1441M95G03: SHROUD SEGMENT,TURBINE,AIRCRAFT.
SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: ALUMINUM ALLOY 6061 OVERALL, overall_length: 3.922 INCHES MINIMUM AND 3.932 INCHES MAXIMUM IN, special_features: FRONT FRAME, end_item_identification: F110GE129 AIRCRAFT ENGINE, engine_section_location: TURBINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-347-8985, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | ALUMINUM ALLOY 6061 OVERALL |
| overall_length | 3.922 INCHES MINIMUM AND 3.932 INCHES MAXIMUM IN |
| special_features | FRONT FRAME |
| end_item_identification | F110GE129 AIRCRAFT ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS4127 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-347-8985 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS4127 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 3.922 INCHES MINIMUM AND 3.932 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | FRONT FRAME |
| END ITEM IDENTIFICATION | F110GE129 AIRCRAFT ENGINE |
| MATERIAL | ALUMINUM ALLOY 6061 OVERALL |
No substitute or cross-reference records for this part.