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S1107-3 (s1107-3--mas.jpg)

Part Number S1107-3

S1107-3, ROD END

Part # S1107-3

ROD END


$59.33 Retail Price: $74.17
In Stock

Get everything you need

STEERING TUBE (Left)

MC0743008-1

STEERING TUBE (Left)

$1,054.28 / was $6,597.54

In Stock
STEERING TUBE (Right)

MC0743008-2

STEERING TUBE (Right)

$993.33 / was $1,145.27

Expected ship date is 12-14-2026.
TUBE STEERING (Right)

MC0543022-4

TUBE STEERING (Right)

$719.90 / was $899.88

In Stock
DOUBLER (Steering Boot)

$80.05 / was $81.36

In Stock
BOOT 150-152 STEERING (Kevlar)

$100.66 / was $122.25

In Stock
DOUBLER, Steering Boot

$89.45 / was $832.99

In Stock
TUBE STEERING (Left)

MC0543022-3

TUBE STEERING (Left)

$719.90 / was $899.88

In Stock

Product Details

Specifications

Approval
FAA TC
Condition
New
Manufacturer
Cessna Aircraft Company
Dimensions
L: 4 x W: 4 x H: 1 in
Weight
0.0062 lbs
Unit of Measure
Each
McFarlane Part Number
S1107-3

Product Description

Nose Gear Steering Rod Ends

Steering rods, boots and doublers also available.

Rod End Dimensions

Part Number Thread Bore/Eye Eligibility*

CA452-334A

1/4-28 External

0.19"

CA452-335A

1/4-28 Internal RH

0.19"

CA452-336A

1/4-28 Internal LH

0.19"

CA452-368

1/2-20 Internal

0.50"

CA452-382

1/2-20 Internal

0.50"

CA452-412

5/16-24 External

0.25"

CA452-439

External

0.19"

CA452-860A

1/4-28 External

0.25"

GMW-3M-470

1/4-28 Internal RH

0.19"

GMW-4M-470

1/4-28 Internal RH

0.25"

MC002-381003-5

1/4-28 External

0.25"

MC002-381003-7

1/4-28 External

0.25"

MCMM3M12

1/4-28 External

0.19"

MCS1104-3

10-32 Internal

0.19"

MCS1105-3

10-32 Internal

0.19"

MCS1106-3

1/4-28 Internal

0.19"

MCS1106-4

1/4-28 Internal

0.25"

MCS1819-4

1/4-28 Internal

0.25"

MM-3M-500

10-32 External RH

0.19"

MW-3M-500

10-32 External RH

0.19"

S1107-3

3/8-24 External

0.19"

S1819-3

1/4-28 Internal RH

0.19"

S1823-3

3/8-24 External

0.19"

S2022-3

3/8-24 External RH

0.25"

S2022-3L

3/8-24 External LH

0.25"

* See the Rod End Eligibility and Application Charts for specific model eligibility.

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

Eligible Aircraft
Make Model Start S/N End S/N Eligibility Chart
Cessna 150150S/N 17001 – 5901859018Eligibility Chart
Cessna 150A150AS/N 15059019 – 1505935015059350Eligibility Chart
Cessna 150B150BS/N 15059351 – 1505970015059700Eligibility Chart
Cessna 150C150CS/N 15059701 – 1506008715060087Eligibility Chart
Cessna 150D150DS/N 15060088 – 1506077215060772Eligibility Chart
Cessna 150E150ES/N 15060773 – 1506153215061532Eligibility Chart
Cessna 150F150FS/N 15061533 – 1506453215064532Eligibility Chart
Cessna 150G150GS/N 15064533 – 1506719815067198Eligibility Chart
Cessna 150H150HS/N 15067199 – 1506930815069308Eligibility Chart
Cessna 172172S/N 28000 – 4675446754Eligibility Chart
Cessna 172A172AS/N 46755 – 4774647746Eligibility Chart
Cessna 172B172BS/N 17247747 – 1724873417248734Eligibility Chart
Cessna 172C172CS/N 17248735 – 1724954417249544Eligibility Chart
Cessna 175175S/N 55001 – 5623856238Eligibility Chart
Cessna 175A175AS/N 56239 – 5677756777Eligibility Chart
Cessna 175B175BS/N 17556778 – 1755700217557002Eligibility Chart
Cessna 175C175CS/N 17557003 – 1755711917557119Eligibility Chart
Cessna 182182S/N 33000 – 3384233842Eligibility Chart
Cessna 182A182AS/N 33843 – 5155651556Eligibility Chart
Cessna 182B182BS/N 51557 – 5235852358Eligibility Chart
Cessna 182C182CS/N 52359 – 5300753007Eligibility Chart
Cessna 182D182DS/N 18253008 – 1825359818253598Eligibility Chart
Cessna 208208S/N 20800001 – 2089999920899999Eligibility Chart
Cessna 208A208AS/N 20800007 – 2080010220800102Eligibility Chart
Cessna 208B208BS/N 208B0001 – 208B9999208B9999Eligibility Chart
Cessna 210K210KS/N 21059200 – 2105950221059502Eligibility Chart
Cessna 210L210LS/N 21059503 – 2106157321061573Eligibility Chart
Cessna 210M210MS/N 21061574 – 2106295421062954Eligibility Chart
Cessna 210N210NS/N 21062955 – 2106413521064135Eligibility Chart
Cessna 210N210NS/N 21064136 – 2106489721064897Eligibility Chart
Cessna 210R210RS/N 21064898 – 2106500921065009Eligibility Chart
Cessna P210NP210NS/N P21000001 – P21000834P21000834Eligibility Chart
Cessna P210RP210RS/N P21000835 – P21000874P21000874Eligibility Chart
Cessna T210KT210KS/N 21059200 – 2105950221059502Eligibility Chart
Cessna T210LT210LS/N 21059503 – 2106157321061573Eligibility Chart
Cessna T210MT210MS/N 21061574 – 2106295421062954Eligibility Chart
Cessna T210NT210NS/N 21062955 – 2106413521064135Eligibility Chart
Cessna T210NT210NS/N 21064136 – 2106489721064897Eligibility Chart
Cessna T210RT210RS/N 21064898 – 2106500921065009Eligibility Chart
Cessna 337337S/N 337-0002 – 337-0239337-0239Eligibility Chart
Cessna 337A (USAF O2B)337A (USAF O2B)S/N 337-0240 – 337-0525337-0525Eligibility Chart
Cessna 337B337BS/N 337-0526 – 337-0755337-0755Eligibility Chart
Cessna 337C337CS/N 337-0756 – 337-0978337-0978Eligibility Chart
Cessna 337D337DS/N 337-0979 – 337-1193337-1193Eligibility Chart
Cessna 337E337ES/N 33701194 – 3370131633701316Eligibility Chart
Cessna 337F337FS/N 33701317 – 3370146233701462Eligibility Chart
Cessna 337G337GS/N 33701463 – 3370181533701815Eligibility Chart
Cessna 337H337HS/N 33701816 – 3370195033701950Eligibility Chart
Cessna F337EF337ES/N F3370001 – F3370024F3370024Eligibility Chart
Cessna F337FF337FS/N F3370025 – F3370055F3370055Eligibility Chart
Cessna F337GF337GS/N F3370056 – F3370084F3370084Eligibility Chart
Cessna F337HF337HS/N F3370085 – F3370086F3370086Eligibility Chart
Cessna FT337EFT337ES/N FT3370001 – FT3370024FT3370024Eligibility Chart
Cessna FT337FFT337FS/N FT3370025 – FT3370055FT3370055Eligibility Chart
Cessna FT337GP (FP337)FT337GP (FP337)S/N FP3370001 – FP3370022FP3370022Eligibility Chart
Cessna FT337HP (FP337H)FT337HP (FP337H)S/N FP3370023 – FP3370023FP3370023Eligibility Chart
Cessna P337HP337HS/N P3370293 – P3370356P3370356Eligibility Chart
Cessna T337BT337BS/N 337-0526 – 337-0755337-0755Eligibility Chart
Cessna T337CT337CS/N 337-0756 – 337-0978337-0978Eligibility Chart
Cessna T337DT337DS/N 337-0979 – 337-1193337-1193Eligibility Chart
Cessna T337ET337ES/N 33701194 – 3370131633701316Eligibility Chart
Cessna T337FT337FS/N 33701317 – 3370139833701398Eligibility Chart
Cessna T337GT337GS/N P3370001 – P3370292P3370292Eligibility Chart
Cessna T337HT337HS/N 33701816 – 3370195033701950Eligibility Chart
Cross Reference

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

  • S1107-3
FAQs

The free play movement of my new steering rod has a little drag when I push it in and out. My old steering rod does not have much shaft drag. Is there something wrong with my new steering rod?

No. A little drag is expected and normal on a new McFarlane steering rod. The drag is caused by the thickness of the dry lubricant painted on the spring rubbing on the shaft. The drag is actually a good thing as it prevents vibration wear and will go away as the dry lubricant is worn in. The drag is acceptable when the weight of the spring and housing overcome the drag when the steering rod is held vertical by the threaded shaft.

What else can cause poor steering response besides the steering rods?

We have seen torn brackets on the rudder bar torque tube cause lose of rudder motion and steering movement. The earlier Cessna airplanes had less reinforcing of the rudder bar torque tubes where the steering rod attachment brackets are welded on than the later model airplanes. An overload of rudder pedal pressure or prior nose gear damage can cause failure of the bracket attachment. Inspect all of the rudder and steering system when poor steering authority is detected.

How do I know if my steering rods are working properly?

The Cessna steering system is an engineering masterpiece that is simple in function while allowing good directional control throughout the transition from flight to ground or ground to flight, even in crosswind conditions. A key part of this system is the steering rods. The steering rods are a spring loaded device that applies spring pressure to pull on one side of the nose gear when it is activated and yet have a specified amount of free play in the opposite direction until a solid push is required for positive steering.

 

The following are some common symptoms of worn out or failed steering rods:

  1. Weak steering (You can push on the rudder but not much happens and you have to use a lot of brake to steer. Often the weakness is one direction only.) The early Cessna steering rod springs were designed such that if the rudder pedal was pushed hard in one direction while the nose gear was pointed all the way the other direction and had some resistance to moving such as soft ground or snow, the spring could be compressed to an extent that it would be permanently shortened leaving it weak. McFarlane has redesigned the spring so this cannot happen.
  2. More or less than 1.2 inches of free play movement or inconsistent free play of the steering rod shaft is present. The spring is retained by a washer that was stop swaged into the steering rod housing. During an overload, such as extra hard pedal force applied with the nose wheel pointed all the way in the opposite direction and restricted or undetected damage from a previous hard landing, the spring retaining washer can be deformed and forced past the swaged stop. This will result in inconsistent free play and erratic function of the steering rod shaft as the washer passes past its designed swaged stop in both directions. The rudder rigging in flight might also be inconsistent. This is a dangerous situation that results in inconsistent steering and the steering rod must be replaced. McFarlane has redesigned the washer and shaft machining to prevent the washer stop failure.
  3. Rust and corrosion can make the steering rods unreliable. The steering rods get water and contaminates from the runway that the nose tire throws at them. The fit of the shaft into the bushing that is swaged into the housing is not a precision fit. This can allow internal contamination, moisture, and salt that will rust the springs and steel housing interior, leaving the components weak and subject to failure. Red rust streaking on the shaft exit area or bubbling of the exterior paint indicate corrosion failure. The McFarlane steering rods are made from 304 stainless steel and have a special corrosion preventative and lubricating coating on the springs to fight against corrosion and wear.
  4. Wear of the shaft and bushing is caused by steering movement and aerodynamic pulse vibrations created by the rotating propeller. This wear can be detected as looseness of the shaft in the end bushing. Some wear is acceptable.
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