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TL-KT-1 (tl-kt-7--mas1.jpg)

Part Number TL-KT-11

TL-KT-11, TORQUE LINK KIT, Cessna, Nose Gear

Part # TL-KT-11

TORQUE LINK KIT, Cessna, Nose Gear


$280.46 Retail Price: $393.34
In Stock

Included Components (16 Part Types)

Details
Buy
AN310-3

NUT, Castellated, 10-32

$3.01/each

Kit includes 1

In Stock
AN310-4

NUT

$2.37/each

Kit includes 2

In Stock
Sold in quantities of 5
MC0543047-1

SPACER, Torque Link

$80.53/each

Kit includes 1

In Stock
MC0543047-2

SPACER, Torque Link

$71.02/each

Kit includes 1

In Stock
MCS1450-6B14-007

SHIM TORQUE LINK

$4.05/each

Kit includes 2

In Stock
MCS1450-6B14-010

SHIM TORQUE LINK

$3.92/each

Kit includes 5

In Stock
MCS1450-6B14-012

SHIM TORQUE LINK

$3.28/each

Kit includes 2

In Stock
MCS1450-6B14-015

SHIM TORQUE LINK

$3.31/each

Kit includes 2

In Stock
MS24665-132

COTTER PIN, 1/16" X 1/2"

$0.080/each

Kit includes 3

In Stock
Sold in quantities of 25
NAS1149F0332P

WASHER, 3/16, Steel, .032

$0.040/each

Kit includes 4

In Stock
Sold in quantities of 100
NAS1149F0432P

WASHER, 1/4, Steel, .032

$0.040/each

Kit includes 4

In Stock
Sold in quantities of 100
NAS1149F0463P

WASHER, 1/4, Steel, .063

$0.070/each

Kit includes 4

In Stock
Sold in quantities of 100
NAS6203-22D

BOLT

$3.31/each

Kit includes 1

In Stock
Sold in quantities of 5
NAS6204-43D

BOLT

$17.70/each

Kit includes 2

In Stock
NAS77-3-023

BUSHING

$6.22/each

Kit includes 4

In Stock
NAS77-6-088

BUSHING

$4.28/each

Kit includes 4

In Stock

Get everything you need

SPACER, Torque Link

MC0543047-1

SPACER, Torque Link

$80.53 / was $94.66

In Stock
SPACER, Torque Link

MC0543047-2

SPACER, Torque Link

$71.02 / was $94.24

In Stock
SHIM TORQUE LINK

MCS1450-6B14-005

SHIM TORQUE LINK

$3.96 / was $9.39

In Stock
SHIM TORQUE LINK

MCS1450-6B14-007

SHIM TORQUE LINK

$4.05 / was $9.59

In Stock
SHIM TORQUE LINK

MCS1450-6B14-010

SHIM TORQUE LINK

$3.92 / was $4.51

In Stock
WASHER, 3/16, Steel, .016

$0.090 / was $0.14

In Stock
SHIM KIT, Torque Link

TL-SHIM-KT-1

SHIM KIT, Torque Link

$40.86 / was $60.51

In Stock

Product Details

Specifications

Approval
FAA PMA
Condition
New
Manufacturer
McFarlane Aviation
Dimensions
L: 4.25 x W: 3.75 x H: 1 in
Weight
1.27 lbs
Unit of Measure
Each
McFarlane Part Number
TL-KT-11

Product Description

Solves and prevents many wheel shimmy problems

  • Complete McFarlane manufactured FAA-PMA kits include all commonly replaced torque link parts
  • Only McFarlane has shims in three thicknesses for a precision fit
  • Fits most single engine Cessna aircraft
  • Now with specific model eligibility 

Can You Stop Nose Gear Shimmy? by Dave McFarlane

Width Across Hex Flats Bolt Total Length Bolt Dia. Kit Part Numbers

.490- .502

1.82- 1.88

.311- .312

TL-KT-8

.428- .440

1.89- 1.94

.246- .249

TL-KT-10

.428- .440

3.01- 3.07

.246- .249

TL-KT-6

.428- .440

3.13- 3.20

.246- .249

TL-KT-1 TL-KT-4 TL-KT-5 TL-KT-6 TL-KT-7

.428- .440

4.13- 4.20

.246- .249

TL-KT-10

.428-.440

4.31-4.26

.248-249

TL-KT-1-H

.553- .565

3.18- 3.24

.371- .374

TL-KT-8

.428- .440

4.12- 4.20

.248- .249

TL-KT-10

.367- .376

1.79- 1.84

.188- .189

TL-KT-1 TL-KT-1-H TL-KT-2 TL-KT-4 TL-KT-5 TL-KT-6 TL-KT-7 TL-KT-11

.429- .439

3.16- 3.24

.248- .249

TL-KT-2 TL-KT-4 TL-KT-5 TL-KT-11

Eligibility Notes:

Note 1: TL-KT-8 torque link kit is used on Cessna model aircraft with heavy duty landing gear that utilizes AN6 size (3/8-24 UNF) bolts in the upper and lower torque link joints. The normal duty landing gear uses AN4 size (1/4-28 UNF) bolts in the upper and lower torque link joints.

Note 2: Aircraft models in this serial range may use one of two choices for McFarlane Torque Link Kits. The aircraft that have both upper and lower spacers measuring ~2 inches long will use McFarlane Torque Link Kit TL-KT-1 (containing two MC0543047-1 spacers). The aircraft that has an upper spacer measuring ~2.6 inches and a lower spacer measuring ~2 inches will use McFarlane Torque Link Kit TL-KT-2 (containing one MC0543047-1 and one MC0543047-2 spacer).

Note 3: Aircraft models in this serial range may use one of two choices for McFarlane Torque Link Kits. The aircraft that have both upper and lower spacers measuring ~2 inches long will use McFarlane Torque Link Kit TL-KT-5 (containing two MC0543047-1 spacers). The aircraft that has an upper spacer measuring ~2.6 inches and a lower spacer measuring ~2 inches will use McFarlane Torque Link Kit TL-KT-4 (containing one MC0543047-1 and one MC0543047-2 spacer).

Note 4: Aircraft models in this serial range may use one of two choices for McFarlane Torque Link Kits. The aircraft that have both upper and lower spacers measuring ~2 inches long will use McFarlane Torque Link Kit TL-KT-1 (containing two MC0543047-1 spacers). The aircraft that has an upper spacer measuring ~2.6 inches and a lower spacer measuring ~2 inches will use McFarlane Torque Link Kit TL-KT-7 (containing one MC0543047-1 and one MC0543047-2 spacer).

Note 5: Aircraft models in this serial range may use one of two choices for McFarlane Torque Link Kits. The aircraft that have both upper and lower spacers measuring ~2 inches long will use McFarlane Torque Link Kit TL-KT-1 (containing two MC0543047-1 spacers). The aircraft that has an upper spacer measuring ~2.6 inches and a lower spacer measuring ~2 inches will use McFarlane Torque Link Kit TL-KT-11 (containing one MC0543047-1 and one MC0543047-2 spacer).

Can't decide if you have the standard or heavy duty nose wheel?

The bolt sizes on your torque link can help you decide. Use the following table to help you determine the correct torque link kit for your application.

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

Eligible Aircraft
Make Model Start S/N End S/N Quantity Per Aircraft Location Comment Eligibility Chart
Cessna P206BP206BS/N P206-0307 – P206-0419P206-0419Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna P206CP206CS/N P206-0420 – P206-0519P206-0519Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna P206DP206DS/N P206-0520 – P206-0603P206-0603Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna P206EP206ES/N P20600604 – P20600641P20600641Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna P206EP206ES/N P20600642 – P20600647P20600647Quantity Per Aircraft 1Location nose strut torque linkComment Eligibility Chart 6167
Cessna TP206BTP206BS/N P206-0307 – P206-0419P206-0419Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna TP206CTP206CS/N P206-0420 – P206-0519P206-0519Quantity Per Aircraft 1Location nose strut torque linkComment See Note 2Eligibility Chart 6167
Cessna TP206DTP206DS/N P206-0520 – P206-0603P206-0603Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna TP206ETP206ES/N P20600604 – P20600647P20600647Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna TU206BTU206BS/N U206-0657 – U206-0914U206-0914Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna TU206CTU206CS/N U206-0915 – U206-1234U206-1234Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna TU206DTU206DS/N U206-1235 – U206-1444U206-1444Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna TU206ETU206ES/N U20601445 – U20601537U20601537Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna TU206FTU206FS/N U20601701 – U20602199U20602199Quantity Per Aircraft 1Location nose strut torque linkComment Eligibility Chart 6167
Cessna U206BU206BS/N U206-0657 – U206-0914U206-0914Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna U206CU206CS/N U206-0915 – U206-1234U206-1234Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna U206DU206DS/N U206-1235 – U206-1444U206-1444Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna U206EU206ES/N U20601445 – U20601700U20601700Quantity Per Aircraft 1Location nose strut torque linkComment See Note 5Eligibility Chart 6167
Cessna U206FU206FS/N U20601701 – U20602199U20602199Quantity Per Aircraft 1Location nose strut torque linkComment Eligibility Chart 6167
Cross Reference

Reference only: Please verify the product is eligible for your aircraft before adding to your cart.

  • TCTL
  • TCTL-KT
FAQs

How do you remove torque link bushings to install new ones?

Removing the flanged bushings from the torque link forging can be difficult as there is not a good surface to press against or grab onto. An easy way to remove them is to thread them with a tap, screw a bolt in the thread you made, and then drive or press against the bolt. The thread does not have to be a full depth thread for the bolt to hold securely in the bushing. The bushing material is somewhat hard, but not so hard that a standard hardware store tap will not do the job. Use cutting oil on the tap to prevent tap damage. Normally the bushing will then come out easily.

 

For stubborn bushings, soak the link assembly in boiling water before pressing the bushing. The heat will expand the aluminum forging more than the steel bushing. This helps loosen the press fit while limiting the temperature to prevent from overheating and harming the heat treat of the aluminum forging. A controlled oven can be substituted for boiling water as a heat source, but do not exceed 350° F. Do not use flame or other non-controlled heat sources.

 

An alternate method is to put dry ice in the bushing before driving or pressing on the bolt you threaded into the bushing. Do not over-press or hammer as the aluminum can gall to the bushing and leave a damaged bushing bore. If the bushing does not come out with light to moderate force take the time to use some heat or cold to help.

I installed a torque link kit and serviced my shimmy dampener; why do I still have a shimmy problem?

There are many components all connected to keep the nose gear in line. If one component is worn or out of tolerance it can cause shimmy problem. Reference Dave McFarlane’s article: Can You Stop Nose Gear Shimmy instructions and suggestions.

 

Overlooked items also include the rod ends, shimmy dampener mounting and attachment, shimmy dampener, and steering collar. The steering collar is where the steering rod tubes connect and the upper torque link is attached to, along with the shimmy dampener on most aircraft. If the steering collar has play vertically and laterally and is allowed to tilt; that will cause excessive wear and force on the torque links, steering, and strut components. There are three different thicknesses of shims to help get the collar in place.

 

Ensure that the shimmy dampener is working properly with no dead spots in dampening action. The cylinder could be worn on the inside or on a piston that warrants replacement of components. All of the nose strut components are tied to each other and any movement is transmitted through to the tire and back through the dampening system, which if remedied will continue to be more pronounced.

Do I need anything else besides the torque link repair kit?

You might need a few of the NAS1149F0316P ultra-thin washers to fine tune the center “knee” joint fit on most of the Cessna airplanes. They are not included in the kit.

Is the proper nut and bolt torque important?

It is very important to maintain proper torque for the bolts that clamp the chrome bushing/spacer at the upper attachments to the steering collar and the lower attachment to the nose gear strut. It is commonly thought that the chrome bushing/spacer is kept in position by the bolt filling the center bore of the bushing/spacer. This is not correct as the inner bore of the chrome bushing/spacer and the bolt are a loose non-precision fit. The bushing/spacer is secured by the bolt end, clamping the spacer so that it is tight between the arms of the aluminum forgings. Any looseness of this end clamp will allow movement of the chrome bushing/spacer. This movement will erode the aluminum forgings and create more free motion of the torque link.

 

All shimming of the torque links must be done with proper torque on the bolts. Periodically and during nose gear inspections, check the torque on the upper and lower torque link bolts. If the chrome bushing/spacer is allowed to move, the resultant wear can require replacement of the expensive aluminum forgings. McFarlane is working on a repair for the worn aluminum forgings. Unlike our competitors, extra care is given to the machining of the McFarlane chrome bushing/spacers to give the largest possible bearing surface to the ends that bear against the aluminum forgings. Chamfers or bevels are kept very small.

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