Showing 1 – 40 out of 40

Page 1 out of 1

Part Number Description Equivalents Action
AIRBUS CARBON LAMINATE THICKNESS REFERENCE STANDARD SET A318-A321 51-10-06-PB4 Multidirectional Fabric Material, BLOCKS 01-06 includes waterproof case. Nominal Thicknesses of 1mm, 3mm, 5mm, 9mm, 15mm, 19mm. Includes Test Report and Certificate of Conformance.
AIRBUS A318/A319/A320/A321 CARBON STANDARD PT 4 51-10-06 PAGE 7. MULTIDIRECTIONAL TAPE MATERIAL BLOCK SET OF 4 includes waterproof case. NOMINAL THICKNESS (1mm, 3mm, 5mm, 7mm). Includes Test Report and Certificate of Conformance.
AIRBUS A318/A319/A320/A321 CARBON STANDARD PT 4 51-10-06 PAGE 7. MULTIDIRECTIONAL TAPE MATERIAL BLOCK NOMINAL THICKNESS (1mm). Includes Test Report and Certificate of Conformance.
COMPOSITE STEPWEDGE .05-.90″
ST8871 CARBON LAMINATE STEP WEDGE HOLDER. Includes Certificate of Conformance.

TEK-9012

COMPOSITE STEP WEDGE SOLID CFRP TAPE, BMS 8-276 Cytec. PAD SIZE: 3.0″ WIDE by 2.0″ LONG. STEP SIZES .100” to 1.0” in INCREMENTS of .100″.
Custom 20 ply 12″ x 12″ CFRP Test Panel with 4 random defects(grafoil delaminations) between the ply layup in random locations. Autoclave cured per Boeing Specification BAC 5317. Includes C-Scan image to identify defects and Certificate of Conformance.
REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP DELAM DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance…
REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP DISBOND and CORE LAMINATE INTERFACE. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance.
REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP POTTED HOLE and SPLICE CORE DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance…
REPAIR REFERENCE STANDARD GR/EP LAMINATE STEP POTTED CORE and CORE DEFECT. ALL BOEING AIRCRAFT MODELS PART 1 51-01-01. Includes C-SCAN Certification and Certificate of Conformance…
ALUMINUM TO ALUMINUM SKIN REFERENCE STANDARD WITH A TOTAL OF 10 BONDED SHIMS .016″-.125″ THICK. 100 THICKNESS COMBINATIONS WITH SIMULATED DISBOND DEFECTS. PART 4 51-00-01
Boeing Composite Standard, 777 PT4 51-00-04:PG3 FIG1, 3PLY, 5″ x 3″ x1″. Includes C-Scan and Certificate of Conformance.
BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 10 PLY / 20 PLY. Includes C-Scan and Certificate of Conformance.
BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 12 PLY / 24 PLY. Includes C-Scan and Certificate of Conformance.
BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 20 PLY / 31 PLY. Includes C-Scan and Certificate of Conformance.
BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 3 PLY / 10 PLY. Includes C-Scan and Certificate of Conformance.
BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 3 PLY / 11 PLY. Includes C-Scan and Certificate of Conformance.
BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 3 PLY / 5 PLY. Includes C-Scan and Certificate of Conformance.
BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 3 PLY / 7 PLY. Includes C-Scan and Certificate of Conformance.
BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 3 PLY / 9 PLY. Includes C-Scan and Certificate of Conformance.
BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 3 PLY / 11 PLY. Includes C-Scan and Certificate of Conformance.
BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 6 PLY / 10 PLY. Includes C-Scan and Certificate of Conformance.
BOEING 747 COMPOSITE REFERENCE STANDARD PART 4 57-22-01 FIGURE 2. Includes C-Scan Report and Certificate of Conformance.
BOEING COMPOSITE REFERENCE STANDARD 767 PT 4 57-40-01. AULUMINUM to ALUMINUM HONEYCOMB CORE. Includes C-Scan Report and Certificate of Conformance. 2 year Unconditional Warranty.
BOEING REFERENCE STANDARD 757 Part 4 51-00-05 Page 7 Figure 2. 777-200/300 Part 4 51-00-05 Page 8 Figure 1. Includes Test Report and Certificate of Conformance.
BOEING COMPOSITE REFERENCE STANDARD 51-04-00, PAGE 20 FIGURE 7. GR/EP SKIN/NOMEX CORE DISBOND DEFECT
BOEING COMPOSITE REFERENCE STANDARD 51-04-00, PAGE 19 FIGURE 6. GR/EP SKIN/NOMEX CORE DISBOND DEFECT
BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE( 1-10 PLY), PT 1 51-04-00, PAGE 21 FIGURE 8. SUPPLIED WITH HOLDING BLOCK
BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE( 11-20 PLY), PT 1 51-04-00, PAGE 21 FIGURE 8. SUPPLIED WITH HOLDING BLOCK
BOEING REFERENCE STANDARD, COMPOSITE LAMINATE STEP WEDGE( 21-30 PLY), PT 1 51-04-00, PAGE 19 FIGURE 8. SUPPLIED WITH HOLDING BLOCK
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.
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.
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.
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.
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.
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.
BOEING PERFORATED BONDED REFERENCE STANDARD ALUMINUM HONEYCOMB ALL PT4 78-30-01; PG.18 FIG.3
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.
BOEING COMPOSITE REFERENCE STANDARD 5-10-15 PLY 737 PT 4; 78-30-02 PG.10 FIGURE 4 & 777 PT 4 78-30-03