Removal of the Hydraulic Suction Tubes
TASK 29-11-49-000-010-A
Removal of the Hydraulic Suction Tubes
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Work Zones and Access Panels
C. Referenced Information
3. Job Set-up
Subtask 29-11-49-860-051-A ** ON A/C NOT FOR ALL
Subtask 29-11-49-020-050-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 07:59:11 UTC
Removal of the Hydraulic Suction Tubes
WARNING:
BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE ENGINE SHUTDOWN. USE APPLICABLE THERMAL GLOVES. THE ENGINE PARTS CAN STAY HOT FOR ONE HOUR AFTER SHUTDOWN AND CAN BURN YOU.
WARNING:
DO NOT GET HYDRAULIC FLUID ON YOUR SKIN, IN YOUR EYES OR IN YOUR MOUTH. HYDRAULIC FLUID IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY. FLUSH HYDRAULIC FLUID FROM YOUR EYES, MOUTH OR SKIN WITH WATER. GET MEDICAL AID IF YOU GET HYDRAULIC FLUID IN YOUR EYES OR MOUTH.
CAUTION:
DO NOT LET HYDRAULIC FLUID FALL ON THE ENGINE. UNWANTED HYDRAULIC FLUID MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FLUID CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | 1 | ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE |
| No specific | AR | CONTAINER 5 L (1.32 USGAL) |
| No specific | AR | COVER - BLANKING |
| No specific | AR | WARNING NOTICE(S) |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| FOR [1000EM1] (ENGINE-1) | |
| 437AL, 438AR | |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 29-10-00-864-001-A | Depressurize the Green Hydraulic System |
| TASK 29-14-00-614-001-A | Depressurization of the Hydraulic Reservoirs |
| FOR [1000EM1] (ENGINE-1) | |
| TASK 71-13-00-010-010-A | Opening of the Fan Cowls 437AL(447AL),438AR(448AR) |
Subtask 29-11-49-860-051-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) Depressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001).
(2) Depressurize the Green hydraulic reservoir (Ref. AMM TASK 29-14-00-614-001).
(3) Put WARNING NOTICE(S) in position to tell persons not to pressurize the Green hydraulic system:
Subtask 29-11-49-941-050-A ** ON A/C NOT FOR ALL (1) Depressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001).
(2) Depressurize the Green hydraulic reservoir (Ref. AMM TASK 29-14-00-614-001).
(3) Put WARNING NOTICE(S) in position to tell persons not to pressurize the Green hydraulic system:
- on the ground service panel 197CB.
B. Safety Precautions
(1) On the center pedestal, on the ENG panel 115VU:
(3) Put WARNING NOTICE(S) in position to tell persons not to pressurize the Green hydraulic system:
(6) Put a CONTAINER 5 L (1.32 USGAL) below the suction-hose adapter connection to the hydraulic pump.
Subtask 29-11-49-010-050-A ** ON A/C NOT FOR ALL (1) On the center pedestal, on the ENG panel 115VU:
- put WARNING NOTICE(S) to tell persons not to start the engine.
(3) Put WARNING NOTICE(S) in position to tell persons not to pressurize the Green hydraulic system:
- in the cockpit, on the HYD section of the overhead panel 40VU.
- make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(6) Put a CONTAINER 5 L (1.32 USGAL) below the suction-hose adapter connection to the hydraulic pump.
C. Get Access
(1) Open the fan-cowl doors:
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR (Ref. AMM TASK 71-13-00-010-010).
(2) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the engine.
4. Procedure(1) Open the fan-cowl doors:
(a) FOR [1000EM1] (ENGINE-1)
437AL 438AR (Ref. AMM TASK 71-13-00-010-010).
(2) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the engine.
Subtask 29-11-49-020-050-A ** ON A/C NOT FOR ALL
A. Removal of the Hydraulic Suction Tubes.
(1) Drain the hydraulic fluid from the suction tubes.
(a) Cut and discard the lockwire from the hose (9).
(b) Hold the union (56) with an applicable wrench and disconnect the hose (9) from the union.
(c) Let the hydraulic fluid drain into the container.
(2) Write the positions of these parts before removal:
(a) The clamps (17), (37) and (39).
(b) The bolts (16), (36) and (40).
(c) The hoses (12) and (9) and the tube (10).
(a) Remove the bolt (16) from the clamp (17).
(b) Hold the union (33) with an applicable wrench and disconnect the hose (12).
(c) Remove the hose (12) from the clamp (17).
(d) Disconnect the quick release coupling (1) at the aircraft pylon interface and remove the hose (12).
(4) Remove the lower hose (9).
(a) Hold the connection on the tube (10) with an applicable wrench and loosen the hose.
(b) Disconnect and remove the lower hose.
(5) Remove the tube (10).
(a) Attach temporary ties to safety the tube (10).
(b) Hold the union (33) with an applicable wrench and disconnect the tube (10).
(c) Remove the three bolts (40) and the top of the clamp (39) from the engine.
(d) Safety the bottom of the clamp (39) to the raft (38) with the temporary ties.
(e) Remove the three bolts (36) and the top of the clamp (37) from the engine.
(f) Safety the bottom of the clamp (37) to the raft (34) with the temporary ties.
(g) Remove the temporary ties from the tube (10) and remove the tube from the engine.
(6) Hold the quick release coupling (1) with an applicable wrench and loosen the hose (12).
(7) Remove the quick release coupling (1) from the hose (12).
(8) Put the applicable COVER - BLANKING on all the openings.
(1) Drain the hydraulic fluid from the suction tubes.
(a) Cut and discard the lockwire from the hose (9).
(b) Hold the union (56) with an applicable wrench and disconnect the hose (9) from the union.
(c) Let the hydraulic fluid drain into the container.
(2) Write the positions of these parts before removal:
(a) The clamps (17), (37) and (39).
(b) The bolts (16), (36) and (40).
(c) The hoses (12) and (9) and the tube (10).
NOTE: The position of these parts must be written. This makes sure that they are installed in the correct position during the installation task.
(3) Remove the upper hose (12). (a) Remove the bolt (16) from the clamp (17).
(b) Hold the union (33) with an applicable wrench and disconnect the hose (12).
(c) Remove the hose (12) from the clamp (17).
(d) Disconnect the quick release coupling (1) at the aircraft pylon interface and remove the hose (12).
(4) Remove the lower hose (9).
(a) Hold the connection on the tube (10) with an applicable wrench and loosen the hose.
(b) Disconnect and remove the lower hose.
(5) Remove the tube (10).
(a) Attach temporary ties to safety the tube (10).
(b) Hold the union (33) with an applicable wrench and disconnect the tube (10).
(c) Remove the three bolts (40) and the top of the clamp (39) from the engine.
(d) Safety the bottom of the clamp (39) to the raft (38) with the temporary ties.
(e) Remove the three bolts (36) and the top of the clamp (37) from the engine.
(f) Safety the bottom of the clamp (37) to the raft (34) with the temporary ties.
(g) Remove the temporary ties from the tube (10) and remove the tube from the engine.
(6) Hold the quick release coupling (1) with an applicable wrench and loosen the hose (12).
(7) Remove the quick release coupling (1) from the hose (12).
(8) Put the applicable COVER - BLANKING on all the openings.
Hydraulic Tube Details