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TLSL-KT-2 (tlsl-kt-2-4--mas.jpg)
Part Number TLSL-KT-4

TLSL-KT-4, STOP LUG KIT, Torque Link

Part # TLSL-KT-4

STOP LUG KIT, Torque Link


$299.47 Retail Price: $673.44
Expected ship date is 10-19-2026.

Included Components (3 Part Types)

Details
Buy
AN3H3A

BOLT, 3/16, Drilled Head

$0.95/each

Kit includes 2

In Stock
Sold in quantities of 5
MC0442506-11

STOP LUG, Torque Link

$230.66/each

Kit includes 1

In Stock
MC0442506-9

SAFETY PLATE, Stop Lug, Torque Link

$46.83/each

Kit includes 1

In Stock

Product Details

Specifications

Approval
Kit with Approved Contents
Condition
New
Manufacturer
McFarlane Aviation
Dimensions
L: 7 x W: 5 x H: 2 in
Weight
0.107 lbs
Unit of Measure
Each
McFarlane Part Number
TLSL-KT-4

Product Description

Torque Link Stop Lugs and Safety Plate

This often overlooked but important part is affordable at McFarlane!
The torque link stop lug is a sacrificial part that hammers against a flat spot on the lower part of the shock strut outer tube when the strut extends after takeoff. This prevents the strut from overextending and forces the nose wheel and rudder system into proper alignment for flight.

Due to repeated hammering with every takeoff, these stop lugs must be periodically replaced. Excessive wear can allow overextension of the strut. They also often wear unevenly resulting in inconsistent alignment of the nose wheel in flight which then causes extra drag and yaw. The extra yaw can require increased rudder trim which causes even more drag. So yes, replacing a torque link stop lug can reduce drag!

  • Safety plate features bend up tabs to secure stop lug bolts
  • Super tough 4130 alloy steel for corrosion resistance
  • Kits include stop lug, safety plate and applicable 3/16" bolts

More important than you think
Overextension of the nose strut due to a worn out stop lug can lead to a cascade of problems. McFarlane A&P mechanics have seen struts over extend to the point where the metering pin comes out of the orifice. This results in loss of dampening action and the pin hammering the orifice every landing, and distorting and enlarging it. Over time, the excess nose strut travel and lack of dampening can result in fatigue cracks in the torque link arms. McFarlane recommends thoroughly inspecting all nose strut components when replacing a severely worn stop lug.

Maintenance Tip:

Replace the stop lug if it is no longer flush with the strut, mushroomed, worn, rounded, bent away from the torque link, or if it has stress cracks. The safety plate should not be reused.

WARNING: Cancer and/or Reproductive Harm - California Proposition 65 Resources

Eligible Aircraft
Make Model Start S/N End S/N Quantity Per Aircraft Location Eligibility Chart
Cessna 182K182KS/N 18257626 – 1825850518258505Quantity Per Aircraft 1Location Nose StrutEligibility Chart 6745
Cessna 182L182LS/N 18258506 – 1825930518259305Quantity Per Aircraft 1Location Nose StrutEligibility Chart 6745
Cessna 182M182MS/N 18259306 – 1826005518260055Quantity Per Aircraft 1Location Nose StrutEligibility Chart 6745
Cessna 182N182NS/N 18260056 – 1826082518260825Quantity Per Aircraft 1Location Nose StrutEligibility Chart 6745
Cessna 182P182PS/N 18260826 – 1826246518262465Quantity Per Aircraft 1Location Nose StrutEligibility Chart 6745
Cessna 182P182PS/N 18262466 – 1826517518265175Quantity Per Aircraft 1Location Nose StrutEligibility Chart 6745
Cessna 182Q182QS/N 18265176 – 1826771518267715Quantity Per Aircraft 1Location Nose StrutEligibility Chart 6745
Cessna 182R182RS/N 18267716 – 1826858618268586Quantity Per Aircraft 1Location Nose StrutEligibility Chart 6745
Cessna F182PF182PS/N F18200001 – F18200025F18200025Quantity Per Aircraft 1Location Nose StrutEligibility Chart 6745
Cessna F182QF182QS/N F18200026 – F18200169F18200169Quantity Per Aircraft 1Location Nose StrutEligibility Chart 6745
FAQs

What does the Torque Link Stop Lug do?

The torque link stop lugs are more important than you would think. Overextension of the nose strut due to a worn out stop lug can lead to a cascade of problems. McFarlane A&P mechanics have seen struts over extend to the point where the metering pin comes out of the orifice. This results in loss of damping action and the pin hammering the orifice every landing and distorting and enlarging it. Over time, the excess nose strut travel and lack of damping can result in fatigue cracks in the torque link arms. McFarlane recommends thoroughly inspecting all nose strut components when replacing a severely worn stop lug.

 

The stop lug also acts as a centering device aligning the nose wheel and wheel pant straight with the airplane and slip stream after it has left the runway. Worn stop lugs can allow the nose wheel to lock in a turned position in flight that will require holding rudder for coordinated flight. Retractable gear aircraft depend on the stop lug to properly center the nose gear steering before it retracts into the wheel well.

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