Item Name | Sheet Metal |
Federal Supply Group (FSG) | Metal Bars Sheets and Shapes |
Federal Supply Class (FSC) | 9535 Plate Sheet Strip and Foil Nonferrous Base Metal |
National Item Identification Number (NIIN) | 01-532-0297 (015320297) |
NCB Code | USA (01) |
Manufacturer | Sae International, Society Of Automotive Engineers Inc |
Part Number | Manufacturer | Item Name | Cage Code | RFQ |
---|---|---|---|---|
AMS QQ A 250 5 | sae international | sheet metal | 0u583 | RFQ |
AMS-QQ-A-250 5 | society of automotive engineers inc | sheet metal | 81343 | RFQ |
AMS-QQ-A-250 5-CD0-0 032X6X36 | society of automotive engineers inc | sheet metal | 81343 | RFQ |
AMS-QQ-A-250 5-O-0.032X6X36 | sae international | sheet metal | 0u583 | RFQ |
AMS-QQ-A-250 5-O-0.032X6X36 | society of automotive engineers inc | sheet metal | 81343 | RFQ |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
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; |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
AARN | FABRICATION METHOD | ROLLED |
ABGL | WIDTH | 6.000 INCHES NOMINAL |
ABRY | LENGTH | 36.000 INCHES NOMINAL |
ADVM | CROSS-SECTIONAL THICKNESS | 0.0320 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | FUSELAGE F4F JET AIRCRAFT |
AGTA | BASIC SHAPE STYLE | SOLID |
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; |
HEAT | HEAT TREATMENT | O-ANNEALED |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-250/5 |
Relevant Components for NSN - 9535-01-532-0297, 9535015320297 | ||||
9535-01-531-2517 (9535015312517) | 9510-00-843-3325 (9510008433325) | 9530-00-203-1851 (9530002031851) | 9535-01-383-7886 (9535013837886) | |
9535-01-633-4616 (9535016334616) | 9510-00-189-0673 (9510001890673) | 9535-00-982-6450 (9535009826450) | 9535-01-548-6411 (9535015486411) | |
9510-00-956-6537 (9510009566537) | 9540-00-529-9342 (9540005299342) | 9535-01-632-9314 (9535016329314) | 9540-00-250-3605 (9540002503605) | |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
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