Thank you for taking interest in General Electric Company part number 111R108P4, which is listed with the NSN 2840-01-106-2588 and a product description of “Blade Compressor Aircraft Gas Tu.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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Alongside part number 111R108P4, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Blade Compressor Aircraft Gas Tu part with the NSN 2840-01-106-2588. For example, you can browse other General Electric Company components that were produced under CAGE Code 07482 or listings that belong to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number 111R108P4 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-106-2588 Item PartTypeName: BLADE,COMPRESSOR,AIRCRAFT GAS TU | 2840 | 011062588 | N | |||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | ||||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 108R11P1 | 2 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 8.403 INCHES NOMINAL |
| ABPX | MATERIAL THICKNESS | 0.010 INCHES MINIMUM AND 0.020 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG J79 |
| APGF | DESIGN TYPE | COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND ABPX AND APGF AND CZBJ |
| CZBJ | ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| CZCJ | STAGE NUMBER | 2 |
| FEAT | SPECIAL FEATURES | ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE |
| MATT | MATERIAL | STEEL BLADE |
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