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R  1-8 ∞ Label Identifier 
R  ------------------------------------------------------------------------------
R  9 ∞ SDI 
R  10 ∞ SDI 
R  ------------------------------------------------------------------------------
R  11-29 ∞ Spare 
R  ------------------------------------------------------------------------------
R  30 ∞ SSM 
R  31 ∞ SSM 
R  ------------------------------------------------------------------------------
R  32 ∞ Parity 
R  ------------------------------------------------------------------------------
2. TABLE 2_______
 A. PPU DATA DISPLAY.
 (1) When on the submenu pages SYSTEM DATA FLAP, the Line Key "1L" "PPU "
 is pressed, the named SFCC transmits the following page to the CFDS.
 |"""""""""""""""""""""""""""""""""""""|

 |  SFCC- X  |
 |  PPU DATA (DEG)  |
 1L  | DATE:  UTC:  |  1R
 | LH APPU  FPPU  RH APPU |
 2L  | XXX.X  XXX.X  XXX.X |  2R
 | ***HEX  ***HEX  ***HEX |
 3L  |  |  3R
 |  OTHER SFCC  |
 4L  | LH APPU  FPPU  RH APPU |  4R
 | XXX.X  XXX.X  XXX.X |
 5l  | ***HEX  ***HEX  ***HEX |  5R
 |  |
 6l  | <RETURN  PRINT> |

 """""""""""""""""""""""""""""""""""""""

 (2) The XXX.X fields are replaced with the decimal value of the synchro angle.
R (3) The *** fields are replaced with the hexadecimal value of the synchro R angle.
 (4) If no data is available then the decimal value is replaced with
 XXX.X.
 3. TABLE 3
_______
 A. Slat Operating System.
 (1) Mechanical and Electronic Interface Data.
 -------------------------------------------------------------------------------CONTROL LEVER SURFACE ANGLE SYHCHRO ANGLE POSITION APPU FPPU IPPU -------------------------------------------------------------------------------
Mech.Stop retr -2.81 deg 0 0 deg 0 deg 1 Auto 18 deg 222.77 deg 1 Norm 18 deg 222.77 deg 2 22 deg 272.27 deg 3 22 deg 272.27 deg FULL 27 deg 334.16 deg Mech. Stop ext 336. 97 deg
 NOTE : The APPUs should agree within 0.45 deg. At position 0
____ APPU/FPPU should agree within 0.9 deg., at positions 1, 2, 3 and FULL, the APPU/FPPU should agree within 1.3 deg.
 4. TABLE 4
_______
 A. WTB RESET Page.
 (1) When on the submenu pages SFCC-(1) (2) TEST/RESET the Line Key "1R" "WTB-RESET" is pressed, the named SFCC transmits the following page to the CFDS.

 (2) In line 3 "CAUTION: XXXX WILL MOVE" the "XXXX" field is replaced with the the word FLAPS in the amber colour code.

 (3) When on the WTB RESET instruction page the key 5L "START WTB RESET"is pressed.

 (4) The related WTB relays in the SFCC are reset and the result is

 

 |  SFCC- X  |
 |  --- WTB=RESET  |
 1L  | CAUTION:  XXXX  WILL  MOVE  |  1R
 | ENSURE  THAT  SURFACE  |
 2L  | MOVEMENT  IS  POSSIBLE  |  2R
 | WITHOUT  DANGER  TO  |
 3L  | PERSONNEL  OR  |  3R
 | AIRCRAFT  OR  |
 4L  | MECHANICAL  SYSTEM  |  4R
 |  |
 5l  | < START  WTB  RESET  |  5R
 |  |
 6l  | <RETURN  PRINT> |
 """""""""""""""""""""""""""""""""""""""

 transmitted to the CFDS as |"""""""""""""""""""""""""""""""""""""| | SFCC- X | | ---- WTB RESET |
 1L | | 1R | PERFORMED | 2L | | 2R | | 3L | | 3R | | 4L | | 4R | | 5l | | 5R
　
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