Removal of the Horizontal Stabilizer Support Bearings
TASK 55-16-38-000-001-A
Removal of the Horizontal Stabilizer Support Bearings
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 55-16-38-860-051-A
Subtask 55-16-38-020-050-A
[Rev.10 from 2021]
2026.04.01 02:05:10 UTC
Removal of the Horizontal Stabilizer Support Bearings
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 TRAVEL RANGES OF THE FLIGHT CONTROLS SURFACES ARE CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE TO EQUIPMENT.
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:
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.
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.
CAUTION:
DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF CARBONFIBER REINFORCED PLASTIC.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 3M (10 FT) |
| No specific | AR | SAFETY CLIP - CIRCUIT BREAKER |
| No specific | AR | WARNING NOTICE(S) |
| 98D27407505000 | 1 | EXTRACTOR - CENTERING BUSH, THS |
| 98D27903500000 | 2 | PIN-SIDE STICK LOCKING |
| 98D55109009000 | 1 | WRENCH, GROOVE NUT |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 314AR, 333AB, 333AT, 334AB, 334AT, 343AB, 343AT, 344AB, 344AT |
| REFERENCE | DESIGNATION |
|---|---|
| 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 52-41-23-010-801-A | Opening of Access Door 314AR |
| TASK 53-56-11-000-001-A | Removal of the Support Fittings of the Trimmable Horizontal Stabilizer (THS) |
| TASK 55-13-11-000-001-A | Remove/Open of the Trimmable Horizontal Stabilizer (THS) Trailing-Edge Access-Panels |
| TASK 55-15-11-000-001-A | Removal of the Apron 333AT/333AB/343AT/343AB |
Subtask 55-16-38-860-051-A
A. Aircraft Maintenance Configuration
(1) Make sure that the horizontal stabilizer pitch trim control is set to zero.
(2) Make sure that the elevators touch their travel limit stops.
Subtask 55-16-38-860-050-A (1) Make sure that the horizontal stabilizer pitch trim control is set to zero.
(2) Make sure that the elevators touch their travel limit stops.
B. Depressurize Hydraulic Systems
(1) Depressurize the Green, Blue and Yellow hydraulic systems (Ref. AMM TASK 29-10-00-864-001) (Ref. AMM TASK 29-10-00-864-002) (Ref. AMM TASK 29-10-00-864-003).
Subtask 55-16-38-865-050-A (1) Depressurize the Green, Blue and Yellow hydraulic systems (Ref. AMM TASK 29-10-00-864-001) (Ref. AMM TASK 29-10-00-864-002) (Ref. AMM TASK 29-10-00-864-003).
C. Open, safety and tag this(these) circuit breaker(s):
Subtask 55-16-38-481-050-A | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B11 |
| 49VU | FLIGHT CONTROLS/THS/ACTR/MOT2 | 19CE2 | B09 |
| ** ON A/C NOT FOR ALL | |||
| 49VU | FLIGHT CONTROLS/ELAC1/NORM/SPLY | 15CE1 | B06 |
| 49VU | FLIGHT CONTROLS/THS/ACTR/MOT2 | 19CE2 | B04 |
| ** ON A/C ALL | |||
| 105VU | FLT CTL/ELAC1/STBY SPLY | 16CE1 | A01 |
| 121VU | FLIGHT CONTROLS/THS ACTR/MOT3 | 19CE3 | Q17 |
| 121VU | FLIGHT CONTROLS/THS ACTR/MOT1 | 19CE1 | Q16 |
D. Install Locking Devices
(1) Put the 98D27903500000 PIN-SIDE STICK LOCKING in the CAPT and F/O side stick controllers.
Subtask 55-16-38-941-050-A (1) Put the 98D27903500000 PIN-SIDE STICK LOCKING in the CAPT and F/O side stick controllers.
E. Safety Precautions
(1) Put the WARNING NOTICE(S) in the flight compartment to tell persons not to operate the flight controls.
(2) Put the WARNING NOTICE(S) in position to tell persons not to operate the hydraulic systems.
(3) Put the ACCESS PLATFORM 3M (10 FT) in position, at zones 314, 334 and 344.
(4) Put on and attach a safety harness before you start work in the work area
Subtask 55-16-38-010-050-A (1) Put the WARNING NOTICE(S) in the flight compartment to tell persons not to operate the flight controls.
(2) Put the WARNING NOTICE(S) in position to tell persons not to operate the hydraulic systems.
(3) Put the ACCESS PLATFORM 3M (10 FT) in position, at zones 314, 334 and 344.
(4) Put on and attach a safety harness before you start work in the work area
F. Access
(1) Open the access door 314AR (Ref. AMM TASK 52-41-23-010-801).
(2) Be careful not to step on a closed access door.
(3) Set the light switch to on.
(4) Remove aprons 333AT 333AB 343AT and 343AB (Ref. AMM TASK 55-15-11-000-001).
(5) Remove trailing edge panels 334AT 344AT 334AB 344AB (Ref. AMM TASK 55-13-11-000-001).
4. Procedure(1) Open the access door 314AR (Ref. AMM TASK 52-41-23-010-801).
(2) Be careful not to step on a closed access door.
(3) Set the light switch to on.
(4) Remove aprons 333AT 333AB 343AT and 343AB (Ref. AMM TASK 55-15-11-000-001).
(5) Remove trailing edge panels 334AT 344AT 334AB 344AB (Ref. AMM TASK 55-13-11-000-001).
Subtask 55-16-38-020-050-A
A. Removal of the Fittings and Support Bearings
(1) Remove the fittings (1) at the pivot points of the horizontal stabilizer (Ref. AMM TASK 53-56-11-000-001).
(2) Remove the horizontal stabilizer support bearings.
(a) Remove the sealing rings (2).
(b) Release the tab washers (4) and (7).
(c) Use 98D55109009000 WRENCH, GROOVE NUT to remove the ring nut (8).
(d) Remove the tabwasher (7).
(e) Remove the bearing (6) from the bearing housing (5).
(f) Use 98D55109009000 WRENCH, GROOVE NUT to remove the ring nut (3).
(g) Remove the tabwasher (4).
(h) Use 98D27407505000 EXTRACTOR - CENTERING BUSH, THS to remove the bearing housing (5).
(1) Remove the fittings (1) at the pivot points of the horizontal stabilizer (Ref. AMM TASK 53-56-11-000-001).
(2) Remove the horizontal stabilizer support bearings.
(a) Remove the sealing rings (2).
(b) Release the tab washers (4) and (7).
(c) Use 98D55109009000 WRENCH, GROOVE NUT to remove the ring nut (8).
(d) Remove the tabwasher (7).
(e) Remove the bearing (6) from the bearing housing (5).
(f) Use 98D55109009000 WRENCH, GROOVE NUT to remove the ring nut (3).
(g) Remove the tabwasher (4).
(h) Use 98D27407505000 EXTRACTOR - CENTERING BUSH, THS to remove the bearing housing (5).
Support Bearings - Horizontal Stabilizer Removal/Installation