Green Hydraulic System Low Pressure/Overheat Caused by User System Fault
TASK 29-11-00-810-816-A
Green Hydraulic System Low Pressure/Overheat Caused by User System Fault
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 29-11-00-700-050-A
Subtask 29-11-00-810-072-A
Subtask 29-11-00-942-050-A
[Rev.8 from Aug 2018]
2026.04.04 04:29:21 UTC
Green Hydraulic System Low Pressure/Overheat Caused by User System Fault
1. Possible Causes
- user system component internal leak
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 29-11-00-810-802-A | Overheat Indication of the Green Hydraulic System |
| TSM TASK 29-11-00-810-805-A | Loss of the System Pressure of the Green Hydraulic System |
Subtask 29-11-00-700-050-A
A. Test
(1) If there are overheat and or low pressure indications:
(a) Do the Fault Isolation.
4. Fault Isolation(1) If there are overheat and or low pressure indications:
(a) Do the Fault Isolation.
NOTE: A low pressure or overheat indication can be caused by a user system component internal leak .
Subtask 29-11-00-810-072-A
A. Procedure
(1) Make sure that all the user systems of the Green HYD system that follow have no defects:
(a) Do the procedures for Green System Low Pressure and Overheat, (Ref. TSM TASK 29-11-00-810-805) and (Ref. TSM TASK 29-11-00-810-802).
(3) If the aircraft is on a remote site and the necessary metering equipment is not available, do the procedures as far as possible:
(a) Examine the user system components for an unusual increase in noise and temperature.
(b) Replace a system component that shows an unusual increase in noise or temperature.
(4) Do the applicable test in Para. 3. A. of (Ref. TSM TASK 29-11-00-810-802) and (Ref. TSM TASK 29-11-00-810-805).
5. Close-up(1) Make sure that all the user systems of the Green HYD system that follow have no defects:
- LH and RH Ailerons
- LH and RH Spoilers 5
- LH and RH Spoilers 1
- LH Elevator
- THS
- LH and RH Slats Wing Tip Brake
- RH Flaps Wing Tip Brake
- Rudder
- Yaw Damper
- Reverse Eng 1
- Normal Brakes
- Flaps
- Slats
- Landing Gear
- Nose Wheel Steering.
(a) Do the procedures for Green System Low Pressure and Overheat, (Ref. TSM TASK 29-11-00-810-805) and (Ref. TSM TASK 29-11-00-810-802).
(3) If the aircraft is on a remote site and the necessary metering equipment is not available, do the procedures as far as possible:
(a) Examine the user system components for an unusual increase in noise and temperature.
(b) Replace a system component that shows an unusual increase in noise or temperature.
(4) Do the applicable test in Para. 3. A. of (Ref. TSM TASK 29-11-00-810-802) and (Ref. TSM TASK 29-11-00-810-805).
Subtask 29-11-00-942-050-A
A. Put the aircraft back to the serviceable condition.