W DOC AIRBUS | AMM A320F

Removal of the Fan Rotor Blades [CFMB]


TASK 72-21-00-000-007-A
Removal of the Fan Rotor Blades


CAUTION: ALL FAN ROTOR BLADES SHALL BE MATCHMARKED OR NUMBERED FOR ASSEMBLY IN ORIGINAL ALIGNMENT AND POSITION USING ONLY APPROVED MARKING MATERIAL.
ZONE: 400
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
1
ACCESS PLATFORM 1M(3 FT)
No specific
1
MAT - PROTECTIVE
No specific
AR
MAT - RUBBER
No specific
AR
WARNING NOTICE(S)
856A2631
1
STAND,STORAGE-FAN BLADES
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.CP5061)
temporary marking
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
400
POWER PLANT, NACELLES AND PYLONS
 D. Referenced Information
REFERENCE
DESIGNATION
TASK 72-21-00-000-005-A
Removal of the Spinner Front Cone
TASK 72-21-00-000-006-A
Removal of the Spinner Rear Cone
3. Job Set-up
Subtask 72-21-00-941-069-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Put the ACCESS PLATFORM 1M(3 FT) in position.
   (2) On the center pedestal, on the ENG panel 115VU:
     (a) Put a WARNING NOTICE(S) to tell persons not to start the engine.
   (3) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
   (4) 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).
   (5) Install a MAT - PROTECTIVE in lower half of the inlet cowl.
Subtask 72-21-00-010-058-A ** ON A/C NOT FOR ALL
B. Preparation for Removal of the Fan Blades:
   (1) Install a MAT - RUBBER in the inlet cowl before you go into it.
   (2) Remove spinner front cone. (Ref. AMM TASK 72-21-00-000-005)
   (3) Remove spinner rear cone. (Ref. AMM TASK 72-21-00-000-006)
NOTE: Removal will be easier if fan blade to be removed is placed at the 12 o'clock position.
4. Procedure
Subtask 72-21-00-020-065-A ** ON A/C NOT FOR ALL
A. Removal of the fan blades:
CAUTION: USE ONLY APPROVED MARKING MATERIAL TO PREVENT DAMAGE TO THE BLADES.
   (1) Temporarily mark each blade (80) from 1 to 36 on their convex side. Use a temporary marking (Material No.CP5061) . Blade No. 1 will be the blade immediately above the offset hole in the fan disk bolt flange. Numbering is counter-clockwise (CCW), forward looking aft.
   (2) Removal of the first and second fan blades circled 1 and 2.
NOTE: The removal of blades (80) is counterclockwise (CCW) after the first blade removed.
NOTE: Put the first blade to be removed at the 12 o'clock position to ease the removal.
     (a) Remove spacer (70) from the fan blade circled 2 located immediately at left of the first blade circled 1 you want to remove.
Carefully lower blade circled 2 in its dovetail recess (this unlocks it from its engagement on the booster spool), and move it at a slope (inclined) to the left. Do not try to remove it now.
     (b) Remove spacer (70) from the first blade circled 1 to be removed.
     (c) Lower blade circled 1 in its dovetail recess (this unlocks it), and carrefully pull it forward while you move its left midspan shroud above the right midspan shroud of the (sloped) blade circled 2 at left. Remove blade circled 1.
     (d) Remove blade.
   (3) Removal of the 3rd to the 36th blades:
     (a) The removal of the following blades is easier, done CCW, and as follows for each blade:
       1 Remove spacer (70)
       2 Remove blade (80).
   (4) Put spacer (70) and fan blades from 1 through 36 in their related compartements on 856A2631 STAND,STORAGE-FAN BLADES (865A2631G01)
[Rev.10 from 2021] 2026.04.01 12:59:41 UTC