AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
| Item Name | Shaft Turbine Aircraft Gas Turbi |
| Federal Supply Group (FSG) | Engines Turbines and Components |
| Federal Supply Class (FSC) | 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| National Item Identification Number (NIIN) | 01-136-0551 (011360551) |
| NCB Code | USA (01) |
| Manufacturer | Rolls Royce Corporation, Allison Transmission Inc |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 6.417 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG TF41 |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND CZBJ AND MATT AND MDCL |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| FEAT | SPECIAL FEATURES | K1ST END EXTERNALLY SPLINED; 23 TEETH,0.4792 IN PITCH DIA FOR 1.520 IN.; FOR BLEED VALVE ACTUATOR; 2ND END BORED 0.6265-0.6295 IN. DIA. FOR 0.720 IN HAS FORKED PROTRUSION W/0.50 IN. DIA. HOLE THROUGH BOTH FORKS |
| MATT | MATERIAL | STEEL SHAFT |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5613 ASSN STD SINGLE MATERIAL RESPONSE SHAFT |
| Relevant Components for NSN - 2840-01-136-0551, 2840011360551 | ||||
| 2825-00-790-8901 (2825007908901) | 2825-01-010-8535 (2825010108535) | 2825-00-371-7811 (2825003717811) | 2805-01-264-5598 (2805012645598) | |
| 2840-01-375-6452 (2840013756452) | 2805-01-130-2594 (2805011302594) | 2835-01-234-6845 (2835012346845) | 2805-01-714-1073 (2805017141073) | |
| 2840-00-837-2120 (2840008372120) | 2840-01-708-1715 (2840017081715) | 2840-01-200-9553 (2840012009553) | 2805-00-710-5355 (2805007105355) | |
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