W DOC AIRBUS | AMM A320F

Protection of the Ram Air Turbine (RAT) Blades (Aluminum Blades) from Corrosion


TASK 29-22-00-916-801-A
Protection of the Ram Air Turbine (RAT) Blades (Aluminum Blades) from Corrosion


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: 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: MAKE SURE THAT THE RAT TRAVEL RANGE IS CLEAR BEFORE YOU EXTEND/RETRACT THE RAT.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 195
1. Reason for the Job
NOTE: This procedure gives the instruction to prevent corrosion of the RAT blades.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
SAFETY BARRIER(S)
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.08BBD1)
Non Aqueous Cleaner-- Isopropyl Alcohol -
(Material No.12ABD1)
Corrosion Preventive Compound-Water Displacing Ultra-thin Film -
(Material No.14SBA1)
Textile-Lint free Cotton -
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
195
HYDRAULIC COMPT AND FAIRINGS
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 29-00-00-864-001-A
Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action
TASK 29-00-00-910-002-A
Safety Procedures of the Hydraulic System
TASK 29-14-00-614-001-A
Depressurization of the Hydraulic Reservoirs
TASK 29-22-00-869-005-A
Extension of the Ram Air Turbine (RAT) on the Ground
TASK 29-22-00-869-006-A
Retraction of the Ram Air Turbine (RAT) on the Ground
3. Job Set-up
Subtask 29-22-00-860-144-A
A. Aircraft Maintenance Configuration
WARNING: OBEY THE HYDRAULIC SAFETY PROCEDURES.
   (1) Obey the hydraulic safety procedures (Ref. AMM TASK 29-00-00-910-002).
   (2) Put the SAFETY BARRIER(S) in position.
   (3) Put the WARNING NOTICE(S) in position to tell persons not to pressurize the Blue hydraulic system:
  • In the cockpit, on hydraulic section 40VU of the overhead panel
  • On the ground service panel of the Blue hydraulic system.
   (4) Depressurize the Blue hydraulic system and put it in the maintenance configuration (Ref. AMM TASK 29-00-00-864-001).
   (5) Depressurize the reservoir of the Blue hydraulic system.
(Ref. AMM TASK 29-14-00-614-001).
WARNING: MAKE SURE THAT THE RAT TRAVEL RANGE IS CLEAR BEFORE YOU EXTEND/RETRACT THE RAT.
   (6) Extend the RAT (Ref. AMM TASK 29-22-00-869-005).
   (7) Put the WARNING NOTICE(S) in position to tell persons not to operate the RAT:
  • On overhead panels 21VU and 40VU.
Subtask 29-22-00-865-153-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUHYD/RAT/CTL2801GED14
** ON A/C NOT FOR ALL
49VUHYD/RAT/CTL2801GEB13
** ON A/C ALL
106VUCSM/G /EV/MAN/SPLY6XEB04
121VUHYDRAULIC/RAT/SPLY/EXTN/SOL12803GEP33
4. Procedure
Subtask 29-22-00-916-050-A
A. Protection of the RAT Blades
   (1) Clean the RAT blades with Textile-Lint free Cotton - (Material No.14SBA1) and Non Aqueous Cleaner-- Isopropyl Alcohol - (Material No.08BBD1) .
   (2) Put the RAT blades in horizontal position and rub Corrosion Preventive Compound-Water Displacing Ultra-thin Film - (Material No.12ABD1) fully around the front and back surfaces of each blade.
     (a) Be careful to apply Corrosion Preventive Compound-Water Displacing Ultra-thin Film - (Material No.12ABD1) only to the blade surfaces and do not let it flow into the turbine blade bearing.
NOTE: It is not possible to apply Corrosion Preventive Compound-Water Displacing Ultra-thin Film - (Material No.12ABD1) too frequently or too much with this procedure.
   (3) After you apply the Corrosion Preventive Compound-Water Displacing Ultra-thin Film - (Material No.12ABD1) , make sure that the RAT blades have a tack-free moist surface.
5. Close-up
Subtask 29-22-00-865-154-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
49VUHYD/RAT/CTL2801GED14
** ON A/C NOT FOR ALL
49VUHYD/RAT/CTL2801GEB13
** ON A/C ALL
106VUCSM/G /EV/MAN/SPLY6XEB04
121VUHYDRAULIC/RAT/SPLY/EXTN/SOL12803GEP33
Subtask 29-22-00-860-145-A
B. Put the aircraft back to the serviceable condition.
   (1) Make sure that the work area is clean and clear of tools and other items.
WARNING: MAKE SURE THAT THE RAT TRAVEL RANGE IS CLEAR BEFORE YOU EXTEND/RETRACT THE RAT.
   (2) Retract the RAT (Ref. AMM TASK 29-22-00-869-006).
   (3) Remove the SAFETY BARRIERS.
   (4) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 00:25:55 UTC