PartsTable TECHNICAL DATA SHEET
JULY 2026Technical Data Sheet

HL97DJ-8Collar,pin-Rivet

Lisi Aerospace Canada Corp Div Hi Shear Holdings Inc · NSN 5320-01-257-1714 · FSC 5320 · No Item Name Available
Verified by PartsTable
NSN 5320-01-257-1714 — this item is cataloged by the U.S. Government under National Stock Number 5320-01-257-1714. Primary manufacturer part number: HL97DJ-8.
Features
  • Collar,pin-Rivet — FSC 5320
  • Thread Direction: RIGHT-HAND
  • Thread Series Designator: UNIFIED NATIONAL JOINT FINE (UNJF)
  • Material: IRON ALLOY 660 OVERALL
  • Thread Quantity Per Inch: 28
  • Collar Inside Diameter: 0.254 INCHES MINIMUM AND 0.258 INCHES MAXIMUM IN
  • Nominal Thread Size: 0.250 INCHES IN
  • Thread Class: 3B
Applications
  • Applications requiring Iron Alloy 660 Overall construction
General Description

The Collar,pin-Rivet, cataloged under National Stock Number 5320-01-257-1714, is classified within Federal Supply Class 5320 (No Item Name Available) of the Hardware and Abrasives group. The primary manufacturer of record is Lisi Aerospace Canada Corp Div Hi Shear Holdings Inc. Government technical data includes 12 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 6 commercial cross-references from 6 manufacturers, enabling identification through both NSN and commercial part number lookups. 2 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.

Technical Specifications
ParameterValue
NSN5320-01-257-1714
Primary Part NumberHL97DJ-8
Item NameCollar,pin-Rivet
FSC / FSG5320 / 53 — No Item Name Available
ManufacturerLisi Aerospace Canada Corp Div Hi Shear Holdings Inc
StatusACTIVE
Thread DirectionRIGHT-HAND
Thread Series DesignatorUNIFIED NATIONAL JOINT FINE (UNJF)
MaterialIRON ALLOY 660 OVERALL
Thread Quantity Per Inch28
Collar Inside Diameter0.254 INCHES MINIMUM AND 0.258 INCHES MAXIMUM IN
Nominal Thread Size0.250 INCHES IN
Thread Class3B
Material Document and ClassificationAMS 5731 ASSN STD SINGLE MATERIAL RESPONSE OR AMS 5734 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
Collar StyleTHREADED (BREAK OFF) TYPE
Collar Outside Diameter0.408 INCHES MINIMUM AND 0.412 INCHES MAXIMUM IN
LubricationSOLID FILM
Collar Overall Height0.532 INCHES MINIMUM AND 0.552 INCHES MAXIMUM IN
Lifecycle & Compliance
Acquisition StatusACTIVE
HAZMATNo
Verified Substitutes 2
2530-00-741-1016 INTERCHANGEABLE
Brake Shoe
6730-01-353-8438 INTERCHANGEABLE
Encoder,rotary
Cross-Reference Index
Part NumberManufacturer
HL97DJ-8 PRIMARY Lisi Aerospace Canada Corp Div Hi Shear Holdings Inc (CAN)
HL97DJ-8 Sps Technologies, Llc Dba PB Fasteners (USA)
HL97DJ-8 Howmet Global Fastening Systems Inc Div Torrance Operations (USA)
30-241-8 PRIMARY Bell Textron Inc (USA)
HL97DJ-8 West Coast Aerospace, Inc. (USA)
HL97DJ-8 PRIMARY Hi-Shear Corporation (USA)
Related Parts
2530-00-741-1016INTERCHANGEABLE
BRAKE SHOE
6730-01-353-8438INTERCHANGEABLE
ENCODER,ROTARY

Frequently Asked Questions

What is NSN 5320-01-257-1714?

NSN 5320-01-257-1714 is a Collar,pin-Rivet, manufactured by Lisi Aerospace Canada Corp Div Hi Shear Holdings Inc, classified under FSC 5320 (No Item Name Available). Status: active.

What are the part numbers for NSN 5320-01-257-1714?

NSN 5320-01-257-1714 has 6 cross-referenced part numbers: HL97DJ-8 (Lisi Aerospace Canada Corp Div Hi Shear Holdings Inc), HL97DJ-8 (Sps Technologies, Llc Dba PB Fasteners), HL97DJ-8 (Howmet Global Fastening Systems Inc Div Torrance Operations), 30-241-8 (Bell Textron Inc), HL97DJ-8 (West Coast Aerospace, Inc.) and 1 more.

What NSN replaces 5320-01-257-1714?

There are 2 known substitutes for 5320-01-257-1714: 2530-00-741-1016, 6730-01-353-8438. Verify interchangeability with system specifications before substitution.

What are the specifications of HL97DJ-8?

Key specifications for HL97DJ-8: Thread Direction: RIGHT-HAND; Thread Series Designator: UNIFIED NATIONAL JOINT FINE (UNJF); Material: IRON ALLOY 660 OVERALL; Thread Quantity Per Inch: 28. 12 total characteristics are documented in the Federal Logistics Information System.

Validated with multiple authoritative sources, including Government, OEM, and Certified sources.
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