BOEING REFERENCE STANDARD-1083-0.787 (Inch Version) BOEING REFERENCE STANDARD 767 PT 6 51-00-16 PAGE 7 FIG 3. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION - 4" (L) X 2.4" (W) X 0.2" (T) DIA – Ø 0.8". NOTCH SIZE – 0.04" X 0.04". NOTCH WIDTH - 0.006". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 1083-0.787 MATERIAL: ALUMINUM. NOTE: For special alloy request by mail.

BOEING REFERENCE STANDARD-1083-0.161 (Inch Version) BOEING REFERENCE STANDARD 767, PT 6 51-00-16 PAGE 7 AND 777, PART 6 51-00-02 PAGE 8 FIG. 3. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION - 4" (L) X 2.4" (W) X 0.2" (T) DIA – Ø 0.161". NOTCH SIZE – 0.04" X 0.04". NOTCH WIDTH - 0.006". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 1083-0.161 MATERIAL: ALUMINUM. NOTE: For special alloy request by mail.

BOEING REFERENCE STANDARD-1083-0.697 (Inch Version) BOEING REFERENCE STANDARD 767 PT 6 51-00-16 PAGE 7 FIG 3. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION - 4" (L) X 2.4" (W) X 0.2" (T) DIA – Ø 0.697". NOTCH SIZE – 0.04" X 0.04". NOTCH WIDTH - 0.006". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 1083-0.697 MATERIAL: ALUMINUM. NOTE: For special alloy request by mail.

BOEING REFERENCE STANDARD-1084-0.787 (Inch Version) BOEING REFERENCE STANDARD ALL PT 6 51-00-16 FIGURE 3, PAGE 7. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION - 4" (L) X 2.4" (W) X 0.2" (T) DIA – Ø 0.8". NOTCH SIZE – 0.04" X 0.04". NOTCH WIDTH - 0.006". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 1084-0.787 MATERIAL: TITANIUM. NOTE: For special alloy request by mail.

BOEING REFERENCE STANDARD-1084-1.125 (Inch Version) BOEING REFERENCE STANDARD ALL PT 6 51-00-16 FIGURE 3, PAGE 7. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION - 4" (L) X 2.4" (W) X 0.2" (T) DIA – Ø 1.125". NOTCH SIZE – 0.04" X 0.04". NOTCH WIDTH - 0.006". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 1084-1.125 MATERIAL: 7075-T6 ALUMINUM. NOTE: For special alloy request by mail.

BOEING REFERENCE STANDARD-1084-1.125 (Inch Version) 2024-T3 ALUMINUM BOEING REFERENCE STANDARD ALL PT 6 51-00-16 FIGURE 3, PAGE 7. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION - 4" (L) X 2.4" (W) X 0.2" (T) DIA – Ø 1.2". NOTCH SIZE – 0.04" X 0.04". NOTCH WIDTH - 0.006". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 1084-1.125 MATERIAL: 2024-T3 ALUMINUM. NOTE: For special alloy request by mail.

BOEING REFERENCE STANDARD-1084-1.312 (Inch Version) ALUMINUM ALLOY BOEING REFERENCE STANDARD ALL PT 6 51-00-16 FIGURE 3, PAGE 7. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION - 4" (L) X 2.4" (W) X 0.2" (T) DIA – Ø 1.312". NOTCH SIZE – 0.04" X 0.04". NOTCH WIDTH - 0.006". STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 1084-1.312 MATERIAL: ALUMINUM ALLOY. NOTE: For special alloy request by mail.

BOEING REFERENCE STANDARD-1084-33 (Metric Version) ALUMINUM ALLOY BOEING REFERENCE STANDARD ALL PT 6 51-00-16 FIGURE 3, PAGE 7. Includes Test Report and Certificate of Conformance. OVERALL DIMENSION - 100mm (L) X 60mm (W) X 5mm (T) DIA – Ø 33mm NOTCH SIZE - 1mm X 1mm NOTCH WIDTH - 0.15mm STANDARD/MANUFACTURE REFERENCE/PART NUMBER: 1084-33 MATERIAL: ALUMINUM ALLOY. NOTE: For special alloy request by mail.

BOEING 53-10-01 REFERENCE STANDARD (Inch Version) ASME SA516 Gr 70 BOEING REFERENCE STANDARD 737 PT 6 53-10-01. Includes Test Report and Certificate of Conformance. DIMENSION: 2" (L) x 1" (W) x 0.24" (T). BLOCK CONTAIN TWO HOLES Ø0.2" (1) Hole with flaw – 0.1" (L) x 0.005" (W) x 0.02" (Deep) (1) Hole without flaw MATERIAL: ASME SA516 Gr 70. NOTE: For special alloy request by mail.

BOEING 53-10-01 REFERENCE STANDARD (Inch Version) ASME SA517 BOEING REFERENCE STANDARD 737 PT 6 53-10-01. Includes Test Report and Certificate of Conformance. DIMENSION: 2" (L) x 1" (W) x 0.24" (T). BLOCK CONTAIN TWO HOLES Ø0.2" (1)Hole with flaw – 0.1" (L) x 0.005" (W) x 0.02" (Deep) (1)Hole without flaw MATERIAL: ASME SA517. NOTE: For special alloy request by mail.

BOEING 53-10-01 REFERENCE STANDARD (Inch Version) ASME SA36 / A36 BOEING REFERENCE STANDARD 737 PT 6 53-10-01. Includes Test Report and Certificate of Conformance. DIMENSION: 2" (L) x 1" (W) x 0.24" (T). BLOCK CONTAIN TWO HOLES Ø0.2" (1)Hole with flaw – 0.1" (L) x 0.005" (W) x 0.02" (Deep) (1)Hole without flaw MATERIAL: ASME SA36 / A36. NOTE: For special alloy request by mail.

BOEING 53-10-01 REFERENCE STANDARD (Inch Version) STAINLESS STEEL 304 BOEING REFERENCE STANDARD 737 PT 6 53-10-01. Includes Test Report and Certificate of Conformance. DIMENSION: 2" (L) x 1" (W) x 0.24" (T). BLOCK CONTAIN TWO HOLES Ø0.2" (1)Hole with flaw – 0.1" (L) x 0.005" (W) x 0.02" (Deep) (1)Hole without flaw MATERIAL: STAINLESS STEEL 304. NOTE: For special alloy request by mail.

BOEING 53-10-01 REFERENCE STANDARD (Inch Version) STAINLESS STEEL 316 BOEING REFERENCE STANDARD 737 PT 6 53-10-01. Includes Test Report and Certificate of Conformance. DIMENSION: 2" (L) x 1" (W) x 0.24" (T). BLOCK CONTAIN TWO HOLES Ø0.2" (1)Hole with flaw – 0.1" (L) x 0.005" (W) x 0.02" (Deep) (1)Hole without flaw MATERIAL: STAINLESS STEEL 316. NOTE: For special alloy request by mail.

BOEING 53-10-01 REFERENCE STANDARD (Inch Version) TITANIUM BOEING REFERENCE STANDARD 737 PT 6 53-10-01. Includes Test Report and Certificate of Conformance. DIMENSION: 2" (L) x 1" (W) x 0.24" (T). BLOCK CONTAIN TWO HOLES Ø0.2" (1)Hole with flaw – 0.1" (L) x 0.005" (W) x 0.02" (Deep) (1)Hole without flaw MATERIAL: TITANIUM. NOTE: For special alloy request by mail.

BOEING 53-10-01 REFERENCE STANDARD (Inch Version) ALUMINUM BOEING REFERENCE STANDARD 737 PT 6 53-10-01. Includes Test Report and Certificate of Conformance. DIMENSION: 2" (L) x 1" (W) x 0.24" (T). BLOCK CONTAIN TWO HOLES Ø0.2" (1)Hole with flaw – 0.1" (L) x 0.005" (W) x 0.02" (Deep) (1)Hole without flaw MATERIAL: ALUMINUM. NOTE: For special alloy request by mail.

BOEING 53-10-01 REFERENCE STANDARD (Inch Version) COPPER BOEING REFERENCE STANDARD 737 PT 6 53-10-01. Includes Test Report and Certificate of Conformance. DIMENSION: 2" (L) x 1" (W) x 0.24" (T). BLOCK CONTAIN TWO HOLES Ø0.2" (1)Hole with flaw – 0.1" (L) x 0.005" (W) x 0.02" (Deep) (1)Hole without flaw MATERIAL: COPPER. NOTE: For special alloy request by mail.

BOEING 53-10-01 REFERENCE STANDARD (Inch Version) INCONEL 625 BOEING REFERENCE STANDARD 737 PT 6 53-10-01. Includes Test Report and Certificate of Conformance. DIMENSION: 2" (L) x 1" (W) x 0.24" (T). BLOCK CONTAIN TWO HOLES Ø0.2" (1)Hole with flaw – 0.1" (L) x 0.005" (W) x 0.02" (Deep) (1)Hole without flaw MATERIAL: INCONEL 625. NOTE: For special alloy request by mail.

BOEING 53-10-01 REFERENCE STANDARD (Inch Version) INCONEL 825 BOEING REFERENCE STANDARD 737 PT 6 53-10-01. Includes Test Report and Certificate of Conformance. DIMENSION: 2" (L) x 1" (W) x 0.24" (T). BLOCK CONTAIN TWO HOLES Ø0.2" (1)Hole with flaw – 0.1" (L) x 0.005" (W) x 0.02" (Deep) (1)Hole without flaw MATERIAL: INCONEL 825. NOTE: For special alloy request by mail.

BOEING 53-10-01 REFERENCE STANDARD (Inch Version) MONAL 800 BOEING REFERENCE STANDARD 737 PT 6 53-10-01. Includes Test Report and Certificate of Conformance. DIMENSION: 2" (L) x 1" (W) x 0.24" (T). BLOCK CONTAIN TWO HOLES Ø0.2" (1)Hole with flaw – 0.1" (L) x 0.005" (W) x 0.02" (Deep) (1)Hole without flaw MATERIAL: MONAL 800. NOTE: For special alloy request by mail.

BOEING 53-10-01 REFERENCE STANDARD (Inch Version) MAGNESIUM BOEING REFERENCE STANDARD 737 PT 6 53-10-01. Includes Test Report and Certificate of Conformance. DIMENSION: 2" (L) x 1" (W) x 0.24" (T). BLOCK CONTAIN TWO HOLES Ø0.2" (1)Hole with flaw – 0.1" (L) x 0.005" (W) x 0.02" (Deep) (1)Hole without flaw MATERIAL: MAGNESIUM. NOTE: For special alloy request by mail.