Installation of the Servo-Valve on the Spoiler Servo-Control
TASK 27-64-51-400-002-A
Installation of the Servo-Valve on the Spoiler Servo-Control
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Expendable Parts
E. Referenced Information
3. Job Set-up
Subtask 27-64-51-941-059-A
Subtask 27-64-51-942-052-A
[Rev.10 from 2021]
2026.03.31 23:56:01 UTC
Installation of the Servo-Valve on the Spoiler Servo-Control
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.
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.
WARNING:
YOU MUST PUT ON AND ATTACH A SAFETY HARNESS BEFORE YOU START WORK:
- ON THE THS OR IN THE REAR FUSELAGE
- ON TOP OF THE WINGS OR PYLONS.
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 | 1 | ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE |
| No specific | AR | BRUSH - BRISTLED, SOFT |
| No specific | AR | SAFETY BARRIER(S) |
| No specific | AR | WARNING NOTICE(S) |
| No specific | Torque wrench: range to between 0.759 and 0.621 m.daN (67.17 and 54.96 lbf.in ) ![]() | |
| 98D27603002000 | 1 | KEY-SPOILER MAINTENANCE |
| 98D27603002001 | 1 | KEY-SPOILER MAINTENANCE |
| 98L12003001000 | 1 | HARNESS,SAFETY |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.02ABA1) | Phosphate Ester Hydraulic Fluid-General Power - - |
| (Material No.03JDA1) | Silicone base Grease-Bearings - - |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.14QFB1) | Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 574 | FALSE SPAR BOX |
| 582 | SPOILER N° 1 |
| 583 | SPOILER N° 2 |
| 584 | SPOILER N° 3 |
| 674 | FALSE SPAR BOX |
| 682 | SPOILER N° 1 |
| 683 | SPOILER N° 2 |
| 684 | SPOILER N° 3 |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 3 | SERVO-VALVE | AIPC 27-64-51-01-030 |
| 2 | O-RING | AIPC 27-64-51-01-050 |
| 5 | GASKET | AIPC 27-64-51-01-060 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 12-12-29-611-001-A | Fill the Hydraulic Fluid Reservoir with a Hand Pump |
| 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 29-10-00-864-001-A | Depressurize the Green Hydraulic System |
| TASK 29-10-00-864-002-A | Depressurize the Yellow Hydraulic System |
| TASK 29-10-00-864-003-A | Depressurize the Blue Hydraulic System |
| TASK 29-14-00-614-001-A | Depressurization of the Hydraulic Reservoirs |
Subtask 27-64-51-941-059-A
A. Safety Precautions
(1) Make sure that the SAFETY BARRIER(S) are in position.
(2) Make sure that the WARNING NOTICE(S) are in the cockpit to tell persons not to operate the flight controls.
(3) Make sure that the WARNING NOTICE(S) is in the cockpit to tell persons not to pressurize the hydraulic systems.
Subtask 27-64-51-860-055-B (1) Make sure that the SAFETY BARRIER(S) are in position.
(2) Make sure that the WARNING NOTICE(S) are in the cockpit to tell persons not to operate the flight controls.
(3) Make sure that the WARNING NOTICE(S) is in the cockpit to tell persons not to pressurize the hydraulic systems.
B. Aircraft Maintenance Configuration
(2) Make sure that the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE is below the applicable servo-valve (3).
(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 installed.
(5) Make sure that the applicable spoiler (Ref. AMM TASK 27-60-00-866-002) has been extended.
(6) Make sure that the 98D27604000000 COLLAR-SAFETY, SPOILER or 98D27604004000 COLLAR SAFETY SPOILER is on the piston rod of the servo-control.
(7) Make sure that the applicable hydraulic system is depressurized:
Subtask 27-64-51-875-057-A 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) Put on a safety harness: WARNING:
BEFORE YOU START WORK, YOU MUST PUT ON A SAFETY HARNESS AND ATTACH IT TO THE ACCESS PLATFORM. WITHOUT A SAFETY HARNESS, YOU CAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.
(a) Put on and attach a 98L12003001000 HARNESS,SAFETY before you start work in the work area. (2) Make sure that the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE is below the applicable servo-valve (3).
(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 installed.
(5) Make sure that the applicable spoiler (Ref. AMM TASK 27-60-00-866-002) has been extended.
(6) Make sure that the 98D27604000000 COLLAR-SAFETY, SPOILER or 98D27604004000 COLLAR SAFETY SPOILER is on the piston rod of the servo-control.
(7) Make sure that the applicable hydraulic system is depressurized:
- For the spoiler 1 and the spoiler 5, depressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-864-001) and the green hydraulic reservoir (Ref. AMM TASK 29-14-00-614-001)
- For the spoiler 2 and the spoiler 4, depressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-864-002) and the yellow hydraulic reservoir (Ref. AMM TASK 29-14-00-614-001)
- For the spoiler 3, depressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-864-003) and the blue hydraulic system reservoir (Ref. AMM TASK 29-14-00-614-001).
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
Subtask 27-64-51-865-054-A | 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 |
| ** ON A/C ALL | |||
| 49VU | HYD/HYD PWR/B WARN/& CTL | 2702GJ | C12 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | HYDRAULIC/G HYD/PUMP ENG1/CTL | 1701GK | H12 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B03 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| ** ON A/C ALL | |||
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/G HYD/PUMP ENG1/CTL | 1701GK | R35 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N30 |
| 121VU | HYDRAULIC/G HYD/PUMP ENG1/MONG | 1702GK | R34 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/SOL VALVES/G/Y/PTU | 1801GL | N34 |
| 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 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N31 |
| 121VU | HYDRAULIC/G HYD/PUMP ENG1/MONG | 1702GK | R33 |
| ** ON A/C ALL | |||
| 123VU | B HYD/ELEC PUMP | 2701GJ | AB09 |
| 123VU | Y HYD/ELEC/PUMP | 3802GX | AB06 |
| 123VU | Y HYD/ELEC/ELEC PUMP/NORM | 3801GX | AB03 |
DELETED
4. ProcedureCAUTION:
BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
Subtask 27-64-51-420-057-A - 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
(1) Remove the blanking cover from the servo-control (1) interface.
(2) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) and a BRUSH - BRISTLED, SOFT with Non Aqueous Cleaner-General - - (Material No.08BAA9) to clean the servo-valve (3) and the servo-control (1) interfaces.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Examine the AIPC 27-64-51-01-060 GASKET (5) for the correct condition and replace the item if it is damaged.
(5) Make sure that the parts retained from the removed component are clean and in the correct condition.
(6) Lubricate the new AIPC 27-64-51-01-050 O-RING (2) with Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) .
(7) Apply a layer of Silicone base Grease-Bearings - - (Material No.03JDA1) to the threads of the bolts (4).
Subtask 27-64-51-420-058-B (1) Remove the blanking cover from the servo-control (1) interface.
(2) Use a clean Textile-Lint free Cotton - (Material No.14SBA1) and a BRUSH - BRISTLED, SOFT with Non Aqueous Cleaner-General - - (Material No.08BAA9) to clean the servo-valve (3) and the servo-control (1) interfaces.
(3) Do an inspection of the component interfaces and the adjacent area.
(4) Examine the AIPC 27-64-51-01-060 GASKET (5) for the correct condition and replace the item if it is damaged.
(5) Make sure that the parts retained from the removed component are clean and in the correct condition.
(6) Lubricate the new AIPC 27-64-51-01-050 O-RING (2) with Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) .
(7) Apply a layer of Silicone base Grease-Bearings - - (Material No.03JDA1) to the threads of the bolts (4).
B. Installation of the Servo-Valve on the Spoiler Servo-Control
(1) If necessary, install a new AIPC 27-64-51-01-030 SERVO-VALVE (3).
(2) Install the gasket (5) on the servo-valve (3).
(4) Put the servo-valve (3) into position on the spoiler servo-control (1).
(5) Install the bolts (4) through the servo-valve (3) and into the spoiler servo-control (1).
(6) TORQUE the bolts (4) to between 0.759 and 0.621 m.daN (67.17 and 54.96 lbf.in )
:
14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - .
(7) Lower the applicable spoiler (Ref. AMM TASK 27-60-00-866-002).
(8) On the servo-control, turn the 98D27603002000 KEY-SPOILER MAINTENANCE or the 98D27603002001 KEY-SPOILER MAINTENANCE in the maintenance device to the operation position and then remove it.
(9) Remove the access platform(s).
Subtask 27-64-51-875-058-A (1) If necessary, install a new AIPC 27-64-51-01-030 SERVO-VALVE (3).
(2) Install the gasket (5) on the servo-valve (3).
NOTE: It is not necessary to lubricate the mating surface of the servo-valve (3) with the gasket (5).
The mating surface of the servo-valve (3) must be clean and dry.
(3) Install the new O-ring (2) on the servo-valve (3). The mating surface of the servo-valve (3) must be clean and dry.
(4) Put the servo-valve (3) into position on the spoiler servo-control (1).
(5) Install the bolts (4) through the servo-valve (3) and into the spoiler servo-control (1).
(6) TORQUE the bolts (4) to between 0.759 and 0.621 m.daN (67.17 and 54.96 lbf.in )
: WARNING:
USE PROTECTIVE GOGGLES AND GLOVES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(a) Safety the bolts (4) with (7) Lower the applicable spoiler (Ref. AMM TASK 27-60-00-866-002).
(8) On the servo-control, turn the 98D27603002000 KEY-SPOILER MAINTENANCE or the 98D27603002001 KEY-SPOILER MAINTENANCE in the maintenance device to the operation position and then remove it.
(9) Remove the access platform(s).
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 27-64-51-865-055-A | 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 |
| ** ON A/C ALL | |||
| 49VU | HYD/HYD PWR/B WARN/& CTL | 2702GJ | C12 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | HYDRAULIC/G HYD/PUMP ENG1/CTL | 1701GK | H12 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/SEC1/NORM/SPLY | 21CE1 | B03 |
| 49VU | FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 | 6CV | B02 |
| ** ON A/C ALL | |||
| 105VU | FLT CTL/SEC1/STBY SPLY | 22CE | B01 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/G HYD/PUMP ENG1/CTL | 1701GK | R35 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N30 |
| 121VU | HYDRAULIC/G HYD/PUMP ENG1/MONG | 1702GK | R34 |
| ** ON A/C ALL | |||
| 121VU | HYDRAULIC/SOL VALVES/G/Y/PTU | 1801GL | N34 |
| 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 |
| ** ON A/C NOT FOR ALL | |||
| 121VU | HYDRAULIC/HYD POWER/Y | 3803GX | N31 |
| 121VU | HYDRAULIC/G HYD/PUMP ENG1/MONG | 1702GK | R33 |
| ** ON A/C ALL | |||
| 123VU | B HYD/ELEC PUMP | 2701GJ | AB09 |
| 123VU | Y HYD/ELEC/PUMP | 3802GX | AB06 |
| 123VU | Y HYD/ELEC/ELEC PUMP/NORM | 3801GX | AB03 |
DELETED
Subtask 27-64-51-863-050-A E. Fill and Pressurize the Hydraulic Systems
Subtask 27-64-51-870-052-A 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.
WARNING:
MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE ITEMS THEY OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM. UNWANTED MOVEMENT OF HYDRAULICALLY OPERATED ITEMS CAN CAUSE SERIOUS INJURY AND/OR DAMAGE.
(1) Fill the applicable hydraulic system reservoir (Ref. AMM TASK 12-12-29-611-001). F. Bleed the Servo-Controls
(1) Do a minimum of ten full travel operations of the spoilers, to bleed all the air from the servo-controls (Ref. AMM TASK 27-64-00-710-001).
Subtask 27-64-51-710-051-A (1) Do a minimum of ten full travel operations of the spoilers, to bleed all the air from the servo-controls (Ref. AMM TASK 27-64-00-710-001).
G. Test
(1) Do an operational test of the spoilers (Ref. AMM TASK 27-64-00-710-001).
(2) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position below the applicable spoiler servo-valve (3).
(3) Examine the servo-valve (3) and its interface with the spoiler servo-control (1) for leaks.
5. Close-up(1) Do an operational test of the spoilers (Ref. AMM TASK 27-64-00-710-001).
(2) Put the ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position below the applicable spoiler servo-valve (3).
(3) Examine the servo-valve (3) and its interface with the spoiler servo-control (1) for leaks.
Subtask 27-64-51-942-052-A
A. Removal of Equipment
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Retract the flaps.
(3) Remove the SAFETY BARRIER(S).
(4) Remove the access platform(s).
(5) Remove the WARNING NOTICE(S).
(6) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Retract the flaps.
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.
(a) Retract the flaps fully (Ref. AMM TASK 27-50-00-866-009). (3) Remove the SAFETY BARRIER(S).
(4) Remove the access platform(s).
(5) Remove the WARNING NOTICE(S).
(6) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
Servo-Valve - Location and Detail