A320 Trouble Shooting Manual 排故手册 飞行操纵 2(25)

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R  31 ∞ SSM 
R  ------------------------------------------------------------------------------
R  32 ∞ Parity 
R  ------------------------------------------------------------------------------
R  J. LABEL 066 SPARE TEST DATA WORD 
R  ------------------------------------------------------------------------------
R  Bit ∞ Function 
R  Number ∞ 
R  ------------------------------------------------------------------------------
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  ------------------------------------------------------------------------------

 3. TABLE 3
_______

 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.

 (3) The *** fields are replaced with the hexadecimal value 0f the synchro angle.

 (4) If no data is available then the decimal value is replaced with

 XXX.X.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 313
 Feb 01/05R
 CES

 4. TABLE 4
_______

 A. A320 Flap Operating System.
 (1) Mechanical and Electronic Interface Data.
 -------------------------------------------------------------------------------CONTROL LEVER SURFACE ANGLE SYHCHRO ANGLE POSITION APPU FPPU IPPU -------------------------------------------------------------------------------
Mech.Stop retr -1.91 deg 0 0 deg 0 deg 1 Auto 0 deg 0 deg 1 Norm 10 deg 120.22 deg 2 15 deg 145.51 deg 3 20 deg 168.34 deg
 FULL Configuration Pin Prog. Operation Mode 3 35 deg 231.24 deg Configuration Pin Prog. Operation Mode 4
 40 deg 251. 91 deg Mech. Stop ext 253. 91 deg Relief 30 deg1) 210. 68 deg Relief 35 deg1) 231. 24 deg
 NOTE : The APPUs should agree within 0.45 deg. At position 0 the
____ APPU/FPPU should agree within 0.9 deg. At positions 1, 2, 3 and FULL, the APPU/FPPU should agree within 1.3 deg.
 B. A321 Flap Operating System.
 (1) Mechanical and Electronic Interface Data.
 -------------------------------------------------------------------------------CONTROL LEVER SURFACE ANGLE SYHCHRO ANGLE POSITION APPU FPPU IPPU -------------------------------------------------------------------------------
Mech.Stop retr -3.73 deg 0 0 deg 0 deg 1 Auto 0 deg 0 deg 1 Norm 10 deg 153.09 deg 2 14 deg 179.21 deg 3 21 deg 220.17 deg
 FULL 25 deg 242.12 deg Mech. Stop ext deg Relief 30 deg1) 242.12 deg
 NOTE : The APPUs should agree within 0.45 deg. At position 0 the
____ APPU/FPPU should agree within 0.9 deg. At positions 1, 2, 3 and FULL, the APPU/FPPU should agree within 1.3 deg.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 314
　
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