Thank you for taking an interest in the Mount Resilient Weapon System NSN parts that we carry here on Buy Military Ground Vehicle Parts. You have reached the RFQ page for part number HT1821-10, an item that traces back to the manufacturer Lord Corporation. Listed with NSN 5342008649514, this listing is available for purchase from our website at any time. If you are interested in part number HT1821-10 and wish to learn more, be sure to fill out and submit the RFQ form found on this page. By presenting us information such as your target price and expected delivery date, we can best formulate and present a solution that closely caters to your unique needs and restrictions alike.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5342-00-864-9514 Item PartTypeName: MOUNT,RESILIENT,WEAPON SYSTEM | 5342 | 008649514 | W | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
HT1697-10 | 6 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AFQM | DISTANCE BETWEEN MOUNTING HOLE CENTERS | 1.371 INCHES MINIMUM AND 1.379 INCHES MAXIMUM |
AGXF | STUD LENGTH | 0.310 INCHES NOMINAL ALL THREADED STUD |
BXCH | SHORTEST DISTANCE BETWEEN MOUNTING HOLE CENTERS | 1.371 INCHES MINIMUM AND 1.379 INCHES MAXIMUM |
BXCQ | FLANGE MOUNTING HOLE DIAMETER | 0.200 INCHES MINIMUM AND 0.205 INCHES MAXIMUM |
MATT | MATERIAL | ALUMINUM ALLOY OVERALL |
ABUJ | THREAD SIZE | 1/4-28UNF-2B OR 1/4-28NF-2B ALL THREADED PORTIONS |
AFQN | FLANGE LENGTH | 1.820 INCHES NOMINAL |
AGFF | FLANGE WIDTH | 1.820 INCHES NOMINAL |
AYXK | MAXIMUM LOAD RATING | 10.000 POUNDS |
BXCT | STATIC LOAD RATING AT SPECIFIED DEFLECTION | 10 LB LOAD RATING AT 0.205 IN. DEFLECTION |
BXCW | LOAD/FREQUENCY RANGE | 9 LB LOAD FOR 20 HZ |
HGTH | HEIGHT | 1.060 INCHES NOMINAL |
SFTT | SURFACE TREATMENT | ANODIZE OVERALL |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
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