1. Possible Causes
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- SFCC-1 (21CV)
- SFCC-2 (22CV)
- POWER CONTROL UNIT (6201CM)
- aircraft wiring
2. Job Set-up Information
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A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 27-51-00-710-001 Operational Test of the Wing Tip Brake and the
Pressure Off Brake AMM 27-51-34-000-001 Removal of the SFCC (21CV,22CV) AMM 27-51-34-400-001 Installation of the SFCC (21CV,22CV) AMM 27-54-51-000-001 Removal of the Power Control Unit 6201CM of the Flap
System AMM 27-54-51-400-001 Installation of the Power Control Unit 6201CM of the Flap System
3. Fault Confirmation
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A. Test
(1) Do an operational test of the wing-tip brake and the pressure-off brake (Ref. AMM TASK 27-51-00-710-001):
- if the test does not complete in less than 2 minutes do the fault isolation procedure in Para. 4.
- if the test is OK, no more maintenance work is necessary.
4. Fault Isolation
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A. Procedure
(1) Abort the test as follows:
(a) Reset the circuit breaker of the channel on test.
(2) Interchange the SFCCs (Ref. AMM TASK 27-51-34-000-001) and (Ref. AMM TASK 27-51-34-400-001).
(a) Do the test in Para. 3. A.
- if the test is OK, do step (3)
- if the test does not complete, do step (4).
「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 A215
May 01/05R CES
(3) Replace the unserviceable SFCC-1 (21CV) or SFCC-2 (22CV) that was the source of the initial fault.
(a) Do the test in Para. 3. A.
- if the test does not complete, do the next step.
(4) Replace the POWER CONTROL UNIT (6201CM) (Ref. AMM TASK 27-54-51-000-001) and (Ref. AMM TASK 27-54-51-400-001).
(a) Do the test in Para. 3. A:
- if the test does not complete, do the next step.
(5) Do a check of the aircraft wiring between the applicable SFCC and the PCU:
- do the repair.
(a) Do the test in Para. 3. A.
FLAPS ELECTRICAL CONTROL AND MONITORING - TASK SUPPORTING DATA
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1. TABLE 1
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A. The DISCRETE I/P STATUS page diplay for the CSU Track Switch Bank A and B R comparison checks.
------------------------------------------------------------------------------SFCC=(1) or (2) ZZZZ DISCRETE I/P STATUS
------------------------------------------------------------------------------CSU TRACK 12345 SWITCH BANK A : ..... SWITCH BANK B : ..... DISCRETE I/P 1 : %%%%%%%% DISCRETE I/P 2 : %%%%%%%% DISCRETE I/P 3 : %%%%%%%% DISCRETE I/P 4 : %%%%%%%% XXXX XXXXX XXXXXXXX XXXX YYY YYYY YYYYY YYYY AOG : * A/C:???? SGOI : . <RETURN> <PRINT>
Explanation: Where the * = FLAP 1 or 2 (dependent on the selection) Where the ZZZZ is = SLAT or FLAP Where the XX------XX is = FLAP RELIEF ENABLED.
or = FLAP RELIEF DISABLED. or = FLAP RELIEF CODING FAIL.
Where the YY------YY is = MAX FLAP 35 DEG (CMF).
or = MAX FLAP 40 DEG (IAE).
or = MAX FLAP CODING FAIL.
Where the . is function set (1) or function reset (0).
Where the % is a logic 1 or a logic 0 as given by the input circuit.
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 2(19)
