Products

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

.050" 7075-T6 ALUMINUM WITH THREE FLAT BOTTOM HOLES (2/64", 3/64", and 5/64") DRAWING "A" (PS21211.3 FOR F/A-18 OUTER WING FORWARD SPAR)

.080" 7075-T6 ALUMINUM WITH THREE FLAT BOTTOM HOLES (2/64", 3/64", and 5/64") DRAWING "A" (PS21211.3 FOR F/A-18 OUTER WING FORWARD SPAR)

.125" 7075-T6 ALUMINUM WITH THREE FLAT BOTTOM HOLES (2/64", 3/64", and 5/64") DRAWING "A" (PS21211.3 FOR F/A-18 OUTER WING FORWARD SPAR)

2/64" FLAT BOTTOM HOLE EQUIVALENT SURFACE NOTCH STANDARD (*ABOVE DESCRIPTION MUST BE ENGRAVED ON THE REFERENCE STANDARD) ..DRAWING "B" (PS21211.3 FOR F/A-18 OUTER WING FORWARD SPAR) MATERIAL=7075-T6

MIL-STD-2154A, STANDARD ULTRASONIC TEST BLOCK FOR AGNLE BEAM EXAMINATION, 7075-t6

Avcon Industries LFEC Calibration Reference Standard. BNC Document: 00107021, Rev. B Figure 7 Page 22. Material: 2024-T3 Aluminum. Includes Test Report and Certificate of Conformance.

Custom Radius Channel Standard Material: 7075-T651 ALUMINUM. Standard to include a total of 62 EDM flaws identified as A, B,C, D, E, and F in the drawing. Includes test report traceable to NIST standards which comply with MIL-Q-9858A, Mil-4-45208A.

Custom Radius Channel Standard Material: 6AL-4V Titanium. Standard to include a total of 62 EDM flaws identified as A, B,C, D, E, and F in the drawing. Includes test report traceable to NIST standards which comply with MIL-Q-9858A, Mil-4-45208A.

BAE 146-RJ SERIES REFERENCE STANDARD 53-20-26 PT 6 FIGURE 6&7 PAGES 12&13. Includes Test Report and Certificate of Conformance.

BAE 146-RJ SERIES REFERENCE STANDARD 57-55-09 PT 6 FIGURE 6&7 PAGES 12&13. Includes Test Report and Certificate of Conformance.