 9535-00-003-5520 | SHEET,METAL | 05/26/1972 |
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 9535-00-003-5520 | SHEET,METAL | | 0 |
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 AMS-QQ-A-250/30 | MATERIAL | GALI CORPORATION | 31 | QQ-A-250/30 | ALUMINUM | GALI CORPORATION | 8 | For additional information Register for Free Trial
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For additional information Register for Free Trial
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 AMS-QQ-A-250/30 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | 81343 | DMS 1719,2219-T81,0.063X48X144 | DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER | 14153 | QQ-A-250/30 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERV | 81348 | QQ-A-250/30-T81,0.063X48X12 | DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER | 14153 | QQ-A-250/30-T81,0.063X48X144 | DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER | 14153 | STM07-101 | LOCKHEED MARTIN CORP | 98897 | 063/2219T81 | AMI METALS, INC | 8Y468 | AMS-QQ-A-250/30 | SAE INTERNATIONAL | 0U583 | For additional information Register for Free Trial
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 FABRICATION METHOD | ROLLED | LENGTH | 12.000 FEET NOMINAL | CROSS-SECTIONAL THICKNESS | 0.0630 INCHES NOMINAL | BASIC SHAPE STYLE | SOLID | CLADDING THICKNESS | 0.0025 INCHES OVERALL | MINIMUM TENSILE STRENGTH | 55000 POUNDS PER SQUARE INCH | MINIMUM YIELD STRENGTH | 41000 POUNDS PER SQUARE INCH | HEAT TREATMENT | T-81 SOLUTION HEAT TREATED | MATERIAL | ALUMINUM ALLOY 2219 | MATERIAL DOCUMENT AND CLASSIFICATION | ST-07-101, ALLOY 2219, LOCKHEED AIRCRAFT CORP MFR REF SINGLE MATERIAL RESPONSE | For additional information Register for Free Trial
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