W DOC AIRBUS | AMM A320F

Removal of the Seal and V-Band at the Nacelle Inlet Aft Bulk Interface


TASK 30-21-49-000-809-A
Removal of the Seal and V-Band at the Nacelle Inlet Aft Bulk Interface


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.
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
CAP - PROTECTION
No specific
AR
COVER - PROTECTION
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENGINE 1)
437AL, 438AR
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENGINE 2)
447AL, 448AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-803-A
Opening of the Fan Cowl Doors
3. Job Set-up
Subtask 30-21-49-941-110-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 WARNING NOTICE(S) in position to tell persons not to operate the ENG/MODE selector switch and 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 30-21-49-865-111-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
FOR FIN: 4020KM1 (POWER PLANTDEMOUNTABLE, ENGINE 1)
122VUANTI ICE/ENG/11DN1X10
FOR FIN: 4020KM2 (POWER PLANTDEMOUNTABLE, ENGINE 2)
122VUANTI ICE/ENG/21DN2W10
Subtask 30-21-49-010-151-A
C. 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
4. Procedure
Subtask 30-21-49-020-092-A
A. Removal of the Seal and V-Band at the Nacelle Inlet Aft Bulk Interface
   (1) Loosen the coupling nut and disconnect the indicating tube (1) from the anti-ice duct section (7).
   (2) Cut the two coupling bands (6) and discard them.
   (3) Remove the insulation boot (4) at the forward end of the anti-ice duct section (7).
   (4) Open and remove the V-band clamp (3) at the forward end of the anti-ice duct section (7).
   (5) Remove the two bolts (9) that attach the flange on the anti-ice duct section (7) to the support bracket (8).
   (6) Move the anti-ice duct section (7) away from the flange on the inlet (5).
   (7) Remove the E-seal (2) from the inlet (5).
   (8) Install COVER - PROTECTION and CAP - PROTECTION on all the open ports, open tubes, open hoses and connectors.
[Rev.10 from 2021] 2026.04.01 00:29:52 UTC