Slat System Uncommanded Movement
TASK 27-81-00-810-817-A
Slat System Uncommanded Movement
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 27-81-00-740-058-A
Subtask 27-81-00-810-066-A
Subtask 27-81-00-942-066-A
[Rev.8 from Aug 2018]
2026.04.04 04:27:48 UTC
Slat System Uncommanded Movement
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 27-54-00-710-002 | Operational Test of the Flap and Slat Systems |
| AMM 27-80-00-869-004 | Reset of the Wing Tip Brake (WTB) of the Slat System on the Ground |
| AMM 27-81-00-710-001 | Operational Test of the Wing-Tip Brake and the Pressure-Off Brake |
| AMM 27-81-19-000-001 | Removal of the Feed Back Position Pick-Off Unit |
| AMM 27-81-19-400-001 | Installation of the Feed Back Position Pick-Off Unit |
| AMM 27-84-51-000-001 | Removal of the Power Control Unit of the Slat System |
| AMM 27-84-51-400-001 | Installation of the Power Control Unit of the Slat System |
| AMM 27-84-52-000-001 | Removal of the Pressure-Off Brake of the Slat Power Control Unit |
| AMM 27-84-52-400-001 | Installation of the Pressure-Off Brake of the Slat Power Control Unit |
Subtask 27-81-00-740-058-A
A. For the fault confirmation do the fault isolation.
4. Fault IsolationSubtask 27-81-00-810-066-A
A. Procedure
(1) Do the reset of the WTB's AMM 27-80-00-869-004.
(2) Do the operational test of the flap and slat system, AMM 27-54-00-710-002.
(a) If failure is detected, replace the FPPU-SLAT [28CV] , AMM 27-81-19-000-001 and AMM 27-81-19-400-001.
(b) If fault continues, replace the SLAT-PCU [6001CM] , AMM 27-84-51-000-001and AMM 27-84-51-400-001.
(3) If the fault cannot be reproduced on ground, do the test that follows:
(a) Do the operational test of the wing tip brake and the pressure-off brake AMM 27-81-00-710-001 to find the defective system.
(b) Replace the applicable Pressure-off Brake , AMM 27-84-52-000-001 and AMM 27-84-52-400-001.
5. Close-up(1) Do the reset of the WTB's AMM 27-80-00-869-004.
(2) Do the operational test of the flap and slat system, AMM 27-54-00-710-002.
(a) If failure is detected, replace the FPPU-SLAT [28CV] , AMM 27-81-19-000-001 and AMM 27-81-19-400-001.
(b) If fault continues, replace the SLAT-PCU [6001CM] , AMM 27-84-51-000-001and AMM 27-84-51-400-001.
(3) If the fault cannot be reproduced on ground, do the test that follows:
(a) Do the operational test of the wing tip brake and the pressure-off brake AMM 27-81-00-710-001 to find the defective system.
(b) Replace the applicable Pressure-off Brake , AMM 27-84-52-000-001 and AMM 27-84-52-400-001.
Subtask 27-81-00-942-066-A
A. Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Subtask 27-81-00-860-067-A B. Put the aircraft back to its initial configuration.