(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

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 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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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