Installation of the Check Valve
TASK 27-64-48-400-001-A
Installation of the Check Valve
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 27-64-48-941-056-A ** ON A/C NOT FOR ALL
Subtask 27-64-48-410-051-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.03.31 23:55:56 UTC
Installation of the Check Valve
WARNING:
MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING NOTICES ARE IN POSITION.
WARNING:
MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING GEAR. THIS WILL PREVENT UNWANTED MOVEMENT OF THE LANDING GEAR, AND THUS POSSIBLE INJURY TO PERSONS AND DAMAGE TO THE AIRCRAFT AND/OR EQUIPMENT.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
1. Reason for the Job- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
- MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE |
| No specific | AR | CONTAINER - HYDRAULIC FLUID RESISTANT |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | WARNING SIGN - DANGER |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.02ABA1) | Phosphate Ester Hydraulic Fluid-General Power - - |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| FOR [3626GM] | |
| 575CB | |
| FOR [3627GM] | |
| 675CB | |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 12-12-29-611-001-A | Fill the Hydraulic Fluid Reservoir with a Hand Pump |
| TASK 12-12-29-611-002-A | Fill the Hydraulic Fluid Reservoir with a Hydraulic Service Cart |
| TASK 27-50-00-866-008-A | Extension of the Flaps on the Ground |
| TASK 27-50-00-866-008-A-01 | Extension of the Flaps/Slats on the Ground |
| TASK 27-50-00-866-009-A | Retraction of the Flaps on the Ground |
| TASK 27-50-00-866-009-A-01 | Retraction of the Flaps/Slats on the Ground |
| TASK 27-60-00-866-002-A | Extension-Retraction of the Spoilers for Maintenance |
| TASK 27-64-00-710-001-A | Operational Test of the Spoiler Hydraulic Actuation |
| TASK 29-14-00-614-001-A | Depressurization of the Hydraulic Reservoirs |
| TASK 29-14-00-614-002-A | Pressurization of the Hydraulic Reservoirs through the Ground Connector |
| TASK 29-14-00-614-002-A-01 | Pressurization of the Hydraulic Reservoirs with the Auxiliary Power Unit (APU) |
| TASK 29-23-00-860-001-A | Disconnection of the Isolation Coupling of the Power Transfer Unit (PTU) |
| TASK 29-23-00-860-002-A | Connection of the Isolation Coupling of the Power Transfer Unit (PTU) |
| TASK 57-51-37-000-004-A | Removal of the Access Panels 575AB(675AB), 575BB(675BB), 575CB(675CB), 575DB(675DB), 575EB(675EB), 575FB(675FB), 575GB(675GB), 575HB(675HB) |
| FOR [3626GM] | |
| TASK 57-51-37-400-004-A | Installation of the Access Panels 575AB(675AB), 575BB(675BB), 575CB(675CB), 575DB(675DB), 575EB(675EB), 575FB(675FB), 575GB(675GB), 575HB(675HB) |
| FOR [3627GM] | |
| TASK 57-51-37-400-004-A | Installation of the Access Panels 575AB(675AB), 575BB(675BB), 575CB(675CB), 575DB(675DB), 575EB(675EB), 575FB(675FB), 575GB(675GB), 575HB(675HB) |
Subtask 27-64-48-941-056-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(1) Make sure that the SAFETY BARRIER(S) are in position.
(2) Make sure there are WARNING SIGN - DANGER to tell persons not to pressurize the Yellow hydraulic system.
(3) Make sure there are WARNING SIGN - DANGER to tell persons not to operate the flight control system.
Subtask 27-64-48-860-053-A ** ON A/C NOT FOR ALL (1) Make sure that the SAFETY BARRIER(S) are in position.
(2) Make sure there are WARNING SIGN - DANGER to tell persons not to pressurize the Yellow hydraulic system.
(3) Make sure there are WARNING SIGN - DANGER to tell persons not to operate the flight control system.
B. Aircraft Maintenance Configuration
(1) Make sure that the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE is below the applicable zone 575 or 675.
(2) Make sure that the applicable access panels 575CB, 675CB have been removed (Ref. AMM TASK 57-51-37-000-004).
(3) Make sure that the flaps are fully extended (Ref. AMM TASK 27-50-00-866-008).
(4) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is on the flap/slat control lever.
(5) Make sure that spoilers 2 and 3 are lifted (Ref. AMM TASK 27-60-00-866-002).
(6) Make sure that the 98D27604000000 COLLAR-SAFETY, SPOILER or 98D27604004000 COLLAR SAFETY SPOILER is on the applicable rod of the servocontrol.
(7) Make sure that the PTU is disconnected (Ref. AMM TASK 29-23-00-860-001).
(8) Make sure that the Yellow hydraulic-system reservoir is depressurized (Ref. AMM TASK 29-14-00-614-001).
Subtask 27-64-48-865-051-A ** ON A/C NOT FOR ALL (1) Make sure that the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE is below the applicable zone 575 or 675.
(2) Make sure that the applicable access panels 575CB, 675CB have been removed (Ref. AMM TASK 57-51-37-000-004).
(3) Make sure that the flaps are fully extended (Ref. AMM TASK 27-50-00-866-008).
(4) Make sure that the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION is on the flap/slat control lever.
(5) Make sure that spoilers 2 and 3 are lifted (Ref. AMM TASK 27-60-00-866-002).
(6) Make sure that the 98D27604000000 COLLAR-SAFETY, SPOILER or 98D27604004000 COLLAR SAFETY SPOILER is on the applicable rod of the servocontrol.
(7) Make sure that the PTU is disconnected (Ref. AMM TASK 29-23-00-860-001).
(8) Make sure that the Yellow hydraulic-system reservoir is depressurized (Ref. AMM TASK 29-14-00-614-001).
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
4. Procedure| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B08 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| 49VU | HYD/FIRE VALVE/Y/ENG2 | 3702GD | C14 |
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N30 |
| 121VU | HYDRAULIC/Y HYD/PUMP ENG2/MONG | 3700GD | Q37 |
| 121VU | HYDRAULIC/Y HYD/PUMP ENG2/CTL | 3701GD | Q36 |
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
| 121VU | FLIGHT CONTROLS/SEC3/SPLY | 21CE3 | Q19 |
| 121VU | FLIGHT CONTROLS/SEC2/SPLY | 21CE2 | Q18 |
| 123VU | Y HYD/ELEC/PUMP | 3802GX | AB06 |
| 123VU | Y HYD/ELEC/ELEC PUMP/NORM | 3801GX | AB03 |
CAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
Subtask 27-64-48-420-051-A ** ON A/C NOT FOR ALL - DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
- DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
- MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
A. Preparation for Installation
(2) Do an inspection of the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) Remove the blanking caps from the line ends.
(5) Apply Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) to the threads on the check valve (3) and the coupling nuts (1) and (2).
Subtask 27-64-48-420-050-A ** ON A/C NOT FOR ALL WARNING:
OBEY THE HYDRAULIC SAFETY PROCEDURES.
(1) Clean the component interface and/or the adjacent area with Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) . (2) Do an inspection of the component interfaces and the adjacent area.
(3) Make sure that the parts retained from the removed component are clean and in the correct condition.
(4) Remove the blanking caps from the line ends.
(5) Apply Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) to the threads on the check valve (3) and the coupling nuts (1) and (2).
B. Installation of the Check Valve
(1) Install the check valve (3) and tighten the coupling nuts (1) and (2). If removed, install the clamp block adjacent to the check valve (3).
(2) Remove the CONTAINER - HYDRAULIC FLUID RESISTANT from below the check valve (3).
Subtask 27-64-48-866-053-A ** ON A/C NOT FOR ALL (1) Install the check valve (3) and tighten the coupling nuts (1) and (2). If removed, install the clamp block adjacent to the check valve (3).
(2) Remove the CONTAINER - HYDRAULIC FLUID RESISTANT from below the check valve (3).
C. Retract the Spoilers
(2) On the servo-control, make sure that the pointer on the hex. head is opposite the letter 'O' (Operation) on the housing.
Subtask 27-64-48-865-052-A ** ON A/C NOT FOR ALL WARNING:
MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
(1) Retract the spoilers (Ref. AMM TASK 27-60-00-866-002). (2) On the servo-control, make sure that the pointer on the hex. head is opposite the letter 'O' (Operation) on the housing.
D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 27-64-48-860-054-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | HYD/FIRE VALVE/Y/ENG2 | 3702GD | C14 |
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N30 |
| 121VU | HYDRAULIC/Y HYD/PUMP ENG2/MONG | 3700GD | Q37 |
| 121VU | HYDRAULIC/Y HYD/PUMP ENG2/CTL | 3701GD | Q36 |
| 123VU | Y HYD/ELEC/PUMP | 3802GX | AB06 |
| 123VU | Y HYD/ELEC/ELEC PUMP/NORM | 3801GX | AB03 |
E. Aircraft Maintenance Configuration
(1) Fill the Yellow hydraulic reservoir (Ref. AMM TASK 12-12-29-611-001), (Ref. AMM TASK 12-12-29-611-002).
(2) Pressurize the Yellow hydraulic system-reservoir (Ref. AMM TASK 29-14-00-614-002).
(3) Connect the PTU (Ref. AMM TASK 29-23-00-860-002).
Subtask 27-64-48-865-054-A ** ON A/C NOT FOR ALL (1) Fill the Yellow hydraulic reservoir (Ref. AMM TASK 12-12-29-611-001), (Ref. AMM TASK 12-12-29-611-002).
(2) Pressurize the Yellow hydraulic system-reservoir (Ref. AMM TASK 29-14-00-614-002).
(3) Connect the PTU (Ref. AMM TASK 29-23-00-860-002).
F. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 27-64-48-866-052-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B08 |
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| 121VU | FLIGHT CONTROLS/SEC3/SPLY | 21CE3 | Q19 |
| 121VU | FLIGHT CONTROLS/SEC2/SPLY | 21CE2 | Q18 |
G. Bleed the Spoilers
Subtask 27-64-48-710-050-A ** ON A/C NOT FOR ALL WARNING:
MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
(1) Extend and retract the spoilers five times (Ref. AMM TASK 27-64-00-710-001), to bleed the Yellow hydraulic system. H. Test
(1) Do an operational test of the spoilers (Ref. AMM TASK 27-64-00-710-001).
(2) Make sure that there are no leaks from the check valve (3) or the coupling nuts (1) and (2).
Subtask 27-64-48-865-055-A ** ON A/C NOT FOR ALL (1) Do an operational test of the spoilers (Ref. AMM TASK 27-64-00-710-001).
(2) Make sure that there are no leaks from the check valve (3) or the coupling nuts (1) and (2).
I. Open, safety and tag this(these) circuit breaker(s):
5. Close-up| PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B08 |
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| 121VU | FLIGHT CONTROLS/SEC3/SPLY | 21CE3 | Q19 |
| 121VU | FLIGHT CONTROLS/SEC2/SPLY | 21CE2 | Q18 |
Subtask 27-64-48-410-051-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) If removed, install the applicable access panel:
(a) FOR [3626GM]
install 575CB (Ref. AMM TASK 57-51-37-400-004)
(b) FOR [3627GM]
install 675CB (Ref. AMM TASK 57-51-37-400-004).
(c) Remove the access platform(s).
Subtask 27-64-48-865-056-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) If removed, install the applicable access panel:
(a) FOR [3626GM]
install 575CB (Ref. AMM TASK 57-51-37-400-004)
(b) FOR [3627GM]
install 675CB (Ref. AMM TASK 57-51-37-400-004).
(c) Remove the access platform(s).
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 27-64-48-866-051-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B08 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B07 |
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| 121VU | FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 | 8CV | Q21 |
| 121VU | FLIGHT CONTROLS/SEC3/SPLY | 21CE3 | Q19 |
| 121VU | FLIGHT CONTROLS/SEC2/SPLY | 21CE2 | Q18 |
C. Move the Flaps
(2) Retract the flaps fully (Ref. AMM TASK 27-50-00-866-009).
Subtask 27-64-48-942-053-A ** ON A/C NOT FOR ALL WARNING:
MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
(1) Remove the 98D27803000000 LOCKING TOOL-FLAP SLAT LEVER,INT. POSITION from the flap/slat control lever. (2) Retract the flaps fully (Ref. AMM TASK 27-50-00-866-009).
D. Removal of Equipment
(1) Remove the safety barriers.
(2) Remove the WARNING NOTICE(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Remove the safety barriers.
(2) Remove the WARNING NOTICE(S).
(3) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Check Valves