W DOC AIRBUS | AMM A320F

Detailed Visual Inspection (DVI) of the Engine Mount Lugs (Engine Removed) [PW11]


TASK 72-00-00-220-802-A
Detailed Visual Inspection (DVI) of the Engine Mount Lugs (Engine Removed)


WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AND THE ADJACENT COMPONENTS AFTER ENGINE SHUTDOWN. THE ENGINE, THE ENGINE OIL AND THE ADJACENT COMPONENTS 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.
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
FLASHLIGHT
No specific
1
MIRROR - INSPECTION
 B. Referenced Information
REFERENCE
DESIGNATION
3. Job Set-up
Subtask 72-00-00-869-089-A ** ON A/C NOT FOR ALL
A. Not Applicable
4. Procedure
Subtask 72-00-00-220-178-A ** ON A/C NOT FOR ALL
A. Detailed Visual Inspection (DVI) of the Engine Mount Lugs (Engine Removed)
   (1) Examine the forward mount lugs for damage per limits. See the table that follows:
EXAMINE
DAMAGE
DISPOSITION
Nicks and scratches
Any quantity
Not permitted
Round bottom dents
Any quantity
Not permitted
Cracks
Any quantity
Not permitted
NOTE: Use this inspection for serviceability limits of the engine mounting lugs and bushings only.
NOTE: This inspection is only for the visible portion of the engine mount lugs with the mounts installed. Use a FLASHLIGHT and MIRROR - INSPECTION to visually examine the engine mount lug area for damage, loose or missing parts, and to check for the correct installation.
   (2) Examine the thrust link lugs for damage per limits. See the table that follows:
EXAMINE
DAMAGE
DISPOSITION
Nicks and scratches
Any quantity up to 0.010 in. (0.254 mm) maximum depth
Permitted for continued service use

Any quantity over 0.010 in. (0.254 mm) maximum depth
Not permitted
Round bottom dents
Any quantity up to 0.010 in. (0.254 mm) maximum depth and 0.500 in. (12.700 mm) maximum diameter
Permitted for continued service use

Over 0.010 in. (0.254 mm) depth or 0.500 in. (12.700 mm) diameter
Not permitted
Cracks
Any quantity
Not permitted
   (3) Examine the aft mount and fail safe lugs per limits. See the table that follows:
EXAMINE
DAMAGE
DISPOSITION
Nicks and scratches
Any quantity up to 0.010 in. (0.254 mm) maximum depth
Permitted for continued service use

Any quantity over 0.010 in. (0.254 mm) maximum depth
Not permitted
Round bottom dents
Any quantity up to 0.010 in. (0.254 mm) maximum depth and 0.500 in. (12.700 mm) maximum diameter
Permitted for continued service use

Over 0.010 in. (0.254 mm) depth or 0.500 in. (12.700 mm) diameter
Not permitted
Cracks
Any quantity
Not permitted
   (4) Examine the forward mount lug bushings (4 locations) for damage per limits. See the table that follows:
EXAMINE
DAMAGE
DISPOSITION
Scratches and scoring
Any quantity
Not permitted
Visible wear or hole elongation
Any quantity
Not permitted
Cracks
Any quantity
Not permitted
NOTE: Do the engine mount lug and mount lug bushing inspection only if the engine mounts and attaching hardware have been removed for other reasons. Use a FLASHLIGHT and MIRROR - INSPECTION to visually examine the bushings.
   (5) Examine the thrust link lug bushings on the compressor intermediate case (4 locations) per limits. See the table that follows:
EXAMINE
DAMAGE
DISPOSITION
Scratches and scoring
Any quantity up to 0.005 in. (0.127 mm) maximum depth
Permitted for continued service use

Any quantity over 0.005 in. (0.127 mm) up to 0.010 in. (0.254 mm) depth
Not permitted

Any quantity over 0.010 in. (0.254 mm) depth
Not permitted
Wear or hole elongation
Any quantity
Not permitted
Cracks
Any quantity
Not permitted
   (6) Examine the aft mount lug bushings (4 locations) for damage per limits. See the table that follows:
EXAMINE
DAMAGE
DISPOSITION
Scratches and scoring
Any quantity up to 0.004 in. (0.102 mm) maximum depth
Permitted for continued service use

Any quantity over 0.004 in. (0.102 mm) up to 0.008 in. (0.203 mm) depth
Not permitted

Any quantity over 0.008 in. (0.203 mm) depth
Not permitted
Wear or hole elongation
Any quantity
Not permitted
Cracks
Any quantity
Not permitted
   (7) Examine the aft mount lugs and fail safe lug for damage per limits. See the table that follows:
EXAMINE
DAMAGE
DISPOSITION
Nicks and scratches
Any quantity up to 0.010 in. (0.254 mm) maximum depth
Permitted for continued service use

Any quantity over 0.010 in. (0.254 mm) maximum depth
Not permitted
Round bottom dents
Any quantity up to 0.010 in. (0.254 mm) maximum depth and 0.500 in. (12.700 mm) maximum diameter
Permitted for continued service use

Over 0.010 in. (0.254 mm) depth or 0.500 in. (12.700 mm) diameter
Not permitted
Cracks
Any quantity
Not permitted
   (8) Examine the assembly for foreign objects, damage, and correct assembly.
[Rev.10 from 2021] 2026.04.01 02:47:25 UTC