- if the source of the message is BSCU SYS2, do a check and repair the wiring from the BSCU (10GG) to the transmitter unit (9GG) pins AA/5A, 1A, 7A to pins A/P, H, Y (Ref. ASM 32-42/01).
(4) If the fault continues and the TROUBLE SHOOTING DATA gives the fault code 0F:
- if the source of the message is BSCU SYS1, do a check and repair the wiring from the BSCU (10GG) to the transmitter unit (9GG) pins AA/4K, 2K, 8K to pins A/B, K, V (Ref. ASM 32-42/01).
- if the source of the message is BSCU SYS2, do a check and repair the wiring from the BSCU (10GG) to the transmitter unit (9GG) pins AA/4A, 2A, 8A to pins A/D, J, Z (Ref. ASM 32-42/01).
(5) If the fault continues and the TROUBLE SHOOTING DATA gives the fault code 10:
- if the source of the message is BSCU SYS1, do a check and repair the wiring from the BSCU (10GG) to the transmitter unit (9GG) pins AA/6K, 2K, 8K to pins A/N, K, V (Ref. ASM 32-42/01).
- if the source of the message is BSCU SYS2, do a check and repair the wiring from the BSCU (10GG) to the transmitter unit (9GG) pins AA/6A, 2A, 8A to pins A/R, J, Z (Ref. ASM 32-42/01).
R **ON A/C ALL
B. Test
(1) Do the test given in Para. 3.A.
TASK 32-42-00-810-839
No Braking of the Wheels during the Landing Gear Retraction
1. Possible Causes
_______________
- LEVER-L/G NORM CTL (6GA)
- BSCU (10GG)
- wiring from the L/G Normal control lever (6GA) to the BSCU (10GG)
- wiring from the L/G Normal control lever (6GA) pin A/H to the ground terminal
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 32-31-11-000-001 Removal of the Landing Gear Normal Control lever (6GA) AMM 32-31-11-400-001 Installation of the Landing Gear Normal Control Lever (6GA) AMM 32-42-00-710-004 Operational Test of the Automatic Braking when the Landing Gear is retracted AMM 32-42-34-000-001 Removal of the Braking/Steering Control Unit (BSCU) (10GG) AMM 32-42-34-400-001 Installation of the Braking/Steering Control Unit (BSCU) (10GG) ASM 32-42/01
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the automatic braking when the landing gear is retracted (Ref. AMM TASK 32-42-00-710-004).
(2) Make sure that the brake unit pistons do not come out of their housings.
4. Fault Isolation
_______________
A. If the test confirms the fault:
- replace the LEVER-L/G NORM CTL (6GA) (Ref. AMM TASK 32-31-11-000-001) and (Ref. AMM TASK 32-31-11-400-001).
(1) If the fault continues:
- replace the BSCU (10GG) (Ref. AMM TASK 32-42-34-000-001) and (Ref. AMM TASK 32-42-34-400-001).
「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 ∞∞32-42-00∞∞∞∞∞∞∞∞∞∞Page 262
Feb 01/04R CES
(2) If the fault continues:
- do a check for a ground signal at the L/G Normal control lever (6GA) pin A/H (Ref. ASM 32-42/01).
(a) If there is a ground signal:
- do a check and repair the wiring from the L/G Normal control lever (6GA) to the BSCU (10GG) pin A/B to pin AA/12E.
(b) If there is no ground signal:
- repair the wiring from the L/G Normal control lever (6GA) pin A/H to the ground terminal.
B. Test Do the test given in Para. 3.A.(1).
「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 ∞∞32-42-00∞∞∞∞∞∞∞∞∞∞Page 263
Feb 01/04R
CES
TASK 32-42-00-810-840
Loss of the Pin Programming Data of the BSCU
1. Possible Causes
_______________
- BSCU (10GG)
- wiring of the PIN PROGRAMMING of the BSCU (10GG)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 32-42-34-000-001 Removal of the Braking/Steering Control Unit (BSCU) (10GG) AMM 32-42-34-400-001 Installation of the Braking/Steering Control Unit
(BSCU) (10GG)
AMM 32-46-00-740-001 BITE Test of the BSCU
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 起落架 LANDING GEAR 1(117)
