| Part Number : AMS-QQ-A-250 5-T3-0.040X6X36 | Manufacturer : Society Of Automotive Engineers Inc | ||
| NSN : 9535-01-531-7789 (9535015317789) | |||
| Item Name : Sheet Metal | CAGE Code : 81343 | ||
| NIIN : 01-531-7789 (015317789) | |||
| FSC Code : 9535 Plate Sheet Strip and Foil Nonferrous Base Metal | |||
| FSG Code : 95 Metal Bars Sheets and Shapes | |||
| INC Code : 37015 | |||
| NCB Code : 01 | Country : USA | ||
| Alternate P/N: AMSQQA2505T30.040X6X36 | |||
Thank you for taking an interest in part number AMS-QQ-A-250 5-T3-0.040X6X36, that of which is listed with the description Sheet Metal; Manufactured by Society Of Automotive Engineers Inc and listed alongside the NSN 9535015317789, part number AMS-QQ-A-250 5-T3-0.040X6X36 is available for immediate purchase on our website. As such, to learn more about this offering while receiving a competitive quote for your comparisons, be sure to fill out and submit the RFQ form presented on this page. Within 15 minutes of us receiving and reviewing a completed form, a member of our staff will contact you to present a tailored solution for your comparisons.
| Part Number : AMS-QQ-A-250 5-T3-0.040X6X36 | Manufacturer : Society Of Automotive Engineers Inc | ||
| NSN Number : 9535-01-531-7789 (9535015317789) | |||
| Item Name : Sheet Metal | CAGE Code : 81343 | ||
| NIIN : 015317789 | |||
| FSC CODE : 9535 Plate Sheet Strip and Foil Nonferrous Base Metal | |||
Thank you for taking an interest in part number AMS-QQ-A-250 5-T3-0.040X6X36, that of which is listed with the description Sheet Metal; Manufactured by Society Of Automotive Engineers Inc and listed alongside the NSN 9535015317789, part number AMS-QQ-A-250 5-T3-0.040X6X36 is available for immediate purchase on our website. As such, to learn more about this offering while receiving a competitive quote for your comparisons, be sure to fill out and submit the RFQ form presented on this page. Within 15 minutes of us receiving and reviewing a completed form, a member of our staff will contact you to present a tailored solution for your comparisons.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9535-01-531-7789 Item PartTypeName: SHEET,METAL | 9535 | 015317789 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| AMS-QQ-A-250/5-T3-0.040X6X36 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| MATT | Material | ALUMINUM ALLOY 2024 |
| MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
| CQHQ | Minimum Yield Strength | 39000 POUNDS PER SQUARE INCH |
| AGTA | Basic Shape Style | SOLID |
| ABRY | Length | 36.000 INCHES NOMINAL |
| HEAT | Heat Treatment | T-3 SOLUTION HEAT TREATED |
| AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
| ABGL | Width | 6.000 INCHES NOMINAL |
| CQBC | Minimum Tensile Strength | 59000 POUNDS PER SQUARE INCH |
| MRC | Decoded Requirement | Clear Text Reply |
| ALBY | Usage Design | AIRCRAFT |
| FEAT | Special Features | THIN LAYERS APPROXIMATELY EQUAL THICKNESS, OF ALUMINUM ALLOY 1230 ANODIC TO THE CORE ARE BONDED TO BOTH SURFACES; NOMINAL CLADDING THICKNESS FOR EACH LAYER TO BE 5.0 PERCENT OF COMPOSITE THICKNESS OR 4.0 PERCENT OF FINISHED SHEET THICKNESS |
| AARN | Fabrication Method | ROLLED |
| ADVM | Cross-Sectional Thickness | 0.0400 INCHES NOMINAL |
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