1. Possible Causes
_______________
- SEC-2 (1CE2)
- wiring of the ANI 2-7 signal from the SEC 2 (1CE2) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
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 27-96-00-710-020 Operational Test of the Side Stick Assembly
(Activation for the BITE Test) R AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) ASM 27-94/03
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the side stick assembly (activation for the BITE test) (Ref. AMM TASK 27-96-00-710-020).
(2) Do the BITE test of the EFCS (Ground Scanning) (Ref. AMM TASK 27-96-00-740-001).
4. Fault Isolation
_______________
A. If the BITE test gives the maintenance message:
SEC2 COM OR WIRING FROM R SPLR5 POS XDCR 31CE10
or
SEC2 MON OR WIRING FROM R SPLR5 POS XDCR 31CE10
- replace the SEC-2 (1CE2), (Ref. AMM TASK 27-94-34-000-001) and (Ref. AMM TASK 27-94-34-400-001).
(1) If the fault continues:
- do a check and repair the wiring of the ANI 2-7 signal from the SEC 2 (1CE2) to the first terminal block COM part or MON part as shown in the maintenance message (Ref. ASM 27-94/03).
B. Do the tests given in Para. 3.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞27-60-00∞∞∞∞∞∞∞∞∞∞Page 279
May 01/00 CES Failure of the Right Spoiler 5 Position Transducer
1. Possible Causes
_______________
- SERVO CTL-SPLR5, R G (31CE10)
- wiring of the POS XDCR SPLY signal from the servo control (31CE10) to the first terminal block
- wiring of the POS XDCR V1, V2 signals from the servo control (31CE10) to the first terminal block
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
27-90-00-810-804 Loss of the ACS2 Signal of the SEC2 MON Side
AMM 27-64-52-000-006 Removal of the Spoiler Servo-Control 32CE4
AMM 27-64-52-400-006 Installation of the Spoiler Servo-Control 32CE4
AMM 27-96-00-710-020 Operational Test of the Side Stick Assembly
(Activation for the BITE Test) R AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) ASM 27-94/03
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the side stick assembly (activation for the BITE test) (Ref. AMM TASK 27-96-00-710-020).
(2) Do the BITE test of the EFCS (Ground Scanning) (Ref. AMM TASK 27-96-00-740-001).
(a) If the ground scanning gives the maintenance message: R SPLR5 POS XDCR 31CE10
- refer to the Para. Fault Isolation.
(b) If the ground scanning gives the maintenance messages: R SPLR5 POS XDCR 31CE10 L SPLR5 POS XDCR 31CE9
- refer to this procedure (Ref. TASK 27-90-00-810-804).
4. Fault Isolation
_______________
A. If the BITE test gives the maintenance message: R SPLR5 POS XDCR 31CE10
- replace the SERVO CTL-SPLR5, R G (31CE10), (Ref. AMM TASK 27-64-52-000-006) and (Ref. AMM TASK 27-64-52-400-006).
NOTE : The resistance of primary and secondary windings must be between
____
30 ohms and 500 ohms.
(1) If the fault continues:
- do a check and repair the wiring of the POS XDCR SPLY signal from the servo control (31CE10) to the first terminal block, (Ref. ASM 27-94/03).
(2) If the fault continues:
- do a check and repair the wiring of the POS XDCR V1, V2 signals from the servo control (31CE10) to the first terminal block, (Ref. ASM 27-94/03).
B. Do the tests given in Para. 3.
Loss of the Left Spoiler 5 Servo Valve Signal for the SEC 2
1. Possible Causes
_______________
- SEC-2 (1CE2)
- servo valve of the servo control (31CE9)
- wiring of the SV signal from the servo control (31CE9) to the SEC 2 (1CE2)
2. Job Set-up Information
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 飛行操縱 2(51)
