- TU 01R is the first tapping unit on the RH side,
- TU 04R is the forth tapping unit on the RH side.
B. Do the test as given in Para. 3.
TASK 23-36-00-810-812
SCU uses own Default Layout
1. Possible Causes
_______________
- SYSTEM CONTROL UNIT (11MH)
- DIR-CIDS, 1 (101RH)
- MODULE-CABIN ASSIGNMENT (115RH)
- aircraft wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 23-36-00-740-002 BITE Test of the Passenger Entertainment (Video) AMM 23-73-19-000-001 Removal of the Cabin Assignment Module (115RH) AMM 23-73-19-400-001 Installation of the Cabin Assignment Module (115RH) ASM 23-36/01
3. Fault Confirmation
__________________
A. If the BITE test of the video sytem gives the maintenance message: DEF LAY
- do the BITE test of the video system again (Ref. AMM TASK 23-36-00-740-002)
4. Fault Isolation
_______________
A. Maintenance Action
(1) If the BITE test gives the maintenance message: DEF LAY
- do a check and repair the aircraft wiring between the SYSTEM CONTROL UNIT (11MH) connector J1C/10 thru J1C/13, and the DIR-CIDS, 1 (101RH) connector AA/F8, G8, J13 and K13 respectively (Ref. ASM 23-36/01).
(2) If the fault continues:
- replace the MODULE-CABIN ASSIGNMENT (115RH) (Ref. AMM TASK 23-73-19-000-001) and (Ref. AMM TASK 23-73-19-400-001)
B. Do the test as given in Para. 3.
「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 : 151-199, 201-210, ∞∞23-36-00∞∞∞∞∞∞∞∞∞∞Page 217
Aug 01/02 CES TASK 23-36-00-810-813
SCU uses own Invalid Layout
1. Possible Causes
_______________
- SYSTEM CONTROL UNIT (11MH)
- DIR-CIDS, 1 (101RH)
- MODULE-CABIN ASSIGNMENT (115RH)
- aircraft wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 23-36-00-740-002 BITE Test of the Passenger Entertainment (Video) AMM 23-73-19-000-001 Removal of the Cabin Assignment Module (115RH) AMM 23-73-19-400-001 Installation of the Cabin Assignment Module (115RH) ASM 23-36/01
3. Fault Confirmation
__________________
A. If the BITE test of the video sytem gives the maintenance message: INV LAY
- do the BITE test of the video system again (Ref. AMM TASK 23-36-00-740-002)
4. Fault Isolation
_______________
A. Maintenance Action
(1) If the BITE test gives the maintenance message: INV LAY
- do a check and repair the aircraft wiring between the SYSTEM CONTROL UNIT (11MH) connector J1C/10 thru J1C/13, and the DIR-CIDS, 1 (101RH) connector AA/F8, G8, J13 and K13 respectively (Ref. ASM 23-36/01).
(2) If the fault continues:
- replace the MODULE-CABIN ASSIGNMENT (115RH) (Ref. AMM TASK 23-73-19-000-001) and (Ref. AMM TASK 23-73-19-400-001).
B. Do the test as given in Para. 3.
「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 : 151-199, 201-210, ∞∞23-36-00∞∞∞∞∞∞∞∞∞∞Page 218
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