We appreciate your interest in Marson Corp part number AB4-5A, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number AB4-5A is listed with the NSN 5320-00-052-1972 and description “Rivet Blind.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Marson Corp under the CAGE Code 10054 or that similarly fall under the FSC 5320 Rivets, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 5320-00-052-1972 parts and Rivet Blind items your operations require, so request a quote today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5320-00-052-1972 Item PartTypeName: RIVET,BLIND | 5320 | 000521972 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
AB4-5A | 2 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AASB | FASTENER LENGTH | 0.409 INCHES MINIMUM AND 0.439 INCHES MAXIMUM |
AASK | HEAD STYLE | UNIVERSAL |
AASU | HEAD HEIGHT | 0.030 INCHES MINIMUM AND 0.040 INCHES MAXIMUM |
AAZE | SHANK DIAMETER | 0.124 INCHES MINIMUM AND 0.128 INCHES MAXIMUM |
AAZF | SHANK STYLE | SELF-PLUGGING |
AAZG | HEAD MAJOR DIAMETER | 0.238 INCHES MINIMUM AND 0.262 INCHES MAXIMUM |
ABAF | EXPANSION DEVICE | PLAIN STEM-TYPE T |
AGAV | END ITEM IDENTIFICATION | AIRCRAFT,T-39;ENGINE,AIRCRAFT,F100-PW-200(F-16A/BC/D) |
ANEE | GRIP LENGTH | 0.251 INCHES MINIMUM AND 0.312 INCHES MAXIMUM |
MATT | MATERIAL | ALUMINUM ALLOY 5052 BODY |
MATT | MATERIAL | ALUMINUM ALLOY 7178 MANDREL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/13 FED SPEC SINGLE MATERIAL RESPONSE MANDREL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-430 FED SPEC SINGLE MATERIAL RESPONSE BODY |
SFTT | SURFACE TREATMENT | ANODIZE OVERALL OR CHROMATE OVERALL |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 MIL SPEC 1ST TREATMENT RESPONSE OVERALL OR MIL-C-5541 MIL SPEC 2ND TREATMENT RESPONSE OVERALL |
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