W DOC AIRBUS | AMM A320F

Removal of the Reservoir to Manifold Pressurized Air Drain Tube [CFMB]


TASK 71-73-49-000-002-B
Removal of the Reservoir to Manifold Pressurized Air Drain Tube


FIN: 1000EM1 ** ON A/C NOT FOR ALL
FIN: 1000EM2 ** 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
COVER - PROTECTION
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-040-B
Opening of the Fan Cowl Doors
3. Job Set-up
Subtask 71-73-49-941-064-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) On the center pedestal, on the ENG panel 115VU:
     (a) Put a WARNING NOTICE(S) to tell persons not to start the engine.
   (2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
   (3) On the overhead maintenance panel 50VU:
     (a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
     (b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
Subtask 71-73-49-010-064-A ** ON A/C NOT FOR ALL
B. Open the fan cowl doors: (Ref. AMM TASK 71-13-00-010-040)
   (1) FOR [1000EM1] (ENGINE-1)
437AL 438AR
   (2) FOR [1000EM2] (ENGINE-2)
447AL 448AR
4. Procedure
Subtask 71-73-49-020-063-A ** ON A/C NOT FOR ALL
A. Removal of the Reservoir to Manifold Pressurized Air Drain Tube
   (1) Disconnect the reservoir to manifold pressurized air drain tube (5) from the manifold module.
   (2) Disconnect the drain tube (5) from the drain reservoir module.
   (3) Remove the drain tube (5) from the engine.
   (4) Put COVER - PROTECTION on the manifold module, the drain reservoir, and the drain tube (5).
[Rev.10 from 2021] 2026.04.01 02:27:36 UTC