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Showing 10401 - 10420 out of 10420
Page 521 out of 521
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AIRBUS REFERENCE STANDARD A318-A321 51-63-07-PB1, PAGE 2 SHEET 01. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
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AIRBUS REFERENCE STANDARD, NTM 53-41-86, A300-600 PT 6 51-10-01, A318-A321 51-63-07-PB1, PAGE 2 SHEET 01. MATERIAL: 7075-T6 ALUMINUM. Includes Test Report and Certificate of Conformance.
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AIRBUS SPLIT CALIBRATION REFERENCE STANDARD A318-A321 51-63-07-991-002 PB1. MATERIAL: 6AL-4V TITANIUM. Includes Test Report and Certificate of Conformance.
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Custom 6 Step Wedge .020", .040", .080", .150" ,0.300", 0.600" +/-.001", Per Drawing Specification TXX003503. Material: 2219-T81 Aluminum. Includes Teflon Base.
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Custom 6 Step Wedge .040", .050", .060", .075" ,0.090", 0.110" +/-.001", Per Drawing Specification TXX003461. Material: 718 Inconel. Includes Teflon Base.
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V-1 (A-2) IIW Angle Beam Calibration Block (Metric). Made to British Standard: BS-2704, German Standard: DIN 54-120, Australian Standard AS 2803 and ISO 2400. Material: A36/1018 Carbon Steel. Thickness of 1" / 25 mm, Height of 4" / 100 mm for straight beam calibration. 4" / 100 mm radius with saw cut at Index Point for Angle Beam Calibration: Determining Beam Index Point and Distance Calibration (signals at 4" / 100 and 8" / 200 mm). 2" / 50 mm bore hole for Probe Angle verification. 0.06" / 1.5 mm bore hole for sensitivity adjustment. Includes Form Fitted Wood Case.
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MINI ANGLE BEAM ALUM V2 BLOCK ½" (12.5mm) or 1" (25.4 mm) thick, 1" radius opposite 2" radius, with 5/64" diameter side drilled hole (3/4" deep flat bottom hole in 1" thick version). Aluminum 7075-T6. Includes form fitted case.
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V2 7075-T6 ALUMINUM 98S51605001-206 |
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MINI ANGLE BEAM BLOCK CS V2 BLOCK.½" (12.5mm) or 1" (25.4 mm) thick, 1" radius opposite 2" radius, with 5/64" diameter side drilled hole (3/4" deep flat bottom hole in 1" thick version).1018 Carbon Steel with form fitted case
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V2 1018 CARBON STEEL |
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MINI ANGLE BEAM BLOCK CS V2 BLOCK.½" (12.5mm) or 1" (25.4 mm) thick, 1" radius opposite 2" radius, with 5/64" diameter side drilled hole (3/4" deep flat bottom hole in 1" thick version). ..304 Stainless Steel with case
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V2 304 STAINLESS STEEL |
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Boeing Reference Standard For MR-TCDL Modification (L3H). Material: 7050-T7451 or 7075-T7351 & 2024-T351 Aluminum. Includes Test Report and Certificate of Conformance.
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Boeing Reference Standard For MR-TCDL Modification (L3H). Material: 7050-T7451 or 7075-T7351 & 2024-T351 Aluminum. Includes Test Report and Certificate of Conformance.
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BOEING R & D LFEC REFERENCE STANDARD Material: 7076-T6 Clad Aluminum. Fasteners HL18PB6-3, NAS620-10L, MS21042. Includes Test Report and Certificate of Conformance.
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N/A |
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Boeing W-19 Reference Standard.-1 Assembly
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LUCITE 70 DEGREE WEDGE MSWQC STYLE
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W-203 |
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BOEING REFERENCE STANDARD. W-87 INBOARD 360 REFERENCE STANDARD. Materials: 2024-T351 and 7075-T651 Aluminum. Includes Test Report Traceable to NIST.
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BOEING REFERENCE STANDARD. W-87 OUTBOARD 360 REFERENCE STANDARD. Materials: 2024-T351 and 7075-T651 Aluminum. Includes Test Report Traceable to NIST.
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LUCITE WEDGE 45° SHEAR WAVE IN ALUMINUM USED WITH .25" ELEMENT TRANSDUCER (.75"L x .45"W x .37"H)
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60° IN ALUMINUM LUCITE (PLEXIGLASS) WEDGE, 3/8-32 THREAD USED WITH A .25"Ø DIAMETER TRANSDUCER WITH A 3/8-32 THREAD. Includes Certificate of Conformance.(1.0"L x .45"W x .50"H). MSWQCW 203-70. Includes Certificate of Conformance.
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LUCITE WEDGE 70° SHEAR WAVE IN ALUMINUM USED WITH .25" ELEMENT TRANSDUCER (1.0"L x .45"W x .50"H)
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Boeing Custom Contact Radius Shoe WS400 with a 0.400" radius. Material: Lucite/Cast Acrylic. 787 Part 4 51-00-23. Includes Certificate of Conformance.
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