Thank you for taking interest in Blades Technology Ltd part number P200P04, which is listed with the NSN 2840-01-435-9541 and a product description of “Vane Compressor Aircraft Gas Tur.” 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 P200P04, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Vane Compressor Aircraft Gas Tur part with the NSN 2840-01-435-9541. For example, you can browse other Blades Technology Ltd components that were produced under CAGE Code S0635 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 P200P04 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-435-9541 Item PartTypeName: VANE,COMPRESSOR,AIRCRAFT GAS TUR | 2840 | 014359541 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| P200P04 | 5 | 1 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| APGF | Design Type | AXIAL COMPRESSOR |
| FEAT | Special Features | T.O. 2J-F110-14, FIG 62 IND 5; INLET GUIDE VANE NEAR 1ST VANE,COMPRESSOR |
| MRC | Decoded Requirement | Clear Text Reply |
| AGAV | End Item Identification | F110 AIRCRAFT GAS TURBINE ENGINE |
| BGLW | Blade Attachment Method | PIN |
| CRTL | Criticality Code Justification | CZBJ AND BGLW AND FEAT |
| CZBJ | Engine Section Location | HIGH PRESSURE COMPRESSOR |
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