Loss of the Left Spoiler 1 Servo Valve Signal for the SEC 3
1. Possible Causes
_______________
- SEC-3 (1CE3)
- servo valve of the servo control (31CE1)
- wiring of the SV signal from the servo control (31CE1) to the SEC 3 (1CE3)
2. Job Set-up Information
______________________
A. Referenced Information
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REFERENCE DESIGNATION
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AMM 27-64-51-000-001 Removal of the Spoiler Servo-Control
R 31CE1(31CE2)/31CE3(31CE4)/31CE5(31CE6) AMM 27-64-51-400-001 Installation of the Spoiler Servo-Control
R 31CE1(31CE2)/31CE3(31CE4)/ 31CE5(31CE6) AMM 27-94-34-000-001 Removal of the SEC (1CE1,1CE2,1CE3) AMM 27-94-34-400-001 Installation of the SEC (1CE1,1CE2,1CE3) AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) AMM 29-10-00-863-001 Pressurize the Green Hydraulic System AMM 29-10-00-864-001 Depressurize the Green Hydraulic System ASM 27-94/04
3. Fault Confirmation
__________________
A. Job Set-Up
(1) Pressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-863-001).
(2) Pull the speedbrake control lever (7CE) up to the armed position on the panel 11VU.
B. Test
(1) Do the BITE test of the EFCS (Ground Scanning) (Ref. AMM TASK 27-96-00-740-001).
C. Put the aircraft back to its initial configuration.
(1) Depressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001).
(2) Disarm the speedbrake control lever (7CE) on the panel 11VU.
「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 ∞∞27-60-00∞∞∞∞∞∞∞∞∞∞Page 226
Nov 01/02 CES
4. Fault Isolation
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A. If the BITE test gives the maintenance message: L SPLR 1 SERVO VLV 31CE1 OR OUTPUT FROM SEC 3
- replace the SEC-3 (1CE3), (Ref. AMM TASK 27-94-34-000-001) and (Ref. AMM TASK 27-94-34-400-001).
(1) If the fault continues:
- replace the servo valve of the servo control (31CE1), (Ref. AMM TASK 27-64-51-000-001) and (Ref. AMM TASK 27-64-51-400-001).
NOTE : The resistance must be 500 ohms +/- 10 %.
____
(2) If the fault continues:
- do a check and repair the wiring of the SV signal from the servo control (31CE1) to the SEC 3 (1CE3), (Ref. ASM 27-94/04).
B. Do the test given in Para. 3.
Loss of the Right Spoiler 1 Servo Valve Signal for the SEC 3
1. Possible Causes
_______________
- SEC-3 (1CE3)
- servo valve of the servo control (31CE2)
- wiring of the SV signal from the servo control (31CE2) to the SEC 3 (1CE3)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 27-64-51-000-002 Removal of the Servo-Valve from the Spoiler
Servo-Control
AMM 27-64-51-400-002 Installation of the Servo-Valve on the Spoiler
Servo-Control
AMM 27-94-34-000-001 Removal of the SEC (1CE1,1CE2,1CE3)
AMM 27-94-34-400-001 Installation of the SEC (1CE1,1CE2,1CE3)
R AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) AMM 29-10-00-863-001 Pressurize the Green Hydraulic System AMM 29-10-00-864-001 Depressurize the Green Hydraulic System ASM 27-94/04
3. Fault Confirmation
__________________
A. Job Set-Up
(1) Pressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-863-001).
(2) Pull the speedbrake control lever (7CE) up to the armed position on the panel 11VU.
B. Test
(1) Do the BITE test of the EFCS (Ground Scanning) (Ref. AMM TASK 27-96-00-740-001).
C. Put the aircraft back to its initial configuration.
(1) Depressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001).
(2) Disarm the speedbrake control lever (7CE) on the panel 11VU.
「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 ∞∞27-60-00∞∞∞∞∞∞∞∞∞∞Page 228
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 2(35)
