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 condition, turn off the hydraulic system, remove the
 eletrical connector D1710 from the slat bypass valve V10059
 (AMM 27-51-00) and manually position the valve to the bypass
 position. Then turn the hydraulic system back on and set the
 flap lever to the 5 position.
 
 GUN 001-008, 010, 101 POST-EO B531006;  ú 31-31-00
 GUN 051, 102-999  ú CONFIG 2 ú 06 Page 524 ú Sep 28/01

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 (d)  Set the L.E. slats back to the normal position.
 S 735-747-002
 (3)  Alternate Slats Position Test (a) On the tester, set the SUBFRAME to 2 and the WORD to 45. (b) On the P3 panel, set the L.E. flap switch to the in position. (c) Make sure that the BIT (DISCRETE) 1 shows a 1. (d) On the P3 panel, set the L.E. flap switch to the out position. (e) Make sure the BIT (DISCRETE) 1 shows a 0.
 S 865-842-002
 (4)  Remove the power from the left , right and center hydraulic system (AMM 29-11-00).

 AA. Brake Pressure Test
 S 735-725-002
 (1)  Do the brake pressure test that follows:
 (a)  
Pressurize the right hydraulic system and reservoir (AMM 29-11-00).

 (b)  
Make sure the EICAS is operational (AMM 31-41-00).

 (c)  
Push the ELEC/HYD switch on the EICAS MAINT panel on the right side panel, P61.

 (d)  
Make sure the parking brake is released.

 (e)  
On the tester, set the SUBFRAME to 0 and the WORD to 47.

 (f)  
Push the captain's left brake pedal to the full stop position.

 (g)  
Make sure the tester display shows the value shown in Table 501.

 NOTE: The value must agree with the nearest hydraulic system
____ pressure.
 NOTE: X = DON'T CARE
____
 
 GUN 001-008, 010, 101 POST-EO B531006;  ú 31-31-00
 GUN 051, 102-999  ú CONFIG 2 ú 06 Page 525 ú Sep 28/01

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MAINTENANCE MANUAL

 ~............................................................ | GUN 102-999 | | Table 501 | ..............................................................
 |  HYDRAULIC SYSTEM  |  |
 | (Pressure as displayed  |  TESTER  |
 |  on EICAS status page)  |  DISPLAY  |

 .............................................................. | 2300 | 52XX-60XX | .............................................................. | 2400 | 54XX-62XX | .............................................................. | 2500 | 55XX-63XX | .............................................................. | 2600 | 57XX-65XX | .............................................................. | 2700 | 61XX-67XX | .............................................................. | 2800 | 63XX-71XX | .............................................................. | 2900 | 65XX-74XX | .............................................................. | 3000 | 67XX-75XX | 2..........................….................................1
　
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本文鏈接地址：757 AMM 飛機維護手冊 儀表 CHAPTER 31 - INSTRUMENTS 1(93)