NSN 5310-00-167-0739
Part Details | FLAT WASHER
5310-00-167-0739 A washer having a centrally located hole with a solid or laminated cross-section and two flat parallel bearing surfaces. The hole must be 75 percent or less than the largest dimension and the bearing surface finish is greater than 32 microinch (0.8 micrometer). The thickness cannot exceed 25 percent of the largest outside dimension. When the largest outside dimension is less than 1/4 inch or 6mm, the thickness must be 0.006 inches (0.15mm) or greater and for items 1/4 inch (6mm) or larger, the thickness must be 0.016 inches (0.4mm) or greater. The maximum tolerance is applied to dimensions and used as a determining factor. Items with separable lamination use SHIM. For items fabricated from ceramic or electrically rated materials by specification or industry standards use INSULATOR (1), WASHER. Excludes DISK, VALVE, graphite impregnated and lubricated items.
Alternate Parts: AN960D8, AN9608D, AN960-8D, 431265063, 43126-506-3, 2411396, 2411396, 2411396, 01496, 1290636, 12906-36, 10087987, 8807935, 5310-00-167-0739, 00-167-0739, 5310001670739, 001670739
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 53 | JAN 01, 1963 | 00-167-0739 | 13393 ( WASHER, FLAT ) |
REFERENCE DRAWINGS & PICTURES
RECTANGULAR
ROUND
ROUND
Cross Reference | NSN 5310-00-167-0739
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AN960D8 | 88044 | AERONAUTICAL STANDARDS GROUPDEPT OF NAVY AND AIR FORCE |
| AN960-8D | 88044 | AERONAUTICAL STANDARDS GROUPDEPT OF NAVY AND AIR FORCE |
| 43126-506-3 | 94756 | BOEING COMPANY, THEDBA BOEING |
| 2411396 | FB459 | EMBRAER AVIATION INTERNATIONAL |
| 2411396 | S4956 | EMBRAER EMPRESA BRASILEIRA DEAERONAUTICA SA |
| 2411396 | 001JK | EMBRAER S.A.DBA EMBRAER |
| 01496 | 75547 | LAWRENCE AERONAUTICAL CORP |
| 12906-36 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| 10087987 | A486G | NIMIKKEISTOKESKUS NCB FINLAND |
| 8807935 | 19203 | PICATINNY ARSENAL |
Technical Data | NSN 5310-00-167-0739
| Characteristic | Specifications |
|---|---|
| HOLE DIAMETER | 0.164 INCHES MINIMUM AND 0.184 INCHES MAXIMUM |
| PERIPHERAL SHAPE STYLE | ROUND |
| OVERALL DIAMETER | 0.370 INCHES MINIMUM AND 0.395 INCHES MAXIMUM |
| CENTER HOLE SHAPE STYLE | ROUND |
| CROSS-SECTIONAL SHAPE STYLE | RECTANGULAR |
| THICKNESS | 0.028 INCHES MINIMUM AND 0.036 INCHES MAXIMUM |
| END ITEM IDENTIFICATION | W/S:ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); MISSILE, ADVANCED MEDIUM RANGE AIR-TO-AIR (AMRAAM)/AIM120A; AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130); SUPPORT EQUIPMENT, B-1 AIRCRAFT; SUPPORT EQUIPMENT, B-52 AIRCRAFT; MISSILE, TOMAHAWK; TEST CONSOLES, MINI-SACE; AIRCRAFT, THUNDERBOLT II, A-10; AIRCRAFT, EAGLE F-15; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H) |
