(a)
Push ECS/MSG to set the format.
(b)
Push EVENT READ-AUTO to set the format.
(c)
Write down the EICAS messages shown on the non-volatile EICAS message list.
(d)
Push and hold the ERASE switch until the EICAS messages go out of view.
(e)
Do the last three steps again, until all the EICAS memory has been erased.
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S 865-013
(3) Move the EICAS computer select switch to the L position.
(a) Make sure the NOSE A/G DISAGREE, AIR/GND DISAGREE, NOSE A/G
SYS, and AIR/GND SYS messages are not shown on the EICAS.
S 865-014
(4) Move the EICAS computer select switch to the R position.
(a) Make sure the NOSE A/G DISAGREE, AIR/GND DISAGREE, NOSE A/G
SYS, and AIR/GND SYS messages are not shown on the EICAS.
S 965-015
(5) Install or remove the switch actuators or deactuators on the
proximity sensors as shown below:
~..........................................................
| SENSOR | LOCATION | ACTUATOR | DEACTUATOR |
............................................................
| S10067 | Nose Gear | Install | - - |
2.........…..............…..............…..................1
S 865-016
(6)
Make sure the NOSE A/G DISAGREE message is shown on the EICAS.
S 865-071
(7)
Make sure the NOSE A/G SYS message shows on the EICAS.
S 865-017
(8)
Move the EICAS computer select switch to the L position.
(a)
Make sure the NOSE A/G DISAGREE message is shown on the EICAS.
(b)
Make sure the NOSE A/G SYS message shows on the EICAS.
S 765-018
(9)
Use a volt/ohmmeter to measure the voltage between pins 6 (+ voltage) and 12 (ground). The connectors to be measured are in column A of Tables 1 and 2. The measured voltage of each connector must be the same as the voltage shown in column C1 of Table 1 and column B of Table 2.
S 865-019
(10)
Pressurize the left hydraulic system (Ref 29-11-00).
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本文鏈接地址：757 AMM 飛機維護手冊 起落架 CHAPTER 32 - LANDING GEAR 1(40)
