We appreciate your interest in General Electric Company part number 1864M44P001A, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number 1864M44P001A is listed with the NSN 2840-01-496-1184 and description “Plate Component Mounting Aircraf.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by General Electric Company under the CAGE Code 07482 or that similarly fall under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 2840-01-496-1184 parts and Plate Component Mounting Aircraf items your operations require, so request a quote today.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-496-1184 Item PartTypeName: PLATE,COMPONENT MOUNTING,AIRCRAF | 2840 | 014961184 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | A | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1864M44P001A | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABPX | MATERIAL THICKNESS | 0.018 INCHES MINIMUM AND 0.022 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF-39 ENGINE |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| FEAT | SPECIAL FEATURES | MATL; B50TF25 CL-A (HAST X);HIGH PRESSURE TURBINE N0ZZLE STAGE 2 |
| ABPX | MATERIAL THICKNESS | 0.018 INCHES MINIMUM AND 0.022 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF-39 ENGINE |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| FEAT | SPECIAL FEATURES | MATL; B50TF25 CL-A (HAST X);HIGH PRESSURE TURBINE N0ZZLE STAGE 2 |
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