Inspection Plug Location
 Figure 201/TASK 27-51-00-991-001

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-51-00∞∞∞∞∞∞∞∞∞∞Page 289
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 (c) If water is found replace the defective rotary actuator as follows:

 - for actuator assembly 6205CM (6255CM) (Ref. AMM TASK 27-54-49-000-001) and (Ref. AMM TASK 27-54-49-400-001)

 - for actuator assembly 6211CM (6261CM) (Ref. AMM TASK 27-54-49-000-002) and (Ref. AMM TASK 27-54-49-400-002)

 - for actuator assembly 6221CM (6271CM) (Ref. AMM TASK 27-54-49-000-003) and (Ref. AMM TASK 27-54-49-400-003)

 - for actuator assembly 6233CM (6283CM) (Ref. AMM TASK 27-54-49-000-004) and (Ref. AMM TASK 27-54-49-400-004).

 (d) If no water is found, make sure that the WTB reset is done (Ref. para 4. A.(1)) and move the flaps (Ref. AMM TASK 27-50-00-866-008) and (Ref. AMM TASK 27-50-00-866-009).

 (e) While the flaps move do a check for incorrect noise at the WTB.

 (f) If there is an incorrect noise at the WTB, replace the BRAKE-L WING TIP (33CV) or BRAKE-R WING TIP (34CV) (Ref. AMM TASK 27-51-51-000-001) and (Ref. AMM TASK 27-51-51-400-001).

 (g) If there is no incorrect noise at the WTB, disconnect the transmission shafts on each side of the WTB (Ref. para (3)(f)).

 (4) Make sure that the WTB is easily turned, if it is not easily turned, replace the WTB (Ref. para (3)(f)).
 NOTE : The breakout torque of the WTB must not be more than 0.5 NM.
____

 (a) If no fault is found replace the rotary actuator 6211CM (6261CM) at flap track position 2, (Ref para (3)(c)).
 「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 290
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 Wrong Inhibit Sign From Cargo Door Yellow System.
 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE

_______
 CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.

 1. Possible Causes
_______________
 - RELAY-SCCB PWR SPLY 3811GX

 - TIME RELAY 3816GX

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM  31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST F/CTL Page ASM 29-24/01
 3. Fault Confirmation
__________________
 A. Test
 (1) Get access to the SYSTEM REPORT/TEST F/CTL page (Ref. AMM TASK 31-32-00-860-006).

 (2) Get access to the SFCC-2 flap discrete i/p status page: NOTE : The cargo door signal status is shown as follows:

____

 - sgoi: 0 = cargo door closed

 - sgoi: 1 = cargo door open

 (3) Make sure that the cargo doors are closed.
 4. Fault Isolation
_______________
 A. Procedure
 (1) If the SFCC-2 flap dicrete i/p status page shows sgoi: 1:
 (a) Do a check for 28VDC at the RELAY-SCCB PWR SPLY 3811GX connector pin X1 (Ref. ASM 29-24/01).

 (b) If there is no 28VDC replace the RELAY-SCCB PWR SPLY 3811GX.

 (c) If there is 28VDC replace the TIME RELAY 3816GX (Ref. ASM 2924/01).

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 (2) Do the test in para 3A. and make sure that the cargo door indications are correct.

 (3) Get access to the SFCC-2 system status flap, and make sure that the message 'inhibit signal from cargo yellow door system' is not shown.

 「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 292
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 Flap SFCS Status Message.
 1. Possible Causes_______________
 - Not applicable
 2. Job Set-up Information______________________
 Not Applicable
 3. Fault Confirmation__________________
 A. If the SFCS STATUS MAINTENANCE message has been shown on the ECAM. If there are no flap/slat system fault messages shown on the post flight report, maintenance steps are Not applicable.
　
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