HL86-6 – Textron Aviation OEM Hi-Lok Collar
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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.
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- 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 |