| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| C12-DEL-3C1N | COMPOSITE STANDARD | 3 | |
| C12-DIS-3C1N | COMPOSITE STANDARD | 3 | |
| C12-DIS-3C2N | COMPOSITE STANDARD | 1 | |
| ST8870-9 | COMPOSITE STANDARD | 4 | |
| SWREF1 | COMPOSITE STANDARD | 2 | |
| TEK-SWREF1 | COMPOSITE STANDARD | 1 |
Partial Match
| Part Number | Description | Sources Available | Tool Request Qty |
|---|---|---|---|
| (CALIB) C12-PCS-3C1N | REFERENCE STANDARD COMPOSITE (CALIBRATION) | 1 | |
| (CALIB) TEK-SWREF1 | COMPOSITE STANDARD (CALIBRATION) | 1 | |
| 1353316 | SOLID COMPOSITE LAMINATE NDI REFERENCE STANDARDS | 1 | |
| 4.1MM | 0.1614 CARBIDE COMPOSITE DRILL BIT-3, ( NON-STANDARD ) | 1 | |
| 98S57205030-004 | COMPOSITE LIGHTNING REFERENCE STANDARD..FOR ATR72 PT 4 51-40-00: REFERENCE DRAWING | 5 | |
| 98S57205030.001 | COMPOSITE LIGHTNING REFERENCE STANDARD..FOR ATR72 PT 4 51-40-00: REFERENCE DRAWING | 4 | |
| 98S57205030.004 | COMPOSITE LIGHTNING REFERENCE STANDARD..FOR ATR72 PT 4 51-40-00: REFERENCE DRAWING | 5 | |
| 99D51407291001 | AIRBUS COMPOSITE REFERENCE STANDARD KIT | 7 | |
| C12-DEL-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 12PLY CARBON FIBER, (DEL) INTERPLY DELAMANATIONS | 3 | |
| C12-DEL-3C2N | Composite Standard, Boeing All PT 51-01-01, 12ply carbon fiber, (DEL) interply delamanations | 1 | |
| C12-DIS-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 12PLY CARBON FIBER, (DIS) SKIN TO CORE DISBONDS | 3 | |
| C12-DIS-3C2N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 12PLY CARBON FIBER, (DIS) SKIN TO CORE DISBONDS | 1 | |
| C12-PCS-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 12PLY CARBON FIBER, (PCS) POTTING AND CORE SPLICE | 3 | |
| C12-PCS-3C2N | Composite Standard, Boeing All PT 51-01-01, 12ply carbon fiber, (PCS) potting and core splice | 1 | |
| C12-POT-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 12PLY CARBON FIBER, (POT) SKIN TO POTTING DISBONDS | 3 | |
| C12-POT-3C2N | Composite Standard, Boeing All PT 51-01-01, 12ply carbon fiber, (POT) skin to potting disbonds | 1 | |
| C24-DEL-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 24PLY | 1 | |
| C24-DIS-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 24PLY | 1 | |
| C24-PCS-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 24PLY | 1 | |
| C24-POT-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 24PLY | 1 | |
| CE9900085-101 | COMPOSITE LAMINATE CALIBRATION REFERENCE STANDARD | 1 | |
| CE9900086-101 | COMPOSITE LAMINATE CALIBRATION REFERENCE STANDARD | 1 | |
| CE9900088-001 | COMPOSITE SANDWICH CALIBRATION REFERENCE STANDARD | 1 | |
| CE9900088-003 | COMPOSITE SANDWICH CALIBRATION REFERENCE STANDARD | 1 | |
| CE9900088-007 | COMPOSITE SANDWICH CALIBRATION REFERENCE STANDARD | 1 | |
| CE9900088-009 | COMPOSITE SANDWICH CALIBRATION REFERENCE STANDARD | 1 | |
| CE9900430-001 | COMPOSITE SANDWICH CALIBRATION REFERENCE STANDARD | 1 | |
| CHRS-1-12 | Composite Standard, Boeing 767 PT1 51-01-01 PG14- R&D | 1 | |
| CHRS-1-3 | Composite Standard Boeing 767 PT1 51-01-01 PG14 R&D | 1 | |
| CHRS-1-6 | Composite Standard Boeing 767 PT1 51-01-01 PG14 R&D | 1 | |
| CHRS-1-9 | Composite Standard, Boeing 767 PT1 51-01-01 PG 14 R&D | 1 | |
| COMPOSITE STANDARD 1-10 PLIES | COMPOSITE STANDARD, BOEING 737 PT1 51-04-00 FIG. 8 SHEET 2: BMS 8-79, TYPE1581, CL3 GR1, 1-10 PLIES | 1 | |
| COMPOSITE STANDARD 11-20 PLIES | COMPOSITE STANDARD, BOEING 737 PT1 51-04-00 FIG. 8 SHEET 2: BMS 8-79, TYPE1581, CL3 GR1, 11-20 PLIES | 1 | |
| COMPOSITE STANDARD 21-30 PLIES | COMPOSITE STANDARD, BOEING 737 PT1 51-04-00 FIG. 8 SHEET 2: BMS 8-79, TYPE1581, CL3 GR1, 21-30 PLIES | 1 | |
| F12-DEL-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 12PLY FIBERGLASS, (DEL) INTERPLY DELAMANATIONS | 1 | |
| F12-DIS-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 12PLY FIBERGLASS, (DIS) SKIN TO CORE DISBONDS | 1 | |
| F12-PCS-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 12PLY FIBERGLASS, (PCS) POTTING AND CORE SPLICE | 1 | |
| F12-POT-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 12PLY FIBERGLSS, (POT) SKIN TO POTTING DISBONDS | 1 | |
| F24-DEL-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 24PLY | 1 | |
| F24-DIS-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 24PLY | 1 | |
| F24-PCS-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 24PLY | 1 | |
| F24-POT-3C1N | COMPOSITE STANDARD, BOEING ALL PT 51-01-01, 24PLY | 1 | |
| NDT1046 | Boeing Composite Standard, 777 PT4 51-00-04:PG3 FIG1, 3PLY, 5" x 3" x1". Includes C-Scan and Certificate of Conformance. | 3 | |
| NDT1046-10-20 | BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 10 PLY / 20 PLY. Includes C-Scan and Certificate of Conformance. | 1 | |
| NDT1046-12-24 | BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 12 PLY / 24 PLY. Includes C-Scan and Certificate of Conformance. | 1 | |
| NDT1046-20-31 | BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 20 PLY / 31 PLY. Includes C-Scan and Certificate of Conformance. | 1 | |
| NDT1046-3-10 | BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 3 PLY / 10 PLY. Includes C-Scan and Certificate of Conformance. | 1 | |
| NDT1046-3-11 | BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 3 PLY / 11 PLY. Includes C-Scan and Certificate of Conformance. | 1 | |
| NDT1046-3-5 | BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 3 PLY / 5 PLY. Includes C-Scan and Certificate of Conformance. | 1 | |
| NDT1046-3-7 | BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 3 PLY / 7 PLY. Includes C-Scan and Certificate of Conformance. | 1 | |
| NDT1046-3-9 | BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 3 PLY / 9 PLY. Includes C-Scan and Certificate of Conformance. | 1 | |
| NDT1046-3/11 MOD | BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 3 PLY / 11 PLY. Includes C-Scan and Certificate of Conformance. | 1 | |
| NDT1046-6-10 | BOEING COMPOSITE STANDARD, ALL PT9 51-00-01 PG. 6 FIGURE 1. 6 PLY / 10 PLY. Includes C-Scan and Certificate of Conformance. | 2 | |
| NDT1106 | Boeing Reference Standard composite..737 PT4 51-00-05 PG 5-6 FG 1 | 2 | |
| NDT1106-1 | Boeing Reference Standard composite..737 PT4 51-00-05 PG 5-6 FG 1 With top plate thickness of .060", .080" .100".. | 1 | |
| NDT4150 | Composite/Bonded Standard, Boeing 747 PT4 57-22-01 | 1 | |
| NDT629 | 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. | 2 | |
| ST8870-1 | Composite Standard, Boeing All PT1 51-04-00:PG21 FIG7 | 4 | |
| ST8870-1-F | Composite Standard, Boeing All PT1 51-04-00:PG21 FIG7 *Fiberglass skin instead of carbon fiber* | 1 | |
| ST8870-4 | Composite Standard, Boeing All PT1 51-04-00:PG20 FIG6 | 4 | |
| ST8870-4-F | Composite Standard, Boeing All PT1 51-04-00:PG20 FIG6, *Fiberglass skin instead of carbon fiber | 1 | |
| ST8870-7 | Composite Standard, Boeing All PT1 51-04-00:PG19 FIG8 | 4 | |
| ST8870-8 | Composite Standard, Boeing All PT1 51-04-00:PG19 FIG8 | 5 | |
| ST8870-9 | Composite Standard, Boeing All PT1 51-04-00:PG19 FIG8 | 4 | |
| ST8870B-7 | 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. | 3 | |
| ST8870B-8 | 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. | 3 | |
| ST8870B-9 | 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. | 3 | |
| ST8870C-7 | 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. | 2 | |
| ST8870C-8 | 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. | 2 | |
| ST8870C-9 | 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. | 2 | |
| ST8871 | REFERENCE STANDARD COMPOSITE | 4 | |
| ST8871D | BOEING COMPOSITE REFERENCE STANDARD 5-10-15 PLY 737 PT 4; 78-30-02 PG.10 FIGURE 4 & 777 PT 4 78-30-03 | 4 | |
| SWREF1 | COMPOSITE STANDARD (CALIBRATION) | 2 | |
| TEK-SWREF1 | Composite Standard; R&D | 1 | |
| ZC12-DEL-3C1N | Composite Standard, Boeing All PT1 51-01-01 | 1 |
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