Installation of the Rudder Servo Control
TASK 27-24-51-400-001-A
Installation of the Rudder 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 27-24-51-865-051-A
Subtask 27-24-51-860-055-A
[Rev.10 from 2021]
2026.03.31 23:49:27 UTC
Installation of the Rudder Servo Control
WARNING:
PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU START A TASK ON OR NEAR:
- THE FLIGHT CONTROLS
- THE FLIGHT CONTROL SURFACES
- THE LANDING GEAR AND THE RELATED DOORS
- COMPONENTS THAT MOVE.
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:
PRESSURIZE ONLY THE HYDRAULIC SYSTEM(S) THAT IS (ARE) NECESSARY FOR THE TASK. ISOLATE THE OTHER HYDRAULIC SYSTEM(S) BEFORE YOU SUPPLY HYDRAULIC POWER TO THE AIRCRAFT.
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
CAUTION:
DO THIS PROCEDURE IN A HANGAR IF THERE ARE WIND GUSTS. WIND GUSTS CAN CAUSE DAMAGE TO THE LINKAGE WHEN THE RIGGING PINS ARE IN POSITION ON THE RUDDER CONTROL.
CAUTION:
MAKE SURE THAT ONE SERVO CONTROL IS INSTALLED AT ALL TIMES. IF YOU MUST REMOVE ALL THREE SERVO CONTROLS, FIRST DO THE INSTALLATION, ADJUSTMENT AND TEST PROCEDURES FOR ONLY ONE OF THE SERVO CONTROLS. IF YOU REMOVE ALL THREE SERVO CONTROLS AT THE SAME TIME, DAMAGE TO THE AIRCRAFT CAN OCCUR.
NOTE: This procedure includes the installation of the rudder servo control with the eye-end with integrated roller bearing and grease nipple (post modification 154553 and post SB 27-1224).
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 10M (33 FT) - ADJUSTABLE |
| No specific | 1 | CALIPER |
| No specific | 2 | CAP - BLANKING |
| No specific | 1 | CONTAINER 5 L (1.32 USGAL) |
| No specific | 2 | GAGE - FEELER |
| No specific | 1 | GUN - GREASE |
| No specific | AR | WARNING NOTICE(S) |
| No specific | Torque wrench: range to between 1.7 and 1.5 m.daN (12.54 and 11.06 lbf.ft ) ![]() | |
| No specific | Torque wrench: range to between 2.3 and 2.0 m.daN (16.96 and 14.75 lbf.ft ) ![]() | |
| No specific | Torque wrench: range to between 8.0 and 7.0 m.daN (59.00 and 51.62 lbf.ft ) ![]() | |
| 98D27207546000 | 1 | PIN-RIGGING |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.02ABA1) | Phosphate Ester Hydraulic Fluid-General Power - - |
| (Material No.03FDB1) | Mineral Oil base Grease-Anti-Fretting Paste - |
| (Material No.03GBC1) | Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. - |
| (Material No.03GBD1) | Synthetic Oil base Grease-General Purpose Lithium Thickened - |
| (Material No.03HBD9) | Synthetic Ester base Grease-General Purpose Low Temp - |
| (Material No.08BAA9) | Non Aqueous Cleaner-General - - |
| (Material No.12AGC2) | Corrosion Preventive Compound-- Soft Film System |
| (Material No.14QFB1) | Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - |
| (Material No.14SBA1) | Textile-Lint free Cotton - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 325 | VERTICAL STABILIZER TRAILING EDGE |
| 325BL, 325CL, 325CR, 325DL |
| FIG.ITEM | DESIGNATION | IPC-CSN |
|---|---|---|
| 27 | COTTER PIN | AIPC 27-21-04-08-050 |
| 27 | COTTER PIN | AIPC 27-21-84-11-010 |
| 88 | COTTER PIN | AIPC 27-24-04-20-050 |
| 98 | COTTER PIN | AIPC 27-24-04-20-050 |
| 13 | COTTER PIN | AIPC 27-24-04-20-220 |
| 74 | QUAD RINGS | AIPC 27-24-51-01-070 |
| 35 | QUAD RINGS | AIPC 27-24-51-01-075 |
| 88 | COTTER PIN | AIPC 27-24-84-20-050 |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 20-23-22-910-001-A | Marking of the Unions after Application of Standard or Specific Tightening Torque |
| TASK 20-28-00-912-802-A | Electrical Bonding - General Maintenance Procedure |
| TASK 27-24-00-710-001-A | Operational Test of the Rudder Hydraulic Actuation |
| TASK 27-24-00-710-002-A | Operational Test of the Rudder Servocontrols with Individual Hydraulic System |
| TASK 27-24-00-820-001-A | Adjustment of the Rudder Neutral Position |
| TASK 27-24-00-820-001-A-01 | Adjustment of the Rudder Neutral Position |
| TASK 27-24-00-820-001-B | Adjustment of the Rudder Neutral Position |
| TASK 29-00-00-864-001-A | Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action |
| TASK 29-10-00-863-001-A | Pressurize the Green Hydraulic System with a Hydraulic Ground Power-Cart |
| TASK 29-10-00-863-002-A | Pressurize the Yellow Hydraulic System with a Hydraulic Ground Power-Cart |
| TASK 29-10-00-863-003-A | Pressurize the Blue Hydraulic System with a Hydraulic Ground Power-Cart |
| TASK 29-10-00-863-003-A-01 | Pressurize the Blue Hydraulic System with the Blue Electric Pump |
| 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 |
| 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 51-75-13-916-002-A | Repair to a layer of Corrosion Preventive Compound |
| TASK 55-33-13-010-002-A | Opening/Removal of the Trailing Edge Access-Panels of the Vertical Stabilizer |
| TASK 55-33-13-410-002-A | Closing/Installation of the Trailing Edge Access-Panels of the Vertical Stabilizer |
Subtask 27-24-51-865-051-A
A. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
Subtask 27-24-51-860-053-B | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | B04 |
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | B03 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | H10 |
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | H09 |
| ** ON A/C ALL | |||
| 121VU | AUTO FLT/FAC2/28VDC | 5CC2 | M19 |
| 121VU | AUTO FLT/FAC2/26VAC | 14CC2 | M18 |
B. Aircraft Maintenance Configuration
(1) Make sure that the ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE is in position at zone 325.
(2) Make sure that the access panels 325CL 325CR, 325BL 325DL at the trailing edge of the vertical stabilizer are opened (Ref. AMM TASK 55-33-13-010-002).
(3) Make sure that the rudder pedals are in the neutral position.
(4) Make sure that the rudder trim control is set at the zero position.
(5) Make sure that the WARNING NOTICE(S) are in the flight compartment to tell persons not to operate the flight controls.
(6) Make sure that the hydraulic systems are depressurized and put them in the maintenance configuration
(Ref. AMM TASK 29-00-00-864-001).
(7) Make sure that the reservoirs of the Green, Blue and Yellow hydraulic systems are depressurized.
(Ref. AMM TASK 29-14-00-614-001).
(8) Make sure that the 98D27207546000 PIN-RIGGING (3) is installed in the bellcrank assy (6) at the lower servo control 1025GM (5).
4. Procedure(1) Make sure that the ACCESS PLATFORM 10M (33 FT) - ADJUSTABLE is in position at zone 325.
(2) Make sure that the access panels 325CL 325CR, 325BL 325DL at the trailing edge of the vertical stabilizer are opened (Ref. AMM TASK 55-33-13-010-002).
(3) Make sure that the rudder pedals are in the neutral position.
(4) Make sure that the rudder trim control is set at the zero position.
(5) Make sure that the WARNING NOTICE(S) are in the flight compartment to tell persons not to operate the flight controls.
(6) Make sure that the hydraulic systems are depressurized and put them in the maintenance configuration
(Ref. AMM TASK 29-00-00-864-001).
(7) Make sure that the reservoirs of the Green, Blue and Yellow hydraulic systems are depressurized.
(Ref. AMM TASK 29-14-00-614-001).
(8) Make sure that the 98D27207546000 PIN-RIGGING (3) is installed in the bellcrank assy (6) at the lower servo control 1025GM (5).
CAUTION:
MAKE SURE THAT ONE SERVO CONTROL IS INSTALLED AT ALL TIMES. IF YOU MUST REMOVE ALL THREE SERVO CONTROLS, FIRST DO THE INSTALLATION, ADJUSTMENT AND TEST PROCEDURES FOR ONLY ONE OF THE SERVO CONTROLS. IF YOU REMOVE ALL THREE SERVO CONTROLS AT THE SAME TIME, DAMAGE TO THE AIRCRAFT CAN OCCUR.
CAUTION:
YOU MUST INSTALL HYDRAULIC TUBES WITH HYDRAULIC FLUID AS LUBRICANT.
CAUTION:
USE A SECOND WRENCH TO APPLY COUNTERTORQUE TO THE UNION WHEN YOU DISCONNECT/CONNECT HYDRAULIC LINES ON UNIONS. IF YOU DO NOT USE THE SECOND WRENCH, THERE IS A RISK THAT YOU WILL LOOSEN OR TIGHTEN THE UNION TOO MUCH.
Subtask 27-24-51-910-051-A A. Preparation for the Installation
(1) Do a visual check of the identification placard on the servo control:
(3) Clean the attachment brackets, the bushes and the locking plates with the Non Aqueous Cleaner-General - - (Material No.08BAA9) and let them dry.
(4) Make sure that the bolts, the screws, the nuts, the bushes and the locking plates show no corrosion and are not damaged.
(5) If you install the upper rudder servo control 2025GM (5):
(a) Install the clamp (10) to the new rudder servo control (5).
Subtask 27-24-51-560-051-A ** ON A/C NOT FOR ALL (1) Do a visual check of the identification placard on the servo control:
- 1025GM.
for the lower servo control connected to the Green hydraulic system, - 3025GM
for the center servo control connected to the Yellow hydraulic system, - 2025GM
for the upper servo control connected to the Blue hydraulic system.
(3) Clean the attachment brackets, the bushes and the locking plates with the Non Aqueous Cleaner-General - - (Material No.08BAA9) and let them dry.
(4) Make sure that the bolts, the screws, the nuts, the bushes and the locking plates show no corrosion and are not damaged.
(5) If you install the upper rudder servo control 2025GM (5):
(a) Install the clamp (10) to the new rudder servo control (5).
B. Preparation for the Installation of the Rudder Servo Control with the Eye-End WITHOUT Integrated Roller Bearing and Grease Nipple
(1) If you install this type of rudder servo control:
(a) This preparation is not applicable.
Subtask 27-24-51-560-051-B ** ON A/C NOT FOR ALL (1) If you install this type of rudder servo control:
(a) This preparation is not applicable.
B. Preparation for the Installation of the Rudder Servo Control with the Eye-End WITH Integrated Roller Bearing and Grease Nipple
(1) If you install this type of rudder servo control:
(a) Make sure that the rudder servo control is in the correct condition:
Subtask 27-24-51-420-051-E (1) If you install this type of rudder servo control:
(a) Make sure that the rudder servo control is in the correct condition:
- Examine the eye-end with the grease nipple and
make sure that the grease nipple is on the same side as the servocontrol lever.
C. Installation of the Rudder Servo Control 1025GM/2025GM/3025GM
(2) Install the bushes (34) and (36) in the bracket (52) of the vertical stabilizer (1).
(3) Install the washer (58), the locking plate (53) in the bracket (52) of the vertical stabilizer (1).
(4) Install the bushes (73) and (75) in the bracket (65) of the rudder (2).
(5) Install the washer (77) and the locking plate (64) in the bracket (65) of the rudder (2).
(6) Put the clamp (10) on the servo control (5).
(7) Put the servo control (5) in position at the bracket (52), (65).
(8) Make sure that the items that follow are correctly installed in the brackets (52) and (65):
(b) Attach the new quad rings (35) in position at the eye-end bearing of the servo control (5).
(c) Use the two GAGE - FEELER 0.25 mm (0.0098 in.) thick to carefully move the servo control (5) into the bracket (52).
(d) Align the eye-end bearing of the servo control (5) and the new quad rings (35). Do this with the bolt hole in the bracket (52).
(e) Install the bolt (55) through the connection of the bracket (52) and the servo control.
(f) Install the washer (85), the washers (89) and the nut (86) on the bolt (55).
(g) TORQUE the nut (86) to between 8.0 and 7.0 m.daN (59.00 and 51.62 lbf.ft )
.
(h) Install the locking cap (87) and the new AIPC 27-24-04-20-050 COTTER PIN (88) or AIPC 27-24-84-20-050 COTTER PIN (88).
(i) Measure the dimension between the nut and the locking cap with a CALIPER:
(a) If you install the servo control with integrated roller bearing and grease nipple (item 100 on the related figure):
(d) Apply a thin layer of the Synthetic Oil base Grease-General Purpose Lithium Thickened - (Material No.03GBD1) or the Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) to the new AIPC 27-24-51-01-070 QUAD RINGS (74).
(e) Attach the new quad rings (74) in position at the eye-end bearing of the servo control (5).
(f) Use the two GAGE - FEELER 0.25 mm (0.0098 in.) thick to carefully move the servo control (5) into the bracket (65).
(g) Align the eye-end bearing of the servo control (5) and the new quad rings (74). Do this with the bolt hole in the bracket (65).
(h) For the servo control (100):
Put the servo control (100) in position in the bracket (65) and make sure that the grease nipple is on the same side as the servo control lever.
(i) Install the bolt (62) through the connection of the bracket (65) and the servo control (5).
(j) Install the washer (95), the washers (90) and the nut (96) on the bolt (62).
(k) TORQUE the nut (96) to between 8.0 and 7.0 m.daN (59.00 and 51.62 lbf.ft )
.
(l) Install the locking cap (97) and the new AIPC 27-24-04-20-050 COTTER PIN (98) or AIPC 27-24-84-20-050 COTTER PIN (88).
(m) Measure the dimension between the nut and the locking cap with a CALIPER:
(12) Connect the spring rod (21) to the input lever (17) of the servo control (5) as follows:
(a) Make sure that the items that follow are clean and correctly installed in the input lever (17):
(c) Apply the Corrosion Preventive Compound-- Soft Film System (Material No.12AGC2) to the screw (18).
(d) Put the screw (18) into the connection of the input lever (17), and the eye-end of the spring rod (21).
(e) Install the washer (25) and the nut (26) on the screw (18).
(f) Tighten the nut (26).
(g) Safety the nut (26) with a new AIPC 27-21-04-08-050 COTTER PIN (27) or AIPC 27-21-84-11-010 COTTER PIN (27).
(13) Connect the hydraulic system as follows:
(a) Remove the CAP - BLANKING from the unions (28) and (39) of the servo control (5).
(b) Remove the CAP - BLANKING from the pipes (30) and (37).
(c) Make sure that the hydraulic line end-fittings are serviceable.
(d) Apply the Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) to the threads of the line end-fittings.
(e) Connect the union nut (38) of the pipe (37) to the union (39). Do this at the pressure port of the servo control (5).
(f) TORQUE the union nut (38) to between 1.7 and 1.5 m.daN (12.54 and 11.06 lbf.ft )
.
(g) Connect the union nut (29) of the pipe (30) to the union (28). Do this at the return port of the servo control (5).
(h) TORQUE the union nut (29) to between 2.3 and 2.0 m.daN (16.96 and 14.75 lbf.ft )
.
(i) Make sure that the pipes (30) and (37) have no deformation when you tighten the union nuts (29) and (38). Make sure that the pipes (30) and (37) do not touch the rear spar of the vertical stabilizer (1).
(j) Identify the tightened union nuts with a red line
(Ref. AMM TASK 20-23-22-910-001).
(14) Put the bonding jumper (33) in position at the servo control (5). Attach it with the screw (31) and the washer (32) (Ref. AMM TASK 20-28-00-912-802).
(15) Install the cable assembly (11) to the clamp (10) as follows:
(a) Put the eye-end of the cable assembly (11) in position.
(b) Put the screw (9) into the clamp (10) and the eye-end of the cable assembly (11).
(c) Install the washer (8) and the nut (12) on the screw (9).
(d) Tighten and safety the nut (12) with a new AIPC 27-24-04-20-220 COTTER PIN (13).
Subtask 27-24-51-640-050-A NOTE: The installation of the upper servo control 2025GM is given. The installation of the center servo control 3025GM and the lower servo control 1025GM is the same but with different hydraulic systems.
NOTE: You can also install the servo control with the integrated roller bearing and grease nipple on the rudder side.
The installation of this servo control with the roller bearing is different.
Refer to step (10) to see the difference.
(1) Apply the Mineral Oil base Grease-Anti-Fretting Paste - (Material No.03FDB1) to all the bolts and the bushes but not to bolt (62). The installation of this servo control with the roller bearing is different.
Refer to step (10) to see the difference.
(2) Install the bushes (34) and (36) in the bracket (52) of the vertical stabilizer (1).
(3) Install the washer (58), the locking plate (53) in the bracket (52) of the vertical stabilizer (1).
(4) Install the bushes (73) and (75) in the bracket (65) of the rudder (2).
(5) Install the washer (77) and the locking plate (64) in the bracket (65) of the rudder (2).
(6) Put the clamp (10) on the servo control (5).
(7) Put the servo control (5) in position at the bracket (52), (65).
(8) Make sure that the items that follow are correctly installed in the brackets (52) and (65):
- The locking plates (53) and (64)
- The washers (58) and (77)
- The bushes (34), (36), (73) and (75).
NOTE: In this procedure it is necessary for two persons to install the items that follow in the bracket (52):
(a) Apply a thin layer of the Synthetic Oil base Grease-General Purpose Lithium Thickened - (Material No.03GBD1) or the Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) to the new AIPC 27-24-51-01-075 QUAD RINGS (35). - The servo control (5)
- The quad rings (35).
(b) Attach the new quad rings (35) in position at the eye-end bearing of the servo control (5).
(c) Use the two GAGE - FEELER 0.25 mm (0.0098 in.) thick to carefully move the servo control (5) into the bracket (52).
(d) Align the eye-end bearing of the servo control (5) and the new quad rings (35). Do this with the bolt hole in the bracket (52).
(e) Install the bolt (55) through the connection of the bracket (52) and the servo control.
(f) Install the washer (85), the washers (89) and the nut (86) on the bolt (55).
(g) TORQUE the nut (86) to between 8.0 and 7.0 m.daN (59.00 and 51.62 lbf.ft )
. (h) Install the locking cap (87) and the new AIPC 27-24-04-20-050 COTTER PIN (88) or AIPC 27-24-84-20-050 COTTER PIN (88).
(i) Measure the dimension between the nut and the locking cap with a CALIPER:
- Make sure that the dimension is between 0.3 mm (0.01 in.) and 1.7 mm (0.07 in.).
(a) If you install the servo control with integrated roller bearing and grease nipple (item 100 on the related figure):
- It is not necessary to install quad rings.
- Because of this fact, the steps (d) thru (g) are NOT applicable.
- Two persons are necessary to install the servo control (5) AND the quad rings (74) into the bracket (65).
(d) Apply a thin layer of the Synthetic Oil base Grease-General Purpose Lithium Thickened - (Material No.03GBD1) or the Synthetic Ester base Grease-General Purpose Low Temp - (Material No.03HBD9) to the new AIPC 27-24-51-01-070 QUAD RINGS (74).
(e) Attach the new quad rings (74) in position at the eye-end bearing of the servo control (5).
(f) Use the two GAGE - FEELER 0.25 mm (0.0098 in.) thick to carefully move the servo control (5) into the bracket (65).
(g) Align the eye-end bearing of the servo control (5) and the new quad rings (74). Do this with the bolt hole in the bracket (65).
(h) For the servo control (100):
Put the servo control (100) in position in the bracket (65) and make sure that the grease nipple is on the same side as the servo control lever.
(i) Install the bolt (62) through the connection of the bracket (65) and the servo control (5).
(j) Install the washer (95), the washers (90) and the nut (96) on the bolt (62).
(k) TORQUE the nut (96) to between 8.0 and 7.0 m.daN (59.00 and 51.62 lbf.ft )
. (l) Install the locking cap (97) and the new AIPC 27-24-04-20-050 COTTER PIN (98) or AIPC 27-24-84-20-050 COTTER PIN (88).
(m) Measure the dimension between the nut and the locking cap with a CALIPER:
- Make sure that the dimension is between 0.3 mm (0.01 in.) and 1.7 mm (0.07 in.).
(12) Connect the spring rod (21) to the input lever (17) of the servo control (5) as follows:
(a) Make sure that the items that follow are clean and correctly installed in the input lever (17):
- The flanged bushes (19) and (24)
- The sliding bush (20).
(c) Apply the Corrosion Preventive Compound-- Soft Film System (Material No.12AGC2) to the screw (18).
(d) Put the screw (18) into the connection of the input lever (17), and the eye-end of the spring rod (21).
(e) Install the washer (25) and the nut (26) on the screw (18).
(f) Tighten the nut (26).
(g) Safety the nut (26) with a new AIPC 27-21-04-08-050 COTTER PIN (27) or AIPC 27-21-84-11-010 COTTER PIN (27).
(13) Connect the hydraulic system as follows:
(a) Remove the CAP - BLANKING from the unions (28) and (39) of the servo control (5).
(b) Remove the CAP - BLANKING from the pipes (30) and (37).
(c) Make sure that the hydraulic line end-fittings are serviceable.
(d) Apply the Phosphate Ester Hydraulic Fluid-General Power - - (Material No.02ABA1) to the threads of the line end-fittings.
(e) Connect the union nut (38) of the pipe (37) to the union (39). Do this at the pressure port of the servo control (5).
(f) TORQUE the union nut (38) to between 1.7 and 1.5 m.daN (12.54 and 11.06 lbf.ft )
. (g) Connect the union nut (29) of the pipe (30) to the union (28). Do this at the return port of the servo control (5).
(h) TORQUE the union nut (29) to between 2.3 and 2.0 m.daN (16.96 and 14.75 lbf.ft )
. (i) Make sure that the pipes (30) and (37) have no deformation when you tighten the union nuts (29) and (38). Make sure that the pipes (30) and (37) do not touch the rear spar of the vertical stabilizer (1).
(j) Identify the tightened union nuts with a red line
(Ref. AMM TASK 20-23-22-910-001).
(14) Put the bonding jumper (33) in position at the servo control (5). Attach it with the screw (31) and the washer (32) (Ref. AMM TASK 20-28-00-912-802).
(15) Install the cable assembly (11) to the clamp (10) as follows:
(a) Put the eye-end of the cable assembly (11) in position.
(b) Put the screw (9) into the clamp (10) and the eye-end of the cable assembly (11).
(c) Install the washer (8) and the nut (12) on the screw (9).
(d) Tighten and safety the nut (12) with a new AIPC 27-24-04-20-220 COTTER PIN (13).
D. Lubrication of the Servo Control with the Integrated Roller Bearing
(2) Use a GUN - GREASE to apply the Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. - (Material No.03GBC1) through the grease nipple until the new grease comes out.
(3) Remove the unwanted grease from the grease nipple with a clean Textile-Lint free Cotton - (Material No.14SBA1) .
Subtask 27-24-51-080-050-A NOTE: This lubrication is only necessary if you have installed the servo control with the integrated roller bearing.
(1) Clean the grease nipple of the rudder servo control rod eye-end bearing with a clean Textile-Lint free Cotton - (Material No.14SBA1) . (2) Use a GUN - GREASE to apply the Synthetic Oil base Grease-General Purpose Lithium Thickened Low Temp. - (Material No.03GBC1) through the grease nipple until the new grease comes out.
(3) Remove the unwanted grease from the grease nipple with a clean Textile-Lint free Cotton - (Material No.14SBA1) .
E. Removal of the Rigging Pin
(1) Remove the 98D27207546000 PIN-RIGGING (3) from the bellcrank assy (6) at the lower servo control 1025GM (5).
Subtask 27-24-51-865-052-A (1) Remove the 98D27207546000 PIN-RIGGING (3) from the bellcrank assy (6) at the lower servo control 1025GM (5).
F. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
Subtask 27-24-51-870-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | B04 |
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | B03 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | AUTO FLT/FAC1/28VDC | 5CC1 | H10 |
| 49VU | AUTO FLT/FAC1/26VAC | 14CC1 | H09 |
| ** ON A/C ALL | |||
| 121VU | AUTO FLT/FAC2/28VDC | 5CC2 | M19 |
| 121VU | AUTO FLT/FAC2/26VAC | 14CC2 | M18 |
G. Bleeding Procedure of the Rudder Servo Control
(2) Pressurize the reservoirs of the hydraulic systems (Ref. AMM TASK 29-14-00-614-002).
(3) Pressurize the Blue hydraulic system (see NOTE above) (Ref. AMM TASK 29-10-00-863-003).
(4) Make sure that the travel range of the servo controls and the rudder are clear of tools and other items.
(5) Operate the left and the right rudder pedals to move the rudder surface.
(7) Make sure that there are no leaks at the hydraulic connections to the servo control.
(8) Depressurize the Blue hydraulic system (see NOTE above) (Ref. AMM TASK 29-10-00-864-003).
(9) Remove the CONTAINER 5 L (1.32 USGAL).
(10) Remove all the signs of hydraulic fluid from the components in the work area.
Subtask 27-24-51-869-053-B NOTE: The bleeding procedure of the upper servo control 2025GM (Blue hydraulic system) is given. If you want to bleed the lower servo control 1025GM (Green hydraulic system) or the center servo control 3025GM (Yellow hydraulic system) you must pressurize/depressurize the related hydraulic system.
(1) Put the switch, A/SKID & N/W STRG, on the center panel 402VU to the OFF position. (2) Pressurize the reservoirs of the hydraulic systems (Ref. AMM TASK 29-14-00-614-002).
(3) Pressurize the Blue hydraulic system (see NOTE above) (Ref. AMM TASK 29-10-00-863-003).
(4) Make sure that the travel range of the servo controls and the rudder are clear of tools and other items.
(5) Operate the left and the right rudder pedals to move the rudder surface.
NOTE: Make sure that there is full and free movement of the rudder pedals.
(6) Operate the rudder pedals ten times and then put them in the neutral position. (7) Make sure that there are no leaks at the hydraulic connections to the servo control.
(8) Depressurize the Blue hydraulic system (see NOTE above) (Ref. AMM TASK 29-10-00-864-003).
(9) Remove the CONTAINER 5 L (1.32 USGAL).
(10) Remove all the signs of hydraulic fluid from the components in the work area.
H. Check of the Rudder Position
(2) In the cockpit: Make sure that the RUD TRIM indicator on the center pedestal panel 110VU, shows zero.
(3) Do the check of the rudder position with a servo control which you have not replaced (check 1):
(a) Pressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-863-001).
(b) Make sure that the trailing edge of the rudder aligns with the red reference triangle on the tail cone.
(c) If there is no red reference triangle on the tail cone, do the adjustment of the rudder neutral position (Ref. AMM TASK 27-24-00-820-001).
(d) If the trailing edge of the rudder and the red reference triangle do not align:
(a) Pressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-863-002).
(b) Make sure that the trailing edge of the rudder aligns with the red reference triangle on the tail cone.
(c) If there is no red reference triangle on the tail cone, do the adjustment of the rudder neutral position (Ref. AMM TASK 27-24-00-820-001).
(d) If the trailing edge of the rudder and the red reference triangle do not align:
(a) Pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003).
(b) Make sure that the trailing edge of the rudder aligns with the red reference triangle on the tail cone.
(c) If there is no red reference triangle on the tail cone, do the adjustment of the rudder neutral position (Ref. AMM TASK 27-24-00-820-001).
(d) If the trailing edge of the rudder and the red reference triangle do not align:
(a) For check 1: Use the Green hydraulic system.
(b) For check 2: Use the Blue hydraulic system.
(c) For check 3: Use the Yellow hydraulic system.
(7) If you have replaced the lower servo control 1025GM (Green hydraulic system):
(a) For check 1: Use the Yellow hydraulic system.
(b) For check 2: Use the Blue hydraulic system.
(c) For check 3: Use the Green hydraulic system.
Subtask 27-24-51-820-050-B NOTE: This procedure describes checks to make sure that the rudder is in the neutral position.
First you do the checks with the servo controls which you have NOT replaced (check 1 and 2). After this you do the check with the servo control which you have replaced (check 3).
In this procedure we describe the 3 checks of the replaced upper servo control 2025GM (Blue hydraulic system).
If you have replaced a different servo control refer to the steps (6) and (7) for details.
First you do the checks with the servo controls which you have NOT replaced (check 1 and 2). After this you do the check with the servo control which you have replaced (check 3).
In this procedure we describe the 3 checks of the replaced upper servo control 2025GM (Blue hydraulic system).
If you have replaced a different servo control refer to the steps (6) and (7) for details.
NOTE: The rudder is in the neutral position if the trailing edge of the rudder aligns with the red reference triangle on the tail cone.
(1) Install the 98D27207546000 PIN-RIGGING (3) in the bellcrank assy (6) at the lower servo control 1025GM. (2) In the cockpit: Make sure that the RUD TRIM indicator on the center pedestal panel 110VU, shows zero.
(3) Do the check of the rudder position with a servo control which you have not replaced (check 1):
(a) Pressurize the Green hydraulic system (Ref. AMM TASK 29-10-00-863-001).
(b) Make sure that the trailing edge of the rudder aligns with the red reference triangle on the tail cone.
(c) If there is no red reference triangle on the tail cone, do the adjustment of the rudder neutral position (Ref. AMM TASK 27-24-00-820-001).
(d) If the trailing edge of the rudder and the red reference triangle do not align:
- Do the adjustment procedure of the spring rod of the lower rudder servo control 1025GM (refer to the procedure below).
- If you need to adjust the spring rod:
Do not depressurize the Green hydraulic system at this time.
(a) Pressurize the Yellow hydraulic system (Ref. AMM TASK 29-10-00-863-002).
(b) Make sure that the trailing edge of the rudder aligns with the red reference triangle on the tail cone.
(c) If there is no red reference triangle on the tail cone, do the adjustment of the rudder neutral position (Ref. AMM TASK 27-24-00-820-001).
(d) If the trailing edge of the rudder and the red reference triangle do not align:
- Do the adjustment procedure of the spring rod of the center rudder servo control 3025GM (refer to the procedure below).
- If you need to adjust the spring rod:
Do not depressurize the Yellow hydraulic system at this time.
(a) Pressurize the Blue hydraulic system (Ref. AMM TASK 29-10-00-863-003).
(b) Make sure that the trailing edge of the rudder aligns with the red reference triangle on the tail cone.
(c) If there is no red reference triangle on the tail cone, do the adjustment of the rudder neutral position (Ref. AMM TASK 27-24-00-820-001).
(d) If the trailing edge of the rudder and the red reference triangle do not align:
- Do the adjustment procedure of the spring rod of the upper rudder servo control 2025GM (refer to the procedure below).
- If you need to adjust the spring rod:
Do not depressurize the Blue hydraulic system at this time.
(a) For check 1: Use the Green hydraulic system.
(b) For check 2: Use the Blue hydraulic system.
(c) For check 3: Use the Yellow hydraulic system.
(7) If you have replaced the lower servo control 1025GM (Green hydraulic system):
(a) For check 1: Use the Yellow hydraulic system.
(b) For check 2: Use the Blue hydraulic system.
(c) For check 3: Use the Green hydraulic system.
I. Adjustment Procedure of the Spring Rod
(2) Loosen the nuts (22) and the serrated locking device (23).
(3) Turn the body of the spring rod (21) until the rudder (2) is in the neutral position.
(5) Tighten the nuts (22) against the serrated locking device (23).
(6) Make sure that the threads of the rod end, block the inspection holes in the body of the spring rod (21).
(7) Safety the nuts (22) with14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - to the serrated locking device (23).
(8) After the adjustment: Depressurize the related hydraulic system
(Ref. AMM TASK 29-10-00-864-001) or (Ref. AMM TASK 29-10-00-864-002) or (Ref. AMM TASK 29-10-00-864-003).
Subtask 27-24-51-860-054-A NOTE: This adjustment is only necessary if the rudder is not in the neutral position.
NOTE: The related hydraulic system must be pressurized for this adjustment (Refer to the subtask 'Check of the Rudder Position' above).
(1) Cut and remove the lockwire from the nuts (22) of the spring rod (21). (2) Loosen the nuts (22) and the serrated locking device (23).
(3) Turn the body of the spring rod (21) until the rudder (2) is in the neutral position.
NOTE: The trailing edge of the rudder is in line with the red triangle on the tail cone.
(4) Engage the serrated locking device (23). (5) Tighten the nuts (22) against the serrated locking device (23).
(6) Make sure that the threads of the rod end, block the inspection holes in the body of the spring rod (21).
(7) Safety the nuts (22) with
(8) After the adjustment: Depressurize the related hydraulic system
(Ref. AMM TASK 29-10-00-864-001) or (Ref. AMM TASK 29-10-00-864-002) or (Ref. AMM TASK 29-10-00-864-003).
J. Preparation for the Test
(1) Remove the 98D27207546000 PIN-RIGGING (3) from the bellcrank assy (6) at the lower servo control 1025GM.
Subtask 27-24-51-710-050-A (1) Remove the 98D27207546000 PIN-RIGGING (3) from the bellcrank assy (6) at the lower servo control 1025GM.
K. Test Procedure
(1) Do an operational test of the rudder system (Ref. AMM TASK 27-24-00-710-001).
(2) Do an operational test of the rudder servo controls (Ref. AMM TASK 27-24-00-710-002), if all three servo controls are replaced.
5. Close-up(1) Do an operational test of the rudder system (Ref. AMM TASK 27-24-00-710-001).
(2) Do an operational test of the rudder servo controls (Ref. AMM TASK 27-24-00-710-002), if all three servo controls are replaced.
Subtask 27-24-51-860-055-A
A. Put the aircraft back to the serviceable condition.
(1) Put the switch A/SKID & N/W STRG on the center panel 402VU to the ON position.
(2) Remove the WARNING NOTICE(S).
Subtask 27-24-51-410-050-B (1) Put the switch A/SKID & N/W STRG on the center panel 402VU to the ON position.
(2) Remove the WARNING NOTICE(S).
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access panels 325BL 325CL 325CR 325DL at the trailing edge of the vertical stabilizer. (Ref. AMM TASK 55-33-13-410-002).
(3) Remove the access platform(s).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the access panels 325BL 325CL 325CR 325DL at the trailing edge of the vertical stabilizer. (Ref. AMM TASK 55-33-13-410-002).
(3) Remove the access platform(s).
Rudder Servo Controls