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  SAE ARP 1315 : 2013

  SAE ARP 1315 : 2013 SAFETY CONSIDERATIONS FOR AIRPLANE LAVATORIES SAE International

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  SAE AS 24563 : 2013

  SAE AS 24563 : 2013 FLANGE PROFILES, V-COUPLING, DESIGN STANDARD SAE International

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  SAE AS 1960/4 : 2013

  SAE AS 1960/4 : 2013 FLANGE END, DESIGN STANDARD SAE International

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  SAE AIR 1116 : 2013

  SAE AIR 1116 : 2013 FLUID PROPERTIES SAE International

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  SAE AMS 2773 : 2013

  SAE AMS 2773 : 2013 HEAT TREATMENT, CAST NICKEL ALLOY AND COBALT ALLOY PARTS SAE International

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  SAE AMS 4173 : 2013

  SAE AMS 4173 : 2013 ALUMINUM ALLOY, EXTRUSIONS 1.0MG - 0.60SI - 0.30CU - 0.20CR (6061-T6511 OR T6510) SOLUTION HEAT TREATED, STRESS RELIEVED BY STRETCHING, STRAIGHTENED, AND PRECIPITATION HEAT TREATED SAE International ...

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  SAE ARP 5448 : 2013

  SAE ARP 5448 : 2013 PLAIN BEARING TEST METHODS SAE International

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  SAE AS 8027 : 2013

  SAE AS 8027 : 2013 CREW MEMBER OXYGEN REGULATORS, DEMAND SAE International

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  SAE AS 622 : 2013

  SAE AS 622 : 2013 HOSE ASSEMBLY, 3000 PSI, PTFE, FLARELESS, STRAIGHT TO 45 DEGREES, HEAVYWEIGHT SAE International

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  SAE AMS 4204 : 2013

  SAE AMS 4204 : 2013 ALUMINUM ALLOY, PLATE, 6.2ZN - 1.8CU - 2.4MG - 0.13ZR (7010-T7651), SOLUTION HEAT TREATED, STRESS RELIEVED, AND PRECIPITATION HEAT TREATED SAE International

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