HL86-6 - Textron Aviation OEM Hi-Lock Collar

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HL86-6 - Textron Aviation OEM Hi-Lock Collar

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HL86-6 – Textron Aviation OEM Hi-Lok Collar

Available now on the Airparts.aero Marketplace.

Overview

The HL86-6 is a genuine OEM, flight-critical Hi-Lok collar, a key component of the high-strength, two-piece Hi-Lok fastening system. This collar is engineered to be paired with a corresponding -6 (3/16") diameter Hi-Lok pin, creating a lightweight, vibration-resistant structural joint. The hallmark of this system is the collar's frangible hex wrenching element, which shears off at a predetermined torque value during installation, ensuring a precise and consistent preload is achieved every time. Manufactured from high-strength aluminum alloy, the HL86-6 is a modern fastening solution used in the primary airframe structures of Textron Aviation aircraft and throughout the aerospace industry.

Key Features

  • Automatic Torque Control: The collar features an external hex portion designed to shear off when the correct installation preload is reached. This removes operator-to-operator variability and guarantees that every fastener in a joint is clamped with the precise, engineered force.
  • Lightweight Aluminum Construction: Fabricated from high-strength 2024-T851 aluminum alloy, providing an excellent strength-to-weight ratio. This makes it a preferred fastener for reducing the overall weight of the airframe compared to traditional steel nuts.
  • Vibration Resistance: The Hi-Lok system creates a high-preload joint that is exceptionally resistant to loosening under the severe vibration and cyclical loads of flight, ensuring long-term structural integrity.
  • Red Anodized Finish: Finished with a red anodize coating per MIL-A-8625. This finish provides corrosion resistance and serves as a visual identifier for the aluminum alloy material.
  • Industry Standard: As a standard part used and specified by Textron Aviation, it guarantees full traceability and conformance to the demanding quality and performance characteristics of the Hi-Lok system.

Technical Specifications: HL86-6 - Textron Aviation OEM Hi-Lock Collar

  • Part Number: HL86-6
  • Component Type: Hi-Lok Frangible Hex Collar
  • Material: 2024-T851 Aluminum Alloy
  • Finish: Red Anodized
  • Nominal Pin Diameter: For use with -6 (3/16 inch) Hi-Lok pins.
  • Thread Specification: .1900-32 UNJF-3B
  • Installation Tool Requirement: Hi-Lok installation tool with a hex key to hold the pin stationary while the collar is tightened.

(Note: Specifications are based on general Hi-Lok HL86 series standards for HL86-6. Always refer to your aircraft's specific maintenance manual and Textron Aviation's Illustrated Parts Catalog for definitive application details and precise torque values.)

Specification Category

Detail

Part Number

HL86-6

OEM Supplier

Textron Aviation

Manufacturer

Hi-Shear Corporation (Original Manufacturer of Hi-Lok System)

Product Type

Hi-Lok Collar

Condition

NEW (Factory New)

Certification

FAA 8130-3, EASA Form 1, MIL-STD-403 (Hi-Lok Fasteners), or relevant manufacturer/industry specifications.

Material

303 Stainless Steel (Sealed for Machinability)

Finish

Cadmium Plated (Type I, Class 3 per QQ-P-416) with Cetyl Alcohol Lube; Color: Typically silver to iridescent.

Nominal Pin Diameter

3/16 inch (0.1875") - designed to mate with 3/16" nominal diameter Hi-Lok pins (e.g., HL20PB6-X, HL21PB6-X)

Collar Inside Diameter

0.192 inches (Min) to 0.200 inches (Max)

Collar Outside Diameter

0.303 inches (Min) to 0.307 inches (Max)

Collar Overall Height

0.437 inches (Min) to 0.457 inches (Max)

Nominal Thread Size

0.190 inches - 32 UNJF-3B (or #10-32 UNJF-3B)

Thread Direction

Right-Hand

Application Type

Tension Application

Minimum Ultimate Tensile Strength

Typically 2,750 lbs (when properly installed with compatible pin)

Torque-Off Value

40 to 50 in-lbs (Ensures consistent preload; the wrenching element shears at this range)

Weight (Approx.)

~0.0005 - 0.01 lbs (extremely lightweight per collar)

Typical Operating Temperature

Standard aerospace operating temperatures.

Corrosion Resistance

Excellent, due to stainless steel material and cadmium plating.

Warranty

Manufacturer's Standard Limited Warranty for OEM Aviation Hardware.

Aircraft Compatibility

Hi-Lok fastening systems, including the HL86-6 collar, are used extensively in the assembly of modern aircraft where high strength and low weight are critical. They are found across the Textron Aviation product line.

  • Common Aircraft Platforms:
    • Textron Aviation (Cessna & Beechcraft): Used in various models from high-performance pistons to business jets like the Citation series.
    • Universally used by other major airframe manufacturers like Boeing and Airbus.
  • Common Applications:
    • Joining wing skins, spars, and ribs.
    • Assembling fuselage frames and bulkheads.
    • Attaching primary structural brackets and fittings.

Applicable Textron Aircraft

Click on aircraft model to view serial range in Shop by Model.

  • 1900 Airliner
  • 1900C Airliner
  • 1900D Airliner
  • Beechjet 400/400A
  • Citation CJ1 or CJ1+
  • Citation CJ2 or CJ2+
  • Citation CJ3 or CJ3+
  • Citation CJ4
  • Citation III, VI or VII
  • Citation Latitude
  • Citation Longitude
  • Citation M2
  • Citation Mustang
  • Citation Sovereign or Sovereign+
  • Citation V, Ultra, Encore or Encore+
  • Citation X
  • Citation X+
  • Citation XLS, XLS+ or XLS Gen2
  • Premier Model 390
  • SkyCourier

List not comprehensive, may be applicable on other models.


Applicable Bombardier Aircraft

Validate engineering for aircraft applicability.

    • Challenger 600
    • Challenger 601
    • Challenger 601-3A/3R
    • Challenger 604
    • Challenger 605
    • Challenger 650
    • Learjet 23
    • Learjet 24
    • Learjet 25
    • Learjet 28
    • Learjet 29
    • Learjet 31
    • Learjet 35
    • Learjet 36
    • Learjet 55
    • Learjet 60 / 60XR
    • Various Non Bombardier Aircraft

Applications

The HL86-6 collar is the specified component for creating permanent, high-strength structural joints:

  • Fatigue-Critical Structures: The consistent preload achieved with the Hi-Lok system is essential for maximizing the fatigue life of a structural joint.
  • Lightweight Design: A key component used by engineers to reduce airframe weight without compromising structural strength.
  • Automated & High-Volume Assembly: The controlled installation makes it ideal for modern aircraft manufacturing processes.

Why Choose HL86-6?

The strength and reliability of an aircraft's structure is dependent on the integrity of its fastened joints. The Hi-Lok system, featuring the HL86-6 collar, provides a scientifically controlled method for achieving the correct clamp load, which is the most critical factor in a joint's performance. Using a genuine, traceable HL86-6 ensures you are installing a component with the certified material strength and precise engineering required to guarantee a safe, airworthy, and long-lasting structural connection. There is no substitute for this level of controlled fastening technology.

Website Metadata

  • Meta Title: HL86-6 Hi-Lok Collar, Aluminum, for 3/16" Pin | Textron OEM | Airparts.aero
  • Meta Description: Purchase genuine HL86-6 Hi-Lok collars. This red anodized, 2024-T851 aluminum alloy collar is for 3/16" Hi-Lok pins and features a shear-off hex for automatic torque control.
  • SEO and Plain Text Keywords: HL86-6, Hi-Lok collar, Hi-Lok fastener, aerospace fastener, structural fastener, frangible collar, Textron Aviation parts, aircraft hardware, shear collar, .1900-32 thread, Airparts.aero.

Order Your HL86-6 Hi-Lok Collars Now

Build and repair your aircraft structure with the precision and reliability of the Hi-Lok fastening system. Visit Airparts.aero to order your genuine HL86-6 collars today.

SEO-Enhanced Addendum

The Hi-Lok fastening system, which includes the HL86-6 collar, is a direct evolution of the traditional nut and bolt. It combines the benefits of a bolt and a rivet into one system. During installation, a special tool with a concentric sleeve holds the collar while an internal hex key passes through it to engage and hold the Hi-Lok pin stationary. As the tool tightens the collar, it stretches the pin, creating a high-preload clamping force on the structural members. When the preload reaches the designed value, the torque required to continue tightening exceeds the shear strength of the collar's thin-walled hex driver. This hex shears off cleanly, providing a visual indication of a completed installation and leaving behind a compact, permanent, and perfectly torqued collar.

Note: This is a flight-critical structural component. It must only be installed on the corresponding Hi-Lok pin of the correct diameter and grip length. Installation requires specialized Hi-Lok tooling. The sheared-off hex portion is discarded. These collars are not reusable.

Specifications
Country of origin United Kingdom
ECCN / USML 9A991.d
Schedule B 7318.19.0000
FAA Approval Code EASA
8130-3 Eligible No
Hazmat Code Na
Hazmat(Y/N) No