AP/FD LOGIC/MONITOR COMPUTER 5CA1 22-13-34 (5CA2) Removal/Installation 401 ALL

AUTO FLIGHT CONTROL MODE LIGHTING 22-14-00 Description and Operation 1 ALL General 1 ALL Component Location 2 ALL System Description 4 ALL Component Description 6 ALL Lighting Transformers 1CL, 2CL 6 ALL AP/FD LT Selector Switch 5CL 6 ALL Operation 8 ALL Push-Button Illumination 8 ALL Warning Light Illumination 8 ALL Adjustment/Test 501 ALL SPEED - ATTITUDE CORRECTION 22-20-00 ___________________________ Description and Operation 1 ALL

YAW DAMPER 22-21-00 Description and Operation 1 ALL General 1 ALL Component Location 2 ALL Components Specific to Yaw 2 ALL Damper System Components Common to Other 2 ALL Systems System Description 3 ALL Components Specific to the 3 ALL System Components Common to Other 3 ALL Systems Monitoring Components 7 ALL Component Description 11 ALL Engage Unit 12CE 11 ALL Yaw Rate Gyros 3CE1 and 3CE2 13 ALL Accelerometers 15 ALL Servo-Actuator 5CE 17 ALL Slat and Flap Microswitches 20 ALL

22-CONTENTSR Page 8 JAS Mar 01/06

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________ Yaw Damper Computers 1CE1 and 20 ALL 1CE2 Operation 25 ALL System Engagement 25 ALL System Disengagement 28 ALL Computation Channel 28 ALL Power Channel 33 ALL Integration of the Command with 35 ALL Rudder Control Warning and Indicating 35 ALL Interface 38 ALL Connections with AP/FD System 38 ALL Connections with Hydraulic 38 ALL System Connections with Gyroscopic 38 ALL Units Connection with Variable Lever 38 ALL Arm (VLA) Unit Connections with Master Warning 38 ALL Controller Connections with Flight Controls 38 ALL Connection with AFCS Test 38 ALL Computer YAW DAMPER 22-21-00 01 Fault Isolation Manual 101 ALL YAW DAMPER 22-21-00 Adjustment/Test 501 ALL Operation Test 501 ALL YAW DAMPER 1 (2) Engagement Test 502 ALL YAW DAMPER 2 - RUDDER TRAVEL 502 ALL Connection Check System Test 504 ALL Disconnect Test 506 ALL Check of Level Switching 507 ALL Test of Yaw Rate Gyros 510 ALL Lateral Accelerometer Connection 511 ALL Test Turn co-ordination from attitude 513 ALL Variation Test Check of Priority of System 1 516 ALL over System 2 YAW DAMPER ENGAGE UNIT 22-21-12 Removal/installation 401 ALL Removal/installation (Ref. 22-21-45) 404 ALL Removal/installation (Ref. 22-21-46) 404 ALL YAW DAMPER SERVO-ACTUATOR 22-21-29 Removal/Installation 401 ALL YAW DAMPER COMPUTER 1CE1(1CE2) 22-21-34 Removal/Installation 401 ALL YAW RATE-GYRO 22-21-45 Removal/Installation 401 ALL YAW ACCELEROMETER 22-21-46

22-CONTENTSR Page 9 JAS Mar 01/06

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________ Removal/installation 401 ALL

AUTOMATIC PITCH TRIM 22-23-00 Description and Operation 1 ALL General 1 ALL Component Location 2 ALL System Components 2 ALL Components Common to Other 3 ALL Systems System Description 7 ALL Components Specific to the System 7 ALL Components Common to Other 7 ALL Systems System Monitoring Components 11 ALL Component Description 12 ALL Engage Unit 12 ALL Trim Control Switches 7CC and 8CC 14 ALL Pitch Trim Servomotors 3CC1 and 14 ALL 3CC2 Flap Microswitches 20 ALL Slat Microswitches 20 ALL Angle-of-Attack Sensor 27CC 21 103-103, Angle-of-Attack Sensor 27CC 21 001-102,104-104,107-999, Pitch Compensation Computer 19CC1 24 ALL and 19CC2 Pitch Trim Computers 1CC1 and 25 ALL 1CC2 Operation 30 ALL System Engagement 30 ALL System Disengagement 30 ALL Computation Channel 32 ALL Power Channel 39 ALL Integration of THS Control Order 41 ALL Warning Indications 41 ALL Interface 44 ALL Air Data Computer (ADC) 44 ALL AFCS System 44 ALL Master Warning Controller 44 ALL Angle-of-Attack Sensors 4FU1, 44 ALL 4FU2 Landing Gear Relay Box 104VU 44 ALL Connection with Flight Controls 44 ALL Fault Isolation Manual 101 ALL Adjustment/Test 501 ALL Operational Test 501 ALL AP and Autotrim Override Test 503 ALL Engagement and Warning Test 506 ALL Functional Test 508 ALL Check of Landing Gear Relay 509 ALL Contacts, with Aircraft on Ground Check of Landing Gear Relay 509 ALL Contacts, with Aircraft on Jacks

22-CONTENTSR Page 10 JAS Mar 01/07

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________ System Test 516 ALL THS Deflection Test 519 ALL Disconnection Test 521 ALL Override test 522 ALL Test of Auto-Trim Operation 523 ALL Test of MACH TRIM Operation 525 ALL Pitch Trim Neutralization Test 526 ALL Automatic Switching Test 527 ALL Test of PITCH COMPENSATION system 528 ALL PITCH TRIM ENGAGE UNIT 22-23-12 Removal/installation 401 ALL PITCH TRIM SERVOMOTOR 22-23-29 Removal/Installation 401 ALL PITCH TRIM COMPUTER 1CC1 (1CC2) 22-23-34 Removal/installation 401 ALL PITCH COMPENSATION COMPUTER 19CC1 22-23-37 (19CC2) Removal/Installation 401 ALL ANGLE-OF-ATTACK SENSOR 22-23-39 01 Removal/Installation 401 103-103, ANGLE OF ATTACK SENSOR 22-23-39 02 Removal/Installation 401 001-102,104-104,107-999,

TRIM ROTATION INDICATING 22-24-00 Description and Operation 1 ALL General 1 ALL Component Location 1 ALL SENSOR - TRIM ACTUATION 22-24-15 Removal/installation 401 ALL BOX - AURAL WARNING 22-24-21 Removal/Installation 401 ALL AUTOTHROTTLE CONTROL 22-31-00 Description and Operation 1 ALL General 1 ALL Component Location 2 ALL Components Specific to the System 2 ALL Components Common to Other 3 ALL Systems System Description 3 ALL Component Description 10 ALL Autothrottle Module 33CJ 10 ALL Autothrottle Servomotor 12CJ 12 ALL Coupling Units 3CJ1, 3CJ2 15 ALL Dynamometric Rods 32CJ, 34CJ 15 ALL Instinctive Disconnect 5CJ, 6CJ 18 ALL ATS Limiting Microswitches 19 ALL Configuration Microswitches 19 ALL FAST/SLOW Indication 22 ALL Airspeed/Mach Indicator (ASI) 23 ALL Autothrottle Computer 1CJ 24 ALL Operation 30 ALL Computer Channel 30 ALL

22-CONTENTSR Page 11 JAS Mar 01/07

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________ Monitoring 30 ALL ATS Arming 30 ALL ATS Clutching 34 ALL Mode Selection 34 ALL System Disengagement 47 ALL System Override 47 ALL Speed Selection and Indication 48 ALL THR OFF Warning 48 ALL Interface 51 ALL AP/FD System 51 001-101,103-999, AFCS Test 51 001-101,103-999, Air Data Computer (ADC) 1 1FL1 52 ALL Gyroscopic Unit 1FP1 52 ALL N1 Limit System 53 ALL SRS Computer 53 ALL Landing Gear Relay Box 104VU 53 ALL Master Warning System 54 ALL Connection to Throttle Control 54 ALL Levers Fault Isolation Manual 101 ALL Removal/Installation 401 ALL Removal/Installation of Throttle 401 ALL Control Lever Adjustment/Test 501 ALL Operational Test 501 ALL Functional Test 506 ALL General Functional Test 507 ALL Full Throttle Limit Stop Test 507 ALL N1 Throttle Limit Stop Test 508 ALL System Test 511 ALL Conditions for ATS Arming 513 ALL SPD SEL Mode Check 515 ALL Check of Autothrottle System 517 ALL Stops SPD SEL Mode Disengagement With 521 108-999, ATS Armed at Touch-Down SPD SEL Mode Disengagement With 523 001-107, ATS Armed at Touch-Down Override Test 524 ALL N1 Mode Test 526 ALL GA (Go-Around) Mode Test 529 ALL GA (Go-Around) Mode Test on the 531 108-999, Ground GA (Go-Around) Mode Test on the 533 001-107, Ground Threshold Program Test 535 001-107, Speed Derivation Term Test 536 108-999, AP/FD and ATS Interconnection 537 ALL Test Take-Off Function 537 105-105, Take-Off Function 539 ALL Alpha-Floor Protection Using 543 ALL

22-CONTENTSR Page 12 JAS Mar 01/07

SUBJECT CH/SE/SU C PAGE EFFECTIVITY _______ ________ _ ____ ________ Angle-of-Attack Sensor Position Simulator Alpha-Floor Protection Using 544 ALL A/ATTACK TEST Switch ATS MODULE 22-31-12 Removal/Installation 401 ALL AUTOTHROTTLE SERVOMOTOR 22-31-27 Removal/Installation 401 ALL ATS COUPLING UNIT 3CJ1(3CJ2) 22-31-28 Removal/Installation 401 ALL AUTOTHROTTLE COMPUTER 22-31-34 Removal/Installation 401 ALL AFCS TEST 22-42-00 Description and Operation 1 ALL General 1 ALL Component Location 2 ALL System Description 4 ALL Component Description 6 ALL Test Control Panel 6 ALL Test Computer 13 ALL Operation 18 ALL Test Point Acquisition 18 ALL Monitoring of Interlock Signals 18 ALL (logic) Stimuli Command Signals 18 ALL AFCS Monitoring in Flight 22 ALL Complementary Tests on the Ground 22 ALL Safety Tests on the Ground 22 ALL Relationship Between Display and 24 ALL Failure Diagnosis During Complementary Test Displays Associated with Yaw 24 ALL Damper 1 or 2 Displays Associated with 26 ALL PITCH TRIM 1(2) Displays Associated with 28 ALL Autothrottle System Displays Associated with 29 ALL AP/FD 1(2) Adjustement/Test 501 ALL Operational Test 501 ALL Test of Magnetic Indicators 501 ALL Functional Test 503 ALL Safety Tests 503 ALL System Test 506 ALL AFCS TEST CONTROL PANEL 22-42-21 Removal/Installation 401 ALL AFCS TEST COMPUTER 1CU1 (1CU2) 22-42-34 Removal/Installation 401 ALL

22-CONTENTSR Page 13 JAS Mar 01/07

AFCS - DESCRIPTION AND OPERATION ________________________________

1. General _______ (Ref. Fig. 001 ) The AFCS (Automatic Flight Control System) forms a fully integrated, system where identical design and development principles are applied as far as practicable at all levels of the assembly (pitch, roll, yaw channels). The AFCS assembly is made up of five sub-systems, fully duplicated except for the automatic throttle control sub-system (ATS). These subsystems are : - Autopilot/Flight Director (AP/FD) (Ref. 22-10-00) - Autostabilizer (YAW DAMPER) (Ref. 22-21-00) - Automatic pitch trim (Ref. 22-23-00) - Autothrottle (ATS) (Ref. 22-31-00) - AFCS Test (Ref. 22-42-00) The purpose of the AFCS is : - to provide automatic control of the aircraft in climb, cruise and landing operations - to display for the pilots, during the automatic landing phase, information on the landing status as well as on the operational capabilities of sys- tems - to supply the pilots with the flight director data required for flying the aircraft manually in certain mode configurations - to ensure aircraft stability in yaw during manual and automatic flight - to perform electric trim functions in manual flight, and pitch automatic trim functions in automatic flight, through slaving of the trimmable hori- zontal stabilizer (THS) - to control the aircraft speed in all phases of flight through slaving of the throttle control levers - to provide self-test sequences to reach the required levels of safety, in conjunction with functions proper to the flight envelope - to facilitate operational maintenance.

2. Description and Operation _________________________

A. Autopilot/Flight Director (Ref. 22-10-00) The composition of the AP/FD is detailed at subassembly level. The AP/FD comprises the control unit, computers, indicators and sensors required to ensure the following functions: (1)Control of the aircraft in the basic modes which are obtained immediately as the AP/FD subsystem is engaged or in upper modes (flight path hold mo- des) which are generally selected through operation of push-buttons on the control unit. (2)Automatic control of the aircraft all the way to touchdown in Category 3 A operating conditions and, after a failure, in Category 2 operating conditions. (3)Inclusion of a monitored system in cruise flight, and a duplex monitored system in the automatic landing mode.

B. Autostabilization (YAW DAMPER) (Ref. 22-21-00) The YAW DAMPER equipment is detailed at sub-assembly level.

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INTENTIONALLY BLANK

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Block Diagram Figure 001

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The YAW DAMPER sub-system provides the following function: - stabilization in yaw, operating both in manual flight and in auto flight. - The YAW DAMPER sub-system is designed to improve the aircraft flight per- formance and to help in damping the autopilot modes.

C. Automatic Pitch Trim (Ref. 22-23-00) The automatic pitch trim sub-system make-up is detailed at sub-assembly level. The sub-system actuates the trimmable horizontal stabilizer to ensure elec- trically controlled trim in manual flight and automatic trim in automatic flight. A pitch compensation function enables excessive aircraft nose-up to be corrected at certain angles-of-attack and speeds.

D. Autothrottle (Ref. 22-31-00) The autothrottle sub-system make-up is detailed at sub-assembly level. This sub-system operates the throttle control levers throughout the flight envelope to control the selected mode, the engine rpm and the automatic go-around. An internal monitoring channel ensures failure neutralization so that the aircraft never enters a dangerous speed configuration.

E. AFCS Test (Ref. 22-42-00) The test sub-system make-up is detailed at sub-assembly level. The purpose of this sub-system is to facilitate operational maintenance of the AFCS and to ensure the integrity of the system at the required safety levels.

3. Integration in the Aircraft ___________________________ Equipment associated with the AFCS and subject to this integration, e.g. control and indicating items, position returns, stops, overrides, are detai- led at lower levels (sub-assemblies, sub-sub-assemblies, components).

A. Electrical Power

R **ON A/C 001-102, 105-999,

(Ref. Fig. 002 )

R **ON A/C ALL

(Ref. Fig. 003 ) (1)Direct current Two separate DC power supplies are used, one on each side of the AFCS. Side 1 is supplied by the Lultimate emergencyL busbar 3PP and side 2 by the LnormalL busbar 1PP. During the landing maneuver a contactor controlled through a +28VDC Lland mode selectedL signal from the AFCS provides isolation of the two busbars so as to segregate the side 1 and side 2 power supplies. Opening of the contactor is taken into account in the landing status function. A battery supplied 28VDC is used by the two microprocessor TEST compu-

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INTENTIONALLY BLANK

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Electrical Power Figure 002

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Electrical PowerR Figure 003

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ters to sustain memories after shut-down of computer normal electrical power supply. (2)Alternating current All the AFCS sub-systems use single-phase AC 115VAC, 26VAC and 5VAC with the neutral grounded to the structure. Two separate single-phase AC 115VAC power supplies (LAL phase) are used, one on each side of the AFCS. Side 1 is supplied by the LnormalL busbar 1XP and side 2 by the LnormalL busbar 2XP. Two single-phase 26VAC supplies, providing the synchro system referen- ces, are derived from the 115VAC LAL phase, defined above. Only one 5VAC power supply is used for lighting all the faces of the con- trol panels.

B. Hydraulic Power Supply (Ref. Fig. 004 ) The AP servomotors associated with AFCS side 1 are supplied from the Green hydraulic system (which is not affected by an engine failure since it is pressurized by pumps installed on both engine 1 and engine 2). The yaw damper servomotor associated with AFCS side 1 is supplied from the Blue hydraulic system. The AP and yaw damper servomotors associated with AFCS side 2 are supplied from the Yellow hydraulic system. The Blue and Yellow power supplies can be affected by the failure of the corresponding engine. For each hydraulic power supply, a pressure switch delivers to the corres- ponding side the information Lhydraulic supply correctL in the form of an aircraft ground signal.

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Hydraulic Power Supply Figure 004

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C. Controls and Indicators (Ref. Fig. 005 )

R

(Ref. Fig. 006 )

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All the AFCS control and indicating components and equipment are located in the aircraft flight compartment. They are distributed as follows : (1)Glareshield : - AFCS control unit, of modular design, enables engagement and selection of AP/FD modes - AP OFF and AUTOLAND warning lights, in front of each pilot, indicate loss of automatic control capability - FD BARS clearing switches, in front of each pilot

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