W DOC AIRBUS | AMM A320F

Removal of the Sealol Seal [CFMI]


TASK 72-63-00-000-006-A
Removal of the Sealol Seal


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
CONTAINER - STORAGE
No specific
AR
WARNING NOTICE(S)
856A1130
1
TOOL SET - JACK SCREW
856A3576
1
SEALOL AND MAGNETIC SEALS-R/I
 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-A
Opening of the Fan Cowl Doors
3. Job Set-up
Subtask 72-63-00-941-055-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 72-63-00-010-061-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 72-63-00-020-056-A ** ON A/C NOT FOR ALL
A. Removal of the Sealol Seal
CAUTION: THE SEALOL SEALS ARE MATCHED ASSEMBLIES. IF ONE OF THE COMPONENTS IS DAMAGED, YOU MUST REPLACE THE COMPLETE SEAL.
   (1) Remove the 3 nuts (110) and washers (100) which attach the sealol seal housing (90).
   (2) Remove the sealol seal housing (90) with the 856A1130 TOOL SET - JACK SCREW (856A1130P12).
   (3) Remove and discard the O-ring (120).
   (4) Remove the rotating mating ring (130) as follows:
NOTE: For the fuel pump and the hydraulic pump, use sleeve 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P09), for 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P10) and nut, 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P11). and P11. For starter and Integrated Drive Generator (IDG), use sleeve, 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P02), collet 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P03) and nut 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P06).
     (a) Loosen nut, 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P06) or 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P11) and screw, 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P05), of the tool, and install on the rotating mating ring until contact with sleeve 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P02) or 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P09). Tighten screw, 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P05).
     (b) Remove the rotating mating ring with the impact puller.
     (c) For the fuel pump and hydraulic pump drive pads
       1 Remove and discard the o-ring (140) from inner diameter of the rotating mating ring (130).
     (d) For the starter and IDG drive pads

PRE SB CFM 72-474

       1 Remove and discard the O-ring (140) from inner diameter of the rotating mating ring (130)

END OF SB CFM 72-474

POST SB CFM 72-474

       2 Remove and discard the bal-seal (145) from inner diameter of the rotating mating ring (130).

END OF SB CFM 72-474
     (e) Loosen nut, 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P06) or 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P11), and screw, 856A3576 SEALOL AND MAGNETIC SEALS-R/I (856A3576P05). Remove the tool. Remove the rotating mating ring, and put it in the CONTAINER - STORAGE.
[Rev.10 from 2021] 2026.04.01 02:40:21 UTC