(e)
Push the LSK adjacent to <DFCS to show the DFCS BITE TEST LINE MAINT 1/2 page.
(f)
Push the NEXT PAGE key on the CDU keyboard to show the DFCS BITE TEST OVERNIGHT MAINT 2/2 page.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
22-11-01
ú ú 08 Page 533 ú Jul 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
(g)
Push the LSK adjacent to <SENSOR VALUES to show the Sensor Values Test Index.
(h)
Push the LSK adjacent to <DISCRETE INPUT WORDS to get access to the Discrete Input Words Index.
(i)
Push the LSK adjacent to <DISINWD 06.
(j)
Do these steps for each condition in column 1 of the table shown below: 1) Set the EFIS switch to the position shown in column 2. 2) Set the NAV switch to position shown in column 3. 3) Make sure the status of PIN A and B are the same as shown
in column 4.
~.............................................................................. | COL. 1 | COL. 2 | COL. 3 | COL. 4 | ................................................................................ |CONDITION| EFIS SW | NAV SW | DISINWD 06 | | | | ............................................ | | | | PIN | FCC-A | FCC-B | ................................................................................
| 1 | BOTH ON 1 | BOTH ON 1 | J4A-01 | GD | OP |
| 2 | BOTH ON 1 | NORMAL | J4A-01 | GD | OP |
| 3 | BOTH ON 1 | BOTH ON 2 | J4A-01 | OP | GD |
| 4 | BOTH ON 2 | BOTH ON 1 | J4A-01 | GD | OP |
| 5 | BOTH ON 2 | NORMAL | J4A-01 | OP | GD |
| 6 | BOTH ON 2 | BOTH ON 2 | J4A-01 | OP | GD |
2.........…............…............…...................…...........…..........1
(k)
Push the LSK adjacent to <CONTINUE to show the second page of the DISINWD 06.
(l)
Do these steps for each condition in column 1 of the table shown below: 1) Set the EFIS switch to the position shown in column 2. 2) Set the NAV switch to the position shown in column 3. 3) Make sure the status of PIN A and B are the same as shown
in column 4.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH EFIS ú
22-11-01
ú ú 08 Page 534 ú Jul 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
~..............................................................................
| COL. 1 | COL. 2 | COL. 3 | COL. 4 |
................................................................................ ú |CONDITION| EFIS SW | NAV SW | DISINWD 06 |
| | | ............................................
| | | | PIN | FCC-A | FCC-B |
................................................................................
| 1 | BOTH ON 1 | BOTH ON 1 | J4B-11 | OP | GD |
| 2 | BOTH ON 1 | NORMAL | J4B-11 | OP | GD |
| 3 | BOTH ON 1 | BOTH ON 2 | J4B-11 | GD | OP |
| 4 | BOTH ON 2 | BOTH ON 1 | J4B-11 | OP | GD |
| 5 | BOTH ON 2 | NORMAL | J4B-11 | GD | OP |
| 6 | BOTH ON 2 | BOTH ON 2 | J4B-11 | GD | OP |
2.........…............…............…...................…...........…..........1
(m) Do these steps for each condition in column 1 of the table shown below: 1) Set the EFIS switch to the NORMAL position. 2) Set NAV switch to the NORMAL position. 3) Set the AUTO/MANUAL switch on the NAV control panel No. 1
to the position as shown in column 2. 4) Set the AUTO/MANUAL switch on the NAV control panel No. 2 to the position as shown in the column 3. 5) Make sure the status of PIN A and B are the same as shown in column 4.
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本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 自動飛行 AUTOFLIGHT 1(131)
