Maintenance Parts Pro is pleased to offer procurement options for Sae International part number AMS QQ A 250 5, a Sheet Metal product we carry that is listed with the NSN 9535-01-532-0294 for seamless identification. As this item is available for purchase today, be sure to fill out and submit the Request for Quote (RFQ) form on this page if you are interested in obtaining pricing information. All that we ask is that you share details like your budget, desired quantity, and expected fulfillment speed so that we can respond with the most fitting solutions for your comparisons.
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Alongside streamlined quotation processes, we aim to support our customers by providing as much relevant listing information and data with product offerings as possible. For example, part number AMS QQ A 250 5 specifically traces back to Sae International through CAGE Code 0U583, as well as belongs to the FSC [FSC] as per its NSN of 9535-01-532-0294. Referencing such details, you can locate and procure exact specifications with ease. With our various practices in mind, do not hesitate to request a quote on part number AMS QQ A 250 5 using our provided form.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9535-01-532-0294 Item PartTypeName: SHEET,METAL | 9535 | 015320294 | N | A | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
A | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
AMS-QQ-A-250/5-O-0.032X12X36 | 5 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
MDCL | Material Document And Classification | QQ-A-250/5 FED SPEC 1ST MATERIAL RESPONSE |
HEAT | Heat Treatment | O-ANNEALED |
AGTA | Basic Shape Style | SOLID |
ABRY | Length | 36.000 INCHES NOMINAL |
ABGL | Width | 12.000 INCHES NOMINAL |
AGAV | End Item Identification | FUSELAGE F4F JET AIRCRAFT |
ALBY | Usage Design | AIRCRAFT |
MRC | Decoded Requirement | Clear Text Reply |
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; MAXIMUM TENSILE STRENGTH 30000.0 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000.0 POUNDS PER SQUARE INCH |
MATT | Material | ALUMINUM ALLOY 2024 |
AARN | Fabrication Method | ROLLED |
ADVM | Cross-Sectional Thickness | 0.0320 INCHES NOMINAL |
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