NSN 5340-01-110-8125
Part Details | SPACING THREADED STANDOFF
5340-01-110-8125 A standoff that must have a threaded end(s) or be internally threaded its full length. For items having external threads on both ends, see STUD (as modified). For items with an outside contour that is the same for the entire length, are flat on top and bottom, having internal threads its full length, and the length does not exceed twice the width across the flats or outside diameter, see NUT (as modified); use maximum dimensions(s) for compliance.
Alternate Parts: 74A4509072001, 74A450907-2001, 74A4509072001, 74A450907-2001, D0931530093, 74A4509072001, 74A450907-2001, 74A4509072001, 74A450907-2001, 74A4509072001, 74A450907-2001, 74A4509072001, 74A450907-2001, 10154121, 74A4509072001, 74A450907-2001, 5340-01-110-8125, 01-110-8125, 5340011108125, 011108125
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | APR 06, 1981 | 01-110-8125 | 40280 ( STANDOFF, THREADED, SPACING ) |
REFERENCE DRAWINGS & PICTURES
LEFT INTERNAL AND RIGHT INTERNAL THREADS
Cross Reference | NSN 5340-01-110-8125
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 74A450907-2001 | 2U518 | BLAIR INDUSTRIES, INC. |
| 74A450907-2001 | 76301 | BOEING COMPANY, THEDBA BOEING |
| D0931530093 | 1574B | E.A. - MAESTRANZA AEREA DE ALBACETE |
| 74A450907-2001 | 13002 | GOODRICH CORPORATIONDBA GOODRICH LANDING GEAR DIVISION |
| 74A450907-2001 | 5U018 | ISRAEL AIRCRAFT INDUSTRIES LTDMARKETING DIRECTORATE |
| 74A450907-2001 | 85941 | MAGELLAN AEROSPACE, NEW YORK, INC. |
| 74A450907-2001 | 2M490 | NASSAU TOOL WORKS, INC. |
| 10154121 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
| 74A450907-2001 | 35962 | SAFRAN LANDING SYSTEMS CANADA INC |
Technical Data | NSN 5340-01-110-8125
| Characteristic | Specifications |
|---|---|
| CROSS-SECTIONAL SHAPE | ROUND |
| DIAMETER | 0.498 INCHES MINIMUM AND 0.499 INCHES MAXIMUM |
| STYLE DESIGNATOR | LEFT INTERNAL AND RIGHT INTERNAL THREADS |
| LENGTH | 1.120 INCHES MINIMUM AND 1.130 INCHES MAXIMUM |
| DISTANCE FROM END TO HOLE CENTER | 0.560 INCHES MINIMUM AND 0.570 INCHES MAXIMUM |
| HOLE QUANTITY PERPENDICULAR TO AXIS | 1 |
| END ITEM IDENTIFICATION | W/S: AIRCRAFT, HORNET F/A-18; F/A-18E/F HORNET AIRCRAFT |