W DOC AIRBUS | AMM A320F

Visual Check of Engine Booster Antiicing Ducts [CFML]


TASK 75-11-49-210-801-A
Visual Check of Engine Booster Antiicing Ducts


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.
ZONE: 400
1. Reason for the Job
Refer to the MPD TASK: 302149-06
VISUAL CHECK OF ENGINE BOOSTER ANTIICING DUCTS.
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
400
POWER PLANT, NACELLES AND PYLONS
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL, 438AR, 451AL, 452AR
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL, 448AR, 461AL, 462AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-803-A
Opening of the Fan Cowl Doors
TASK 71-13-00-410-803-A
Closing of the Fan Cowl Doors
TASK 78-30-00-040-809-A
Deactivation of the Thrust Reverser System for Ground Maintenance
TASK 78-30-00-440-809-A
Reactivation of the Thrust Reverser System after Ground Maintenance
TASK 78-36-00-010-806-A
Opening of the Thrust Reverser Cowl Doors
TASK 78-36-00-410-806-A
Closing of the Thrust Reverser Cowl Doors
3. Job Set-up
Subtask 75-11-49-941-058-A
A. Safety Precautions
   (1) On the center pedestal, on ENG panel 115VU:
     (a) Make sure that the ENG/MODE selector switch is in the NORM position.
     (b) Make sure that the ENG/MASTER 1(2) control switch was in the OFF position not less than five minutes before you do this procedure.
     (c) Put a WARNING NOTICE(S) in position to tell persons not to operate:
  • The ENG/MODE selector switch
  • The ENG/MASTER 1(2) control switch.
   (2) On the ENG section of maintenance panel 50VU:
     (a) Make sure that the ON legend of the FADEC GND PWR/1(2) pushbutton switch is off.
     (b) Put a WARNING NOTICE(S) in position to tell persons not to energize FADEC 1(2).
Subtask 75-11-49-010-050-A
B. Get Access
   (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-803):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL, 438AR.
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL, 448AR.
   (2) Put an ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position.
Subtask 75-11-49-040-050-A
C. Deactivation of the Thrust Reverser (T/R) System for Maintenance
WARNING: YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE AN INJURY AND/OR DAMAGE.
   (1) Do the deactivation of the T/R system for ground maintenance (Ref. AMM TASK 78-30-00-040-809).
Subtask 75-11-49-010-051-A
D. Get Access
   (1) Open the T/R cowl doors (Ref. AMM TASK 78-36-00-010-806):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
451AL, 452AR.
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
461AL, 462AR.
4. Procedure
Subtask 75-11-49-210-051-A
A. Visual Check of Engine Booster Anti-Icing Ducts
INSPECT/CHECK
MAXIMUM SERVICEABLE LIMITS
REMARKS
1.Examine ducts for:


A.Cracks, splits and kinks
Not serviceable
Replace duct, contact CFM.
B.Wear on welded sleeves
Depth of wear must not be more than 50 percent of the thickness of the sleeve
Replace duct, contact CFM.
2.Examine ducts brackets for:


A.Wear
10 percent of the thickness or 10 percent of the hole diameter
Replace duct, contact CFM.
B.Cracks or separation
Not serviceable
Replace duct, contact CFM.
3.Examine the V-band clamps and retaining strap clamps for:


A.Cracks
Not serviceable
Replace V- band clamp or retaining strap clamp, contact CFM.
4.Make sure that the retaining strap clamps are correctly installed.

If needed, correct position, contact CFM.
5.Make sure that the ducting has no signs of air leaks, on the surrounding surface.

If damage, replace the duct, contact CFM.
5. Close-up
Subtask 75-11-49-410-050-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the T/R cowl doors (Ref. AMM TASK 78-36-00-410-806):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
451AL, 452AR.
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
461AL, 462AR.
Subtask 75-11-49-440-050-A
B. Do the reactivation of the T/R system after ground maintenance (Ref. AMM TASK 78-30-00-440-809).
Subtask 75-11-49-410-051-A
C. Close Access
   (1) Remove the access platform(s).
   (2) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-803):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL, 438AR.
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL, 448AR.
Subtask 75-11-49-942-050-A
D. Put the aircraft back to its initial configuration.
   (1) Remove the access platform(s).
   (2) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 03:14:04 UTC