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Showing 41 - 60 out of 18520
Page 3 out of 926
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Ultrasonic Calibration Sizing Standards 1.0"-1.8". Slot MTD's 1.000", 1.200", 1.400",1.600" and 1.800". Size: 1.250"Wide x 2.000" Tall x 12.00" Long
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Ultrasonic Calibration Sizing Standards 1.0"-1.8". Slot MTD's 1.000", 1.200", 1.400",1.600" and 1.800". Size: 1.250"Wide x 2.000" Tall x 12.00" Long
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Airbus H.12 Sensitivity Test Block AITM6-0013 Issue 7 Page 77/80 per ASTM E127 Specification Figure H.5 . Material: 7075-T6 Aluminum Anodized for Corrosion Protection. Includes Test Report and Certificate of Conformance.
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Airbus H.12 Sensitivity Test Block AITM6-0013 Issue 7 Page 77/80 per ASTM E127 Specification Figure H.5 . Material: 7075-T6 Aluminum Anodized for Corrosion Protection. Includes Test Report and Certificate of Conformance.
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Ultrasonic Calibration Sizing Standards .1"-.45". Slot MTD's .100", .200", .300", .400", and .450" Size: 1.250"Wide x .500" Tall x 12.00" Long
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Ultrasonic Calibration Sizing Standards .1"-.45". Slot MTD's .100", .200", .300", .400", and .450" Size: 1.250"Wide x .500" Tall x 12.00" Long
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Nomad Series N22 & N24 Reference Standard. for the inspection of Wing Strut Upper Fittings, Figure 27 Page 51. Includes Test Report and Certificate of Conformance.....Material #1: 2024-T3 Clad .032" x 5" x 3"..Material #1: 6061-T6 Bare .310" x 5" x 3"....
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Nomad Series N22 & N24 Reference Standard. for the inspection of Wing Strut Upper Fittings, Figure 27 Page 51. Includes Test Report and Certificate of Conformance.....Material #1: 2024-T3 Clad .032" x 5" x 3"..Material #1: 6061-T6 Bare .310" x 5" x 3"....
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BOEING REFERENCE STANDARD, 787 PT 6 51-00-05, 777-200/300 PT 6 51-00-06, PT 6 51-00-00 Part 6 FIG 4. MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD, 787 PT 6 51-00-05, 777-200/300 PT 6 51-00-06, PT 6 51-00-00 Part 6 FIG 4. MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD, 787 PT 6 51-00-05, 777-200/300 PT 6 51-00-06, PT 6 51-00-00 FIG 14 and 51-00-06 FASTENER (BACB30JC8-4 x1, BACB30NY8K4 x1). Includes Test Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD, 787 PT 6 51-00-05, 777-200/300 PT 6 51-00-06, PT 6 51-00-00 FIG 14 and 51-00-06 FASTENER (BACB30JC8-4 x1, BACB30NY8K4 x1). Includes Test Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD, 787 PT 6 51-00-05, 777-200/300 PT 6 51-00-06, PT 6 51-00-0 FIG 14 PARAGRAPH 2.C FASTENER (BACB30NF4-4 x1, AN960-416 x1, BACBNM4K4 x1, AN960D-416 x1). Includes Test Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD, 787 PT 6 51-00-05, 777-200/300 PT 6 51-00-06, PT 6 51-00-0 FIG 14 PARAGRAPH 2.C FASTENER (BACB30NF4-4 x1, AN960-416 x1, BACBNM4K4 x1, AN960D-416 x1). Includes Test Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD, 787 PT 6 51-00-05, 777-200/300 PT 6 51-00-06, PT 6 51-00-00 and 51-00-06, MATERIAL: 6AL-4V TITANIUM FASTENER (BACB30NX6K6 x3, BACC30M6 x3). Includes Test Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD, 787 PT 6 51-00-05, 777-200/300 PT 6 51-00-06, PT 6 51-00-00 and 51-00-06, MATERIAL: 6AL-4V TITANIUM FASTENER (BACB30NX6K6 x3, BACC30M6 x3). Includes Test Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD KC10 Includes Test Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD KC10 Includes Test Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD KC10 FASTENER (NAS1097AD6, S4931919-6 + NAS1252 + NAS21042L) Includes Test Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD KC10 FASTENER (NAS1097AD6, S4931919-6 + NAS1252 + NAS21042L) Includes Test Report and Certificate of Conformance.
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