9940M50P03-110B: SHAFT,TURBINE,AIRCRAFT GAS TURBI.
SHAFT,TURBINE,AIRCRAFT GAS TURBI. Key specifications include material: TITANIUM ALLOY SHAFT, overall_length: 11.714 INCHES MINIMUM AND 11.724 INCHES MAXIMUM IN, end_item_identification: F100-100B 2J-F100-4, engine_section_location: HIGH PRESSURE COMPRESSOR, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-475-3392, 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 | TITANIUM ALLOY SHAFT |
| overall_length | 11.714 INCHES MINIMUM AND 11.724 INCHES MAXIMUM IN |
| end_item_identification | F100-100B 2J-F100-4 |
| engine_section_location | HIGH PRESSURE COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-475-3392 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 11.714 INCHES MINIMUM AND 11.724 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| SPECIAL FEATURES | FRONT END STEPPED FROM 5.008 IN MIN AND 5.009 IN MAX O.D. SPLINED TEETH4.538 IN MIN AND 4.548 IN MAX I.D. AND5.2707 IN MIN AND 5.2712 IN MAX O.D.SECOND END 15.914 IN MIN 14.917 IN MAX.OD.SIX HOLES 0.262 IN MIN 0.269 IN MAX,DIA. 60 HOLES 0.251 IN MIN 0.252 IN MAX. IN |
| END ITEM IDENTIFICATION | F100-100B 2J-F100-4 |
| MATERIAL | TITANIUM ALLOY SHAFT |
No substitute or cross-reference records for this part.