4036462: VANE,COMPRESSOR,AIRCRAFT GAS TUR.
VANE,COMPRESSOR,AIRCRAFT GAS TUR. Key specifications include material: NICKEL ALLOY OVERALL, stage_number: 1212, overall_length: 1.180 INCHES MINIMUM AND 1.180 INCHES MINIMUM AND 1.200 INCHES MAXIMUM1.200 INCHES MAXIMUM IN, special_features: ORIGINAL NAME VANE,COMPRESSOR STATOR,TURBINE ENGINEORIGINAL NAME VANE,COMPRESSOR STATOR,TURBINE ENGINE, end_item_identification: ACFT ENG F100ACFT ENG F100, engine_section_location: COMPRESSORCOMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-090-0122, 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 | NICKEL ALLOY OVERALL |
| stage_number | 1212 |
| overall_length | 1.180 INCHES MINIMUM AND 1.180 INCHES MINIMUM AND 1.200 INCHES MAXIMUM1.200 INCHES MAXIMUM IN |
| special_features | ORIGINAL NAME VANE,COMPRESSOR STATOR,TURBINE ENGINEORIGINAL NAME VANE,COMPRESSOR STATOR,TURBINE ENGINE |
| end_item_identification | ACFT ENG F100ACFT ENG F100 |
| engine_section_location | COMPRESSORCOMPRESSOR |
| criticality_code_justification | AGAVAGAV |
| material_document_and_classification | AMS 5706 ASSN STD SINGLE MATERIAL RESPONSE OVERALLAMS 5706 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-090-0122 |
| STAGE NUMBER | 1212 |
| CRITICALITY CODE JUSTIFICATION | AGAVAGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5706 ASSN STD SINGLE MATERIAL RESPONSE OVERALLAMS 5706 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 1.180 INCHES MINIMUM AND 1.180 INCHES MINIMUM AND 1.200 INCHES MAXIMUM1.200 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSORCOMPRESSOR |
| SPECIAL FEATURES | ORIGINAL NAME VANE,COMPRESSOR STATOR,TURBINE ENGINEORIGINAL NAME VANE,COMPRESSOR STATOR,TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F100ACFT ENG F100 |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.