AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
| Item Name | Case Turbine Aircraft Gas Turbin |
| 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) | 01-448-7540 (014487540) |
| NCB Code | USA (01) |
| Manufacturer | United Technologies Corporation, Samsung Techwin Co Ltd, Numet Machining Techniques Inc |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMZ | DIAMETER | 28.330 INCHES MINIMUM AND 28.350 INCHES MAXIMUM |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| MATT | MATERIAL | NICKEL ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1010 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| ABHP | OVERALL LENGTH | 5.809 INCHES MINIMUM AND 5.813 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | CZBJ AND ABMZ AND ABHP AND FEAT |
| FEAT | SPECIAL FEATURES | NT.O. 2J-F100-54, FIG 89, IND 71; USE ONLY ON P/N 4084522-800, -801, -802, 4082654-803, AND 4082657-808; LOCATION NEAR NO. 4 BEARING FRONT AIR SEALING RING, FRONT SEAL ASSY, COMPRESSOR EXIT STATOR AND DIFFUSER CASE |
| MATT | III MATERIAL | NICKEL ALLOY OVERALL |
| Relevant Components for NSN - 2840-01-448-7540, 2840014487540 | ||||
| 2815-00-273-0517 (2815002730517) | 2840-01-398-9640 (2840013989640) | 2825-00-987-7454 (2825009877454) | 2825-00-134-0173 (2825001340173) | |
| 2840-00-798-7841 (2840007987841) | 2840-00-169-0159 (2840001690159) | 2805-01-330-1825 (2805013301825) | 2835-00-614-6198 (2835006146198) | |
| 2815-01-550-0310 (2815015500310) | 2815-01-395-0527 (2815013950527) | 2840-01-496-0938 (2840014960938) | 2805-00-883-1188 (2805008831188) | |
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