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National Stock Number: 5342-01-353-1953
Federal Supply Class: 5342
National Item Identification Number: 013531953
Description: MOUNT,RESILIENT,WEAPON SYSTEM
Detail: 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.
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Manufacturer Information:
13027494 | 18876 | U S ARMY AVIATION AND MISSILE COMMAND | TTNA-3 | 81860 | HUTCHINSON AEROSPACE & INDUSTRY, INC. |
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Techincal Specification:
FLANGE MOUNTING HOLE DIAMETER | 0.201 INCHES NOMINAL | FLANGE LENGTH | 2.380 INCHES NOMINAL | FLANGE WIDTH | 2.380 INCHES NOMINAL | HEIGHT | 1.030 INCHES NOMINAL | LOAD/FREQUENCY RANGE | 15.0 LB LOAD FOR 14 TO 19 HERTZ | MATERIAL DOCUMENT AND CLASSIFICATION | ASTM B209, ALLOY 6061, T6 ASSN STD SINGLE MATERIAL RESPONSE CORE | MATERIAL DOCUMENT AND CLASSIFICATION | ASTM B209, ALLOY 6061, T6 ASSN STD SINGLE MATERIAL RESPONSE FLANGE | MATERIAL | ALUMINUM ALLOY 6061 CORE | MATERIAL | ALUMINUM ALLOY 6061 FLANGE | MAXIMUM LOAD RATING | 70.0 POUNDS | SHORTEST DISTANCE BETWEEN MOUNTING HOLE CENTERS | 1.937 INCHES NOMINAL | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-C-5541, CLASS 1A MIL SPEC SINGLE TREATMENT RESPONSE CORE | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-C-5541, CLASS 1A MIL SPEC SINGLE TREATMENT RESPONSE FLANGE | SURFACE TREATMENT | CHROMATE CORE | SURFACE TREATMENT | CHROMATE FLANGE |
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