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Showing 10361 - 10380 out of 10421
Page 519 out of 522
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BAE 146-RJ SERIES REFERENCE STANDARD 55-11-10 PT 6 FIGURE 6&7 PAGES 12&13. Includes Test Report and Certificate of Conformance.
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BAE 146-RJ SERIES REFERENCE STANDARD 57-20-50 PT 6 FIGURE 6&7 PAGES 10&11. Includes Test Report and Certificate of Conformance.
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BAE 146-RJ SERIES REFERENCE STANDARD 57-20-50 PT 6 FIGURE 8&9 PAGES 12&13. Includes Test Report and Certificate of Conformance.
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BAE GUIDE MANDREL 146 SERIES / AVRO-RJ SERIES PART 6 57-51-10 PG 6 FIG 2. Includes Certificate of Conformance.
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BOMBARDIER / CANADAIR EDDY CURRENT SURFACE REFERENCE STANDARD PART 6 55-20-001, NOTCHES .008", .020", .040" (.005" Wide +000 / - .002 and +/- .001" Depth), MATERIAL: 4130 STEEL. Includes certification Report and Certificate of Conformance(COC)...
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BOMBARDIER GLOBAL 5000 REFERENECE STANDARD BD-700 PT 6 57-70-001. ALSO IN 53-10-01 PART 6 PAGE 5 FIGURE 1. EDM Notches: .008", .020", .040" ( .005" W +0.00, - .002"), MATERIAL: 4330 or 4340 STEEL. SIZE: 1.5"W x 3.75"L x .25". Includes certification Report Traceable to NIST and Certificate of Conformance(COC).
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BOMBARDIER GLOBAL 5000 REFERENECE STANDARD BD-700 PT 6 57-70-001. ALSO IN 53-10-01 PART 6 PAGE 5 FIGURE 1. EDM Notches: .008", .020", .040" ( .005" W +0.00, - .002"), MATERIAL: 4340 STEEL. SIZE: 1.5"W x 3.75"L x .25". Includes certification Report ...
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BOEING COMPOSITE REFERENCE STANDARD 51-04-00, PAGE 20 FIGURE 7. GR/EP SKIN/NOMEX CORE DISBOND DEFECT
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BOEING COMPOSITE REFERENCE STANDARD 51-04-00, PAGE 19 FIGURE 6. GR/EP SKIN/NOMEX CORE DISBOND DEFECT
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BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE( 1-10 PLY), PT 1 51-04-00, PAGE 21 FIGURE 8. SUPPLIED WITH HOLDING BLOCK
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BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE( 11-20 PLY), PT 1 51-04-00, PAGE 21 FIGURE 8. SUPPLIED WITH HOLDING BLOCK
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BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE( 21-30 PLY), PT 1 51-04-00, PAGE 19 FIGURE 8. SUPPLIED WITH HOLDING BLOCK
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BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATE. MATERIAL: BMS8-79 FIBERGLASS( 1-10 PLY), PT 1 51-04-00, PAGE 27 FIGURE 8. B737 NDT Part 1, 51-04-00. Includes C-Scan, Certification Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATE. MATERIAL: BMS8-79 FIBERGLASS( 11-20 PLY), PT 1 51-04-00, PAGE 27 FIGURE 8. B737 NDT Part 1, 51-04-00. Includes C-Scan, Certification Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATE. MATERIAL: BMS8-79 FIBERGLASS( 21-30 PLY), PT 1 51-04-00, PAGE 27 FIGURE 8. B737 NDT Part 1, 51-04-00. Includes C-Scan, Certification Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATEBMS8-139 FIBERGLASS( 1-10 PLY), PT 1 51-04-00, PAGE 28 FIGURE 8. Includes C-Scan, Certification Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATEBMS8-139 FIBERGLASS( 11-20 PLY), PT 1 51-04-00, PAGE 28 FIGURE 8. Includes C-Scan, Certification Report and Certificate of Conformance.
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BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE WITH HOLDING PLATEBMS8-139 FIBERGLASS( 21-30 PLY), PT 1 51-04-00, PAGE 28 FIGURE 8. Includes C-Scan, Certification Report and Certificate of Conformance.
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BOEING PERFORATED BONDED REFERENCE STANDARD ALUMINUM HONEYCOMB ALL PT4 78-30-01; PG.18 FIG.3
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COMPOSITE 10 STEP WEDGE SOLID LAMINATE, 777 PT 4 51-00-06 PAGE 7 FIGURE 1. BMS 8-276 FABRIC MATERIAL TYPE 35 CL3 GRADE190. STEP SIZES: .050, .100, .200, .300, .400, .500, .600, .700, .800, .900.
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