| U S ARMY AVIATION AND MISSILE COMMAND | 18876 |
| ARMY, UNITED STATES DEPARTMENT OF THE | 19204 |
| CECOM LR CENTER | 97403 |
| CUMMINS POWER GENERATION INC. | 44940 |
| DEPARTMENT OF DEFENSE PROJECT MANAGER-MOBILE ELECTRIC POWER | 30554 |
| LOCKHEED MARTIN CORPORATION | 90536 |
| U S ARMY AVIATION AND MISSILE COMMAND | 18876 |
| DRS SUSTAINMENT SYSTEMS, INC. USE CAGE CODE 98255 FOR CATALOGING | 20418 |
| NORTHROP GRUMMAN SYSTEMS CORPORATION | 26512 |
| LORD CORPORATION | 76005 |
| LORD CORPORATION | 76005 |
| LORD CORPORATION | 76005 |
| FLANGE THICKNESS | 0.170 INCHES NOMINAL |
| THREAD SIZE | 1/4-28UNF-2B ALL THREADED PORTIONS |
| DISTANCE BETWEEN MOUNTING HOLE CENTERS | 1.375 INCHES NOMINAL |
| FLANGE LENGTH | 1.810 INCHES NOMINAL |
| FLANGE WIDTH | 1.810 INCHES NOMINAL |
| STUD LENGTH | 0.290 INCHES NOMINAL ALL THREADED STUD |
| SHORTEST DISTANCE BETWEEN MOUNTING HOLE CENTERS | 1.375 INCHES NOMINAL |
| FLANGE MOUNTING HOLE DIAMETER | 0.201 INCHES NOMINAL |
| STATIC LOAD RATING AT SPECIFIED DEFLECTION | 20 LB LOAD AT UNSPECIFIED DEFLECTION |
| LOAD/FREQUENCY RANGE | RATED AT 20 LB LOAD FOR 25 TO 37 CPS |
| HEIGHT | 1.060 INCHES NOMINAL |
| MATERIAL | ALUMINUM OVERALL |
| SURFACE TREATMENT | ANODIZE OVERALL |
| STYLE DESIGNATOR | ROUND SPRING COMPRESSION FOUR-HOLE FLANGE |
| NONMETALLIC HARDNESS RATING | NOT RATED |
| MAXIMUM LOAD RATING | NOT RATED |
| RIGID MEMBER MATERIAL AND LOCATION | ALUMINUM OVERALL |
| RIGID MEMBER SURFACE TREATMENT AND LOCATION | ANODIZED OVERALL |
| An item made of material having elastic properties. It may have rigid mounting facilities such as a flange(s), sleeve(s), stud(s) or the like. It is designed to isolate or dampen shock and/or vibration of a continuous or intermittent origin and serve as a support for a weapon system component to be isolated. Excludes MOUNT, RESILIENT, GENERAL PURPOSE; SPRING (as modified); BUMPER, NONMETALLIC; BUMPER, RUBBER; BUSHING, NONMETALLIC; hydraulic and pneumatic shock absorbers, dash-pots, grommets, and shock pads. |
