W DOC AIRBUS | AMM A320F

Installation of the Thrust Reverser Opening Actuator [IAE]


TASK 78-36-51-400-010-A
Installation of the Thrust Reverser Opening Actuator


WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE PARTS AFTER THE ENGINE SHUTDOWN. USE APPLICABLE THERMAL GLOVES. THE ENGINE PARTS CAN STAY HOT FOR ONE HOUR AFTER SHUTDOWN AND CAN BURN YOU.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
WARNING: DO NOT LET ENGINE OIL STAY ON YOUR SKIN FOR A LONG TIME. FLUSH THE OIL FROM YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN GO THROUGH YOUR SKIN AND INTO YOUR BODY.
CAUTION: DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. UNWANTED FUEL OR OIL MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.
ZONE: 400
FIN: 3003KM1 ** ON A/C NOT FOR ALL
FIN: 3003KM2 ** ON A/C NOT FOR ALL
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 2M (6 FT)
No specific
AR
COVER - BLANKING
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 255 and 225 lbf.in (2.88 and 2.54 m.daN ) T
IAE1N20009
1
PUMP HYDRAULIC UNIT-REVERSER C-DUCT
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.V10-077)
lubricant (engine oil)
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
400
POWER PLANT, NACELLES AND PYLONS
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 451AL, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL, 462AR
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 70-23-11-911-013-A
General Torque Tightening Techniques
TASK 71-13-00-010-010-A
Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 71-13-00-410-010-A
Closing of the Fan Cowls 437AL(447AL),438AR(448AR)
TASK 78-30-00-040-012-A
Deactivation of the Thrust Reverser Hydraulic Control Unit (HCU) for Ground Maintenance
TASK 78-30-00-440-012-A
Re-activation of the Thrust Reverser Hydraulic Control Unit (HCU) after Ground Maintenance
TASK 78-32-00-010-010-A
Opening of the Thrust Reverser Halves
TASK 78-32-00-410-010-A
Closing of the Thrust Reverser Halves
TASK 78-36-49-400-010-A
Installation of the Thrust Reverser Opening Tubes and Manifold
3. Job Set-up
Subtask 78-36-51-860-051-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
   (1) On the center pedestal, on the ENG panel 115VU, make sure that a WARNING NOTICE(S) is in position to tell persons not to start the engine.
   (2) On the overhead maintenance panel 50VU, make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off. Make sure that a WARNING NOTICE(S) is in position to tell persons not to energize the FADEC 1(2).
   (3) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position.
Subtask 78-36-51-010-057-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Make sure that the fan cowl doors are open: (Ref. AMM TASK 71-13-00-010-010)
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR
   (2) Make sure that the thrust reverser doors are open: (Ref. AMM TASK 78-32-00-010-010)
     (a) FOR [1000EM1] (ENGINE-1)
451AL 452AR
     (b) FOR [1000EM2] (ENGINE-2)
461AL 462AR
Subtask 78-36-51-040-054-A ** ON A/C NOT FOR ALL
C. Make sure that the thrust reverser Hydraulic Control Unit (HCU) is deactivated: (Ref. AMM TASK 78-30-00-040-012)
Subtask 78-36-51-620-052-A ** ON A/C NOT FOR ALL
D. Remove the caps from the opening actuator port.
Subtask 78-36-51-611-050-A ** ON A/C NOT FOR ALL
E. Fill the opening actuator with V10-077lubricant (engine oil) before installation.
   (1) Push the actuator (5) to its fully retracted position.
   (2) Connect the hydraulic hand pump IAE1N20009 PUMP HYDRAULIC UNIT-REVERSER C-DUCT directly to the actuator.
   (3) Use the hand pump to fill and fully extend the actuator with V10-077lubricant (engine oil) and bleed off the air.
   (4) Remove the hand pump from the actuator.
Subtask 78-36-51-620-050-A ** ON A/C NOT FOR ALL
F. Install the COVER - BLANKING to the opening actuator port.
4. Procedure
Subtask 78-36-51-420-051-A ** ON A/C NOT FOR ALL
A. Install the opening actuator.
   (1) Put the opening actuator (5) in position in the mount (15) on the thrust reverser half.
   (2) Install the bolt (13), the washer (14), the bushing (16), the washer (20) and the nut (17) which attach the opening actuator (5) to the pylon hinge beam (1).
   (3) Install the bolt (4), the washer (18), the bushing (3), the washer (19), and the nut (2) which attach the actuator (5) to the mount (15).
   (4) TORQUE the two nuts (2) and (17) to between 255 and 225 lbf.in (2.88 and 2.54 m.daN ) T (Ref. AMM TASK 70-23-11-911-013).
Subtask 78-36-51-620-053-A ** ON A/C NOT FOR ALL
B. Remove the caps from the opening actuator port and the hydraulic hose.
Subtask 78-36-51-420-052-A ** ON A/C NOT FOR ALL
C. Bleed the opening actuator system and connect the hydraulic hose to the opening actuator (Ref. AMM TASK 78-36-49-400-010).
Subtask 78-36-51-410-055-A ** ON A/C NOT FOR ALL
D. Attach the flexible hose upper and cover to the opening actuator (Ref. AMM TASK 78-36-49-400-010).
5. Close-up
Subtask 78-36-51-410-054-A ** ON A/C NOT FOR ALL
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the thrust reverser halves (Ref. AMM TASK 78-32-00-410-010)
     (a) FOR [1000EM1] (ENGINE-1)
451AL 452AR.
     (b) FOR [1000EM2] (ENGINE-2)
461AL 462AR.
Subtask 78-36-51-440-052-A ** ON A/C NOT FOR ALL
B. Activate the thrust reverser HCU (Ref. AMM TASK 78-30-00-440-012).
Subtask 78-36-51-410-056-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Close the fan cowls (Ref. AMM TASK 71-13-00-410-010).
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR.
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
   (2) Remove the WARNING NOTICE(S).
   (3) Remove the access platform(s).
[Rev.10 from 2021] 2026.04.01 03:30:03 UTC