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27-CONTENTS

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2 Feb 20/2010

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9 May 20/2010

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O 25 May 20/2011

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O 30 May 20/2011

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O 32 May 20/2011

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O 35 May 20/2011

O 36 May 20/2011

27-CONTENTS (cont)

O 37 May 20/2011

O 38 May 20/2011

O 39 May 20/2011

O 40 May 20/2011

O 41 May 20/2011

O 42 May 20/2011

O 43 May 20/2011

O 44 May 20/2011

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6 BLANK

27-00-01

1 Feb 20/2010

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R 213 May 20/2011

R 214 May 20/2011

R 215 May 20/2011

R 216 May 20/2011

R 217 May 20/2011

R 218 May 20/2011

R 219 May 20/2011

R 220 May 20/2011

27-00-01 (cont)

R 221 May 20/2011

R 222 May 20/2011

R 223 May 20/2011

224 BLANK

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201 Feb 20/2010

202 BLANK

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501 Feb 20/2010

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27-02-00

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

605 Feb 20/2010

606 Feb 20/2010

607 Feb 20/2010

608 Feb 20/2010

609 Feb 20/2010

610 Feb 20/2010

611 Feb 20/2010

612 Feb 20/2010

613 Feb 20/2010

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616 Feb 20/2010

617 Feb 20/2010

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620 Feb 20/2010

621 Feb 20/2010

622 BLANK

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27-09-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

7 Feb 20/2010

8 Feb 20/2010

9 Feb 20/2010

10 Feb 20/2010

11 Feb 20/2010

12 Feb 20/2010

13 Feb 20/2010

14 Feb 20/2010

15 Feb 20/2010

16 Feb 20/2010

17 Feb 20/2010

18 Feb 20/2010

19 Feb 20/2010

20 Feb 20/2010

21 Feb 20/2010

22 Feb 20/2010

23 Feb 20/2010

24 Feb 20/2010

25 Feb 20/2010

26 Feb 20/2010

27 Feb 20/2010

28 Feb 20/2010

29 Feb 20/2010

30 Feb 20/2010

31 Feb 20/2010

32 Feb 20/2010

33 Feb 20/2010

34 Feb 20/2010

35 Feb 20/2010

36 BLANK

27-09-00

201 Feb 20/2010

202 Feb 20/2010

27-09-00 (cont)

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Feb 20/2010

210 Feb 20/2010

211 Feb 20/2010

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213 Feb 20/2010

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215 Feb 20/2010

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27-11-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

7 Feb 20/2010

8 Feb 20/2010

9 Feb 20/2010

10 Feb 20/2010

11 Feb 20/2010

12 Feb 20/2010

13 Feb 20/2010

14 Feb 20/2010

15 Feb 20/2010

16 Feb 20/2010

27-11-00

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

27-11-00 (cont)

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

511 Feb 20/2010

512 Feb 20/2010

513 Feb 20/2010

514 Feb 20/2010

515 Feb 20/2010

516 Feb 20/2010

517 May 20/2010

518 Feb 20/2010

519 Feb 20/2010

520 Feb 20/2010

521 Feb 20/2010

522 Feb 20/2010

523 Feb 20/2010

524 Feb 20/2010

525 Feb 20/2010

526 Jan 20/2011

527 Feb 20/2010

528 Feb 20/2010

529 Feb 20/2010

530 Feb 20/2010

531 Feb 20/2010

532 BLANK

27-11-02

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

27-11-02

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

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27-11-03

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Feb 20/2010

210 Feb 20/2010

211 Feb 20/2010

R 212 May 20/2011

213 Feb 20/2010

R 214 May 20/2011

215 Feb 20/2010

216 Feb 20/2010

217 Feb 20/2010

218 Feb 20/2010

27-11-14

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

R 207 May 20/2011

208 Feb 20/2010

209 Feb 20/2010

R 210 May 20/2011

211 Feb 20/2010

212 Feb 20/2010

213 Feb 20/2010

214 Feb 20/2010

215 Feb 20/2010

216 Feb 20/2010

217 Feb 20/2010

218 BLANK

27-11-16

401 Feb 20/2010

27-11-16 (cont)

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

R 406 May 20/2011

407 Feb 20/2010

R 408 May 20/2011

409 Feb 20/2010

410 Feb 20/2010

27-11-17

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

R 404 May 20/2011

R 405 May 20/2011

406 Feb 20/2010

407 Feb 20/2010

408 BLANK

27-11-17

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

27-11-20

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 May 20/2010

210 May 20/2010

211 May 20/2010

212 May 20/2010

213 May 20/2010

214 May 20/2010

215 Feb 20/2010

27-11-20 (cont)

216 Feb 20/2010

217 Feb 20/2010

218 BLANK

27-11-20

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

605 Feb 20/2010

606 Feb 20/2010

607 Feb 20/2010

608 BLANK

27-11-21

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 BLANK

27-11-21

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

27-18-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 BLANK

27-18-00

501 Feb 20/2010

502 May 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

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27-18-00 (cont)

508 Sep 20/2010

509 Feb 20/2010

510 Sep 20/2010

511 Sep 20/2010

512 Feb 20/2010

513 Feb 20/2010

514 Feb 20/2010

27-18-01

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

R 404 May 20/2011

405 Jan 20/2011

406 Jan 20/2011

27-21-00 Config 1

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

7 Feb 20/2010

8 Feb 20/2010

9 Feb 20/2010

10 Feb 20/2010

11 Feb 20/2010

12 Feb 20/2010

13 Feb 20/2010

14 Feb 20/2010

15 Feb 20/2010

16 Feb 20/2010

17 Feb 20/2010

18 Feb 20/2010

19 Feb 20/2010

20 Feb 20/2010

21 Feb 20/2010

22 Feb 20/2010

23 Feb 20/2010

24 Feb 20/2010

27-21-00 Config 1 (cont)

25 Feb 20/2010

26 Feb 20/2010

27 Feb 20/2010

28 Feb 20/2010

29 Feb 20/2010

30 Feb 20/2010

31 Feb 20/2010

32 Feb 20/2010

33 Feb 20/2010

34 Feb 20/2010

35 Feb 20/2010

36 Feb 20/2010

27-21-00 Config 1

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

511 Feb 20/2010

512 Feb 20/2010

513 Feb 20/2010

514 Feb 20/2010

515 Feb 20/2010

516 Feb 20/2010

517 Feb 20/2010

518 Feb 20/2010

519 Feb 20/2010

520 Feb 20/2010

521 Feb 20/2010

522 Feb 20/2010

523 Feb 20/2010

524 Feb 20/2010

525 Feb 20/2010

526 Jan 20/2011

27-21-00 Config 1 (cont)

R 527 May 20/2011

528 Sep 20/2010

529 Sep 20/2010

R 530 May 20/2011

531 Sep 20/2010

532 Sep 20/2010

533 Sep 20/2010

534 Jan 20/2011

535 Jan 20/2011

536 Sep 20/2010

537 Sep 20/2010

538 Jan 20/2011

539 Jan 20/2011

R 540 May 20/2011

541 Jan 20/2011

542 Jan 20/2011

543 Jan 20/2011

544 Jan 20/2011

545 Jan 20/2011

546 Jan 20/2011

547 Jan 20/2011

548 Sep 20/2010

549 Sep 20/2010

550 Sep 20/2010

551 Sep 20/2010

552 Sep 20/2010

553 Sep 20/2010

554 Sep 20/2010

555 Sep 20/2010

556 Feb 20/2010

557 Feb 20/2010

558 Feb 20/2010

559 Feb 20/2010

560 Feb 20/2010

561 Feb 20/2010

562 Feb 20/2010

563 Feb 20/2010

564 Feb 20/2010

565 Feb 20/2010

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27-21-00 Config 1 (cont)

566 Feb 20/2010

567 Feb 20/2010

568 Feb 20/2010

569 Feb 20/2010

570 Feb 20/2010

571 Feb 20/2010

572 Feb 20/2010

573 Feb 20/2010

574 Feb 20/2010

575 Feb 20/2010

576 Feb 20/2010

577 Feb 20/2010

578 Feb 20/2010

27-21-02

401 May 20/2010

402 Sep 20/2010

403 Sep 20/2010

404 May 20/2010

405 May 20/2010

406 May 20/2010

407 May 20/2010

408 May 20/2010

409 May 20/2010

410 May 20/2010

27-21-03

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 BLANK

27-21-05

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

27-21-05 (cont)

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 BLANK

27-21-06

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Feb 20/2010

210 Feb 20/2010

211 Feb 20/2010

212 Feb 20/2010

213 Feb 20/2010

214 Feb 20/2010

215 Feb 20/2010

216 Feb 20/2010

27-21-12

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Feb 20/2010

210 Feb 20/2010

211 Feb 20/2010

212 Feb 20/2010

27-21-12 (cont)

213 Feb 20/2010

214 Feb 20/2010

215 Feb 20/2010

216 Feb 20/2010

217 Feb 20/2010

218 Feb 20/2010

219 Feb 20/2010

220 Feb 20/2010

221 Feb 20/2010

222 Feb 20/2010

223 Feb 20/2010

224 Feb 20/2010

27-21-13

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

R 209 May 20/2011

R 210 May 20/2011

O 211 May 20/2011

R 212 May 20/2011

O 213 May 20/2011

214 BLANK

27-21-17

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Sep 20/2010

410 Sep 20/2010

411 Feb 20/2010

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27-21-17 (cont)

412 BLANK

27-21-17

R 601 May 20/2011

R 602 May 20/2011

603 Feb 20/2010

604 Feb 20/2010

605 Feb 20/2010

606 BLANK

27-21-19

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 Feb 20/2010

27-21-20

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Feb 20/2010

210 Feb 20/2010

211 Feb 20/2010

212 Feb 20/2010

213 Feb 20/2010

214 Feb 20/2010

215 Feb 20/2010

27-21-20 (cont)

216 Feb 20/2010

217 Sep 20/2010

218 Sep 20/2010

27-21-21

401 Feb 20/2010

402 Sep 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

R 409 May 20/2011

410 Jan 20/2011

411 Jan 20/2011

412 Jan 20/2011

413 Jan 20/2011

414 BLANK

27-21-21

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

27-21-23

201 Feb 20/2010

202 Feb 20/2010

203 May 20/2010

204 May 20/2010

205 May 20/2010

206 May 20/2010

207 May 20/2010

208 May 20/2010

27-23-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

27-23-00 (cont)

7 Feb 20/2010

8 Feb 20/2010

9 Feb 20/2010

10 Feb 20/2010

27-23-00

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

511 Feb 20/2010

512 BLANK

27-23-01

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 BLANK

27-23-02

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 BLANK

27-23-51

201 Feb 20/2010

R 202 May 20/2011

203 Feb 20/2010

204 Feb 20/2010

R 205 May 20/2011

R 206 May 20/2011

O 207 May 20/2011

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27-23-51 (cont)

208 BLANK

27-28-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

27-28-00

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

27-28-01

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

27-31-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

7 Feb 20/2010

8 Feb 20/2010

9 Feb 20/2010

10 Feb 20/2010

11 Feb 20/2010

12 Feb 20/2010

13 Feb 20/2010

14 Feb 20/2010

27-31-00 (cont)

15 Feb 20/2010

16 Feb 20/2010

17 Feb 20/2010

18 Feb 20/2010

19 Feb 20/2010

20 Feb 20/2010

27-31-00

501 Feb 20/2010

502 May 20/2010

503 May 20/2010

504 May 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

511 Feb 20/2010

512 Feb 20/2010

513 Feb 20/2010

514 Feb 20/2010

515 Feb 20/2010

516 Feb 20/2010

517 Feb 20/2010

518 Feb 20/2010

519 Feb 20/2010

520 Feb 20/2010

521 Feb 20/2010

522 Feb 20/2010

523 Feb 20/2010

524 Feb 20/2010

525 Feb 20/2010

526 Feb 20/2010

527 Feb 20/2010

528 Feb 20/2010

529 Sep 20/2010

R 530 May 20/2011

531 Jan 20/2011

532 Sep 20/2010

27-31-00 (cont)

R 533 May 20/2011

R 534 May 20/2011

535 Sep 20/2010

536 Sep 20/2010

537 Jan 20/2011

538 Jan 20/2011

539 Sep 20/2010

540 Jan 20/2011

541 Sep 20/2010

542 Jan 20/2011

543 Jan 20/2011

544 Sep 20/2010

545 Sep 20/2010

546 Sep 20/2010

547 Sep 20/2010

548 Sep 20/2010

549 Sep 20/2010

550 Sep 20/2010

551 Sep 20/2010

552 Sep 20/2010

553 Sep 20/2010

554 Sep 20/2010

R 555 May 20/2011

556 Sep 20/2010

557 Sep 20/2010

558 Sep 20/2010

559 Sep 20/2010

560 Sep 20/2010

561 Sep 20/2010

562 Sep 20/2010

563 Sep 20/2010

564 Sep 20/2010

565 Sep 20/2010

566 Sep 20/2010

567 Sep 20/2010

568 Sep 20/2010

569 Sep 20/2010

570 Feb 20/2010

571 Feb 20/2010

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27-31-00 (cont)

572 Feb 20/2010

573 Feb 20/2010

574 Feb 20/2010

575 Feb 20/2010

576 Feb 20/2010

577 Feb 20/2010

578 Feb 20/2010

579 Feb 20/2010

580 Feb 20/2010

581 Feb 20/2010

582 Feb 20/2010

583 Feb 20/2010

584 Feb 20/2010

585 Feb 20/2010

586 Feb 20/2010

587 Feb 20/2010

588 Feb 20/2010

589 Feb 20/2010

590 Feb 20/2010

591 May 20/2010

592 Feb 20/2010

593 Feb 20/2010

594 Feb 20/2010

595 Feb 20/2010

596 Feb 20/2010

597 Feb 20/2010

598 Feb 20/2010

598.1 Feb 20/2010

598.2 Feb 20/2010

598.3 Feb 20/2010

598.4 Feb 20/2010

598.5 Feb 20/2010

598.6 Feb 20/2010

27-31-01

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

27-31-01 (cont)

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

R 410 May 20/2011

411 May 20/2010

412 Feb 20/2010

413 Sep 20/2010

414 Jan 20/2011

415 Feb 20/2010

416 BLANK

27-31-01

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 BLANK

27-31-02

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

27-31-03

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

27-31-05

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

27-31-05 (cont)

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 Feb 20/2010

415 Feb 20/2010

416 Feb 20/2010

417 Feb 20/2010

418 Feb 20/2010

419 Feb 20/2010

420 Feb 20/2010

421 Feb 20/2010

422 Feb 20/2010

423 Feb 20/2010

424 Feb 20/2010

425 Feb 20/2010

426 Feb 20/2010

27-31-05

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

605 Feb 20/2010

606 Feb 20/2010

607 Feb 20/2010

608 Feb 20/2010

27-31-06

401 Feb 20/2010

402 May 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

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27-31-06 (cont)

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

27-31-10

R 401 May 20/2011

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

R 406 May 20/2011

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 BLANK

27-31-10

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

27-31-11

401 Feb 20/2010

402 May 20/2010

403 Feb 20/2010

404 May 20/2010

27-31-12

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 BLANK

27-31-13

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

27-31-13 (cont)

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

R 409 May 20/2011

O 410 May 20/2011

411 Feb 20/2010

412 Feb 20/2010

R 413 May 20/2011

414 BLANK

27-31-15

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

27-31-16

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 May 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

27-31-17

201 Feb 20/2010

R 202 May 20/2011

203 Feb 20/2010

27-31-17 (cont)

204 Feb 20/2010

R 205 May 20/2011

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Feb 20/2010

210 Feb 20/2010

211 Feb 20/2010

212 Feb 20/2010

213 Feb 20/2010

214 Feb 20/2010

215 Feb 20/2010

R 216 May 20/2011

R 217 May 20/2011

O 218 May 20/2011

27-31-18

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

R 407 May 20/2011

R 408 May 20/2011

O 409 May 20/2011

O 410 May 20/2011

O 411 May 20/2011

412 BLANK

27-31-19

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 BLANK

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27-31-21

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 BLANK

27-31-21

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

27-31-23

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

27-32-00 Config 4

1 Feb 20/2010

2 Feb 20/2010

R 3 May 20/2011

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

7 Feb 20/2010

8 Feb 20/2010

9 Feb 20/2010

10 Feb 20/2010

27-32-00 Config 5

501 Feb 20/2010

502 Feb 20/2010

503 May 20/2010

504 Sep 20/2010

505 Sep 20/2010

27-32-00 Config 5 (cont)

506 Jan 20/2011

507 Sep 20/2010

508 Sep 20/2010

509 May 20/2010

510 May 20/2010

R 511 May 20/2011

512 Sep 20/2010

513 Sep 20/2010

514 Sep 20/2010

515 Sep 20/2010

516 Sep 20/2010

517 Sep 20/2010

518 Sep 20/2010

519 Sep 20/2010

520 Jan 20/2011

27-32-01

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 BLANK

27-32-02

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 BLANK

27-32-05

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 BLANK

27-38-00

1 Feb 20/2010

2 Feb 20/2010

27-38-00 (cont)

3 Feb 20/2010

4 BLANK

27-38-00

501 May 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Jan 20/2011

508 Feb 20/2010

509 Feb 20/2010

510 Jan 20/2011

511 Feb 20/2010

512 Feb 20/2010

27-38-02

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

27-41-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

7 Feb 20/2010

8 Feb 20/2010

9 Feb 20/2010

10 Feb 20/2010

11 Feb 20/2010

12 Feb 20/2010

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27-41-00 (cont)

13 Feb 20/2010

14 Feb 20/2010

15 Feb 20/2010

16 Feb 20/2010

17 Feb 20/2010

18 Feb 20/2010

19 Feb 20/2010

20 Feb 20/2010

27-41-00

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

R 509 May 20/2011

510 Feb 20/2010

511 Feb 20/2010

512 Feb 20/2010

513 Feb 20/2010

514 Feb 20/2010

515 Feb 20/2010

516 Feb 20/2010

517 Feb 20/2010

518 Feb 20/2010

R 519 May 20/2011

R 520 May 20/2011

R 521 May 20/2011

O 522 May 20/2011

523 Feb 20/2010

524 Feb 20/2010

R 525 May 20/2011

R 526 May 20/2011

R 527 May 20/2011

R 528 May 20/2011

529 Feb 20/2010

530 Feb 20/2010

27-41-00 (cont)

531 Feb 20/2010

532 Feb 20/2010

533 Feb 20/2010

534 Feb 20/2010

R 535 May 20/2011

R 536 May 20/2011

R 537 May 20/2011

R 538 May 20/2011

O 539 May 20/2011

O 540 May 20/2011

541 Feb 20/2010

542 Feb 20/2010

R 543 May 20/2011

R 544 May 20/2011

O 545 May 20/2011

O 546 May 20/2011

R 547 May 20/2011

R 548 May 20/2011

O 549 May 20/2011

R 550 May 20/2011

O 551 May 20/2011

O 552 May 20/2011

O 553 May 20/2011

O 554 May 20/2011

O 555 May 20/2011

O 556 May 20/2011

O 557 May 20/2011

O 558 May 20/2011

O 559 May 20/2011

O 560 May 20/2011

O 561 May 20/2011

R 562 May 20/2011

R 563 May 20/2011

O 564 May 20/2011

O 565 May 20/2011

O 566 May 20/2011

27-41-01

R 401 May 20/2011

402 Feb 20/2010

27-41-01 (cont)

403 Feb 20/2010

R 404 May 20/2011

405 Feb 20/2010

406 Feb 20/2010

27-41-03

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

27-41-05

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

R 206 May 20/2011

R 207 May 20/2011

O 208 May 20/2011

27-41-07

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

27-41-10

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

R 405 May 20/2011

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

R 410 May 20/2011

O 411 May 20/2011

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FLIGHT CONTROLS
27-41-10 (cont)

R 412 May 20/2011

O 413 May 20/2011

O 414 May 20/2011

27-41-10

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

605 Feb 20/2010

606 Feb 20/2010

607 Feb 20/2010

608 Feb 20/2010

R 609 May 20/2011

610 Feb 20/2010

27-41-11

401 Feb 20/2010

R 402 May 20/2011

R 403 May 20/2011

R 404 May 20/2011

R 405 May 20/2011

O 406 May 20/2011

27-41-13

401 Feb 20/2010

402 Feb 20/2010

R 403 May 20/2011

404 Feb 20/2010

R 405 May 20/2011

O 406 May 20/2011

27-41-14

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

605 Feb 20/2010

606 Feb 20/2010

607 Feb 20/2010

608 Feb 20/2010

609 Feb 20/2010

610 Feb 20/2010

27-41-14 (cont)

611 Feb 20/2010

612 BLANK

27-41-17

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 BLANK

27-48-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

7 Feb 20/2010

8 BLANK

27-48-00

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Jan 20/2011

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

511 Feb 20/2010

512 Feb 20/2010

513 Feb 20/2010

514 Feb 20/2010

515 Feb 20/2010

516 Feb 20/2010

517 Feb 20/2010

518 Feb 20/2010

27-48-01

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

27-48-01 (cont)

404 Sep 20/2010

405 Sep 20/2010

406 Feb 20/2010

27-48-03

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

27-48-06

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 BLANK

27-51-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

7 Feb 20/2010

8 Sep 20/2010

9 Feb 20/2010

10 Feb 20/2010

11 Feb 20/2010

12 Feb 20/2010

13 Feb 20/2010

14 Feb 20/2010

15 Feb 20/2010

16 Feb 20/2010

17 Feb 20/2010

18 Feb 20/2010

19 Feb 20/2010

20 Feb 20/2010

21 Feb 20/2010

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27-51-00 (cont)

22 Feb 20/2010

23 Feb 20/2010

24 May 20/2010

25 Feb 20/2010

26 Feb 20/2010

27 Feb 20/2010

28 Feb 20/2010

29 Feb 20/2010

30 Feb 20/2010

31 Feb 20/2010

32 Feb 20/2010

33 Feb 20/2010

34 Feb 20/2010

35 Feb 20/2010

36 Feb 20/2010

37 Feb 20/2010

38 Feb 20/2010

27-51-00

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Feb 20/2010

210 Feb 20/2010

27-51-00

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

27-51-00 (cont)

511 Feb 20/2010

512 Feb 20/2010

513 Jan 20/2011

514 Jan 20/2011

515 Jan 20/2011

516 Jan 20/2011

517 Jan 20/2011

518 Jan 20/2011

519 Jan 20/2011

520 Jan 20/2011

521 Jan 20/2011

522 Jan 20/2011

523 Jan 20/2011

524 Jan 20/2011

525 Jan 20/2011

526 Jan 20/2011

R 527 May 20/2011

528 Jan 20/2011

529 Jan 20/2011

530 Jan 20/2011

531 Jan 20/2011

532 Jan 20/2011

533 Jan 20/2011

534 Jan 20/2011

535 Jan 20/2011

536 Jan 20/2011

537 Jan 20/2011

538 Jan 20/2011

539 Jan 20/2011

540 Jan 20/2011

541 Jan 20/2011

542 Jan 20/2011

543 Jan 20/2011

544 Jan 20/2011

545 Jan 20/2011

546 Jan 20/2011

547 Jan 20/2011

548 Jan 20/2011

549 Jan 20/2011

27-51-00 (cont)

550 Jan 20/2011

551 Jan 20/2011

552 Jan 20/2011

553 Jan 20/2011

554 Jan 20/2011

27-51-00

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

605 Feb 20/2010

606 Feb 20/2010

607 Feb 20/2010

608 Feb 20/2010

609 Feb 20/2010

610 Feb 20/2010

611 Feb 20/2010

612 Feb 20/2010

613 Feb 20/2010

614 Feb 20/2010

615 Feb 20/2010

616 Feb 20/2010

617 Feb 20/2010

618 Feb 20/2010

619 Feb 20/2010

620 Feb 20/2010

621 Feb 20/2010

622 Feb 20/2010

27-51-01

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Feb 20/2010

210 Feb 20/2010

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27-51-01 (cont)

211 Feb 20/2010

212 Feb 20/2010

213 Feb 20/2010

214 Feb 20/2010

215 Feb 20/2010

216 Feb 20/2010

217 Feb 20/2010

218 Feb 20/2010

27-51-02

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 Feb 20/2010

415 Feb 20/2010

416 Feb 20/2010

417 Feb 20/2010

418 Feb 20/2010

419 Feb 20/2010

420 BLANK

27-51-02

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

509 Feb 20/2010

27-51-02 (cont)

510 Feb 20/2010

511 Feb 20/2010

512 Feb 20/2010

513 Feb 20/2010

514 Feb 20/2010

515 Feb 20/2010

516 Feb 20/2010

517 Feb 20/2010

518 Feb 20/2010

519 Feb 20/2010

520 Feb 20/2010

521 Jan 20/2011

522 Jan 20/2011

523 Jan 20/2011

524 Jan 20/2011

525 Jan 20/2011

526 Jan 20/2011

527 Jan 20/2011

528 Jan 20/2011

529 Jan 20/2011

530 Jan 20/2011

27-51-02

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

605 Feb 20/2010

606 Feb 20/2010

607 Feb 20/2010

608 Feb 20/2010

609 Feb 20/2010

610 Feb 20/2010

611 Feb 20/2010

612 Feb 20/2010

613 Feb 20/2010

614 Feb 20/2010

27-51-03

R 401 May 20/2011

R 402 May 20/2011

27-51-03 (cont)

R 403 May 20/2011

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Sep 20/2010

408 Feb 20/2010

R 409 May 20/2011

R 410 May 20/2011

A 411 May 20/2011

A 412 May 20/2011

A 413 May 20/2011

A 414 May 20/2011

A 415 May 20/2011

A 416 BLANK

27-51-05

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 BLANK

27-51-06

401 May 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Jan 20/2011

413 Jan 20/2011

414 Jan 20/2011

415 Jan 20/2011

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27-51-06 (cont)

416 Jan 20/2011

417 Jan 20/2011

418 Jan 20/2011

419 Jan 20/2011

420 Jan 20/2011

421 Jan 20/2011

422 Jan 20/2011

423 Jan 20/2011

424 BLANK

27-51-07

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Jan 20/2011

406 Jan 20/2011

407 Jan 20/2011

408 Jan 20/2011

409 Jan 20/2011

410 BLANK

27-51-08

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Jan 20/2011

405 Feb 20/2010

406 Jan 20/2011

407 Jan 20/2011

408 Jan 20/2011

409 Jan 20/2011

410 Jan 20/2011

27-51-09

401 Feb 20/2010

402 Feb 20/2010

403 Jan 20/2011

404 Feb 20/2010

405 Jan 20/2011

406 Jan 20/2011

407 Jan 20/2011

27-51-09 (cont)

408 Jan 20/2011

409 Jan 20/2011

410 BLANK

27-51-10

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Jan 20/2011

405 Feb 20/2010

406 Jan 20/2011

407 Jan 20/2011

408 Jan 20/2011

409 Jan 20/2011

410 Jan 20/2011

411 Jan 20/2011

412 Jan 20/2011

27-51-11

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 BLANK

27-51-11

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

605 Feb 20/2010

606 Feb 20/2010

607 Feb 20/2010

27-51-11 (cont)

608 Feb 20/2010

609 Feb 20/2010

610 Feb 20/2010

611 Feb 20/2010

612 Feb 20/2010

613 Feb 20/2010

614 Feb 20/2010

615 Feb 20/2010

616 Feb 20/2010

617 Feb 20/2010

618 BLANK

27-51-12

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 May 20/2010

410 May 20/2010

411 May 20/2010

412 May 20/2010

413 May 20/2010

414 BLANK

27-51-12

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

511 Feb 20/2010

512 Feb 20/2010

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27-51-12 (cont)

513 Feb 20/2010

514 Feb 20/2010

27-51-13

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

R 404 May 20/2011

405 Feb 20/2010

406 Feb 20/2010

R 407 May 20/2011

408 Feb 20/2010

409 Feb 20/2010

410 BLANK

27-51-14

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 BLANK

27-51-14

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

511 Feb 20/2010

512 Feb 20/2010

27-51-14 (cont)

513 Feb 20/2010

514 Feb 20/2010

515 Feb 20/2010

516 Feb 20/2010

517 Feb 20/2010

518 Feb 20/2010

519 Feb 20/2010

520 Feb 20/2010

521 Feb 20/2010

522 Feb 20/2010

523 Sep 20/2010

524 Sep 20/2010

525 Sep 20/2010

526 Sep 20/2010

27-51-15

R 401 May 20/2011

O 402 May 20/2011

O 403 May 20/2011

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

R 410 May 20/2011

A 411 May 20/2011

A 412 May 20/2011

A 413 May 20/2011

A 414 May 20/2011

A 415 May 20/2011

A 416 May 20/2011

27-51-15

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 BLANK

27-51-16

401 Feb 20/2010

402 Feb 20/2010

27-51-16 (cont)

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 BLANK

27-51-17

401 Feb 20/2010

402 Sep 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Sep 20/2010

406 Sep 20/2010

407 Sep 20/2010

408 Sep 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 Feb 20/2010

415 Feb 20/2010

416 Feb 20/2010

417 Sep 20/2010

418 Sep 20/2010

419 Sep 20/2010

420 Sep 20/2010

27-51-18

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

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27-51-21

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

27-51-21

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

605 Feb 20/2010

606 Feb 20/2010

607 Feb 20/2010

608 Feb 20/2010

609 Feb 20/2010

610 Feb 20/2010

611 Feb 20/2010

612 Feb 20/2010

613 Feb 20/2010

614 Feb 20/2010

615 Feb 20/2010

616 Feb 20/2010

617 Feb 20/2010

618 BLANK

27-51-22

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

27-51-22 (cont)

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

27-51-22

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

511 Feb 20/2010

512 Feb 20/2010

513 Feb 20/2010

514 BLANK

27-51-23

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

27-51-23

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

27-51-24

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 May 20/2010

405 Jan 20/2011

406 Jan 20/2011

27-51-24 (cont)

407 Jan 20/2011

408 Jan 20/2011

409 Jan 20/2011

410 BLANK

27-51-25

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Jan 20/2011

209 Jan 20/2011

210 Jan 20/2011

211 Jan 20/2011

212 Jan 20/2011

213 Jan 20/2011

214 Jan 20/2011

215 Jan 20/2011

216 Jan 20/2011

217 Jan 20/2011

218 Jan 20/2011

219 Jan 20/2011

220 Jan 20/2011

221 Jan 20/2011

222 Jan 20/2011

223 Jan 20/2011

224 Jan 20/2011

225 Jan 20/2011

226 Jan 20/2011

27-51-26

401 Jan 20/2011

402 Jan 20/2011

403 Jan 20/2011

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

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27-51-26 (cont)

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 Jan 20/2011

415 Jan 20/2011

416 Jan 20/2011

R 417 May 20/2011

R 418 May 20/2011

O 419 May 20/2011

O 420 May 20/2011

421 Jan 20/2011

422 Jan 20/2011

423 Jan 20/2011

424 Jan 20/2011

425 Jan 20/2011

426 Jan 20/2011

27-51-27

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Jan 20/2011

206 Feb 20/2010

207 Feb 20/2010

R 208 May 20/2011

R 209 May 20/2011

R 210 May 20/2011

O 211 May 20/2011

O 212 May 20/2011

O 213 May 20/2011

O 214 May 20/2011

27-51-28

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

27-51-28 (cont)

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Jan 20/2011

209 Jan 20/2011

210 Jan 20/2011

211 Jan 20/2011

212 Jan 20/2011

213 Jan 20/2011

214 Jan 20/2011

R 215 May 20/2011

O 216 May 20/2011

O 217 May 20/2011

O 218 May 20/2011

O 219 May 20/2011

O 220 May 20/2011

O 221 May 20/2011

O 222 May 20/2011

O 223 May 20/2011

O 224 May 20/2011

O 225 May 20/2011

O 226 May 20/2011

O 227 May 20/2011

O 228 May 20/2011

O 229 May 20/2011

230 BLANK

27-51-29

201 Feb 20/2010

202 Jan 20/2011

203 Jan 20/2011

204 Feb 20/2010

205 May 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Jan 20/2011

210 Jan 20/2011

O 211 May 20/2011

R 212 May 20/2011

27-51-29 (cont)

R 213 May 20/2011

O 214 May 20/2011

O 215 May 20/2011

O 216 May 20/2011

217 Jan 20/2011

218 Jan 20/2011

219 Jan 20/2011

220 Jan 20/2011

221 Jan 20/2011

222 Jan 20/2011

223 Jan 20/2011

224 Jan 20/2011

225 Jan 20/2011

226 Jan 20/2011

227 Jan 20/2011

228 Jan 20/2011

229 Jan 20/2011

230 Jan 20/2011

231 Jan 20/2011

232 Jan 20/2011

233 Jan 20/2011

234 Jan 20/2011

235 Jan 20/2011

236 Jan 20/2011

27-51-30

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Feb 20/2010

210 Feb 20/2010

211 Feb 20/2010

212 Feb 20/2010

213 Feb 20/2010

214 Feb 20/2010

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27-51-30 (cont)

215 Feb 20/2010

216 BLANK

27-51-31

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Sep 20/2010

209 Feb 20/2010

210 Feb 20/2010

211 Feb 20/2010

212 May 20/2010

213 Feb 20/2010

214 Sep 20/2010

215 Sep 20/2010

216 BLANK

27-51-32

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 Feb 20/2010

415 Feb 20/2010

416 Feb 20/2010

27-51-32

601 Feb 20/2010

602 Feb 20/2010

27-51-32 (cont)

603 Feb 20/2010

604 BLANK

27-51-33

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 BLANK

27-51-34

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 BLANK

27-58-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

7 Feb 20/2010

8 BLANK

27-58-00

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

27-58-01

501 Sep 20/2010

502 Sep 20/2010

27-58-01 (cont)

503 Sep 20/2010

504 Sep 20/2010

R 505 May 20/2011

R 506 May 20/2011

R 507 May 20/2011

R 508 May 20/2011

509 Feb 20/2010

510 Feb 20/2010

511 Feb 20/2010

512 Feb 20/2010

513 Feb 20/2010

514 Feb 20/2010

515 Feb 20/2010

516 Feb 20/2010

517 Feb 20/2010

518 Feb 20/2010

519 Feb 20/2010

520 Feb 20/2010

521 Feb 20/2010

522 Feb 20/2010

523 Feb 20/2010

524 May 20/2010

525 May 20/2010

526 May 20/2010

527 May 20/2010

528 May 20/2010

529 May 20/2010

530 May 20/2010

531 May 20/2010

532 May 20/2010

533 May 20/2010

534 May 20/2010

535 Feb 20/2010

536 Feb 20/2010

537 Feb 20/2010

538 Feb 20/2010

539 Feb 20/2010

540 Feb 20/2010

541 Feb 20/2010

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27-58-01 (cont)

542 Feb 20/2010

543 Feb 20/2010

544 Feb 20/2010

545 Feb 20/2010

546 BLANK

27-58-02

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 BLANK

27-58-03

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 BLANK

27-60-00

1 Feb 20/2010

2 Feb 20/2010

27-61-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

7 Feb 20/2010

8 Feb 20/2010

9 Feb 20/2010

10 Feb 20/2010

11 Feb 20/2010

12 Feb 20/2010

13 Feb 20/2010

14 Feb 20/2010

15 Feb 20/2010

16 Feb 20/2010

27-61-00 (cont)

17 Feb 20/2010

18 Feb 20/2010

19 Feb 20/2010

20 Feb 20/2010

21 Feb 20/2010

22 BLANK

27-61-00

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Feb 20/2010

210 Feb 20/2010

211 Feb 20/2010

212 Feb 20/2010

213 Feb 20/2010

214 Feb 20/2010

215 Feb 20/2010

216 BLANK

27-61-00

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

R 511 May 20/2011

512 Feb 20/2010

513 Feb 20/2010

514 Feb 20/2010

515 Feb 20/2010

27-61-00 (cont)

516 Feb 20/2010

517 Feb 20/2010

518 Jan 20/2011

519 Jan 20/2011

520 Feb 20/2010

521 Jan 20/2011

522 Jan 20/2011

523 Jan 20/2011

524 Feb 20/2010

525 Feb 20/2010

526 Feb 20/2010

527 Feb 20/2010

528 Feb 20/2010

529 Jan 20/2011

530 Jan 20/2011

531 Jan 20/2011

532 Jan 20/2011

533 Jan 20/2011

534 Jan 20/2011

535 Jan 20/2011

536 Feb 20/2010

537 Feb 20/2010

538 Jan 20/2011

539 Feb 20/2010

540 Feb 20/2010

541 Feb 20/2010

542 Feb 20/2010

R 543 May 20/2011

544 Feb 20/2010

545 Feb 20/2010

546 Feb 20/2010

547 Feb 20/2010

548 Feb 20/2010

549 Feb 20/2010

550 Feb 20/2010

551 Feb 20/2010

552 Feb 20/2010

R 553 May 20/2011

O 554 May 20/2011

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27-61-00 (cont)

R 555 May 20/2011

R 556 May 20/2011

O 557 May 20/2011

R 558 May 20/2011

O 559 May 20/2011

O 560 May 20/2011

R 561 May 20/2011

R 562 May 20/2011

R 563 May 20/2011

R 564 May 20/2011

R 565 May 20/2011

R 566 May 20/2011

O 567 May 20/2011

O 568 May 20/2011

R 569 May 20/2011

O 570 May 20/2011

O 571 May 20/2011

O 572 May 20/2011

O 573 May 20/2011

O 574 May 20/2011

O 575 May 20/2011

576 BLANK

27-61-01

401 Feb 20/2010

402 Feb 20/2010

403 Sep 20/2010

404 Sep 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 Feb 20/2010

415 Feb 20/2010

416 Feb 20/2010

27-61-01 (cont)

417 Feb 20/2010

418 Feb 20/2010

419 Feb 20/2010

420 Sep 20/2010

421 Feb 20/2010

422 Feb 20/2010

423 Feb 20/2010

424 Feb 20/2010

425 Feb 20/2010

426 Feb 20/2010

427 Feb 20/2010

428 Feb 20/2010

429 Feb 20/2010

430 Feb 20/2010

27-61-02

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Sep 20/2010

208 Feb 20/2010

R 209 May 20/2011

O 210 May 20/2011

R 211 May 20/2011

O 212 May 20/2011

O 213 May 20/2011

O 214 May 20/2011

O 215 May 20/2011

216 BLANK

27-61-04

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

27-62-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

7 Feb 20/2010

8 Feb 20/2010

9 Feb 20/2010

10 Feb 20/2010

11 Feb 20/2010

12 BLANK

27-62-00

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

505 Jan 20/2011

506 Sep 20/2010

507 Sep 20/2010

508 Jan 20/2011

509 Jan 20/2011

510 Sep 20/2010

511 Jan 20/2011

512 Sep 20/2010

513 Sep 20/2010

514 Jan 20/2011

515 Sep 20/2010

516 Sep 20/2010

517 Sep 20/2010

518 Sep 20/2010

519 Sep 20/2010

520 Sep 20/2010

R 521 May 20/2011

522 Jan 20/2011

523 Jan 20/2011

524 Sep 20/2010

525 Sep 20/2010

526 Sep 20/2010

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27-62-00 (cont)

527 Sep 20/2010

528 Sep 20/2010

529 Sep 20/2010

530 Sep 20/2010

531 Sep 20/2010

532 Sep 20/2010

533 Sep 20/2010

534 Sep 20/2010

535 Sep 20/2010

536 BLANK

27-62-01

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 BLANK

27-62-02

R 201 May 20/2011

202 Feb 20/2010

R 203 May 20/2011

204 Feb 20/2010

R 205 May 20/2011

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Feb 20/2010

210 Feb 20/2010

211 Feb 20/2010

212 Feb 20/2010

213 Feb 20/2010

214 Feb 20/2010

215 Feb 20/2010

216 Feb 20/2010

217 Feb 20/2010

218 Feb 20/2010

219 Feb 20/2010

27-62-02 (cont)

220 Feb 20/2010

221 Feb 20/2010

222 Feb 20/2010

223 Feb 20/2010

224 BLANK

27-62-07

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

504 Feb 20/2010

27-62-08

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 BLANK

27-81-00

1 Feb 20/2010

2 Feb 20/2010

3 Feb 20/2010

4 Feb 20/2010

5 Feb 20/2010

6 Feb 20/2010

7 Feb 20/2010

8 Feb 20/2010

9 Feb 20/2010

10 Feb 20/2010

11 Feb 20/2010

12 Feb 20/2010

13 Feb 20/2010

14 Feb 20/2010

15 Feb 20/2010

16 May 20/2010

17 Feb 20/2010

18 Feb 20/2010

19 Feb 20/2010

27-81-00 (cont)

20 Feb 20/2010

21 Feb 20/2010

22 Feb 20/2010

23 Feb 20/2010

24 Feb 20/2010

25 Feb 20/2010

26 Feb 20/2010

27 Feb 20/2010

28 Feb 20/2010

29 Feb 20/2010

30 Feb 20/2010

31 Feb 20/2010

32 Feb 20/2010

33 Feb 20/2010

34 Feb 20/2010

35 Feb 20/2010

36 Feb 20/2010

37 Feb 20/2010

38 Feb 20/2010

39 Feb 20/2010

40 Feb 20/2010

41 Feb 20/2010

42 Feb 20/2010

27-81-00

201 Feb 20/2010

202 Feb 20/2010

R 203 May 20/2011

R 204 May 20/2011

R 205 May 20/2011

206 Feb 20/2010

207 Feb 20/2010

R 208 May 20/2011

209 Feb 20/2010

210 Feb 20/2010

211 Feb 20/2010

212 Feb 20/2010

27-81-00

501 Feb 20/2010

502 Feb 20/2010

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27-81-00 (cont)

503 Feb 20/2010

504 Feb 20/2010

505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

511 Feb 20/2010

512 Feb 20/2010

513 May 20/2010

514 Feb 20/2010

515 Feb 20/2010

516 Feb 20/2010

517 Feb 20/2010

518 Feb 20/2010

519 Feb 20/2010

520 Feb 20/2010

521 Feb 20/2010

522 Feb 20/2010

523 May 20/2010

524 Feb 20/2010

525 Feb 20/2010

526 Feb 20/2010

527 Feb 20/2010

528 Feb 20/2010

529 Feb 20/2010

530 Feb 20/2010

531 Feb 20/2010

532 Feb 20/2010

533 Feb 20/2010

534 Feb 20/2010

535 Feb 20/2010

536 Feb 20/2010

537 Feb 20/2010

538 Feb 20/2010

539 Feb 20/2010

540 Feb 20/2010

541 Feb 20/2010

27-81-00 (cont)

542 Feb 20/2010

543 Feb 20/2010

544 Feb 20/2010

545 Feb 20/2010

546 Feb 20/2010

547 Feb 20/2010

548 Feb 20/2010

549 Feb 20/2010

550 Feb 20/2010

551 Feb 20/2010

552 Feb 20/2010

553 Feb 20/2010

554 Feb 20/2010

555 Feb 20/2010

556 Feb 20/2010

557 Feb 20/2010

558 Feb 20/2010

559 Feb 20/2010

560 Feb 20/2010

561 Feb 20/2010

562 Feb 20/2010

563 Feb 20/2010

564 Feb 20/2010

27-81-01

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 Feb 20/2010

415 Feb 20/2010

27-81-01 (cont)

416 Feb 20/2010

417 Feb 20/2010

418 May 20/2010

419 May 20/2010

420 May 20/2010

421 May 20/2010

422 May 20/2010

423 May 20/2010

424 May 20/2010

425 May 20/2010

426 May 20/2010

427 May 20/2010

428 May 20/2010

429 May 20/2010

430 May 20/2010

431 May 20/2010

432 May 20/2010

433 May 20/2010

434 May 20/2010

27-81-01

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

27-81-02

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 Feb 20/2010

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27-81-02 (cont)

415 Feb 20/2010

416 Feb 20/2010

417 Feb 20/2010

418 Feb 20/2010

419 Feb 20/2010

420 Feb 20/2010

421 Feb 20/2010

422 Feb 20/2010

423 Feb 20/2010

424 Feb 20/2010

425 Feb 20/2010

426 Feb 20/2010

427 Feb 20/2010

428 Feb 20/2010

429 Feb 20/2010

430 Feb 20/2010

431 Feb 20/2010

432 Feb 20/2010

433 Feb 20/2010

434 Feb 20/2010

27-81-02

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

605 Feb 20/2010

606 BLANK

27-81-06

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

208 Feb 20/2010

209 Feb 20/2010

210 Feb 20/2010

R 211 May 20/2011

27-81-06 (cont)

R 212 May 20/2011

O 213 May 20/2011

O 214 May 20/2011

215 Feb 20/2010

216 Feb 20/2010

217 Feb 20/2010

218 Feb 20/2010

219 Feb 20/2010

220 BLANK

27-81-07

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 Feb 20/2010

R 415 May 20/2011

R 416 May 20/2011

417 Jan 20/2011

418 Jan 20/2011

R 419 May 20/2011

420 Jan 20/2011

421 Jan 20/2011

422 Jan 20/2011

423 Jan 20/2011

424 Jan 20/2011

27-81-08

201 Feb 20/2010

202 Feb 20/2010

203 Feb 20/2010

204 Feb 20/2010

27-81-08 (cont)

205 Feb 20/2010

206 Feb 20/2010

207 Feb 20/2010

R 208 May 20/2011

R 209 May 20/2011

210 Feb 20/2010

211 Feb 20/2010

212 Feb 20/2010

213 Feb 20/2010

214 BLANK

27-81-09

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

R 407 May 20/2011

R 408 May 20/2011

O 409 May 20/2011

O 410 May 20/2011

A 411 May 20/2011

A 412 BLANK

27-81-10

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

27-81-10

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

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27-81-10 (cont)

605 Feb 20/2010

606 Feb 20/2010

607 Feb 20/2010

608 BLANK

27-81-11

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

27-81-11

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

605 Feb 20/2010

606 Feb 20/2010

607 Feb 20/2010

608 Feb 20/2010

609 Feb 20/2010

610 Feb 20/2010

27-81-12

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 BLANK

27-81-12

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 BLANK

27-81-13

401 Feb 20/2010

402 Feb 20/2010

27-81-13 (cont)

403 Feb 20/2010

404 BLANK

27-81-13

601 Feb 20/2010

602 Feb 20/2010

603 Feb 20/2010

604 Feb 20/2010

27-81-15

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

27-81-18

R 401 May 20/2011

402 Jan 20/2011

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

R 412 May 20/2011

413 Jan 20/2011

414 Jan 20/2011

415 Jan 20/2011

416 Jan 20/2011

417 Jan 20/2011

418 Jan 20/2011

419 Jan 20/2011

420 Jan 20/2011

421 Jan 20/2011

422 BLANK

27-81-18

601 Feb 20/2010

R 602 May 20/2011

603 Jan 20/2011

604 Jan 20/2011

605 Jan 20/2011

606 Jan 20/2011

607 Jan 20/2011

608 Jan 20/2011

609 Feb 20/2010

610 Feb 20/2010

611 Feb 20/2010

612 Feb 20/2010

613 Feb 20/2010

614 Feb 20/2010

615 Feb 20/2010

616 Feb 20/2010

617 Feb 20/2010

618 Feb 20/2010

619 Feb 20/2010

620 Feb 20/2010

621 Feb 20/2010

622 Feb 20/2010

623 Feb 20/2010

624 Feb 20/2010

27-81-20

401 Feb 20/2010

402 Feb 20/2010

403 Feb 20/2010

404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Feb 20/2010

411 Feb 20/2010

412 Feb 20/2010

27-81-20

801 Feb 20/2010

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FLIGHT CONTROLS
27-81-20 (cont)

802 Feb 20/2010

27-81-41

401 Jan 20/2011

402 Jan 20/2011

403 Jan 20/2011

404 Jan 20/2011

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

408 Feb 20/2010

409 Feb 20/2010

410 Jan 20/2011

411 Feb 20/2010

412 Feb 20/2010

413 Feb 20/2010

414 Feb 20/2010

415 Feb 20/2010

416 Feb 20/2010

417 Feb 20/2010

418 Feb 20/2010

419 Jan 20/2011

420 Jan 20/2011

421 Feb 20/2010

422 BLANK

27-81-41

501 Feb 20/2010

502 Feb 20/2010

503 Feb 20/2010

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505 Feb 20/2010

506 Feb 20/2010

507 Feb 20/2010

508 Feb 20/2010

509 Feb 20/2010

510 Feb 20/2010

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514 Feb 20/2010

27-81-42

401 Feb 20/2010

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403 Feb 20/2010

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27-81-42

501 Feb 20/2010

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27-88-00

1 Feb 20/2010

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27-88-00

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27-88-01

401 Feb 20/2010

402 Feb 20/2010

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404 Feb 20/2010

405 Feb 20/2010

406 Feb 20/2010

407 Feb 20/2010

27-88-01 (cont)

408 BLANK

757

AIRCRAFT MAINTENANCE MANUAL

A = Added, R = Revised, D = Deleted, O = Overflow, C = Customer Originated Change

27-EFFECTIVE PAGES

Page 26

May 20/2011 D633N165

BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details

Subject/Page Date COC Subject/Page Date COC Subject/Page Date COC

CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

FLIGHT CONTROLS - DESCRIPTION AND

OPERATION

27-00-00 1 TBC ALL

FLIGHT CONTROL CABLES - DESCRIPTION

AND OPERATION

27-00-01 1 TBC ALL

FLIGHT CONTROL CABLES -

MAINTENANCE PRACTICES

27-00-01 201 TBC ALL

Flight Control Cables Data

TASK 27-00-01-992-001

201 TBC ALL

FLIGHT CONTROL SHEAR RIVETS -

MAINTENANCE PRACTICES

27-00-02 201 TBC ALL

Flight Control Shear Rivets References

TASK 27-00-02-302-003

201 TBC ALL

FLIGHT CONTROL LATERAL TRIM

CORRECTION - ADJUSTMENT TEST

27-01-00 501 TBC ALL

Excessive Lateral Trim Adjustment

TASK 27-01-00-825-001

502 TBC ALL

FLIGHT CONTROLS SURFACE -

INSPECTION/CHECK

27-02-00 601 TBC ALL

Elevator Freeplay - Check

TASK 27-02-00-736-001

601 TBC ALL

Rudder Freeplay - Check

TASK 27-02-00-736-025

610 TBC ALL

Aileron Freeplay - Check

TASK 27-02-00-736-053

615 TBC ALL

Spoiler Freeplay - Check

TASK 27-02-00-736-065

618 TBC ALL

FLIGHT CONTROL SYSTEM ELECTRONICS

UNIT (CSEU) - DESCRIPTION AND

OPERATION

27-09-00 1 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 1

May 20/2011 D633N165

BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details

CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

FLIGHT CONTROL SYSTEM ELECTRONICS

UNIT (CSEU) - MAINTENANCE

PRACTICES

27-09-00 201 TBC ALL

Remove the Module

TASK 27-09-00-002-001

201 TBC ALL

Install the Module

TASK 27-09-00-402-007

206 TBC ALL

CSEU Modules Installation Test

TASK 27-09-00-712-014

208 TBC ALL

AILERON AND AILERON TRIM CONTROL

SYSTEM - DESCRIPTION AND

OPERATION

27-11-00 1 TBC ALL

AILERON AND AILERON TRIM CONTROL

SYSTEM - ADJUSTMENT/TEST

27-11-00 501 TBC ALL

Operational Test - Aileron and Aileron

Trim-Control System

TASK 27-11-00-715-001

501 TBC ALL

Adjust the Aileron and Aileron Trim

Control System

TASK 27-11-00-825-030

508 TBC ALL

System Test - Aileron and Aileron Trim

Control System

TASK 27-11-00-735-091

517 TBC ALL

System Test - Control Wheel Damper

TASK 27-11-00-725-271

526 TBC ALL POST SB

757-27A0146

Aileron Bus Force Limiter and the

Aileron Control Override Mechanism -

Test

TASK 27-11-00-715-183

529 TBC ALL

Single Hydraulic System Aileron

Control - Test

TASK 27-11-00-715-193

530 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 2

Feb 20/2010 D633N165

BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details

CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

LATERAL CONTROL WHEEL - REMOVAL/

INSTALLATION

27-11-02 401 TBC ALL

Remove the Aileron Control Wheel

TASK 27-11-02-024-001

401 TBC ALL

Install the Aileron Control Wheel

TASK 27-11-02-424-010

405 TBC ALL

LATERAL CONTROL WHEEL INSPECTION/

CHECK

27-11-02 601 TBC ALL

Lateral Control Wheel Freeplay - Check

TASK 27-11-02-226-011

601 TBC ALL

AILERON CONTROL DRUM ASSEMBLY -

MAINTENANCE PRACTICES

27-11-03 201 TBC ALL

Remove Aileron Control Drum and

Components

TASK 27-11-03-022-005

201 TBC ALL

Install Aileron Control Drum and

Components

TASK 27-11-03-422-018

212 TBC ALL

Aileron Control Drums and Bus Force

Limiter - Test

TASK 27-11-03-722-072

217 TBC ALL

LATERAL CONTROL FEEL, CENTERING,

AND TRIM MECHANISM - MAINTENANCE

PRACTICES

27-11-14 201 TBC ALL

Feel, Centering, and Trim Mechanism

and Its Components - Removal

TASK 27-11-14-022-008

201 TBC ALL

Feel, Centering, and Trim Mechanism

and Its Components - Installation

TASK 27-11-14-422-022

207 TBC ALL

Feel, Centering, and Trim Mechanism -

Adjustment/Test

TASK 27-11-14-822-070

211 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 3

Feb 20/2010 D633N165

BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details

CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

LATERAL CONTROL OVERRIDE

MECHANISM - REMOVAL/INSTALLATION

27-11-16 401 TBC ALL

Lateral Control Override Mechanism -

Removal

TASK 27-11-16-024-001

401 TBC ALL

Lateral Control Override Mechanism -

Installation

TASK 27-11-16-424-013

406 TBC ALL

AILERON QUADRANT AND OVERRIDE

MECHANISM - REMOVAL/INSTALLATION

27-11-17 401 TBC ALL

Remove the Aileron Quadrant and

Override Mechanism

TASK 27-11-17-024-001

401 TBC ALL

Install Aileron Quadrant and Override

Mechanism

TASK 27-11-17-424-011

404 TBC ALL

AILERON QUADRANT AND OVERRIDE

MECHANISM INSPECTION/CHECK

27-11-17 601 TBC ALL

Aileron Quadrant and Override

Mechanism Wear Limits

TASK 27-11-17-206-001

601 TBC ALL

AILERON POWER CONTROL ACTUATOR

(PCA) AND REACTION LINK -

MAINTENANCE PRACTICES

27-11-20 201 TBC ALL

Aileron PCA and Reaction Link -

Removal

TASK 27-11-20-022-006

201 TBC ALL

Aileron PCA and Reaction Link -

Installation

TASK 27-11-20-422-018

209 TBC ALL

Aileron PCA Filter - Removal

TASK 27-11-20-022-046

214 TBC ALL

Aileron PCA Filter - Installation

TASK 27-11-20-422-065

215 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 4

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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details

CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

AILERON POWER CONTROL ACTUATOR

(PCA) AND REACTION LINKINSPECTION/CHECK

27-11-20 601 TBC ALL

Examine The Aileron PCA For Wear

TASK 27-11-20-206-001

601 TBC ALL

Examine The Aileron-PCA ReactionLink Assembly For Wear

TASK 27-11-20-206-003

607 TBC ALL

AILERON - REMOVAL/INSTALLATION 27-11-21 401 TBC ALL

Remove the Aileron

TASK 27-11-21-024-001

401 TBC ALL

Install the Aileron

TASK 27-11-21-424-013

405 TBC ALL

AILERON - INSPECTION/CHECK 27-11-21 601 TBC ALL

Examine the Aileron for wear

TASK 27-11-21-206-001

601 TBC ALL

AILERON POSITION INDICATING SYSTEM -

DESCRIPTION AND OPERATION

27-18-00 1 TBC ALL

AILERON POSITION INDICATING SYSTEM -

ADJUSTMENT/TEST

27-18-00 501 TBC ALL

Operational Test - Aileron Position

Indicating System

TASK 27-18-00-715-001

501 TBC ALL

Adjustment - Aileron Position Indicating

System

TASK 27-18-00-825-064

508 TBC ALL

AILERON POSITION TRANSMITTER -

REMOVAL/INSTALLATION

27-18-01 401 TBC ALL

Remove Aileron Position Transmitter

TASK 27-18-01-024-003

401 TBC ALL

Install Aileron Position Transmitter

TASK 27-18-01-424-014

404 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 5

Feb 20/2010 D633N165

BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details

CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

RUDDER AND RUDDER TRIM CONTROL

SYSTEM - DESCRIPTION AND

OPERATION

27-21-00 1 1 TBC ALL

RUDDER AND RUDDER TRIM CONTROL

SYSTEM - ADJUSTMENT/TEST

27-21-00 1 501 TBC ALL

Operational Test - Rudder and Rudder

Trim Control System

TASK 27-21-00-715-001-001

1 501 TBC ALL

Adjustment - Rudder and Rudder Trim

Control System

TASK 27-21-00-825-055-001

1 526 TBC ALL

System Test - Rudder and Rudder Trim

Control

TASK 27-21-00-735-169-001

1 550 TBC ALL

RUDDER PEDALS - REMOVAL/

INSTALLATION

27-21-02 401 TBC ALL

Remove Rudder Pedal Assembly

TASK 27-21-02-024-003

401 TBC ALL

Install Rudder Pedal Assembly

TASK 27-21-02-424-013

407 TBC ALL

RUDDER PEDAL ADJUSTMENT CRANK -

REMOVAL/INSTALLATION

27-21-03 401 TBC ALL

Remove Rudder Pedal Adjustment

Crank

TASK 27-21-03-024-006

401 TBC ALL

Install Rudder Pedal Adjustment Crank

TASK 27-21-03-424-015

405 TBC ALL

RUDDER JACKSHAFT AND FORWARD

QUADRANT - REMOVAL/INSTALLATION

27-21-05 401 TBC ALL

Remove Rudder Jackshaft and Forward

Quadrant

TASK 27-21-05-024-052

401 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 6

May 20/2010 D633N165

BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details

CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Install Rudder Jackshaft and Forward

Quadrant

TASK 27-21-05-424-028

410 TBC ALL

AFT QUADRANT, FEEL, CENTERING AND

TRIM MECHANISM - MAINTENANCE

PRACTICES

27-21-06 201 TBC ALL

Aft Quadrant and Components -

Removal

TASK 27-21-06-022-001

201 TBC ALL

Aft Quadrant and Components -

Installation

TASK 27-21-06-422-017

210 TBC ALL

RUDDER RATIO CHANGER MECHANISM -

MAINTENANCE PRACTICES

27-21-12 201 TBC ALL

Remove Rudder Ratio-Changer

Mechanism and Components

TASK 27-21-12-022-011

201 TBC ALL

Install Rudder Ratio-Changer

Mechanism

TASK 27-21-12-422-032

210 TBC ALL

Remove the Rudder Ratio-Changer

Linear Variable Differential Transducer

(LVDT)

TASK 27-21-12-022-088

216 TBC ALL

Install the Rudder Ratio-Changer LVDT

TASK 27-21-12-422-079

218 TBC ALL

Remove the Support Clevis of the

Rudder Ratio Changer

TASK 27-21-12-002-093

220 TBC ALL

Install the Rudder Ratio Actuator

Changer Support Clevis

TASK 27-21-12-402-099

221 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 7

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

RUDDER RATIO CHANGER ACTUATOR

(RRCA) - MAINTENANCE PRACTICES

27-21-13 201 TBC ALL

Remove the Rudder Ratio Changer

Actuator (RRCA) or its Parts

TASK 27-21-13-002-001

201 TBC ALL

Install the Rudder Ratio Changer

Actuator (RRCA) or its Parts

TASK 27-21-13-402-032

208 TBC ALL

YAW DAMPER SUMMING LEVER -

REMOVAL/INSTALLATION

27-21-17 401 TBC ALL

Yaw Damper Summing Lever -

Removal

TASK 27-21-17-024-005

401 TBC ALL

Yaw Damper Summing Lever -

Installation

TASK 27-21-17-414-014

408 TBC ALL

YAW DAMPER SUMMING LEVER -

INSPECTION/CHECK

27-21-17 601 TBC ALL

Yaw Damper Shear Pin (or Rivets) -

Check

TASK 27-21-17-726-001

601 TBC ALL

Yaw Damper Summing Lever -

Inspection

TASK 27-21-17-736-011

604 TBC ALL

RUDDER THERMAL COMPENSATING

LINKAGE - REMOVAL/INSTALLATION

27-21-19 401 TBC ALL

Rudder Thermal Compensating Linkage

and Its Components - Removal

TASK 27-21-19-024-001

401 TBC ALL

Rudder Thermal Compensating Linkage

and Its Components - Installation

TASK 27-21-19-424-020

410 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 8

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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details

CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

RUDDER POWER CONTROL ACTUATOR

(PCA) AND COMPONENTS -

MAINTENANCE PRACTICES

27-21-20 201 TBC ALL

Rudder PCA and Reaction Link -

Removal

TASK 27-21-20-022-001

201 TBC ALL

Rudder PCA and Reaction Link -

Installation

TASK 27-21-20-422-025

210 TBC ALL

RUDDER - REMOVAL/INSTALLATION 27-21-21 401 TBC ALL

Rudder - Removal

TASK 27-21-21-024-039

401 TBC ALL

Rudder - Installation

TASK 27-21-21-424-010

409 TBC ALL

RUDDER INSPECTION/CHECK 27-21-21 601 TBC ALL

Rudder - Wear Limits

TASK 27-21-21-206-001

601 TBC ALL

AILERON AND RUDDER TRIM CONTROL

MODULE - MAINTENANCE PRACTICES

27-21-23 201 TBC ALL

Aileron and Rudder Trim Control

Module - Removal

TASK 27-21-23-022-001

201 TBC ALL

Aileron and Rudder Trim Control

Module - Installation

TASK 27-21-23-422-007

203 TBC ALL

Rudder Trim Indicator - Removal

TASK 27-21-23-002-030

204 TBC ALL

Rudder Trim Indicator - Installation

TASK 27-21-23-402-037

205 TBC ALL

Clean the Rudder Trim Switch

TASK 27-21-23-102-017

207 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 9

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

RUDDER AND ELEVATOR HYDRAULIC

SYSTEMS - DESCRIPTION AND

OPERATION

27-23-00 1 TBC ALL

RUDDER AND ELEVATOR HYDRAULIC

SYSTEMS - ADJUSTMENT/TEST

27-23-00 501 TBC ALL

Rudder/Elevator Shutoff Valves -

System Test

TASK 27-23-00-735-001

501 TBC ALL

Rudder and Elevator PCA Monitoring -

System Test

TASK 27-23-00-735-022

508 TBC ALL

RUDDER AND ELEVATOR HYDRAULIC

SHUTOFF VALVES - MAINTENANCE

PRACTICES

27-23-01 201 TBC ALL

Rudder and Elevator Hydraulic Shutoff

Valves - Removal

TASK 27-23-01-022-003

201 TBC ALL

Rudder and Elevator Hydraulic Shutoff

Valves - Installation

TASK 27-23-01-422-013

204 TBC ALL

RUDDER AND ELEVATOR PCA MONITOR

MODULE - REMOVAL/INSTALLATION

27-23-02 401 TBC ALL

Rudder/Elevator PCA Monitor Module -

Removal

TASK 27-23-02-024-005

401 TBC ALL

Rudder/Elevator PCA Monitor Module -

Installation

TASK 27-23-02-424-012

404 TBC ALL

RUDDER AND ELEVATOR HYDRAULIC FUSE

- MAINTENANCE PRACTICES

27-23-51 201 TBC ALL

Remove the Rudder Hydraulic Fuse

TASK 27-23-51-022-001

201 TBC ALL

Install the Rudder Hydraulic Fuse

TASK 27-23-51-402-006

202 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 10

Feb 20/2010 D633N165

BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details

CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Elevator Hydraulic Fuses - Removal

TASK 27-23-51-002-022

204 TBC ALL

Elevator Hydraulic Fuses - Installation

TASK 27-23-51-402-026

205 TBC ALL

RUDDER POSITION INDICATING SYSTEM -

DESCRIPTION AND OPERATION

27-28-00 1 TBC ALL

RUDDER POSITION INDICATING SYSTEM -

ADJUSTMENT/TEST

27-28-00 501 TBC ALL

Rudder Position Indicating System -

Operational Test

TASK 27-28-00-715-001

501 TBC ALL

Rudder Position Indicating System -

Adjustment

TASK 27-28-00-825-011

506 TBC ALL

RUDDER POSITION TRANSMITTER -

MAINTENANCE PRACTICES

27-28-01 201 TBC ALL

Rudder Position Transmitter - Removal

TASK 27-28-01-022-006

201 TBC ALL

Rudder Position Transmitter -

Installation

TASK 27-28-01-422-016

205 TBC ALL

ELEVATOR CONTROL SYSTEM -

DESCRIPTION AND OPERATION

27-31-00 1 TBC ALL

ELEVATOR CONTROL SYSTEM -

ADJUSTMENT/TEST

27-31-00 501 TBC ALL

Elevator Control System - Operational

Test

TASK 27-31-00-715-331

501 TBC ALL

Elevator Control System - Adjustment

TASK 27-31-00-825-031

526 TBC ALL

Elevator Control System - System Test

TASK 27-31-00-725-090

554 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 11

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Elevator Column and Quadrant

Override Test

TASK 27-31-00-735-199

592 TBC ALL

Elevator Pressure Bypass Valve Test

TASK 27-31-00-735-201

596 TBC ALL

Single Hydraulic Source - Test

TASK 27-31-00-735-250

598.5 TBC ALL

ELEVATOR - REMOVAL/INSTALLATION 27-31-01 401 TBC ALL

Remove the Elevator

TASK 27-31-01-024-001

401 TBC ALL

Install the Elevator

TASK 27-31-01-424-028

410 TBC ALL

ELEVATOR - INSPECTION/CHECK 27-31-01 601 TBC ALL

Elevator Hinge Wear Limits

TASK 27-31-01-226-001

601 TBC ALL

ELEVATOR INDEX PLATE - REMOVAL/

INSTALLATION

27-31-02 401 TBC ALL

Remove the Index Plate

TASK 27-31-02-024-001

401 TBC ALL

Install the Index Plate

TASK 27-31-02-424-014

406 TBC ALL

ASYMMETRY LIMITER ACTUATOR -

REMOVAL/INSTALLATION

27-31-03 401 TBC ALL

Remove the Asymmetry Limiter

Actuator

TASK 27-31-03-024-001

401 TBC ALL

Install the Asymmetry Limiter Actuator

TASK 27-31-03-424-016

406 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 12

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BOEING PROPRIETARY - Copyright#Unpublished Work - See title page for details

CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

ELEVATOR POWER CONTROL ACTUATOR

(PCA)/REACTION LINK/IDLER LINK -

REMOVAL/INSTALLATION

27-31-05 401 TBC ALL

Remove the Power Control Actuator

(PCA)

TASK 27-31-05-024-001

401 TBC ALL

Install the Power Control Actuator (PCA)

TASK 27-31-05-424-067

410 TBC ALL

Remove the Elevator Reaction Link

TASK 27-31-05-024-055

413 TBC ALL

Install the Elevator Reaction Link

TASK 27-31-05-424-068

417 TBC ALL

Remove the Elevator Idler Link

TASK 27-31-05-024-099

421 TBC ALL

Install the Elevator Idler Link

TASK 27-31-05-424-117

424 TBC ALL

ELEVATOR POWER CONTROL ACTUATOR/

REACTION LINK - INSPECTION/CHECK

27-31-05 601 TBC ALL

PCA/Elevator Wear Limits

TASK 27-31-05-226-001

601 TBC ALL

PCA Input Linkage Wear Limits

TASK 27-31-05-226-002

605 TBC ALL

ELEVATOR POWER CONTROL ACTUATOR

(PCA) INPUT LINKAGE - REMOVAL/

INSTALLATION

27-31-06 401 TBC ALL

Remove the PCA Input Linkage

TASK 27-31-06-024-001

401 TBC ALL

Install the PCA Input Linkage

TASK 27-31-06-424-024

408 TBC ALL

CONTROL COLUMN - REMOVAL/

INSTALLATION

27-31-10 401 TBC ALL

Remove the Control Column

TASK 27-31-10-024-001

401 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 13

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Install the Control Column

TASK 27-31-10-424-019

406 TBC ALL

CONTROL COLUMN - INSPECTION/CHECK 27-31-10 601 TBC ALL

Control Column Backlash Check

TASK 27-31-10-716-015

601 TBC ALL

CONTROL COLUMN TORQUE TUBE

BEARING - REMOVAL/INSTALLATION

27-31-11 401 TBC ALL

Remove the Control Column Torque

Tube Bearings

TASK 27-31-11-004-001

401 TBC ALL

Install the Control Column Torque Tube

Bearings

TASK 27-31-11-404-016

402 TBC ALL

ELEVATOR FORWARD QUADRANT/

TENSION REGULATOR - REMOVAL/

INSTALLATION

27-31-12 401 TBC ALL

Remove the Quadrant/Tension

Regulator

TASK 27-31-12-024-001

401 TBC ALL

Install the Quadrant/Tension Regulator

TASK 27-31-12-424-021

408 TBC ALL

ELEVATOR PRESSURE REDUCER/BYPASS

VALVE - REMOVAL/INSTALLATION

27-31-13 401 TBC ALL

Remove the Pressure Reducer Valve

and the Bypass Valve

TASK 27-31-13-024-031

401 TBC ALL

Install the Pressure Reducer Valve and

the Bypass Valve

TASK 27-31-13-424-017

409 TBC ALL

ELEVATOR AFT QUADRANTS - REMOVAL/

INSTALLATION

27-31-15 401 TBC ALL

Remove the Aft Quadrants

TASK 27-31-15-024-001

401 TBC ALL

757

AIRCRAFT MAINTENANCE MANUAL

27-CONTENTS

Page 14

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Install the Aft Quadrant

TASK 27-31-15-424-027

408 TBC ALL

ELEVATOR CONTROL AFT MECHANISM

TORQUE BOX - REMOVAL/

INSTALLATION

27-31-16 401 TBC ALL

Remove the Torque Box

TASK 27-31-16-024-001

401 TBC ALL

Install the Torque Box

TASK 27-31-16-424-062

409 TBC ALL

ELEVATOR FEEL UNIT - MAINTENANCE

PRACTICE

27-31-17 201 TBC ALL

Remove the Feel Unit

TASK 27-31-17-022-001

201 TBC ALL

Install the Feel Unit

TASK 27-31-17-422-020

211 TBC ALL

Remove the Feel Unit Roller Bearing

TASK 27-31-17-022-036

213 TBC ALL

Install the Feel Unit Roller Bearing

TASK 27-31-17-402-053

216 TBC ALL

ELEVATOR FEEL ACTUATOR - REMOVAL/

INSTALLATION

27-31-18 401 TBC ALL

Remove the Feel Actuator

TASK 27-31-18-024-001

401 TBC ALL

Install the Feel Actuator

TASK 27-31-18-424-011

407 TBC ALL

ELEVATOR FEEL COMPUTER - REMOVAL/

INSTALLATION

27-31-19 401 TBC ALL

Remove the Feel Computer

TASK 27-31-19-024-001

401 TBC ALL

Install the Feel Computer

TASK 27-31-19-424-015

406 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

ELEVATOR NEUTRAL SHIFT AND

OVERRIDE MECHANISM - REMOVAL/

INSTALLATION

27-31-21 401 TBC ALL

Remove the Neutral Shift and Override

Mechanism

TASK 27-31-21-024-001

401 TBC ALL

Install the Neutral Shift and Override

Mechanism

TASK 27-31-21-424-018

407 TBC ALL

ELEVATOR NEUTRAL SHIFT AND

OVERRIDE MECHANISM - INSPECTION/

CHECK

27-31-21 601 TBC ALL

Wear Limits for the Elevator Neutral

Shift and Override Mechanism

TASK 27-31-21-226-001

601 TBC ALL

CONTROL COLUMN OVERRIDE ASSEMBLY

- ADJUSTMENT/TEST

27-31-23 501 TBC ALL

Adjust the Override Assembly

TASK 27-31-23-825-001

501 TBC ALL

STALL WARNING SYSTEM - DESCRIPTION

AND OPERATION

27-32-00 4 1 TBC ALL

STALL WARNING SYSTEM - ADJUSTMENT/

TEST

27-32-00 5 501 TBC ALL

Operational Test - Stall Warning System

TASK 27-32-00-715-001-005

5 501 TBC ALL

System Test - Stall Warning System

TASK 27-32-00-735-016-005

5 511 TBC ALL

STALL WARNING MODULE - REMOVAL/

INSTALLATION

27-32-01 401 TBC ALL

Remove the Stall Warning Module

TASK 27-32-01-024-001

401 TBC ALL

Install the Stall Warning Module

TASK 27-32-01-424-005

404 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

WARNING ELECTRONIC UNIT (WEU) BITE

MODULE - REMOVAL/INSTALLATION

27-32-02 401 TBC ALL

Remove WEU BITE Module

TASK 27-32-02-024-001

401 TBC ALL

Install WEU BITE Module

TASK 27-32-02-424-008

404 TBC ALL

CONTROL COLUMN SHAKER - REMOVAL/

INSTALLATION

27-32-05 401 TBC ALL

Remove Control Column Shaker

TASK 27-32-05-024-001

401 TBC ALL

Install Control Column Shaker

TASK 27-32-05-424-013

404 TBC ALL

Test Control Column Shaker

TASK 27-32-05-714-006

404 TBC ALL

ELEVATOR POSITION INDICATING SYSTEM

- DESCRIPTION AND OPERATION

27-38-00 1 TBC ALL

ELEVATOR POSITION INDICATING SYSTEM

- ADJUSTMENT/TEST

27-38-00 501 TBC ALL

Operational Test - Elevator Position

Indicating System

TASK 27-38-00-715-002

501 TBC ALL

Adjustment - Elevator Position

Indicating System

TASK 27-38-00-825-009

507 TBC ALL

ELEVATOR POSITION TRANSMITTER -

REMOVAL/INSTALLATION

27-38-02 401 TBC ALL

Remove the Position Transmitters

TASK 27-38-02-024-001

401 TBC ALL

Install the Position Transmitter

TASK 27-38-02-424-018

408 TBC ALL

HORIZONTAL STABILIZER TRIM CONTROL

SYSTEM - DESCRIPTION AND

OPERATION

27-41-00 1 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

HORIZONTAL STABILIZER TRIM CONTROL

SYSTEM - ADJUSTMENT/TEST

27-41-00 501 TBC ALL

Horizontal Stabilizer Trim Control

System - Operational Test

TASK 27-41-00-715-001

501 TBC ALL

Electrical Travel Limits and Stabilizer

Trim Cutoff Switch Tests

TASK 27-41-00-735-B52

517 TBC ALL

Horizontal Stabilizer Trim Control

System - Adjustment

TASK 27-41-00-825-467

525 TBC ALL

Horizontal Stabilizer Trim Control

System - System Test

TASK 27-41-00-735-468

529 TBC ALL

Stabilizer Trim Secondary Brake Test

TASK 27-41-00-715-643

550 TBC ALL

Stabilizer Trim Shutoff Switches Test

TASK 27-41-00-715-644

551 TBC ALL

Stabilizer Trim Override Capability with

Split Control Column Commands Test

TASK 27-41-00-715-647

553 TBC ALL

Electrical Travel Limits and Stabilizer

Trim Cutoff Switch Tests

TASK 27-41-00-735-648

555 TBC ALL

Horizontal Stabilizer Alternate Electric

Trim System - Operational Check

TASK 27-41-00-715-679

564 TBC ALL

STABILIZER TRIM CONTROL WHEEL

SWITCH - REMOVAL/INSTALLATION

27-41-01 401 TBC ALL

Remove the Control Wheel Switch

TASK 27-41-01-024-001

401 TBC ALL

Install the Control Wheel Switch

TASK 27-41-01-424-011

404 TBC ALL

757

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

ALTERNATE STABILIZER TRIM SWITCH -

REMOVAL/INSTALLATION

27-41-03 401 TBC ALL

Remove the Alternate Stabilizer Trim

Switch

TASK 27-41-03-024-001

401 TBC ALL

Install the Alternate Stabilizer Trim

Switch

TASK 27-41-03-424-011

404 TBC ALL

STABILIZER TRIM CONTROL MODULE -

MAINTENANCE PRACTICES

27-41-05 201 TBC ALL

Remove the Stabilizer Trim Control

Modules (STCMs) and the Solenoid

Valves

TASK 27-41-05-022-001

201 TBC ALL

Install the Stabilizer Trim Control

Modules (STCMs) and the Solenoid

Valves

TASK 27-41-05-422-023

206 TBC ALL

STABILIZER TRIM CONTROL MODULE

BRAKE PRESSURE SWITCH - REMOVAL/

INSTALLATION

27-41-07 401 TBC ALL

Remove the Brake Pressure Switch

TASK 27-41-07-024-001

401 TBC ALL

Install the Brake Pressure Switch

TASK 27-41-07-424-021

405 TBC ALL

STABILIZER TRIM BALLSCREW ACTUATOR

- REMOVAL/INSTALLATION

27-41-10 401 TBC ALL

Remove the Stabilizer Ballscrew

Actuator

TASK 27-41-10-024-001

401 TBC ALL

Install the Stabilizer Ballscrew Actuator

TASK 27-41-10-424-021

410 TBC ALL

757

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

STABILIZER TRIM BALLSCREW FREEPLAY 27-41-10 601 TBC ALL

Check for Stabilizer Ballscrew to

Ballnut Freeplay

TASK 27-41-10-226-052

601 TBC ALL

Stabilizer Ballscrew Assembly Detailed

Visual Inspection

TASK 27-41-10-226-069

607 TBC ALL

STABILIZER TRIM DRIVE HYDRAULIC

MOTOR - REMOVAL/INSTALLATION

27-41-11 401 TBC ALL

Remove the Hydraulic Motor

TASK 27-41-11-024-001

401 TBC ALL

Install the Hydraulic Motor

TASK 27-41-11-424-012

404 TBC ALL

STABILIZER TRIM SECONDARY BRAKE -

REMOVAL/INSTALLATION

27-41-13 401 TBC ALL

Remove the Secondary Brake

TASK 27-41-13-024-001

401 TBC ALL

Install the Secondary Brake

TASK 27-41-13-424-012

404 TBC ALL

STABILIZER TRIM UPPER AND LOWER

GIMBAL - INSPECTION/CHECK

27-41-14 601 TBC ALL

Inspect the Stabilizer Trim Upper and

Lower Gimbals

TASK 27-41-14-216-001

601 TBC ALL

Stabilizer Trim Upper and Lower

Gimbal Wear Limits

TASK 27-41-14-226-015

611 TBC ALL

HORIZONTAL STABILIZER ALIGNMENT

TABS - REMOVAL/INSTALLATION

27-41-17 401 TBC ALL

Install the Stabilizer Alignment Tabs

TASK 27-41-17-424-001

401 TBC ALL

757

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

STABILIZER TRIM POSITION INDICATING

SYSTEM - DESCRIPTION AND

OPERATION

27-48-00 1 TBC ALL

STABILIZER TRIM POSITION INDICATING

SYSTEM - ADJUSTMENT/TEST

27-48-00 501 TBC ALL

Stabilizer Trim Position Indicating

System - Operational Test

TASK 27-48-00-715-001

501 TBC ALL

Stabilizer Takeoff Warning System -

Operational Test

TASK 27-48-00-715-143

507 TBC ALL

Stabilizer Trim Position Indicating

System - Adjustment

TASK 27-48-00-825-040

509 TBC ALL

Stabilizer Trim Position Indicating

System - System Test

TASK 27-48-00-735-074

512 TBC ALL

STABILIZER TRIM LIMIT SWITCH AND

POSITION TRANSMITTER MODULE -

REMOVAL/INSTALLATION

27-48-01 401 TBC ALL

Remove the Limit Switch and Position

Transmitter Module (LSTM)

TASK 27-48-01-024-001

401 TBC ALL

Install the Limit Switch and Position

Transmitter Module (LSTM)

TASK 27-48-01-424-011

404 TBC ALL

STABILIZER POSITION MODULE -

REMOVAL/INSTALLATION

27-48-03 401 TBC ALL

Remove the Stabilizer Position Module

(SPM)

TASK 27-48-03-024-001

401 TBC ALL

Install the Stabilizer Position Module

(SPM)

TASK 27-48-03-424-009

404 TBC ALL

757

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

STABILIZER TRIM POSITION INDICATOR -

REMOVAL/INSTALLATION

27-48-06 401 TBC ALL

Remove the Position Indicator

TASK 27-48-06-024-001

401 TBC ALL

Install the Position Indicator

TASK 27-48-06-424-009

404 TBC ALL

TRAILING EDGE FLAP SYSTEM -

DESCRIPTION AND OPERATION

27-51-00 1 TBC ALL

TRAILING EDGE FLAP SYSTEM -

MAINTENANCE PRACTICES

27-51-00 201 TBC ALL

Deactivation of the Flap Drive System

TASK 27-51-00-042-001

201 TBC ALL

Operation of the TE Flap System

TASK 27-51-00-862-004

207 TBC ALL

TRAILING EDGE FLAP SYSTEM -

ADJUSTMENT/TEST

27-51-00 501 TBC ALL

Operational Test of the TE Flap System

TASK 27-51-00-715-001

501 TBC ALL

Adjustment of the TE Flap System

TASK 27-51-00-825-007

521 TBC ALL

TE Flap System - System Test

TASK 27-51-00-735-036

526 TBC ALL

Operational Test of the Flap/Slat

Alternate Drive System

TASK 27-51-00-715-167

551 TBC ALL

TE Flap Load Relief - System Test

TASK 27-51-00-735-161

553 TBC ALL

INBOARD TRAILING EDGE FLAP DRIVE

SYSTEM - INSPECTION/CHECK

27-51-00 601 TBC ALL

Inboard TE Flap Angle Tee Gearbox

Inspection

TASK 27-51-00-026-001

601 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Inboard TE Flap Outboard Tee Gearbox

Inspection

TASK 27-51-00-026-013

613 TBC ALL

Inboard TE Flap Outbd Angle Gearbox

Inspection

TASK 27-51-00-026-027

616 TBC ALL

TE Flap Drive Shaft Inspection

TASK 27-51-00-026-047

619 TBC ALL

FLAP/SLAT ELECTRONIC UNIT -

MAINTENANCE PRACTICES

27-51-01 201 TBC ALL

Remove Flap/Slat Electronic Unit

TASK 27-51-01-022-006

201 TBC ALL

Install Flap/Slat Electronic Unit

TASK 27-51-01-422-011

207 TBC ALL

Test the FSEU

TASK 27-51-01-722-005

208 TBC ALL

INBOARD TRAILING EDGE FLAP -

REMOVAL/INSTALLATION

27-51-02 401 TBC ALL

Remove the Inboard TE Flap

TASK 27-51-02-024-001

401 TBC ALL

Install the Inboard TE Flap

TASK 27-51-02-424-021

417 TBC ALL

INBOARD TRAILING EDGE FLAP -

ADJUSTMENT/TEST

27-51-02 501 TBC ALL

Adjustment for the Inboard Trailing

Edge Flap

TASK 27-51-02-825-001

501 TBC ALL

Inboard Trailing Edge Flap Test

TASK 27-51-02-705-035

527 TBC ALL

INBOARD TRAILING EDGE FLAPS -

INSPECTION/CHECK

27-51-02 601 TBC ALL

Wear Limits for Inboard Flap Linkage

TASK 27-51-02-226-001

601 TBC ALL

757

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Wear Limits for the Aft Flap Tracks of

the Inboard Flap

TASK 27-51-02-226-002

614 TBC ALL

INBOARD TRAILING EDGE FLAP TRACK -

REMOVAL/INSTALLATION

27-51-03 401 TBC ALL

Remove the Inboard and Outboard Flap

Tracks of the Inboard TE Flaps

TASK 27-51-03-024-001

401 TBC ALL

Install the Inboard and Outboard Tracks

for the Inboard Flap

TASK 27-51-03-424-020

408 TBC ALL

TE Flap Track Fuse Pin - Removal

TASK 27-51-03-000-801

411 TBC ALL

TE Flap Track Fuse Pin - Installation

TASK 27-51-03-400-801

414 TBC ALL

INBOARD TRAILING EDGE FLAP CARRIAGE

- REMOVAL/INSTALLATION

27-51-05 401 TBC ALL

Remove the Carriages for the Inboard

Trailing Edge (TE) Flap

TASK 27-51-05-024-029

401 TBC ALL

Install the Carriages for the Inboard TE

Flap

TASK 27-51-05-424-026

405 TBC ALL

INBOARD TRAILING EDGE FLAP

TRANSMISSIONS - REMOVAL/

INSTALLATION

27-51-06 401 TBC ALL

Remove the Inboard and Outboard

Transmissions for the TE Flap

TASK 27-51-06-024-001

401 TBC ALL

Install Inboard and Outboard

Transmissions for the TE Flap

TASK 27-51-06-424-021

419 TBC ALL

757

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

INBOARD TRAILING EDGE FLAP DRIVE

INBOARD TEE GEARBOX - REMOVAL/

INSTALLATION

27-51-07 401 TBC ALL

Remove the Inboard Tee Gearbox for

the Inboard TE Flap

TASK 27-51-07-024-024

401 TBC ALL

Install the Inboard Tee Gearbox for the

Inboard TE Flap

TASK 27-51-07-424-027

407 TBC ALL

INBOARD TRAILING EDGE FLAP DRIVE

OUTBOARD TEE GEARBOX - REMOVAL/

INSTALLATION

27-51-08 401 TBC ALL

Remove the Outboard Tee Gearbox for

the Inboard TE Flap

TASK 27-51-08-024-001

401 TBC ALL

Install the Outboard Tee Gearbox for

the Inboard TE Flap

TASK 27-51-08-424-004

408 TBC ALL

INBOARD TRAILING EDGE FLAP DRIVE

INBOARD ANGLE GEARBOX - REMOVAL/

INSTALLATION

27-51-09 401 TBC ALL

Remove the Inboard Angle Gearbox

TASK 27-51-09-024-005

401 TBC ALL

Install the Inboard Angle Gearbox

TASK 27-51-09-424-013

407 TBC ALL

INBOARD TRAILING EDGE FLAP DRIVE

OUTBOARD ANGLE GEARBOX -

REMOVAL/INSTALLATION

27-51-10 401 TBC ALL

Remove the Outboard Angle Gearbox

from the Inboard TE Flap

TASK 27-51-10-024-028

401 TBC ALL

Install the Outboard Angle Gearbox for

the Inboard TE Flap

TASK 27-51-10-424-031

409 TBC ALL

757

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

INBOARD TRAILING EDGE FLAP

BALLSCREW - REMOVAL/INSTALLATION

27-51-11 401 TBC ALL

Remove the Ballscrew for the Inboard

TE Flap

TASK 27-51-11-024-001

401 TBC ALL

Install the Ballscrew for the Inboard TE

Flap

TASK 27-51-11-424-020

410 TBC ALL

INBOARD TRAILING EDGE FLAP

BALLSCREW - INSPECTION/CHECK

27-51-11 601 TBC ALL

Inboard Trailing Edge Flap Ballscrew

Backlash Check

TASK 27-51-11-226-001

601 TBC ALL

Inboard Trailing Edge Flap Ballscrew

Nut Return Tube Check

TASK 27-51-11-226-024

608 TBC ALL

Inboard Trailing Edge Flap Ballscrew

Inspection

TASK 27-51-11-226-049

613 TBC ALL

INBOARD TRAILING EDGE FLAP-AFT FLAP -

REMOVAL/INSTALLATION

27-51-12 401 TBC ALL

Remove the Aft Flap for the Inboard TE

Flap

TASK 27-51-12-024-001

401 TBC ALL

Install the Aft Flap for the Inboard TE

Flap

TASK 27-51-12-424-006

409 TBC ALL

INBOARD TRAILING EDGE FLAP-AFT FLAP -

ADJUSTMENT/TEST

27-51-12 501 TBC ALL

Inboard Aft Flap Adjustment

TASK 27-51-12-825-001

501 TBC ALL

Operational Test for the Aft Flap

TASK 27-51-12-715-022

512 TBC ALL

757

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

INBOARD TRAILING EDGE FLAP AFT FLAP

LINKAGE - REMOVAL/INSTALLATION

27-51-13 401 TBC ALL

Remove the Aft Flap Linkage for the

Inboard TE Flap

TASK 27-51-13-024-001

401 TBC ALL

Install the Aft Flap Linkage for the

Inboard TE Flap

TASK 27-51-13-424-005

406 TBC ALL

OUTBOARD TRAILING EDGE FLAP -

REMOVAL/INSTALLATION

27-51-14 401 TBC ALL

Remove the Outboard TE Flap

TASK 27-51-14-024-001

401 TBC ALL

Install the Outboard TE Flap

TASK 27-51-14-424-014

409 TBC ALL

OUTBOARD TRAILING EDGE FLAP -

ADJUSTMENT/TEST

27-51-14 501 TBC ALL

Adjust the Outboard TE Flap

TASK 27-51-14-825-001

501 TBC ALL

The Outboard Trailing Edge Flap Test

TASK 27-51-14-715-049

523 TBC ALL

OUTBOARD TRAILING EDGE FLAP TRACK -

REMOVAL/INSTALLATION

27-51-15 401 TBC ALL

Remove the Track for the Outboard TE

Flap

TASK 27-51-15-024-001

401 TBC ALL

Install the Track for the Outboard TE

Flap

TASK 27-51-15-424-003

407 TBC ALL

TE Flap Track Fuse Bolt - Removal

TASK 27-51-15-000-801

410 TBC ALL

TE Flap Track Fuse Bolt - Installation

TASK 27-51-15-400-801

414 TBC ALL

757

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

OUTBOARD TE FLAP TRACK - INSPECTION/

CHECK

27-51-15 601 TBC ALL

Wear Limits for the Outboard TE Flap

Tracks

TASK 27-51-15-206-001

601 TBC ALL

OUTBOARD TRAILING EDGE FLAP

CARRIAGE - REMOVAL/INSTALLATION

27-51-16 401 TBC ALL

Remove the Flap Carriage for the

Outboard TE Flap

TASK 27-51-16-024-008

401 TBC ALL

Install the Flap Carriage for the

Outboard TE Flap

TASK 27-51-16-424-012

404 TBC ALL

OUTBOARD TRAILING EDGE FLAP

TRANSMISSION - REMOVAL/

INSTALLATION

27-51-17 401 TBC ALL

Remove the Transmissions for the

Outboard TE Flap

TASK 27-51-17-024-001

401 TBC ALL

Install the Transmissions for the

Outboard TE Flap

TASK 27-51-17-424-020

416 TBC ALL

OUTBOARD TRAILING EDGE FLAP TEE

GEARBOX - REMOVAL/INSTALLATION

27-51-18 401 TBC ALL

Remove the Tee Gearbox for the

Outboard TE Flap

TASK 27-51-18-024-001

401 TBC ALL

Install the Tee Gearbox for the

Outboard TE Flap

TASK 27-51-18-424-019

408 TBC ALL

OUTBOARD TRAILING EDGE FLAP

BALLSCREW - REMOVAL/INSTALLATION

27-51-21 401 TBC ALL

Remove the Ballscrew for the Outboard

TE Flap

TASK 27-51-21-024-001

401 TBC ALL

757

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Install the Ballscrew for the Outboard

TE Flap

TASK 27-51-21-424-004

409 TBC ALL

OUTBOARD TRAILING EDGE FLAP

BALLSCREW - INSPECTION/CHECK

27-51-21 601 TBC ALL

Outboard Trailing Edge Flap Ballscrew

Backlash Check

TASK 27-51-21-226-001

601 TBC ALL

Outboard Trailing Edge Flap Ballscrew

Nut Return Tube Check

TASK 27-51-21-226-018

607 TBC ALL

Outboard Trailing Edge Flap Ballscrew

Inspection

TASK 27-51-21-226-039

613 TBC ALL

OUTBOARD TE FLAP AFT FLAP - REMOVAL/

INSTALLATION

27-51-22 401 TBC ALL

Remove the Aft Flap From the Outboard

TE Flap

TASK 27-51-22-024-026

401 TBC ALL

Install the Aft Flap to the Outboard TE

Flap

TASK 27-51-22-424-028

408 TBC ALL

OUTBOARD TE FLAP AFT FLAP -

ADJUSTMENT/TEST

27-51-22 501 TBC ALL

Adjust the Aft Flap for the Outboard TE

Flap

TASK 27-51-22-825-001

501 TBC ALL

Test of the Aft Flap Installation

TASK 27-51-22-705-037

511 TBC ALL

OUTBOARD TRAILING EDGE FLAP AFT

FLAP LINKAGE - REMOVAL/

INSTALLATION

27-51-23 401 TBC ALL

Remove the Aft Flap Linkage for the

Outboard TE Flap

TASK 27-51-23-024-001

401 TBC ALL

757

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Install the Aft Flap Linkage for the

Outboard TE Flap

TASK 27-51-23-424-018

406 TBC ALL

OUTBOARD TRAILING EDGE FLAP AFT

FLAP LINKAGES - INSPECTION/CHECK

27-51-23 601 TBC ALL

Wear Limits for the Aft Flap Linkages,

Outboard Flaps

TASK 27-51-23-226-001

601 TBC ALL

LEFT HYDRAULIC SYSTEM PRESSURE

SENSITIVE FLOW LIMITER - REMOVAL/

INSTALLATION

27-51-24 401 TBC ALL

Remove the Pressure-Sensitive Flow

Limiter for the Left Hydaulic System

TASK 27-51-24-024-001

401 TBC ALL

Install the Pressure-Sensitive Flow

Limiter for the Left Hydraulic System

TASK 27-51-24-424-006

404 TBC ALL

Operational Test for the Flow Limiter for

the Left Hydraulic System

TASK 27-51-24-714-028

404 TBC ALL

TRAILING EDGE FLAP TORQUE TUBES -

MAINTENANCE PRACTICES

27-51-25 201 TBC ALL

Remove the Torque Tubes for the TE

Flap

TASK 27-51-25-022-001

201 TBC ALL

Install the Torque Tubes for the TE Flap

TASK 27-51-25-422-016

210 TBC ALL

Approved Repairs for the Torque Tubes

of the TE Flap System

TASK 27-51-25-302-025

214 TBC ALL

Torque Tube Coupling Inspection at the

Angle Gearboxes

TASK 27-51-25-202-182

215 TBC ALL PRE SB

757-27A0125

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Remove the Torque Tube Support

Bearing for the TE Flaps

TASK 27-51-25-022-155

222 TBC ALL

Install the Torque Tube Support Bearing

TASK 27-51-25-422-158

224 TBC ALL

TRAILING EDGE FLAP POWER DRIVE UNIT -

REMOVAL/INSTALLATION

27-51-26 401 TBC ALL

Remove the PDU for the TE Flap

TASK 27-51-26-034-001

401 TBC ALL

Install the PDU for the TE Flap

TASK 27-51-26-434-012

416 TBC ALL

TRAILING EDGE FLAP POWER DRIVE UNIT

COMPONENTS - MAINTENANCE

PRACTICES

27-51-27 201 TBC ALL

Remove the PDU Components

TASK 27-51-27-022-001

201 TBC ALL

Install the PDU Components

TASK 27-51-27-422-012

208 TBC ALL

TRAILING EDGE FLAP POWER DRIVE UNIT

CONTROL VALVE MODULE AND

COMPONENTS - MAINTENANCE

PRACTICES

27-51-28 201 TBC ALL

Control Valve Module Removal

TASK 27-51-28-022-001

201 TBC ALL

Control Valve Module Installation

TASK 27-51-28-422-152

214 TBC ALL

Flap Load Relief Solenoid Valve

Removal

TASK 27-51-28-022-070

219 TBC ALL

Flap Load Relief Solenoid Valve

Installation

TASK 27-51-28-422-183

220 TBC ALL

Flap Load Relief Solenoid Valve Coil

Removal

TASK 27-51-28-022-090

222 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Flap Load Relief Solenoid Valve Coil

Installation

TASK 27-51-28-422-091

224 TBC ALL

Control Valve Module Component Test

TASK 27-51-28-722-218

225 TBC ALL

FLAP/SLAT DEPRESSURIZATION MODULE

AND COMPONENTS - MAINTENANCE

PRACTICES

27-51-29 201 TBC ALL

Remove the Flap/Slat Depressurization

Module and Components

TASK 27-51-29-022-001

201 TBC ALL

Install the Flap/Slat Depressurization

Module and Components

TASK 27-51-29-422-026

211 TBC ALL

Operational Test for the Flap/Slat

Depressurization Module

TASK 27-51-29-712-067

215 TBC ALL

Operational Test for the Flap/Slat

Depressurization Module with Primary

Control

TASK 27-51-29-712-172

227 TBC ALL

Operational Test for the Priority Valve

TASK 27-51-29-712-173

229 TBC ALL

[Scheduled Maintenance Task] Flap/

Slat Depressurization Module Priority

Valve - Removal/Installation

TASK 27-51-29-000-801

235 TBC ALL

INBOARD TRAILING EDGE FLAP TRACK

FAIRING - MAINTENANCE PRACTICES

27-51-30 201 TBC ALL

Remove the Fairings for the Inboard TE

Flap Track

TASK 27-51-30-022-001

201 TBC ALL

Install the Fairing for the Inboard TE

Flap Tracks

TASK 27-51-30-422-039

210 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Adjustment/Test of the Fairing for the

Inboard TE Flap Track

TASK 27-51-30-702-055

212 TBC ALL

OUTBOARD TRAILING EDGE FLAP TRACK

FAIRINGS - MAINTENANCE PRACTICES

27-51-31 201 TBC ALL

Remove the Fairings for the Outboard

TE Flap Tracks

TASK 27-51-31-022-001

201 TBC ALL

Install the Fairings for the Outboard TE

Flap Tracks

TASK 27-51-31-422-068

210 TBC ALL

Adjustment/Test of the Forward and Aft

Fairings

TASK 27-51-31-822-045

213 TBC ALL

FLAP CONTROL LEVER - REMOVAL/

INSTALLATION

27-51-32 401 TBC ALL

Remove the Flap Control Lever

TASK 27-51-32-024-001

401 TBC ALL

Install the Flap Control Lever

TASK 27-51-32-424-015

412 TBC ALL

FLAP CONTROL LEVER - INSPECTION/

CHECK

27-51-32 601 TBC ALL

Wear Limits for the Flap Control Lever

TASK 27-51-32-206-001

601 TBC ALL

FLAP CONTROL LEVER POSITION

TRANSMITTER - REMOVAL/

INSTALLATION

27-51-33 401 TBC ALL

Remove the Position Transmitter for the

Flap Control Lever

TASK 27-51-33-024-001

401 TBC ALL

Install the Position Transmitter for the

Flap Control Lever

TASK 27-51-33-424-010

406 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

TRAILING EDGE FLAP DRIVESHAFT -

REMOVAL/INSTALLATION

27-51-34 401 TBC ALL

Remove the Drive Shaft for the TE Flap

TASK 27-51-34-024-001

401 TBC ALL

Install the Drive Shaft for the TE Flap

TASK 27-51-34-424-018

407 TBC ALL

TRAILING EDGE FLAP POSITION

INDICATING SYSTEM - DESCRIPTION

AND OPERATION

27-58-00 1 TBC ALL

TRAILING EDGE FLAP POSITION

INDICATING SYSTEM - ADJUSTMENT/

TEST

27-58-00 501 TBC ALL

Test of the Position Indicating System

for the TE Flaps

TASK 27-58-00-705-001

501 TBC ALL

TRAILING EDGE FLAP SYSTEM AND

LEADING EDGE SLAT SYSTEM POSITION

TRANSMITTER - ADJUSTMENT/TEST

27-58-01 501 TBC ALL

Adjust the Position Transmitters for the

TE Flaps and LE Slats

TASK 27-58-01-825-003

501 TBC ALL

Adjust the Position Transmitter with

Angle Position Indicator

TASK 27-58-01-825-066

524 TBC ALL WITHOUT

FSEU 285N0011-40

Test of the Position Transmitter

Installation

TASK 27-58-01-715-112

534 TBC ALL

FLAP POSITION INDICATOR (N15)

REMOVAL/INSTALLATION

27-58-02 401 TBC ALL

Flap Position Indicator - Removal

TASK 27-58-02-004-001

401 TBC ALL

Flap Position Indicator - Installation

TASK 27-58-02-404-015

401 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Flap Position Indicator - Test

TASK 27-58-02-704-010

402 TBC ALL

FLAP POSITION TRANSMITTER - REMOVAL/

INSTALLATION

27-58-03 401 TBC ALL

Remove the Position Transmitter for the

TE Flaps

TASK 27-58-03-024-001

401 TBC ALL

Install the Flap Position Transmitter

TASK 27-58-03-424-015

406 TBC ALL

SPOILERS AND DRAG DEVICES -

DESCRIPTION AND OPERATION

27-60-00 1 TBC ALL

SPOILER/SPEEDBRAKE CONTROL SYSTEM

- DESCRIPTION AND OPERATION

27-61-00 1 TBC ALL

SPOILER/SPEEDBRAKE CONTROL SYSTEM

- MAINTENANCE PRACTICES

27-61-00 201 TBC ALL

Spoiler/Speedbrake Deactivation

TASK 27-61-00-042-008

201 TBC ALL

Spoiler/Speedbrake Activation

TASK 27-61-00-442-036

210 TBC ALL

SPOILER/SPEEDBRAKE CONTROL SYSTEM

- ADJUSTMENT/TEST

27-61-00 501 TBC ALL

Operational Test - Spoiler/Speedbrake

Control System

TASK 27-61-00-715-409

501 TBC ALL

Adjustment - Spoiler/Speedbrake

Control System

TASK 27-61-00-825-085

518 TBC ALL

System Test - Spoiler/Speedbrake

Control System

TASK 27-61-00-735-204

548 TBC ALL

SPOILERS - REMOVAL INSTALLATION 27-61-01 401 TBC ALL

Spoilers - Removal

TASK 27-61-01-024-011

401 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Spoiler - Installation

TASK 27-61-01-424-040

419 TBC ALL

SPOILER POWER CONTROL ACTUATOR

(PCA) - MAINTENANCE PRACTICES

27-61-02 201 TBC ALL

Spoiler PCA and Its Components -

Removal

TASK 27-61-02-022-001

201 TBC ALL

Spoiler PCA and Its Components -

Installation

TASK 27-61-02-422-027

208 TBC ALL

SPOILER RVDT UNIT - REMOVAL/

INSTALLATION

27-61-04 401 TBC ALL

Spoiler RVDT Unit - Removal

TASK 27-61-04-024-028

401 TBC ALL

Spoiler RVDT Unit - Installation

TASK 27-61-04-424-011

404 TBC ALL

AUTO-SPEEDBRAKE CONTROL SYSTEM -

DESCRIPTION AND OPERATION

27-62-00 1 TBC ALL

AUTO-SPEEDBRAKE CONTROL SYSTEM -

ADJUSTMENT/TEST

27-62-00 501 TBC ALL

Operational Test - Auto-Speedbrake

System

TASK 27-62-00-715-012

501 TBC ALL

Adjustment - Auto-Speedbrake System

TASK 27-62-00-825-031

505 TBC ALL

Speedbrake Lever Force Test

TASK 27-62-00-715-262

521 TBC ALL

System Test - Auto-Speedbrake System

TASK 27-62-00-735-118

522 TBC ALL

SPEEDBRAKE LEVER - REMOVAL/

INSTALLATION

27-62-01 401 TBC ALL

Speedbrake Lever - Removal

TASK 27-62-01-024-004

401 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Speedbrake Lever - Installation

TASK 27-62-01-424-011

405 TBC ALL

SPEEDBRAKE MECHANISM -

MAINTENANCE PRACTICES

27-62-02 201 TBC ALL

Auto-Speedbrake Mechanism and its

Components - Removal

TASK 27-62-02-022-008

201 TBC ALL

Auto-Speedbrake Mechanism and its

Components - Installation

TASK 27-62-02-422-033

212 TBC ALL

Auto-Speedbrake Actuator Arming

Switch (S371) - Removal

TASK 27-62-02-022-072

218 TBC ALL

Arming Switch for the Auto-Speedbrake

Actuator (S371) - Installation

TASK 27-62-02-422-084

219 TBC ALL

FORWARD THRUST LEVER POSITION

SWITCH - ADJUSTMENT/TEST

27-62-07 501 TBC ALL

Position Switch for the Forward Thrust

Levers - Operational Test

TASK 27-62-07-715-003

501 TBC ALL

REVERSE THRUST LEVER POSITION

SWITCH - MAINTENANCE PRACTICES

27-62-08 201 TBC ALL

Position Switch for the Reverse Thrust

Levers - Removal

TASK 27-62-08-022-001

201 TBC ALL

Position Switch for the Reverse Thrust

Levers - Installation

TASK 27-62-08-422-012

205 TBC ALL

LEADING EDGE SLAT SYSTEM -

DESCRIPTION AND OPERATION

27-81-00 1 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

LEADING EDGE SLAT SYSTEM -

MAINTENANCE PRACTICES

27-81-00 201 TBC ALL

Deactivation of the LE Slats

TASK 27-81-00-042-001

201 TBC ALL

Operation of the LE Slat System

TASK 27-81-00-862-045

210 TBC ALL

LEADING EDGE SLAT SYSTEM -

ADJUSTMENT/TEST

27-81-00 501 TBC ALL

Operational Test - LE Slat System

TASK 27-81-00-715-001

501 TBC ALL

Adjustment - LE Slat System

TASK 27-81-00-825-296

523 TBC ALL

System Test - LE Slat System

TASK 27-81-00-735-300

535 TBC ALL

Test of the Auto Slat Extension and

Retraction

TASK 27-81-00-715-290

557 TBC ALL

Test of the LE Slat Loss Detection

Switches

TASK 27-81-00-715-294

560 TBC ALL

INBOARD LEADING EDGE SLAT -

REMOVAL/INSTALLATION

27-81-01 401 TBC ALL

Remove the Inboard LE Slat

TASK 27-81-01-024-001

401 TBC ALL

Install the Inboard LE Slat

TASK 27-81-01-424-019

418 TBC ALL

INBOARD LEADING EDGE SLAT -

INSPECTION/CHECK

27-81-01 601 TBC ALL

Wear Limits for the Inboard Leading

Edge Slat

TASK 27-81-01-226-001

601 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

OUTBOARD LEADING EDGE SLAT -

REMOVAL/INSTALLATION

27-81-02 401 TBC ALL

Remove the Outboard LE Slat

TASK 27-81-02-024-001

401 TBC ALL

Install the Outboard LE Slat

TASK 27-81-02-424-021

420 TBC ALL

OUTBOARD LEADING EDGE SLAT -

INSPECTION/CHECK

27-81-02 601 TBC ALL

Wear Limits for the Outboard Leading

Edge Slat

TASK 27-81-02-226-001

601 TBC ALL

LEADING EDGE SLAT POWER DRIVE UNIT

CONTROL VALVE MODULE AND

COMPONENTS - MAINTENANCE

PRACTICES

27-81-06 201 TBC ALL

Remove the Control Valve Module and

the Autoslat Solenoid Valve

TASK 27-81-06-022-001

201 TBC ALL

Install the Control Valve Module and the

Autoslat Solenoid Valve

TASK 27-81-06-422-024

211 TBC ALL

LEADING EDGE SLAT POWER DRIVE UNIT -

REMOVAL/INSTALLATION

27-81-07 401 TBC ALL

Remove the PDU for the LE Slat

TASK 27-81-07-024-001

401 TBC ALL

Install the LE Slat PDU

TASK 27-81-07-424-027

415 TBC ALL

LEADING EDGE SLAT POWER DRIVE UNIT

COMPONENTS - MAINTENANCE

PRACTICES

27-81-08 201 TBC ALL

Remove the Components for the LE Slat

PDU

TASK 27-81-08-022-001

201 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Install the Components for the LE Slat

PDU

TASK 27-81-08-422-017

208 TBC ALL

LEADING EDGE SLAT BYPASS VALVE -

REMOVAL/INSTALLATION

27-81-09 401 TBC ALL

Remove the Bypass Valve for the LE

Slat

TASK 27-81-09-024-001

401 TBC ALL

Install the Bypass Valve for the LE Slat

TASK 27-81-09-424-016

407 TBC ALL

INBOARD LEADING EDGE SLAT MAIN

TRACK - REMOVAL/INSTALLATION

27-81-10 401 TBC ALL

Remove the Main Track for the Inboard

LE Slat

TASK 27-81-10-024-001

401 TBC ALL

Install the Main Track for the Inboard LE

Slat

TASK 27-81-10-424-017

406 TBC ALL

INBOARD LEADING EDGE SLAT MAIN

TRACK - INSPECTION/CHECK

27-81-10 601 TBC ALL

Wear Limits for the Main Track of the

Inboard Leading Edge Slat

TASK 27-81-10-206-001

601 TBC ALL

INBOARD LEADING EDGE SLAT AUXILIARY

TRACK - REMOVAL/INSTALLATION

27-81-11 401 TBC ALL

Remove the Auxiliary Track for the

Inboard LE Slat

TASK 27-81-11-024-001

401 TBC ALL

Install the Auxiliary Track for the

Inboard LE Slat

TASK 27-81-11-424-005

404 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

INBOARD LEADING EDGE SLAT AUXILIARY

TRACK - INSPECTION/CHECK

27-81-11 601 TBC ALL

Wear Limits for the Inboard Auxiliary

Track of the Inboard Leading Edge Slat

TASK 27-81-11-226-001

601 TBC ALL

Wear Limits for the Outboard Auxiliary

Track of the Inboard Leading Edge Slat

TASK 27-81-11-226-003

610 TBC ALL

Wear Limits for the Inboard Track Yoke

of the Inboard Leading Edge Slat

TASK 27-81-11-226-005

610 TBC ALL

Wear Limits for the Outboard Track

Yoke of the Inboard Leading Edge Slat

TASK 27-81-11-226-007

610 TBC ALL

OUTBOARD LEADING EDGE SLAT MAIN

TRACK - REMOVAL/INSTALLATION

27-81-12 401 TBC ALL

Remove the Main Track for the

Outboard LE Slat

TASK 27-81-12-024-001

401 TBC ALL

Install the Main Track for the Outboard

LE Slat

TASK 27-81-12-424-011

406 TBC ALL

OUTBOARD LEADING EDGE SLAT MAIN

TRACK - INSPECTION/CHECK

27-81-12 601 TBC ALL

Wear Limits for the Main Track,

Outboard Leading Edge Slat

TASK 27-81-12-226-001

601 TBC ALL

OUTBOARD LEADING EDGE SLAT

AUXILIARY TRACK - REMOVAL/

INSTALLATION

27-81-13 401 TBC ALL

Remove the Auxiliary Track for the

Outboard LE Slat

TASK 27-81-13-024-006

401 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

Install the Auxiliary Track for the

Outboard LE Slat

TASK 27-81-13-424-008

403 TBC ALL

OUTBOARD LEADING EDGE SLAT

AUXILIARY TRACK INSPECTION/CHECK

27-81-13 601 TBC ALL

Wear Limits for the Auxiliary Track of

the Outboard Leading Edge Slat.

TASK 27-81-13-226-002

601 TBC ALL

LEADING EDGE SLAT DRIVE ANGLE

GEARBOX - REMOVAL/INSTALLATION

27-81-15 401 TBC ALL

Remove the Angle Gearbox for the LE

Slat

TASK 27-81-15-024-001

401 TBC ALL

Install the Angle Gearbox

TASK 27-81-15-424-014

406 TBC ALL

LEADING EDGE SLAT DRIVE ROTARY

ACTUATOR - REMOVAL/INSTALLATION

27-81-18 401 TBC ALL

Remove the Rotary Actuator for the LE

Slats

TASK 27-81-18-024-001

401 TBC ALL

Install the Rotary Actuator for the LE

Slats

TASK 27-81-18-424-019

412 TBC ALL

LEADING EDGE SLAT DRIVE ROTARY

ACTUATOR - INSPECTION/CHECK

27-81-18 601 TBC ALL

Inspection of the Rotary Actuator

TASK 27-81-18-706-001

601 TBC ALL

LEADING EDGE SLAT DRIVE TORQUE TUBE

- REMOVAL/INSTALLATION

27-81-20 401 TBC ALL

Remove the Torque Tube for the LE Slat

TASK 27-81-20-024-001

401 TBC ALL

Install the Torque Tube for the LE Slat

TASK 27-81-20-424-015

407 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

LEADING EDGE SLAT DRIVE TORQUE TUBE

- APPROVED REPAIRS

27-81-20 801 TBC ALL

Approved Repairs for the Torque Tube

of the Leading Edge Slat

TASK 27-81-20-308-001

801 TBC ALL

INBOARD LE SLAT LOSS SENSING

COMPONENTS - REMOVAL/

INSTALLATION

27-81-41 401 TBC ALL

Loss Sensing Switch and Cable

Assembly Removal

TASK 27-81-41-024-001

401 TBC ALL POST SB

757-27-0117

Loss Sensing Switch for the Inboard LE

Slats Removal

TASK 27-81-41-024-096

410 TBC ALL PRE SB

757-27-0117

Loss Sensing Switch for the Inboard LE

Slats Installation

TASK 27-81-41-424-017

417 TBC ALL PRE SB

757-27-0117

Loss Sensing Switch and Cable

Assembly Installation

TASK 27-81-41-424-097

419 TBC ALL POST SB

757-27-0117

INBOARD LEADING EDGE SLAT LOSS

SENSING SWITCH - ADJUSTMENT/TEST

27-81-41 501 TBC ALL

Adjust the Loss Sensing Switch for the

Inboard LE Slat

TASK 27-81-41-825-001

501 TBC ALL

OUTBOARD LE SLAT LOSS SENSING

SWITCH AND CABLE - REMOVAL/

INSTALLATION

27-81-42 401 TBC ALL

Remove the Loss Sensing Switch and/

or Cable for the Outboard LE Slats

TASK 27-81-42-024-001

401 TBC ALL

Install the Loss Sensing Switch and/or

Cable for the Outboard LE Slats

TASK 27-81-42-424-031

410 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
Subject

Chapter

Section

Subject Conf Page Effect

OUTBOARD LEADING EDGE SLAT LOSS

SENSING SWITCH - ADJUSTMENT/TEST

27-81-42 501 TBC ALL

Adjust the Loss Sensing Switch for the

Outboard LE Slat

TASK 27-81-42-825-032

501 TBC ALL

LEADING EDGE SLAT POSITION

INDICATING SYSTEM - DESCRIPTION

AND OPERATION

27-88-00 1 TBC ALL

LEADING EDGE SLAT POSITION

INDICATING SYSTEM - ADJUSTMENT/

TEST

27-88-00 501 TBC ALL

Adjustment/Test of the Position

Indicating System for the LE Slat

TASK 27-88-00-825-004

501 TBC ALL

LEADING EDGE SLAT POSITION

TRANSMITTER - REMOVAL/

INSTALLATION

27-88-01 401 TBC ALL

Remove the Position Transmitter for the

LE Slat

TASK 27-88-01-024-001

401 TBC ALL

Install Leading Edge Slat Position

Transmitter

TASK 27-88-01-424-015

406 TBC ALL

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CHAPTER 27

FLIGHT CONTROLS
STABILIZER TRIM BALLSCREW ACTUATOR - REMOVAL/INSTALLATION

1. General

A. This procedure contains steps to remove and install the stabilizer ballscrew actuator.

TASK 27-41-10-024-001

2. Remove the Stabilizer Ballscrew Actuator

A. References

Reference Title

06-42-00 P/B 201 EMPENNAGE (MAJOR ZONE 300) ACCESS DOORS AND PANELS -

MAINTENANCE PRACTICES

24-22-00 P/B 201 CONTROL (SUPPLY POWER) - MAINTENANCE PRACTICES

29-11-00 P/B 201 MAIN (LEFT, RIGHT, AND CENTER) HYDRAULIC SYSTEMS -

MAINTENANCE PRACTICES

B. Tools/Equipment

NOTE: When more than one tool part number is listed under the same "Reference" number, the

tools shown are alternates to each other within the same airplane series. Tool part numbers

that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.

Reference Description

SPL-10142 Instl/Rem Equipment - Horiz. Stab. Jackscrew - 757

(Part #: B27011-79, Supplier: 81205, A/P Effectivity: 757-ALL)

C. Location Zones

Zone Area

311 Area Aft of Blkhd to Sta 1787.45, Left

312 Area Aft of Blkhd to Sta 1787.45, Right

D. Access Panels

Number Name/Location

311AL Stab. Trim Ctrl, Actuator, Control Module, Position Transmitter,

Flight Control Cable Instl, APU Fuel Feed Sys., APU Air Supply Sys.,

Pitot Static Sys.

E. Prepare for the Removal

SUBTASK 27-41-10-864-002

(1) Supply electrical power (PAGEBLOCK 24-22-00/201).

SUBTASK 27-41-10-864-003

WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL SURFACES WHEN

HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS,

SPOILERS, AND STABILIZER ARE FULLY POWERED SURFACES. INJURIES TO

PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS

SUPPLIED.

(2) Supply power to the right and center hydraulic systems (PAGEBLOCK 29-11-00/201).

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EFFECTIVITY

TBC ALL 27-41-10

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SUBTASK 27-41-10-864-004

(3) Move the stabilizer to 4 units of trim, as shown on the stabilizer position indicators that are on

the control stand panel, P10.

NOTE: The stabilizer ballscrew actuator can be removed at all positions (if the stabilizer

cannot be moved to the recommended position). But, if the actuator is not in the

recommended position, the telescopic supports can hit the actuator.

SUBTASK 27-41-10-864-005

(4) Remove the pressure from the right and center hydraulic systems and reservoirs

(PAGEBLOCK 29-11-00/201).

SUBTASK 27-41-10-864-006

(5) Put the C and R STAB TRIM SHUTOFF valve switches on the P10 panel to the CUTOUT position.

SUBTASK 27-41-10-864-007

(6) Open these circuit breakers and install safety tags:

Overhead Circuit Breaker Panel, P11

Row Col Number Name

B 19 C01010 STAB TRIM-ALTERNATE CONTROL

TBC ALL POST SB 757-27-0104

C 5 C01017 STAB TRIM CONT L

TBC ALL

C 12 C01528 STAB TRIM SHUTOFF L

C 13 C01529 STAB TRIM SHUTOFF R

H 11 C01017 STAB TRIM CONT L

H 20 C01018 STAB TRIM CONT R

SUBTASK 27-41-10-014-008

WARNING: STAY OFF THE SERVICE ACCESS DOOR, 311AL AND THE ELEVATOR CONTROL

ACCESS DOOR, 313AL. YOUR WEIGHT CAN RELEASE THE SPRING-LOADED

LATCHES ON THE DOOR. IF YOU FALL THROUGH THE DOOR, INJURIES CAN OCCUR.

(7) Open this access panel:

Number Name/Location

311AL Stab. Trim Ctrl, Actuator, Control Module, Position

Transmitter, Flight Control Cable Instl, APU Fuel

Feed Sys., APU Air Supply Sys., Pitot Static Sys.

(PAGEBLOCK 06-42-00/201).

SUBTASK 27-41-10-034-009

(8) Disconnect the eight hydraulic lines that connect to the actuator brakes and motors at the lower

gimbal (there are four on each side of the actuator) (Figure 401).

SUBTASK 27-41-10-034-010

(9) Disconnect the four hydraulic drain seal lines from the actuator brakes and motors.

SUBTASK 27-41-10-034-011

(10) Disconnect the hydraulic lines from the actuator unions and clamps and turn them away from the

actuator.

SUBTASK 27-41-10-034-012

(11) Install plugs and caps on all of the disconnected hydraulic lines and ports.

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SUBTASK 27-41-10-494-013

(12) Do the steps that follow to install the removal equipment for the stabilizer ballscrew, horizontal

stabilizer jackscrew equipment, SPL-10142, (Figure 402):

(a) Do the steps that follow to lock the stabilizer:

1) Install the four bracket assemblies to the first two upper bulkheads aft of the access

door, 311AL.

NOTE: Refer to Figure 402 for the bracket position on the bulkheads in relation to

the airplane centerline.

2) Use the four pins that are supplied to install the I-frame to the brackets.

3) Use the pin that is supplied to install the turnbuckle assembly to the I-frame.

4) Use the bolts and pins that are supplied to install the trunnion assembly to the stabilizer

lugs.

NOTE: The stabilizer lugs are on the top of the stabilizer wing box.

5) Install the lateral frame assembly to the front of the I-frame.

6) Turn the turnbuckle assembly until it can be attached to the trunnion with the pin that is

supplied.

7) If you turn the turnbuckle assembly and it is too short to connect to the trunnion, do the

steps that follow:

a) Remove the mid-length pin.

b) Extend the turnbuckle until it can be connected to the trunnion.

c) Install the mid-length pin.

d) Adjust the turnbuckle and attach it to the trunnion.

e) Make sure that the turnbuckle is installed vertically at the centerline of the airplane.

(b) Do the steps that follow to install the sling:

1) Remove the mid-length safety pin.

2) Install the spring-loaded telescoping beam assembly between the bulkheads on each

side of the access door, 311AL.

NOTE: Refer to Figure 402 for the beam position in relation to the airplane

centerline.

3) Install the mid-length safety pin.

4) Install the inverted T-track and trolley between the lateral front frame of the I-beam and

the rail hanger of the telescoping beam. Use the two pins that are supplied to install the

T-track.

NOTE: This will let you move the stabilizer ballscrew actuator forward and left

outboard to a position above the access door.

5) Attach the fishpole hoist to the trolley.

6) Move the trolley to a position above the stabilizer ballscrew actuator.

7) Install the sling around the upper gimbal of the stabilizer ballscrew actuator.

F. Remove the Stabilizer Ballscrew Actuator

(Figure 402)

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SUBTASK 27-41-10-824-014

WARNING: ONLY APPROVED PERSONS MUST OPERATE THE LEVER CHAIN HOISTS. DO NOT

USE FORCE TO MOVE THE CONTROL LEVER OR KNOB INTO THE NEUTRAL OR THE

FREE CHAIN POSITION. THIS CAN CAUSE A CHAIN HOIST WITH A LIGHT LOAD TO

RELEASE ITS LOAD. INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN

OCCUR.

(1) Adjust the hoist until it holds the weight of the stabilizer ballscrew actuator.

NOTE: A hoist with too much tension will cause the gimbal pins to get caught.

SUBTASK 27-41-10-034-015

(2) Remove the two bolts that attach the anti-rotation cables to the actuator housing.

SUBTASK 27-41-10-034-016

(3) Do the steps that follow to disconnect the upper gimbal:

(a) Loosen the bolts for the upper and lower gimbal pins.

(b) Remove the four bolts that hold the left and right upper gimbal retainers.

CAUTION: DO NOT USE METAL TOOLS TO REMOVE THE RETAINERS. DO NOT USE TOO

MUCH FORCE TO REMOVE THE GIMBAL. DAMAGE TO THE UPPER GIMBAL AND

THE RETAINER FLANGES CAN OCCUR.

(c) Remove the left and right upper gimbal retainers (4 locations).

NOTE: Use hardwood wedges between the retainer flanges and the gimbal to start the

removal of the retainers.

SUBTASK 27-41-10-034-017

(4) Do the steps that follow to disconnect the lower gimbal:

(a) Remove the two bolts that hold the safety shaft.

(b) Remove the four bolts that hold the left and right retainers to the lower gimbal.

CAUTION: DO NOT USE METAL TOOLS TO REMOVE THE RETAINERS. DAMAGE TO THE

UPPER GIMBAL AND THE RETAINER FLANGES CAN OCCUR.

(c) Use a hardwood dowel to remove the retainers and the safety shaft from the lower gimbal.

SUBTASK 27-41-10-024-018

(5) Turn the actuator forward to make sure the upper gimbal will not touch the supports for the

stabilizer ballscrew. Move the trolley if it is necessary.

SUBTASK 27-41-10-024-019

(6) Lift the stabilizer ballscrew actuator away from the lower gimbal attachment lugs.

SUBTASK 27-41-10-024-020

(7) Move the actuator to a position above the access door, 311AL, and lower it through the door.

------------------------- END OF TASK ---------------------------

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Stabilizer Trim Ballscrew Actuator Hydraulic Connections

Figure 401 (Sheet 1 of 2)/27-41-10-990-801

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Stabilizer Trim Ballscrew Actuator Hydraulic Connections

Figure 401 (Sheet 2 of 2)/27-41-10-990-801

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Stabilizer Trim Ballscrew Actuator Installation

Figure 402 (Sheet 1 of 2)/27-41-10-990-804

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Stabilizer Trim Ballscrew Actuator Installation

Figure 402 (Sheet 2 of 2)/27-41-10-990-804

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Measurement of Stabilizer Dimension B

Figure 403/27-41-10-990-806

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TASK 27-41-10-424-021

3. Install the Stabilizer Ballscrew Actuator

A. References

Reference Title

06-42-00 P/B 201 EMPENNAGE (MAJOR ZONE 300) ACCESS DOORS AND PANELS -

MAINTENANCE PRACTICES

12-21-05 P/B 301 HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - SERVICING

(LUBRICATION)

24-22-00 P/B 201 CONTROL (SUPPLY POWER) - MAINTENANCE PRACTICES

27-41-00 P/B 501 HORIZONTAL STABILIZER TRIM CONTROL SYSTEM -

ADJUSTMENT/TEST

27-41-14 P/B 601 STABILIZER TRIM UPPER AND LOWER GIMBAL -

INSPECTION/CHECK

29-11-00 P/B 201 MAIN (LEFT, RIGHT, AND CENTER) HYDRAULIC SYSTEMS -

MAINTENANCE PRACTICES

B. Tools/Equipment

NOTE: When more than one tool part number is listed under the same "Reference" number, the

tools shown are alternates to each other within the same airplane series. Tool part numbers

that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.

Reference Description

SPL-10142 Instl/Rem Equipment - Horiz. Stab. Jackscrew - 757

(Part #: B27011-79, Supplier: 81205, A/P Effectivity: 757-ALL)

C. Consumable Materials

Reference Description Specification

D00013 Grease - Aircraft And Instrument Grease MIL-PRF-23827

(NATO G-354)

(Supersedes

MIL-G-23827)

D00153 Fluid - Hydraulic Fluid, Fire Resistant BMS3-11 Type

IV

D00633 Grease - Aircraft General Purpose BMS3-33

D. Location Zones

Zone Area

311 Area Aft of Blkhd to Sta 1787.45, Left

312 Area Aft of Blkhd to Sta 1787.45, Right

E. Access Panels

Number Name/Location

311AL Stab. Trim Ctrl, Actuator, Control Module, Position Transmitter,

Flight Control Cable Instl, APU Fuel Feed Sys., APU Air Supply Sys.,

Pitot Static Sys.

F. Prepare for the Installation

(Figure 402)

SUBTASK 27-41-10-224-022

(1) Make sure that the stabilizer ballscrew actuator and the attachment locations are in the

permitted wear limits (PAGEBLOCK 27-41-14/601).

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SUBTASK 27-41-10-224-023

(2) Turn the upper gimbal and ballnut until the Dimension B on the stabilizer ballscrew actuator is

19.07 ± 0.50 inches (484.4 +/- 12.7 mm) (Figure 403).

SUBTASK 27-41-10-034-024

(3) Do the steps that follow to remove the upper gimbal retainers:

(a) Remove the nuts and bolts from the left and right retainers.

(b) Remove the left and right retainers.

SUBTASK 27-41-10-034-025

(4) Do the steps that follow to remove the safety shaft and retainers from the lower gimbal:

(a) Remove the nuts and bolts from the safety shaft.

(b) Remove the safety shaft.

(c) Remove the nuts and bolts from the left and right retainers.

(d) Remove the left and right retainers.

SUBTASK 27-41-10-494-026

(5) Attach the lift bracket to the stabilizer ballscrew.

SUBTASK 27-41-10-424-027

(6) Use the fishpole hoist to lift the stabilizer ballscrew actuator through the access door, 311AL.

SUBTASK 27-41-10-424-028

(7) Move the lower gimbal to its correct position on the stabilizer attachment lugs.

G. Install the Stabilizer Ballscrew Actuator

(Figure 402)

SUBTASK 27-41-10-424-029

(1) Do the steps that follow to attach the lower gimbal:

(a) Lightly apply grease, D00633 (or alternate grease, D00013) to these surfaces:

1) Bearing surfaces of the lower gimbal attachment lugs

2) Outer and inner surfaces of the retainers

3) outer surface of safety shaft.

(b) Align the lower gimbal with the attachment lugs and install the left and right retainers with

the grease fittings down.

(c) Install the bolts, washers, and nuts that hold the retainers to the lower gimbal.

NOTE: Install the bolts such that the washers and nuts are on the outer part of the lower

gimbal.

(d) Install the safety shaft and align the holes at each end of the shaft with the retainer holes.

(e) Install the bolts, nuts, and washers that hold the safety shaft.

NOTE: Install the bolts such that the washers and nuts are on the lower side of the

retainer.

SUBTASK 27-41-10-424-030

(2) Do the steps that follow to attach the upper gimbal:

(a) Lightly apply grease, D00633 (or alternate grease, D00013) to the bearing surfaces of the

ballscrew support and the outer surfaces of the retainers.

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(b) Adjust the turnbuckle assembly as necessary until the stabilizer ballscrew actuator will

engage with the ballscrew support.

(c) Turn the actuator aft to engage it with the ballscrew support.

(d) Align the upper gimbal with the ballscrew support and install the left and right retainers.

(e) Align the bolt holes on the retainers with the holes on the upper gimbal.

(f) Install the bolts, washers, and nuts on the retainers and upper gimbal.

SUBTASK 27-41-10-434-031

(3) Connect the anti-rotation cables with a bolt, washer, and nut (2 locations).

SUBTASK 27-41-10-434-032

(4) Remove the plugs and caps from the hydraulic lines and ports.

SUBTASK 27-41-10-434-034

(5) Connect the hydraulic lines and the drain tubes to the stabilizer ballscrew actuator. Use clamps

to hold the hydraulic lines and drain tubes to the supports on the actuator.

NOTE: Before you connect these hydraulic lines, make sure that the drive motor housing is full

of hydraulic hydraulic fluid, D00153.

SUBTASK 27-41-10-094-035

(6) Remove the removal equipment for the stabilizer ballscrew, horizontal stabilizer jackscrew

equipment, SPL-10142.

SUBTASK 27-41-10-214-036

(7) Do a visual check to make sure that you installed the stabilizer ballscrew actuator correctly.

SUBTASK 27-41-10-644-037

(8) Lubricate the stabilizer ballscrew actuator (PAGEBLOCK 12-21-05/301).

H. Stabilizer Ballscrew Actuator Test

SUBTASK 27-41-10-864-038

(1) Remove the safety tags and close these circuit breakers:

Overhead Circuit Breaker Panel, P11

Row Col Number Name

B 19 C01010 STAB TRIM-ALTERNATE CONTROL

TBC ALL POST SB 757-27-0104

C 5 C01017 STAB TRIM CONT L

TBC ALL

C 12 C01528 STAB TRIM SHUTOFF L

C 13 C01529 STAB TRIM SHUTOFF R

H 11 C01017 STAB TRIM CONT L

H 20 C01018 STAB TRIM CONT R

SUBTASK 27-41-10-864-039

(2) Put the RIGHT and CENTER STAB TRIM SHUTOFF valve switches on the control stand panel,

P10, to the NORM position.

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SUBTASK 27-41-10-864-040

WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL SURFACES WHEN

HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS,

SPOILERS, AND STABILIZER ARE FULLY POWERED SURFACES. INJURIES TO

PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS

SUPPLIED.

(3) Supply power to the right or center hydraulic systems (PAGEBLOCK 29-11-00/201).

NOTE: The right hydraulic system only supplies power to the ballscrew actuator’s right side

secondary brake and drive hydraulic motor. The center hydraulic system only supplies

power to the ballscrew actuator’s left side secondary brake and drive hydraulic motor.

If the right and center hydraulic systems are pressurized at the same time, you cannot

find failures.

SUBTASK 27-41-10-864-041

(4) Push and hold the BRAKE BYPASS valve button on the applicable stabilizer trim control module.

NOTE: The button is on the bottom of the unit.

The force necessary to push the button should be less than 25 pounds (111 newtons).

You should push the button smoothly. If the force necessary to push the button is more

than 25 pounds (111 newtons), remove the hydraulic power, push the button more than

once, then supply the hydraulic power.

SUBTASK 27-41-10-864-042

(5) Move the control wheel switches and hold for 10 seconds.

(a) Make sure that the stabilizer does not move.

SUBTASK 27-41-10-864-044

(6) Release the control wheel switches and then release the BRAKE BYPASS valve button.

SUBTASK 27-41-10-864-045

(7) Use the control wheel switches to move the stabilizer through its full travel range.

(a) Make sure the stabilizer moves smoothly and freely through its full travel.

NOTE: The stabilizer can move to two different full-travel positions, depending on the flap

setting. To move the stabilizer to its furthest possible point of travel, you will need

to set the flaps to the 15-unit position.

(b) Make sure that the anti-rotation cables stay loose through the full stabilizer travel.

(c) Make sure there are no leaks or damage in the hydraulic line connections.

SUBTASK 27-41-10-714-054

(8) Do the Alternate-Electric Operation and Travel Limits Test (PAGEBLOCK 27-41-00/501).

I. Put the Airplane Back to Its Usual Condition

SUBTASK 27-41-10-414-047

(1) Close this access panel:

Number Name/Location

311AL Stab. Trim Ctrl, Actuator, Control Module, Position

Transmitter, Flight Control Cable Instl, APU Fuel

Feed Sys., APU Air Supply Sys., Pitot Static Sys.

(PAGEBLOCK 06-42-00/201).

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SUBTASK 27-41-10-864-048

(2) Remove the power from the hydraulic systems (PAGEBLOCK 29-11-00/201).

SUBTASK 27-41-10-864-049

(3) Remove electrical power, if it is not necessary (PAGEBLOCK 24-22-00/201).

------------------------- END OF TASK ---------------------------

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STABILIZER TRIM BALLSCREW FREEPLAY

1. General

A. This procedure contains steps to do the following inspections:

 Stabilizer Ballscrew to Ballnut Freeplay Inspection

 Stabilizer Ballscrew Assembly Detailed Visual Inspection.

TASK 27-41-10-226-052

2. Check for Stabilizer Ballscrew to Ballnut Freeplay

NOTE: This is a scheduled maintenance task.

A. References

Reference Title

06-42-00 P/B 201 EMPENNAGE (MAJOR ZONE 300) ACCESS DOORS AND PANELS -

MAINTENANCE PRACTICES

12-21-05 P/B 301 HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - SERVICING

(LUBRICATION)

24-22-00 P/B 201 CONTROL (SUPPLY POWER) - MAINTENANCE PRACTICES

27-41-10 P/B 401 STABILIZER TRIM BALLSCREW ACTUATOR -

REMOVAL/INSTALLATION

29-11-00 P/B 201 MAIN (LEFT, RIGHT, AND CENTER) HYDRAULIC SYSTEMS -

MAINTENANCE PRACTICES

B. Tools/Equipment

NOTE: When more than one tool part number is listed under the same "Reference" number, the

tools shown are alternates to each other within the same airplane series. Tool part numbers

that are replaced or non-procurable are preceded by "Opt:", which stands for Optional.

Reference Description

SPL-11765 Bracket Assemblies - Horiz. Stab. Jackscrew Inst/Rem (B27011-3, -4

and -77 included in B27011-79 Equip)

(Part #: B27011-79, Supplier: 81205, A/P Effectivity: 757-ALL)

SPL-11766 Frame Assembly - Horiz. Stab. Jackscrew Inst/Rem (B27011-62

included in B27011-79 Equip)

(Part #: B27011-79, Supplier: 81205, A/P Effectivity: 757-ALL)

SPL-11767 Trunnion Assembly - Horiz. Stab. Jackscrew Inst/Rem (B27011-71

included in B27011-79 Equip)

(Part #: B27011-79, Supplier: 81205, A/P Effectivity: 757-ALL)

SPL-11773 Load Assembly - Jackscrew Backlash, Horiz. Stabilizer (B27034-6

included in B27034-1 eqpt)

(Part #: B27034-1, Supplier: 81205, A/P Effectivity: 757-ALL)

STD-6975 Indicator - Dial 25-441P, Universal Indicator Back - 672.2, Magnetic

Base Indicator Holder

C. Location Zones

Zone Area

311 Area Aft of Blkhd to Sta 1787.45, Left

312 Area Aft of Blkhd to Sta 1787.45, Right

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D. Access Panels

Number Name/Location

311AL Stab. Trim Ctrl, Actuator, Control Module, Position Transmitter,

Flight Control Cable Instl, APU Fuel Feed Sys., APU Air Supply Sys.,

Pitot Static Sys.

E. Prepare for the Inspection/Check

SUBTASK 27-41-10-646-054

(1) Lubricate the stabilizer ballscrew (PAGEBLOCK 12-21-05/301).

SUBTASK 27-41-10-866-053

(2) Supply electrical power (PAGEBLOCK 24-22-00/201).

SUBTASK 27-41-10-866-003

WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL SURFACES WHEN

HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS,

SPOILERS, AND STABILIZER ARE FULLY POWERED SURFACES. INJURIES TO

PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS

SUPPLIED.

(3) Supply power to the right and center hydraulic systems (PAGEBLOCK 29-11-00/201).

SUBTASK 27-41-10-866-004

(4) Move the stabilizer to approximately 4 units of trim, as shown on the stabilizer position

indicators that are on the control stand panel, P10.

SUBTASK 27-41-10-866-005

(5) Remove the pressure from the right and center hydraulic system (PAGEBLOCK 29-11-00/201).

SUBTASK 27-41-10-866-006

(6) Put the C and R STAB TRIM SHUTOFF valve switches on the P10 panel to the CUTOUT position.

SUBTASK 27-41-10-866-007

(7) Open these circuit breakers and install safety tags:

Overhead Circuit Breaker Panel, P11

Row Col Number Name

B 19 C01010 STAB TRIM-ALTERNATE CONTROL

TBC ALL POST SB 757-27-0104

C 5 C01017 STAB TRIM CONT L

TBC ALL

C 12 C01528 STAB TRIM SHUTOFF L

C 13 C01529 STAB TRIM SHUTOFF R

H 11 C01017 STAB TRIM CONT L

H 20 C01018 STAB TRIM CONT R

SUBTASK 27-41-10-016-008

WARNING: STAY OFF THE SERVICE ACCESS DOOR, 311AL AND THE ELEVATOR CONTROL

ACCESS DOOR, 313AL. YOUR WEIGHT CAN RELEASE THE SPRING-LOADED

LATCHES ON THE DOOR. IF YOU FALL THROUGH THE DOOR, INJURIES CAN OCCUR.

(8) Open this access panel:

(PAGEBLOCK 06-42-00/201)

Number Name/Location

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(Continued)

Number Name/Location

311AL Stab. Trim Ctrl, Actuator, Control Module, Position

Transmitter, Flight Control Cable Instl, APU Fuel

Feed Sys., APU Air Supply Sys., Pitot Static Sys.

SUBTASK 27-41-10-496-013

(9) Do the steps that follow to install the load assembly, SPL-11773 (B27034-6) between the

horizontal stabilizer and the upper fuselage structure (Figure 601):

(a) Install the four bracket assemblies, SPL-11765 (B27011-3, -4, and -77) to the bulkheads

above the horizontal stabilizer actuator (Figure 601).

(b) Use the four pins to install the frame assembly, SPL-11766 (I-frame, B27011-62) to the four

bracket assemblies that were just installed.

(c) Use the bolts and pins supplied to install the trunnion assembly, SPL-11767 (B27011-71) to

the stabilizer lug.

(d) Install the load assembly, SPL-11773 (B27034-6) to the I-frame and trunnion using the pins.

SUBTASK 27-41-10-866-055

(10) Do the steps that follow to install the dial indicator, STD-6975 on the ballscrew actuator:

(a) Install the magnetic base for the dial indicator on the ballscrew above the upper ballnut.

(b) Install the dial indicator to the magnetic base so that the tip of the dial indicator touches the

flat spot on the top of the ballnut.

NOTE: The dial indicator is installed to measure the downward movement of the ballnut

relative to the ballscrew.

F. Stabilizer Ballnut Freeplay Procedure

(Figure 601)

SUBTASK 27-41-10-826-014

CAUTION: DO NOT APPLY MORE THAN THE SPECIFIED LOADS TO THE STABILIZER WHILE

USING THE LOAD TOOL, B27034-6. DO NOT APPLY POWER TO THE STABILIZER TRIM

ACTUATOR WITH THE LOAD TOOL INSTALLED. IF YOU DO, DAMAGE TO THE

EQUIPMENT OR AIRCRAFT CAN OCCUR.

(1) Zero the dial indicator, STD-6975.

NOTE: At 4 units of trim, the aft stabilizer center of gravity loads the ballscrew in the upward

direction, putting the ballscrew in tension.

SUBTASK 27-41-10-866-056

(2) Use the load assembly, SPL-11773 to slowly apply an upward force of 350 pounds to the

ballscrew as read on the force guage.

NOTE: To apply the upward force to the ballscrew, the stabilizer tool must be turned in the

direction that shortens the tool length. This will apply an upward force on the ballnut

and move the leading edge of the stabilizer up.

SUBTASK 27-41-10-826-061

(3) Zero the dial indicator, STD-6975.

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SUBTASK 27-41-10-826-057

(4) Use the load assembly, SPL-11773 to slowly release the upward force applied in the previous

step and continue adjusting the load tool to apply a downward force of 1000 pounds (4450

newtons).

NOTE: To apply a downward force on the stabilizer, the tool must be turned in a direction that

lengthens the tool. This will apply a downward force on the ballnut.

(a) Make a note of the quantity shown on the dial indicator. This is the stabilizer ballscrew to

ballnut freeplay.

SUBTASK 27-41-10-846-059

(5) Use the load assembly, SPL-11773 to slowly release the downward force that was applied.

SUBTASK 27-41-10-826-062

(6) If the ballscrew to ballnut freeplay is less than 0.004 inch (0.10 mm), then the measurement may

be in error. Do the following to verify that the measurement was not made in error:

NOTE: If the measured freeplay is 0.000 inch (0.00 millimeter), then the freeplay measurement

is probably in error. A small amount (0.004 to 0.007 inch (0.10 to 0.18 millimeter)) of

freeplay is expected in new stabilizer ballscrews.

(a) Check that the stabilizer was loaded in the correct direction for each of the previous steps.

(b) Make sure the dial indicator, STD-6975 is functioning properly.

(c) If the above two checks are complete and the freeplay check was run correctly, the

stabilizer ballscrew to ballnut freeplay check is within the limits and no further checks are

necessary.

You can ignore the next two steps and put the airplane back to its usual condition.

SUBTASK 27-41-10-826-063

(7) If the ballscrew to ballnut freeplay is greater than or equal to 0.004 inch (0.10 mm), and less than

0.016 inch (0.41 mm), the ballscrew to ballnut freeplay is in the acceptable limits.

SUBTASK 27-41-10-826-064

(8) If the ballscrew to ballnut freeplay is greater than or equal to 0.016 inch (0.41 mm), the stab trim

actuator wear is greater than the maximum in-service wear limits. Do the following:

(a) Remove and Replace the Stabilizer Trim Actuator (PAGEBLOCK 27-41-10/401).

G. Put the Airplane Back to Its Usual Condition

SUBTASK 27-41-10-486-065

(1) Remove the load assembly, SPL-11773 from the horizontal stabilizer and the upper fuselage

(Figure 601).

SUBTASK 27-41-10-486-066

(2) Remove the load tool installation bracket assemblies, SPL-11765 from the attach points on the

bulkheads.

SUBTASK 27-41-10-486-067

(3) Remove the dial indicator, STD-6975 and the magnetic base from the ballnut and ballscrew.

SUBTASK 27-41-10-416-049

(4) Close this access panel:

(PAGEBLOCK 06-42-00/201)

Number Name/Location

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(Continued)

Number Name/Location

311AL Stab. Trim Ctrl, Actuator, Control Module, Position

Transmitter, Flight Control Cable Instl, APU Fuel

Feed Sys., APU Air Supply Sys., Pitot Static Sys.

SUBTASK 27-41-10-866-050

(5) Set the C STAB TRIM SHUTOFF switch and R STAB TRIM SHUTOFF switch to the NORM

position.

SUBTASK 27-41-10-866-051

(6) Remove the safety tags and close these circuit breakers:

Overhead Circuit Breaker Panel, P11

Row Col Number Name

B 19 C01010 STAB TRIM-ALTERNATE CONTROL

TBC ALL POST SB 757-27-0104

C 5 C01017 STAB TRIM CONT L

TBC ALL

C 12 C01528 STAB TRIM SHUTOFF L

C 13 C01529 STAB TRIM SHUTOFF R

H 11 C01017 STAB TRIM CONT L

H 20 C01018 STAB TRIM CONT R

------------------------- END OF TASK ---------------------------

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Stabilizer Ballnut Freeplay Inspection

Figure 601/27-41-10-990-807

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TASK 27-41-10-226-069

3. Stabilizer Ballscrew Assembly Detailed Visual Inspection

NOTE: This is a scheduled maintenance task.

A. References

Reference Title

06-42-00 P/B 201 EMPENNAGE (MAJOR ZONE 300) ACCESS DOORS AND PANELS -

MAINTENANCE PRACTICES

12-21-05 P/B 301 HORIZONTAL STABILIZER TRIM CONTROL SYSTEM - SERVICING

(LUBRICATION)

24-22-00 P/B 201 CONTROL (SUPPLY POWER) - MAINTENANCE PRACTICES

27-41-10 P/B 401 STABILIZER TRIM BALLSCREW ACTUATOR -

REMOVAL/INSTALLATION

29-11-00 P/B 201 MAIN (LEFT, RIGHT, AND CENTER) HYDRAULIC SYSTEMS -

MAINTENANCE PRACTICES

B. Location Zones

Zone Area

311 Area Aft of Blkhd to Sta 1787.45, Left

312 Area Aft of Blkhd to Sta 1787.45, Right

C. Access Panels

Number Name/Location

311AL Stab. Trim Ctrl, Actuator, Control Module, Position Transmitter,

Flight Control Cable Instl, APU Fuel Feed Sys., APU Air Supply Sys.,

Pitot Static Sys.

D. Prepare for the Detailed Visual Inspection

SUBTASK 27-41-10-866-071

(1) Supply electrical power (PAGEBLOCK 24-22-00/201).

SUBTASK 27-41-10-866-072

WARNING: KEEP PERSONS AND EQUIPMENT AWAY FROM ALL CONTROL SURFACES WHEN

HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS,

SPOILERS, AND STABILIZER ARE FULLY POWERED SURFACES. INJURIES TO

PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS

SUPPLIED.

(2) Supply power to the right and center hydraulic systems (PAGEBLOCK 29-11-00/201).

SUBTASK 27-41-10-866-073

(3) Move the stabilizer to approximately 4 units of trim, as shown on the stabilizer position

indicators that are on the control stand panel, P10.

SUBTASK 27-41-10-866-074

(4) Remove the pressure from the right and center hydraulic system (PAGEBLOCK 29-11-00/201).

SUBTASK 27-41-10-866-075

(5) Put the C and R STAB TRIM SHUTOFF valve switches on the P10 panel to the CUTOUT position.

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SUBTASK 27-41-10-866-076

(6) Open these circuit breakers and install safety tags:

Overhead Circuit Breaker Panel, P11

Row Col Number Name

B 19 C01010 STAB TRIM-ALTERNATE CONTROL

TBC ALL POST SB 757-27-0104

C 5 C01017 STAB TRIM CONT L

TBC ALL

C 12 C01528 STAB TRIM SHUTOFF L

C 13 C01529 STAB TRIM SHUTOFF R

H 11 C01017 STAB TRIM CONT L

H 20 C01018 STAB TRIM CONT R

SUBTASK 27-41-10-016-077

WARNING: STAY OFF THE SERVICE ACCESS DOOR, 311AL AND THE ELEVATOR CONTROL

ACCESS DOOR, 313AL. YOUR WEIGHT CAN RELEASE THE SPRING-LOADED

LATCHES ON THE DOOR. IF YOU FALL THROUGH THE DOOR, INJURIES CAN OCCUR.

(7) Open this access panel:

Number Name/Location

311AL Stab. Trim Ctrl, Actuator, Control Module, Position

Transmitter, Flight Control Cable Instl, APU Fuel

Feed Sys., APU Air Supply Sys., Pitot Static Sys.

(PAGEBLOCK 06-42-00/201).

E. Stabilizer Ballscrew Assembly Detailed Visual Inspection

(Figure 602)

SUBTASK 27-41-10-216-099

(1) Inspect the ballscrew and ballnut for signs of corrosion.

NOTE: Metallic debris in the grease may indicate degradation of the balls in the ballnut.

(a) Look for metallic dust particles on or around the ballscrew and ballnut.

(b) Examine the grease on the ballscrew for metal debris.

(c) If you find any metal debris or corrosion, replace the stabilizer ballscrew actuator

assembly (PAGEBLOCK 27-41-10/401).

SUBTASK 27-41-10-646-070

(2) Clean the ballscrew by wiping any old grease and dirt from the ballscrew threads.

NOTE: Use a clean, dry, non-abrasive cloth.

SUBTASK 27-41-10-216-101

(3) Inspect the ballnut and four ballnut return tubes for the following:

NOTE: The ballnut return tubes are difficult to view from below. Make sure to view the return

tubes from above the ballnut assembly.

(a) Visually inspect the ballnut return tubes to see if they have lifted from the ballnut or are

damaged in a way that would restrict free movement of the ball bearings.

1) If any of the return tubes have lifted from the ballnut, or are dented or damaged,

replace the stabilizer ballscrew actuator assembly (PAGEBLOCK 27-41-10/401).

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(b) Check the exterior of the ballnut, stabilizer actuator, and the area below and around the

actuator for ball bearings.

NOTE: The ball bearings used inside the ballnut are 0.2188 inch (5.558 millimeter)

diameter.

1) If any ball bearings are found, replace the stabilizer ballscrew actuator assembly

(PAGEBLOCK 27-41-10/401).

SUBTASK 27-41-10-216-102

(4) Examine the ballscrew for the following problems:

(a) Inspect the ballscrew threads for for cross-threading, distortion, or stripping.

(b) Check for metal debris, pitting, gouging, corrosion, spalling or brinelling in the ballscrew

thread.

(c) Check for obvious differences in thread shape between thread grooves in the lower, middle

and upper portions of the ballscrew.

(d) Check the ballscrew for damage or cracking.

SUBTASK 27-41-10-866-095

(5) Move the ballscrew to another location other than the 4 units of trim that it was just at.

SUBTASK 27-41-10-216-104

(6) Repeat the steps above to examine the newly exposed threads of the ballscrew.

SUBTASK 27-41-10-216-105

(7) If you find any problems listed above, replace the stabilizer ballscrew actuator assembly

(PAGEBLOCK 27-41-10/401).

SUBTASK 27-41-10-646-096

(8) Unless you will immediately perform the check for the stabilizer ballscrew to ballnut freeplay

(PAGEBLOCK 27-41-10/601), lubricate the stabilizer ballscrew and ballnut

(PAGEBLOCK 12-21-05/301).

F. Put the Airplane Back to Its Usual Condition

SUBTASK 27-41-10-866-092

(1) Set the C STAB TRIM SHUTOFF switch and R STAB TRIM SHUTOFF switch to the NORM

position.

SUBTASK 27-41-10-866-093

(2) Remove the safety tags and close these circuit breakers:

Overhead Circuit Breaker Panel, P11

Row Col Number Name

B 19 C01010 STAB TRIM-ALTERNATE CONTROL

TBC ALL POST SB 757-27-0104

C 5 C01017 STAB TRIM CONT L

TBC ALL

C 12 C01528 STAB TRIM SHUTOFF L

C 13 C01529 STAB TRIM SHUTOFF R

H 11 C01017 STAB TRIM CONT L

H 20 C01018 STAB TRIM CONT R

------------------------- END OF TASK ---------------------------

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Stabilizer Assembly Detailed Visual Inspection

Figure 602/27-41-10-990-808

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