Record of the Weight of the Elevator

TASK 11-25-55-910-001-A
Record of the Weight of the Elevator

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.

MOVEMENT OF COMPONENTS CAN KILL OR CAUSE INJURY TO PERSONS AND/OR CAN CAUSE DAMAGE TO THE 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: 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.

WITHOUT A SAFETY HARNESS, YOU CAN FALL. THIS CAN KILL YOU OR CAUSE YOU INJURY.

WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.

CAUTION: DO NOT CAUSE DAMAGE TO THE SURFACES. THE COMPONENTS ARE MADE OF CARBONFIBER REINFORCED PLASTIC.

ZONE: 335
ZONE: 345
FIN: 4005KM

1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment

REFERENCE	QTY	DESIGNATION
No specific	AR	ACCESS PLATFORM 4M (13 FT)-ADJUSTABLE
No specific	1	DRILL DIA. 2,5 MM (0,098 IN)
No specific	1	PENCIL - SOFT
No specific	AR	SAFETY CLIP - CIRCUIT BREAKER
No specific	1	VIBRO ENGRAVER
No specific	1	WARNING NOTICE(S)
98D27309009003	2	COLLAR-DEPTH ACTUATOR
98D27309009004	2	COLLAR-DEPTH ACTUATOR
98D27903500000	2	PIN-SIDE STICK LOCKING

B. Consumable Materials

REFERENCE	DESIGNATION
(Material No.08BAA9)	Non Aqueous Cleaner-General - -
(Material No.14SBA1)	Textile-Lint free Cotton -

C. Work Zones and Access Panels

ZONE/ACCESS	ZONE DESCRIPTION
335	ELEVATOR
345	ELEVATOR

D. Referenced Information

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 55-13-11-000-001-A	Remove/Open of the Trimmable Horizontal Stabilizer (THS) Trailing-Edge Access-Panels
TASK 55-13-11-400-001-A	Install/Close of the Trimmable Horizontal Stabilizer (THS) Trailing-Edge Access-Panels
SRM 514211
Weight Identification Plate ** ON A/C NOT FOR ALL
Weight Identification Plate ** ON A/C NOT FOR ALL

3. Job Set-up
Subtask 11-25-55-860-050-A

A. Depressurize Hydraulic Systems
(1) Depressurize the Green, Yellow and Blue 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 11-25-55-865-050-A

B. Open, safety and tag this(these) circuit breaker(s):

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
49VU	FLIGHT CONTROLS/SEC1/NORM/SPLY	21CE1	B08
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/ELAC1/NORM/SPLY	15CE1	B06
49VU	FLIGHT CONTROLS/THS/ACTR/MOT2	19CE2	B04
49VU	FLIGHT CONTROLS/SEC1/NORM/SPLY	21CE1	B03
** ON A/C ALL
105VU	FLIGHT CONTROLS/ELAC2/STBY SPLY	16CE2	A02
105VU	FLT CTL/ELAC1/STBY SPLY	16CE1	A01
105VU	FLT CTL/SEC1/STBY SPLY	22CE	B01
121VU	FLIGHT CONTROLS/SEC3/SPLY	21CE3	Q19
121VU	FLIGHT CONTROLS/SEC2/SPLY	21CE2	Q18
121VU	FLIGHT CONTROLS/THS ACTR/MOT3	19CE3	Q17
121VU	FLIGHT CONTROLS/THS ACTR/MOT1	19CE1	Q16
121VU	FLIGHT CONTROLS/ELAC2/NORM/SPLY	15CE2	R20

Subtask 11-25-55-481-050-A

C. Install Locking Devices
(1) Put the 98D27903500000 PIN-SIDE STICK LOCKING in the CAPT and F/O side stick controllers.
(2) Install the 98D27309009003 COLLAR-DEPTH ACTUATOR or 98D27309009004 COLLAR-DEPTH ACTUATOR on the servocontrol elevators.

NOTE: Only the last version of the 98D27309009003 COLLAR-DEPTH ACTUATOR is applicable to the servo control with a roller bearing.

Subtask 11-25-55-941-050-A

D. 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 4M (13 FT)-ADJUSTABLE in position at zone 330 for the left hand elevator and/or zone 340 for the right hand elevator.

Subtask 11-25-55-020-050-A

E. Get Access
(1) Remove the applicable Trimmable Horizontal Stabilizer (THS) trailing-edge access-panels (Ref. AMM TASK 55-13-11-000-001).

4. Procedure
Subtask 11-25-55-970-050-A ** ON A/C NOT FOR ALL

A. Record of the Weight of the Elevator

WARNING: THIS PROCEDURE IS IN A CATEGORY KNOWN AS A CRITICAL DESIGN CONFIGURATION CONTROL LIMITATION (CDCCL). YOU MUST KEEP ALL CDCCL ITEMS IN THE APPROVED CONFIGURATION. MAKE SURE THAT THE WEIGHT OF THE ELEVATOR IS IN THE SPECIFIED LIMITS.

(1) Record the weight of the elevator on the weight identification plate (1).
(2) Replace the weight identification plate (1) if:
(a) There is no free line to record the new weight of the elevator, and/or
(b) The elevator has a new Part Number (P/N).
(3) Record the P/N on a new weight identification plate (1).
(4) Install the new weight identification plate (1) as follows:
(a) Put the new weight identification plate (1) in the correct position.
(b) Drill holes to install the rivets (2) as follows:
1 Make marks to show the position of the holes with the PENCIL - SOFT.
2 Drill holes with the DRILL DIA. 2,5 MM (0,098 IN).
3 Increase the hole diameter to the correct size of the rivets (2) which you must install.
4 Deburr the holes and remove the unwanted material.
5 Clean the work area with the Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(c) Install the new weight identification plate (1).
(d) Install the rivets (2) SRM 514211.
(5) Send the reporting sheet to AIRBUS.

Subtask 11-25-55-970-050-B ** ON A/C NOT FOR ALL

A. Record of the Weight of the Elevator

(1) Record the weight of the elevator on the weight identification plate (2).
(2) Replace the weight identification plate (1) if:
(a) There is not a free line to record the new weight of the elevator, and/or
(b) The elevator has a new Part Number (P/N):
1 Make a mark on the P/N on the weight identification plate (1) with the VIBRO ENGRAVER. Do this the first time you replace the weight identification plate (1) with the new identification plate (2).
(3) Record the P/N on a new weight identification plate (2).
(4) Install the new weight identification plate (2) as follows:
(a) Put the new weight identification plate (2) in the correct position.

NOTE: There are two possible positions to install the new weight identification plate (2).

(b) Drill holes to install the rivets (3) as follows:
1 Make marks to show the position of the holes with the PENCIL - SOFT.
2 Drill holes with the DRILL DIA. 2,5 MM (0,098 IN).
3 Increase the hole diameter to the diameter of the rivets (3) of 4 mm (0.157 in.).
4 Deburr the holes and remove the unwanted material.
5 Clean the work area with the Textile-Lint free Cotton - (Material No.14SBA1) made moist with Non Aqueous Cleaner-General - - (Material No.08BAA9) .
(c) Install the new weight identification plate (2).
(d) Install the rivets (3) SRM 514211.
(5) Send the reporting sheet to AIRBUS.

5. Close-up
Subtask 11-25-55-410-050-A

A. Close Access
(1) If removed, install the applicable THS trailing-edge access-panels (Ref. AMM TASK 55-13-11-400-001).

Subtask 11-25-55-081-050-A

B. Remove Locking Devices
(1) Remove the 98D27903500000 PIN-SIDE STICK LOCKING from the CAPT and F/O side stick controllers.

CAUTION: MAKE SURE THAT YOU REMOVE THE "COLLAR-ELEVATOR SERVO CONTROL SAFETY" BEFORE YOU PRESSURIZE THE ELEVATOR SERVO CONTROL. IF YOU DO NOT REMOVE THE COLLAR, YOU CAN CAUSE DAMAGE TO THE ELEVATOR SERVO CONTROL.

(2) Remove the 98D27309009003 COLLAR-DEPTH ACTUATOR or 98D27309009004 COLLAR-DEPTH ACTUATOR from the servocontrol elevators.

Subtask 11-25-55-942-050-A

C. Remove Ground Equipment
(1) Remove the ground support and maintenance equipment, the special and standard tools and all other items.
(2) Remove the access platform(s).
(3) Remove the WARNING NOTICE(S).

Subtask 11-25-55-865-051-A

D. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):

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
49VU	FLIGHT CONTROLS/SEC1/NORM/SPLY	21CE1	B08
** ON A/C NOT FOR ALL
49VU	FLIGHT CONTROLS/ELAC1/NORM/SPLY	15CE1	B06
49VU	FLIGHT CONTROLS/THS/ACTR/MOT2	19CE2	B04
49VU	FLIGHT CONTROLS/SEC1/NORM/SPLY	21CE1	B03
** ON A/C ALL
105VU	FLIGHT CONTROLS/ELAC2/STBY SPLY	16CE2	A02
105VU	FLT CTL/ELAC1/STBY SPLY	16CE1	A01
105VU	FLT CTL/SEC1/STBY SPLY	22CE	B01
121VU	FLIGHT CONTROLS/SEC3/SPLY	21CE3	Q19
121VU	FLIGHT CONTROLS/SEC2/SPLY	21CE2	Q18
121VU	FLIGHT CONTROLS/THS ACTR/MOT3	19CE3	Q17
121VU	FLIGHT CONTROLS/THS ACTR/MOT1	19CE1	Q16
121VU	FLIGHT CONTROLS/ELAC2/NORM/SPLY	15CE2	R20

[Rev.10 from 2021] 2026.03.31 22:54:22 UTC