Thank you for taking interest in Society Of Automotive Engineers Inc part number AMS T 9046 COMPCP 1 0 032X36X8, which is listed with the NSN 9535-01-532-3832 and a product description of “Sheet Metal.” 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 AMS T 9046 COMPCP 1 0 032X36X8, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Sheet Metal part with the NSN 9535-01-532-3832. For example, you can browse other Society Of Automotive Engineers Inc components that were produced under CAGE Code 81343 or listings that belong to FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal 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 AMS T 9046 COMPCP 1 0 032X36X8 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-532-3832 Item PartTypeName: SHEET,METAL | 9535 | 015323832 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-T-9046 | 5 | 1 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | ANY ACCEPTABLE |
| ABGL | WIDTH | 36.000 INCHES NOMINAL |
| ABRY | LENGTH | 96.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 80000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 70000 POUNDS PER SQUARE INCH |
| FEAT | SPECIAL FEATURES | MAYBE USED FOR STRUCTURAL APPLICATIONS IN AIRBORNE VEHICLES AND EQUIPMENT |
| HEAT | HEAT TREATMENT | ANNEALED |
| MATL | MATERIAL | TITANIUM |
| AARN | FABRICATION METHOD | ANY ACCEPTABLE |
| ABGL | WIDTH | 36.000 INCHES NOMINAL |
| ABRY | LENGTH | 96.000 INCHES NOMINAL |
| ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
| AGTA | BASIC SHAPE STYLE | SOLID |
| CQBC | MINIMUM TENSILE STRENGTH | 80000 POUNDS PER SQUARE INCH |
| CQHQ | MINIMUM YIELD STRENGTH | 70000 POUNDS PER SQUARE INCH |
| FEAT | SPECIAL FEATURES | MAYBE USED FOR STRUCTURAL APPLICATIONS IN AIRBORNE VEHICLES AND EQUIPMENT |
| HEAT | HEAT TREATMENT | ANNEALED |
| MATL | MATERIAL | TITANIUM |
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