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Phone No.: +1-714-705-4780 Email: sales@justpartsunlimited.com
Phone No.: +1-714-705-4780 Email: sales@justpartsunlimited.com
| Part No. : 4D0047F32-224 | Alternate P/N : 4D0047F32224 | Manufacturer : Boeing Company |
| CAGE Code : 88277 | Item Name : Spacer Plate | FSC : 5365 Bushings Rings Shims and Spacers |
| NSN : 5365-01-499-5529 |
You can send a request for quote for p/n 4D0047F32-224 to ASAP Semiconductor using justpartsunlimited.com. This part is manufactured by Boeing Company (CAGE Code 88277). The description of it is Spacer Plate. The national stock number associated with this part is NSN 5365014995529. This part belongs to FSC Bushings Rings Shims and Spacers part family. An associate from ASAP Semiconductor will respond within 15 minutes to your query. It is our pleasure to help you with 4D0047F32-224 part requirements.
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 5365-01-499-5529 Item Description: Spacer Plate | 5365 | 014995529 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | A | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4d0047f32-224 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| SFTT | Surface Treatment | ANODIZE |
| CXCY | Part Name Assigned By Controlling Agency | SPACER,PLATE-SPLICE JOINT,SHIM |
| MATT | Material | ALUMINUM ALLOY 7075 |
| MDCL | Material Document And Classification | QQ-A-250/13 FED SPEC SINGLE MATERIAL RESPONSE OR QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| STDC | Surface Treatment Document And Classification | MIL-A-8625 MIL SPEC SINGLE TREATMENT RESPONSE |
| STYL | Style Designator | RECTANGULAR |
| ABHP | Overall Length | 6.970 INCHES MINIMUM AND 7.030 INCHES MAXIMUM |
| ABMK | Overall Width | 0.970 INCHES MINIMUM AND 1.030 INCHES MAXIMUM |
| MRC | Decoded Requirement | Clear Text Reply |
| ADUM | Overall Thickness | 0.032 INCHES NOMINAL |
| AGAV | End Item Identification | C-17 |
| FEAT | Special Features | NHA 17P8D9258-501. FINISH MIL-A-8625, TYPE I OR II, CL 1 |
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