W DOC AIRBUS | AMM A320F

Visual Inspection of the Fan Hub Dovetail Slots [PW11]


TASK 72-11-06-210-801-A
Visual Inspection of the Fan Hub Dovetail Slots


WARNING: MAKE SURE THAT THE ENGINE SHUTDOWN OCCURRED NOT LESS THAN FIVE MINUTES BEFORE YOU DO THIS PROCEDURE. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.
WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 430
ZONE: 440
1. Reason for the Job
Use this procedure to do a visual inspection of the dovetail slots of the fan hub.
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
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
430
ENG 1 AIR INTAKE, FAN AND ACCESS GEARBOX
440
ENG 2 AIR INTAKE, FAN AND ACCESS GEARBOX
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 71-00-00-860-833-A
Procedure to Prevent Engine Motoring
TASK 72-11-03-000-801-A
Removal of the Fan Blades
TASK 72-11-03-400-801-A
Installation of the Fan Blades
3. Job Set-up
Subtask 72-11-06-941-052-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Do the procedure to prevent engine motoring (Ref. AMM TASK 71-00-00-860-833).
   (2) Put an ACCESS PLATFORM 1M(3 FT) in the intake cowl.
   (3) Put a MAT - PROTECTIVE in the intake cowl.
   (4) Remove the inlet cone and the fan blades to get access to the inspection area (Ref. AMM TASK 72-11-03-000-801).
4. Procedure
Subtask 72-11-06-210-051-A ** ON A/C NOT FOR ALL
A. Visual Inspection of the Fan Hub Dovetail Slots
F Fan Hub Dovetail Slots ** ON A/C NOT FOR ALL
CAUTION: WIPE CLEAN ALL PARTS AND TOOLS AS NECESSARY TO REMOVE UNWANTED DEBRIS AND PREVENT DAMAGE TO THE ENGINE.
   (1) Do a visual inspection of the fan hub dovetail slots.
   (2) Examine the assembly for foreign objects, damage and correct assembly.

Table 1: Fan Hub Dovetail Slots - Visual Inspection
EXAMINE
DAMAGE
DISPOSITION
Dovetail pressure faces for:


Nicks, dents and scratches
All quantities
Not permitted. Remove the engine or contact Pratt & Whitney before the next flight.
Galling
All quantities
Not permitted. Remove the engine or contact Pratt & Whitney before the next flight.
Dovetail slot bottom for:


Nicks, dents and scratches
All quantities
Not permitted. Remove the engine or contact Pratt & Whitney before the next flight.
Anti-gallant coating
Missing and thinned anti-gallant coating due to rubbing or burnishing with no base metal damage
Permitted

Flaking or gouge of anti-gallant coating
Not permitted. Remove the engine or contact Pratt & Whitney before the next flight.
5. Close-up
Subtask 72-11-06-942-051-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
   (1) Install the inlet cone and the fan blades (Ref. AMM TASK 72-11-03-400-801).
   (2) Remove the MAT - PROTECTIVE from the intake cowl.
   (3) Remove the access platform(s).
   (4) Make sure that the work area is clean and clear of tools and other items.
[Rev.10 from 2021] 2026.04.01 02:48:07 UTC