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)
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Job Set-up
Subtask 72-00-00-869-089-A ** ON A/C NOT FOR ALL
Subtask 72-00-00-220-178-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 13:02:11 UTC
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 JobSelf 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 |
| REFERENCE | DESIGNATION |
|---|---|
Subtask 72-00-00-869-089-A ** ON A/C NOT FOR ALL
A. Not Applicable
4. ProcedureSubtask 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:
(3) Examine the aft mount and fail safe lugs per limits. See the table that follows:
(4) Examine the forward mount lug bushings (4 locations) for damage per limits. See the table that follows:
(6) Examine the aft mount lug bushings (4 locations) for damage per limits. See the table that follows:
(7) Examine the aft mount lugs and fail safe lug for damage per limits. See the table that follows:
(8) Examine the assembly for foreign objects, damage, and correct assembly.
(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 |
| 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 |
| 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 |
| 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 |
| 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 |
Engine Mount Lugs (Engine Removed)