| Mfg Part Number: 709606 | Manufacturer: United Technologies Corporation | NSN : 2840-00-008-6437 |
| Item Name : manifold anti icing | CAGE Code : 77445 | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
When you are in the market for top-quality Manifold Anti Icing parts and components like NSN 2840-00-008-6437, look no further than Integrated Aviation Hardware. This NSN component is listed alongside the part number 709606, originally sourcing from the manufacturer United Technologies Corporation. This 709606 particular item is purchasable from our website at any time, and we encourage you to fill out and submit an RFQ form at your earliest convenience to receive a quote for your comparisons. As you complete our form for 709606, we ask that you offer us as much information as you can so that our team members can best craft a customized solution fit for your needs.
To ensure that you only procure the exact parts that you need, we always list our parts with as much information as we can. For instance, NSN 2840-00-008-6437 was specifically manufactured under the CAGE Code 77445. Additionally, all parts ship out alongside their qualifying certifications and manufacturing trace documentation, as applicable. Whether you require United Technologies Corporation parts or any other items for your operations, we encourage you to get in touch with a representative who will handle all the sourcing, logistics management, shipping, and quality management for you so that you can continue to focus on what you do best.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-00-008-6437 Item Description: Manifold Anti Icing | 2840 | 000086437 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 709606 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 25.415-25.455 IN. WORKING L,0.033-0.037 IN. TUBE THK,1.800 IN. MINOD AT BENDS,1.980-2.020 IN. TUBE OD,FOUR 0.339-0.349 IN. DIA HOLES ON1.188 IN. CENTERLINE RADIUS ON FLANGE END FITTING,P/N 666232,2.395-2.405IN. OD OF FLANGE END FITTING,P/N |
| ZZZV | III FSC APPLICATION DATA | AIRCRAFT JET ENGINE,TF30 |
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