Part Details | PHYSICAL PROPERTIES REFERENCE STANDARD
6635-01-458-4545 Simulates structure of item under test to provide a means to calibrate test equipment. May include carrying case.
Alternate Parts: 17G1104861, 17G110486-1, 6635-01-458-4545, 01-458-4545, 6635014584545, 014584545
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 66 | AUG 26, 1998 | 01-458-4545 | 40786 ( REFERENCE STANDARD, PHYSICAL PROPERTIES ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 6635-01-458-4545
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 17G110486-1 | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 6635-01-458-4545
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 21.000 INCHES NOMINAL |
| OVERALL WIDTH | 23.000 INCHES NOMINAL |
| OVERALL HEIGHT | 5.000 INCHES NOMINAL |
| SPECIAL FEATURES | REFERENCE STANDARD FINISH, A SIMILAR ELASTOMER EROSION COATING AND PAINT THAT CLOSELY MATCHES THE AIRCRAFT DESIGN FINISH; OPERATING TEMPERATURE -40 TO 125 DEG F |
| END ITEM IDENTIFICATION | C-17 NDI SUPPORT |
| FUNCTIONAL DESCRIPTION | TO SETUP THE BONDMASTER FOR NDI OF LRUS CONTRUCTED OF GLASS EPOXY SKINS OVER NOMEX HONEYCOMB CORE |
| RELATIONSHIP TO SIMILAR EQUIPMENT | REPLACES P/N 17G110842-1, NSN 6635-01-407-1504 ON AN ATTRITION BASIS |
| REFERENCE DATA AND LITERATURE | T.O.1C-17A-4-4 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | REFERENCE STANDARD GLASS SKIN TO NOMEX CORE |