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时间:2011-03-28 18:30来源:蓝天飞行翻译 作者:航空
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 AMM 31-38-22-400-001 Installation of the MDDU (1TD)
 ASM 31-38/01

 3. Fault Confirmation

__________________
 A. Do the BITE test of the Multipurpose Disk Drive Unit (MDDU) (Ref. AMM TASK 31-38-00-740-002).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message DMU(1TV)/MDDU(1TD):
 (1) Replace the MDDU (1TD) (Ref. AMM TASK 31-38-22-000-001) and (Ref. AMM TASK 31-38-22-400-001).

 (2) If the fault continues:


 - do a check and repair the wiring from the MDDU (1TD) connector A/24, 25 to the first terminal block 1813VT (Ref. ASM 31-38/01).
 B. Do the test given in Para. 3.A.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 062-099, 106-149, 151-199, 201-299, ∞∞31-38-00∞∞∞∞∞∞∞∞∞∞Page 222
 301-399, 401-499, Aug 01/05 CES

 


 Loss of the MDDU Interface with the ATSU
 1. Possible Causes
_______________
 - MDDU (1TD)

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-38-00-740-002 BITE Test of the Multipurpose Disk Drive Unit (MDDU)
 AMM 31-38-22-000-001 Removal of the MDDU (1TD)
 AMM 31-38-22-400-001 Installation of the MDDU (1TD)
 ASM 31-38/01

 3. Fault Confirmation

__________________
 A. Do the BITE test of the Multipurpose Disk Drive Unit (MDDU) (Ref. AMM TASK 31-38-00-740-002).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message ATSU(1TX1)/MDDU(1TD):
 (1) Replace the MDDU (1TD) (Ref. AMM TASK 31-38-22-000-001) and (Ref. AMM TASK 31-38-22-400-001).

 (2) If the fault continues:


 - do a check and repair the wiring from the MDDU (1TD) connector A/24, 25 to the first terminal block 1813VT (Ref. ASM 31-38/01).
 B. Do the test given in Para. 3.A.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 062-099, 106-149, 151-199, 201-299, ∞∞31-38-00∞∞∞∞∞∞∞∞∞∞Page 223
 301-399, 401-499, Aug 01/05 CES

 

R **ON A/C 106-149, 159-199, 210-299, 301-399, 401-499,
 TASK 31-38-00-810-821
 Loss of the DLRB signal to the FDIMU (FDIU Part)
 1. Possible Causes
_______________
 - ROUTING BOX-DATA LOADING (102TD)

 - DMU/FDIU (FDIMU) (10TV)

 - wiring


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
AMM 31-33-00-710-013 FDIMU (10TV) DFDRS Software Load Procedure
 AMM 31-38-34-000-001 Removal of the Data Loading Routing Box (102TD)
 AMM 31-38-34-400-001 Installation of the Data Loading Routing Box (102TD)
 ASM 31-38/01

 3. Fault Confirmation

__________________
 A. Load the DFDRS software of the FDIMU (Ref. AMM TASK 31-33-00-710-013).
 4. Fault Isolation
_______________
 A. If the fault is identified by the crew observation:
 FDR SYS uploading is not possible.

 (1) Do a check for of the aircraft wiring between the ROUTING BOX-DATA LOADING (102TD) and DMU/FDIU (FDIMU) (10TV) (Ref. ASM 31-38/01):

 - A/25 (102TD) to pin AA/14F (10TV).

 (2) Do a check for of the aircraft wiring between the DMU/FDIU (FDIMU) (10TV) and the ROUTING BOX-DATA LOADING (102TD):

 (a) pin AA/12J, 12K (10TV) to the pin B/12, 28 (102TD).

 (b) pin AB/12C, 12D (10TV) to the pin A/42, 9 (102TD).

 

 (3) if the fault continues:


 - replace the ROUTING BOX-DATA LOADING (102TD) (Ref. AMM TASK 31-38-34-000-001) and (Ref. AMM TASK 31-38-34-400-001).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 106-149, 159-199, 210-299, 301-399, ∞∞31-38-00∞∞∞∞∞∞∞∞∞∞Page 224
 401-499, Aug 01/05 CES

 

 B. Do the test given in Para. 3.A.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 106-149, 159-199, 210-299, 301-399, ∞∞31-38-00∞∞∞∞∞∞∞∞∞∞Page 225
 
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