INSTANT RFQ

Explore Our NSN 5320-01-414-5686 Inventory

If you are looking for NSN 5320-01-414-5686 supplies, turn to Boost AOG and our vast collection of offerings. On this page, we have arranged our NSN 5320-01-414-5686 inventory, where part numbers like HL412VAP-6-8, HL412VAZ-6-8, and others are presented alongside relevant information about this NSN for your perusal. Take the time to browse our ever-expanding selection of components as you see fit, and if any particular items pique your interest, be sure to use our online RFQ service to request quotes for your consideration.

All manufacturers and suppliers whose parts we sell are carefully evaluated by our staff as necessary, and a myriad of products we carry are subjected to diverse levels of testing and inspection for fit, form, and function. Additionally, we are fully committed to addressing the time limitations of our customers who shop on Boost AOG, providing options for accelerated shipping based on availability. Keeping this in mind, do not hesitate to reach out to us directly by phone or email, and our knowledgeable team members would be more than happy to help you obtain the NSN 5320-01-414-5686 parts you desire.

Item Name Pin Rivet
Federal Supply Group (FSG) Hardware and Abrasives
Federal Supply Class (FSC) 5320 Rivets
National Item Identification Number (NIIN) 01-414-5686 (014145686)
NCB Code USA (01)
Manufacturer Lisi Aerospace Canada Corp, Sps Technologies Inc, West Coast Aerospace Inc, Hi Shear Corporation, Alcoa Global Fasteners Inc, Huck International Inc
Part Number Manufacturer Item Name Cage Code RFQ
HL412VAP-6-8 lisi aerospace canada corp pin rivet l4528 RFQ
HL412VAP-6-8 sps technologies inc pin rivet 56878 RFQ
HL412VAP-6-8 west coast aerospace inc pin rivet 60516 RFQ
HL412VAP-6-8 hi shear corporation pin rivet 73197 RFQ
HL412VAP-6-8 alcoa global fasteners inc pin rivet 92215 RFQ
HL412VAP-6-8 huck international inc pin rivet 97928 RFQ
HL412VAZ-6-8 hi shear corporation pin rivet 73197 RFQ

Technical Characteristics of NSN 5320014145686

MRCCriteriaCharacteristic
AASBFastener Length0.815 INCHES MINIMUM AND 0.835 INCHES MAXIMUM
AATBWidth Between Flats0.0791 INCHES MINIMUM AND 0.0806 INCHES MAXIMUM
SFTTSurface TreatmentALUMINUM OVERALL
ABAJLubricationCETYL ALCOHOL, SPEC 305, HI-SHEAR CORP
AAJDThread Class3A
CQSXShear Strength95000 SINGLE POUNDS PER SQUARE INCH
AAZFShank StylePIN-RIVET, STRAIGHT, THREADED
CQBCMinimum Tensile Strength160000 POUNDS PER SQUARE INCH
THSDThread Series DesignatorUNJF
CQJXNominal Thread Size0.188 INCHES
AASUHead Height0.064 INCHES MINIMUM AND 0.074 INCHES MAXIMUM
ANEEGrip Length0.495 INCHES MINIMUM AND 0.505 INCHES MAXIMUM
MATTMaterialTITANIUM ALLOY UNS R56400 OVERALL
MRCDecoded RequirementClear Text Reply
STDCSurface Treatment Document And ClassificationHI KOTE 1, ALUMINUM COATING 294 PER HI-SHEAR MFR REF SINGLE TREATMENT RESPONSE OVERALL
AAZGHead Major Diameter0.370 INCHES MINIMUM AND 0.390 INCHES MAXIMUM
AAZEShank Diameter0.2172 INCHES MINIMUM AND 0.2182 INCHES MAXIMUM
AASKHead StyleERR-090
AAJFThread DirectionRIGHT-HAND
MDCLMaterial Document And ClassificationAMS4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL OR AMS4967 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

Relevant Components for NSN - 5320-01-414-5686, 5320014145686
5320-00-026-3543 (5320000263543) 5310-00-894-4984 (5310008944984) 5310-00-358-9938 (5310003589938) 5310-00-214-1145 (5310002141145)
5360-01-655-4048 (5360016554048) 5305-01-292-4295 (5305012924295) 5310-01-527-8911 (5310015278911) 5330-01-367-6783 (5330013676783)
5340-01-499-2137 (5340014992137) 5355-01-412-9108 (5355014129108) 5331-01-569-7241 (5331015697241) 5305-01-321-4164 (5305013214164)

Submit a Quote and We'll Get Back to You Shortly

Guaranteed quotes back within 15 minutes, 24/7 x 365

Thank You for Visiting.

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.

Request for Quote

We use cookies to ensure that we give you the best experience on our website. If you continue to use this site we will assume that you are happy with it.

bottom to top