(e)  
On the tester, set the SUBFRAME to 4 and the WORD to 17.

 (f)  
Make sure the tester display shows between 6735 and 7045.

 (g)  
Set the T.E. flaps to the 15 units detent position.

 (h)  
Make sure the tester display shows between 1735 and 2045.

 (i)  
Set the T.E. flaps to the full up position.

 S 865-928-001
 (10) Remove the DO-NOT-CLOSE tag and close the P11 panel circuit breaker:
 (a)  11H12, FLAP POS IND LEFT
 
 GUN 001-008, 010, 101 PRE-EO B531006;  ú 31-31-00
 GUN 009  ú CONFIG 1 ú 06 Page 518 ú Sep 28/01

A

757
MAINTENANCE MANUAL

 (b)  
On the tester, set the SUBFRAME to 2 and the WORD to 17.

 (c)  
Set the left T.E. flaps to the 20 unit detent position.

 (d)  
Make sure the tester display shows between 2734 and 3044.

 S 865-927-001
 (11)
 Set the T.E. flaps system back to the full up position.

 S 735-725-001

 (12)
 Leading Edge Slat Position Test

 (a)  
Make sure the leading edge slat system is operational (Ref 27-81-00).

 (b)  
Set the SUBFRAME and WORD for each parameter condition as shown in the table that follows.

 (c)  
Make sure the tester display shows the correct data for each postion.

 ~................................................................ | | TESTER SETUP | TESTER DISPLAY | | L.E. SLATS/CONDITION ........................................... | | SUBFRAME | WORD |BIT (DISCRETE)| VALUE | ..................................................................
 | FULL EXTEND  |  1 (3)  |  17  |  2  |  1  |
 |  |  |  |  |  |
 | NOT FULLY EXTEND  |  |  |  |  0  |
 |  |  |  |  |  |
 | PART EXTEND  |  1 (3)  |  24  |  1  |  1  |
 |  |  |  |  |  |
 | NOT PART EXTEND  |  |  |  |  0  |
 |  |  |  |  |  |
 | RETRACTED  |  1 (3)  |  24  |  2  |  1  |
 |  |  |  |  |  |
 | NOT RETRACTED  |  |  |  |  0  |
 |  |  |  |  |  |
 | FAIL *[1]  |  1 (3)  |  17  |  1  |  1  |
 |  |  |  |  |  |
 | NOT FAIL  |  |  |  |  0  |
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：757 AMM 飛機維護手冊 儀表 CHAPTER 31 - INSTRUMENTS 1(69)