NSN 5310-00-390-1589
Part Details | DOUBLE HEXAGON EXTENDED WASHER SELF-LOCKING NUT
5310-00-390-1589 A nut having 12 drive points, 24 sides, and an integral washer which extends beyond the points or periphery. An integral feature is incorporated for locking on the threads of a mating member.
Alternate Parts: H495957, H49595-7, 4022989, 4054479, LH111957, LH11195-7, 4054479, 4022988, 4065874, 4054479, 4022989, 4022988, 5310-00-390-1589, 00-390-1589, 5310003901589, 003901589
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | MAR 28, 1974 | 00-390-1589 | 29729 ( NUT, SELF-LOCKING, EXTENDED WASHER, DOUBLE HEXAGON ) |
REFERENCE DRAWINGS & PICTURES
DOUBLE HEXAGON
Cross Reference | NSN 5310-00-390-1589
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| H49595-7 | 15653 | ARCONIC GLOBAL FASTENERS & RINGS,INC. |
| 4022989 | 15653 | ARCONIC GLOBAL FASTENERS & RINGS,INC. |
| 4054479 | 019L2 | FITZ AEROSPACE, LLCDBA ESNA |
| LH11195-7 | 72962 | HARVARD INDUSTRIES INC |
| 4054479 | 54636 | SHERWIN-WILLIAMS COMPANY, THEDBA SHERWIN-WILLIAMS |
| 4022988 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 4065874 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4054479 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4022989 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4022988 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 5310-00-390-1589
| Characteristic | Specifications |
|---|---|
| THREAD SERIES | UNJF |
| NOMINAL THREAD SIZE | 0.438 INCHES |
| THREAD QUANTITY PER INCH | 20 |
| THREAD CLASS | 3B |
| THREAD DIRECTION | RIGHT-HAND |
| HARDNESS RATING | 40.0 ROCKWELL C MAXIMUM |
| NUT STYLE | DOUBLE HEXAGON |
| WASHER OUTSIDE DIAMETER | 0.690 INCHES MINIMUM AND 0.700 INCHES MAXIMUM |
| OVERALL HEIGHT | 0.795 INCHES MINIMUM AND 0.810 INCHES MAXIMUM |
| WASHER THICKNESS | 0.227 INCHES MINIMUM AND 0.247 INCHES MAXIMUM |
| WIDTH ACROSS FLATS | 0.553 INCHES MINIMUM AND 0.564 INCHES MAXIMUM |
| LOCKING FEATURE | PREVAILING TORQUE ALL METAL DESIGN |
| TEMP RATING | 900.0 DEG FAHRENHEIT NOMINAL |
| END ITEM IDENTIFICATION | W/S: ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); ENGINE, AIRCRAFT, F119-PW-100 (F-22 RAPTOR); AIRCRAFT, EAGLE F-15; AIRCARFT, F-16 |