Wrong Spoiler Position Indication A320

1. Possible Causes:

-SEC-1 (1CE1)

-SEC-2 (1CE2)

-SEC-3 (1CE3)

-SERVO CTL-SPLR1, L G (31CE1)

-SERVO CTL-SPLR1, R G (31CE2)

-SERVO CTL-SPLR2, L Y (31CE3)

-SERVO CTL-SPLR2, R Y (31CE4)

-SERVO CTL-SPLR3, L B (31CE5)

-SERVO CTL-SPLR3, R B (31CE6)

-SERVO CTL-SPLR4, L Y (31CE7)

-SERVO CTL-SPLR4, R Y (31CE8)

-SERVO CTL-SPLR5, L G (31CE9)

-SERVO CTL-SPLR5, R G (31CE10)

-wiring of the LVDT POS Signal

2. Job Set-up Information

A. Referenced Information

REFERENCEDESIGNATION
Ref. AMM 24-41-00-861-002Energize the Aircraft Electrical Circuits from the External Power
Ref. AMM 27-64-51-000-004Removal of the Spoiler Servo Control
Ref. AMM 27-64-51-400-004Installation of the Spoiler Servo Control
Ref. ASM 27-94-02
Ref. ASM 27-94-04
Ref. AMM 27-94-34-000-001Removal of the SEC
Ref. AMM 27-94-34-400-001Installation of the SEC
Ref. AMM 29-10-00-863-002Pressurize the Yellow Hydraulic System with a Hydraulic Ground Power-Cart
Ref. AMM 29-10-00-863-003Pressurize the Blue Hydraulic System with a Hydraulic Ground Power-Cart
Ref. AMM 29-10-00-864-002Depressurize the Yellow Hydraulic System
Ref. AMM 29-10-00-864-003Depressurize the Blue Hydraulic System
Ref. AMM 29-23-00-863-001Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump
Ref. AMM 29-23-00-864-001Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU
Ref. AMM 31-60-00-860-001EIS Start Procedure
Ref. AMM 31-60-00-860-002EIS Stop Procedure

3. Fault Confirmation

SUBTASK 27-60-00-860-138-A

A. Job Set-up

(1) Energize the aircraft electrical circuits Ref. AMM 24-41-00-861-002.

(2) On the panel 23VU, make sure that the FLT CTL/SEC 1 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legends are off).

(3) On the panel 24VU, make sure that the FLT CTL/ SEC 2 and the FLT CTL/SEC3 pushbutton switches are pushed (on these pushbutton switches, the OFF and FAULT legends are off).

(4) On the center pedestal, make sure that the slats and flaps control lever is in the 0 position, and the SPEED BRAKE control lever is set to RET.

(5) Make sure that the two side stick controllers are in the neutral position.

(6) Do the EIS start procedure (upper ECAM DU and lower ECAM DU only) Ref. AMM 31-60-00-860-001.

(7) Pressurize the Green, Blue and Yellow hydraulic systems Ref. AMM 29-23-00-863-001, Ref. AMM 29-10-00-863-003 and Ref. AMM 29-10-00-863-002.

SUBTASK 27-60-00-710-052-A

B. Test

ACTIONRESULT
1.On the center pedestal, on the ECAM control panel:-push the F/CTL pushbutton switchOn the lower ECAM display unit:-the F/CTL page comes into view.-the triangle of a spoiler does not show the retracted position.

SUBTASK 27-60-00-860-139-A

C. Close-up

(1) Depressurize the Green, Blue and Yellow hydraulic systems Ref. AMM 29-23-00-864-001, Ref. AMM 29-10-00-864-003 and Ref. AMM 29-10-00-864-002.

(2) Do the EIS stop procedure Ref. AMM 31-60-00-860-002.

4. Fault Isolation

SUBTASK 27-60-00-810-100-B

A. If the test confirms the fault:

— replace the SEC in relation to the wrong indication Ref. AMM 27-94-34-000-001 and Ref. AMM 27-94-34-400-001.

for spoilers 3 and 4, replace the SEC-1 (1CE1)

for spoiler 5, replace the SEC-2 (1CE2)

for spoilers 1 and 2, replace the SEC-3 (1CE3).

(1) If the fault continues:

— replace the Spoiler Servo Control in relation to the wrong indication.

SERVO CTL-SPLR1, L G (31CE1), SERVO CTL-SPLR1, R G (31CE2), for spoiler 1

SERVO CTL-SPLR2, L Y (31CE3), SERVO CTL-SPLR2, R Y (31CE4), for spoiler 2

SERVO CTL-SPLR3, L B (31CE5), SERVO CTL-SPLR3, R B (31CE6), for spoiler 3

SERVO CTL-SPLR4, L Y (31CE7), SERVO CTL-SPLR4, R Y (31CE8) for spoiler 4

SERVO CTL-SPLR5, L G (31CE9), SERVO CTL-SPLR5, R G (31CE10) for spoiler 5

Ref. AMM 27-64-51-000-004 and Ref. AMM 27-64-51-400-004.

(2) If the fault continues:

— do a check and repair the wiring of the LVDT POS Signal from the spoiler servocontrol to the SEC COM and MON parts Ref. ASM 27-94-02, Ref. ASM 27-94-04.

5. Close-up

SUBTASK 27-60-00-710-053-A

A. Do the test given in Para 3.

Read me first

All instructions and limitations given in those documents that relate to the resetting of systems both on the ground and in the air must be respected. No reset should be attempted without a thorough appreciation of the technical ramifications. No more than one computer should be reset at any one time. No reset should be attempted in flight unless specifically permitted by the QRH. Maintenance messages remaining after a reset require engineering investigation.

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