W DOC AIRBUS | AMM A320F

Removal of the VBV System Main Flexible Shaft [CFMI]


TASK 75-31-30-000-004-A
Removal of the VBV System Main Flexible Shaft


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
ACCESS PLATFORM 1M(3 FT)
No specific
AR
WARNING NOTICE(S)
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
FOR [1000EM1] (ENGINE-1)
437AL, 438AR, 451AL, 452AR
FOR [1000EM2] (ENGINE-2)
447AL, 448AR, 461AL, 462AR
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-13-00-010-040-A
Opening of the Fan Cowl Doors
TASK 75-31-30-200-001-A
Visual Inspection of the VBV Main Flexible Shaft and the VBV Inter-connecting Flexible Shafts
TASK 75-31-50-000-001-A
Removal of the Bleed Valve and Master Ballscrew Actuator
TASK 78-30-00-481-041-A
Make the Thrust Reverser Unserviceable for Maintenance
TASK 78-36-00-010-040-A
Opening of the Thrust Reverser Doors
3. Job Set-up
Subtask 75-31-30-941-051-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 75-31-30-010-053-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Open the fan cowl doors: (Ref. AMM TASK 71-13-00-010-040)
     (a) FOR [1000EM1] (ENGINE-1)
437AL 438AR
     (b) FOR [1000EM2] (ENGINE-2)
447AL 448AR.
   (2) Put the ACCESS PLATFORM 1M(3 FT) in position.
Subtask 75-31-30-040-052-A ** ON A/C NOT FOR ALL
C. Make the thrust reverser unserviceable (Ref. AMM TASK 78-30-00-481-041).
Subtask 75-31-30-010-054-A ** ON A/C NOT FOR ALL
D. Open the thrust reverser cowl doors: (Ref. AMM TASK 78-36-00-010-040)
   (1) FOR [1000EM1] (ENGINE-1)
451AL 452AR
   (2) FOR [1000EM2] (ENGINE-2)
461AL 462AR.
4. Procedure
Subtask 75-31-30-020-051-A ** ON A/C NOT FOR ALL
A. Removal of the VBV system main flexible shaft
CAUTION: BE CAREFUL NOT TO DAMAGE THE PROTECTING BOOT (PRE CFM56-5 SB 75-0038) ON THE STOP MECHANISM. ONLY BLEED VALVE STOP MECHANISM WHICH INCLUDES PACKED SEALED BEARINGS, HAS NOT A PROTECTING BOOT (POST CFM56-5 SB 75-0038).
   (1) Remove the bleed valve and master ballscrew actuator (Ref. AMM TASK 75-31-50-000-001).
   (2) Pull the main flexible shaft out of the fuel gear motor and stop mechanism assembly, through the protecting boot for stop mechanism equipped with (PRE CFM56-5 SB 75-0038).
   (3) Do the visual inspection of the VBV main flexible shaft and of the inter-connecting flexible shafts (Ref. AMM TASK 75-31-30-200-001).
[Rev.10 from 2021] 2026.04.02 06:36:55 UTC