9992M65G09: SHROUD SEGMENT,TURBINE,AIRCRAFT.
SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: ALUMINUM ALLOY OVERALL, overall_length: 1.019 INCHES MINIMUM AND 1.029 INCHES MAXIMUM IN, end_item_identification: ACFT ENG F108, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-263-3318, 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 OVERALL |
| stage_number | 1 |
| overall_length | 1.019 INCHES MINIMUM AND 1.029 INCHES MAXIMUM IN |
| end_item_identification | ACFT ENG F108 |
| engine_section_location | COMPRESSOR |
| NSN | 2840-01-263-3318 |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 1.019 INCHES MINIMUM AND 1.029 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | ACFT ENG F108 |
| MATERIAL | ALUMINUM ALLOY OVERALL |