AIRCRAFT BRAKING SYSTEMS FIG-11 REFERENCE STANDARD (Inch Version) 2024-T6 ALUMINUM AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PROCEEDURE 1, FIGURE 11, PAGE 15, overall dimension as per end user drawing. Flaw for forged material Notch Dimension – 0.06" (L) x 0.006" (W) MATERIAL: 2024-T6 ALUMINUM. NOTE: For special alloy request by mail.

AIRCRAFT BRAKING SYSTEMS FIG-2 REFERENCE STANDARD (Inch Version) CAST ALUMINUM Aircraft Braking Systems Reference Standard Pt 3 32-42-05, Pages 1-7 Figure 2 and 3, overall dimension as per end user drawing. Flaw for cast material Notch Dimension – 0.12" (L) x 0.006" (W) MATERIAL: CAST ALUMINUM. NOTE: For special alloy request by mail.

AIRCRAFT BRAKING SYSTEMS FIG-11 FORGED REFERENCE STANDARD (Inch Version) 2014-T6 ALUMINUM AIRCRAFT BRAKING SYSTEMS REFERENCE STANDARD PT 3 32-42-05, PROCEEDURE 1, FIGURE 11, PAGE 15, overall dimension as per end user drawing. Flaw for forged material Notch Dimension – 0.06" (L) x 0.006" (W) MATERIAL: 2014-T6 ALUMINUM. NOTE: For special alloy request by mail.