You have arrived on the Request for Quote (RFQ) page for part number 9547M14G08, a General Electric Company component that is listed with the product description “Rotor Compressor Aircraft Gas Tu” and NSN 2840-01-447-2505 for fast identification. By using the form supplied below, you can offer details regarding your requirements to secure customized procurement solutions for your consideration. As our goal is to provide quick service, you can expect a response within 15 minutes of our staff members reviewing your submission. Alternatively, if you use the email or phone number at the bottom of the webpage, you can directly connect with our experts to discuss your needs.
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Alongside General Electric Company part number 9547M14G08, you can seamlessly search for more items from this manufacturer or CAGECode 07482 using our curated catalogs. Similarly, we also offer means for locating other products that belong to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, which this component falls under having the NSN 2840-01-447-2505. Whether you desire part number 9547M14G08 or other NSN components, you can rest assured that our entire inventory is sourced from reputable manufacturers and suppliers. Bearing this in mind, kick off procurement today to see why so many customers select Aero Defence Solutions as their trusted purchasing hub.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-447-2505 Item PartTypeName: ROTOR,COMPRESSOR,AIRCRAFT GAS TU | 2840 | 014472505 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| I | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 9547M14G08 | 1 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 25.577 INCHES MINIMUM AND 25.597 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F110-129 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ AND ABHP |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME ROTOR ASSEMBLY,COMPRESSOR |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | 5INCLUDES STAGES 1-9; HPCR STG 1-2 HAS IMPROVED SPOOL OIL DRAIN HOLES (2) THAT ARE 1.48 TIME LARGER THAN THE CURRENT ELLIPTICAL HOLE; REPLACES P/N 9547M14G03 AND 9547M14G06; CHANGE OF HOLE IS A PHYSICAL CHANGE BUT NOT FUNCTIONALLY INTERCHAN |
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