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S1823-3 (s1823-3--mas2.jpg)

Part Number S1823-3

S1823-3, ROD END

Part # S1823-3

ROD END


$165.05 Retail Price: $199.00
In Stock

Get everything you need

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
STEERING TUBE (Left)

MC0743008-1

STEERING TUBE (Left)

$1,054.28 / was $6,597.54

In Stock
TUBE STEERING (Left)

MC0543022-3

TUBE STEERING (Left)

$719.90 / was $899.88

In Stock
TUBE STEERING (Right)

MC0543022-4

TUBE STEERING (Right)

$719.90 / was $899.88

In Stock
STEERING TUBE (Right)

MC0743008-2

STEERING TUBE (Right)

$993.33 / was $1,145.27

Out of Stock

Product Details

Specifications

Approval
FAA TC
Condition
New
Manufacturer
Cessna Aircraft Company
Dimensions
L: 6 x W: 4 x H: 1 in
Weight
0.0062 lbs
Unit of Measure
Each
McFarlane Part Number
S1823-3

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 150J150JS/N 15069309 – 1507112815071128Eligibility Chart
Cessna 150K150KS/N 15071129 – 1507200315072003Eligibility Chart
Cessna 150L150LS/N 15072004 – 1507578115075781Eligibility Chart
Cessna 150M150MS/N 15075782 – 1507940515079405Eligibility Chart
Cessna A150KA150KS/N A1500001 – A1500226A1500226Eligibility Chart
Cessna A150LA150LS/N A1500227 – A1500523A1500523Eligibility Chart
Cessna A150MA150MS/N A1500524 – A1500734A1500734Eligibility Chart
Cessna F150JF150JS/N F150-0390 – F150-0529F150-0529Eligibility Chart
Cessna F150KF150KS/N F15000530 – F15000658F15000658Eligibility Chart
Cessna F150LF150LS/N F15000659 – F15001143F15001143Eligibility Chart
Cessna F150MF150MS/N F15001144 – F15001428F15001428Eligibility Chart
Cessna FA150KFA150KS/N FA1500001 – FA1500081FA1500081Eligibility Chart
Cessna FA150LFA150LS/N FA1500082 – FA1500120FA1500120Eligibility Chart
Cessna FA150L (when equipped w/FKA150-2311 & FKA150-2316)FA150L (when equipped w/FKA150-2311 & FKA150-2316)S/N FA1500121 – FA1500261FA1500261Eligibility Chart
Cessna FA150M (when equipped w/FKA150-2311 & FKA150-2316)FA150M (when equipped w/FKA150-2311 & FKA150-2316)S/N FA1500262 – FA1500336FA1500336Eligibility Chart
Cessna 152152S/N 15279406 – 1528603315286033Eligibility Chart
Cessna A152A152S/N A1520735 – A1521049A1521049Eligibility Chart
Cessna F152F152S/N F15201429 – F15201980F15201980Eligibility Chart
Cessna FA152FA152S/N FA1520337 – FA1520425FA1520425Eligibility Chart
Cessna 172D172DS/N 17249545 – 1725057217250572Eligibility Chart
Cessna 172E172ES/N 17250573 – 1725182217251822Eligibility Chart
Cessna 172F (T-41A)172F (T-41A)S/N 17251823 – 1725339217253392Eligibility Chart
Cessna 172G172GS/N 17253393 – 1725489217254892Eligibility Chart
Cessna 172H (T-41A)172H (T-41A)S/N 17254893 – 1725651217256512Eligibility Chart
Cessna 172I172IS/N 17256513 – 1725716117257161Eligibility Chart
Cessna 172K172KS/N 17257162 – 1725922317259223Eligibility Chart
Cessna 172L172LS/N 17259224 – 1726075817260758Eligibility Chart
Cessna 172M172MS/N 17260759 – 1726345817263458Eligibility Chart
Cessna 172M172MS/N 17263459 – 1726758417267584Eligibility Chart
Cessna 172N172NS/N 17267585 – 1727400917274009Eligibility Chart
Cessna 172P172PS/N 17274010 – 1727665417276654Eligibility Chart
Cessna 172Q172QS/N 17275869 – 1727621117276211Eligibility Chart
Cessna 172R172RS/N 17280001 – 1729999917299999Eligibility Chart
Cessna 172S172SS/N 172S8001 – 172S99999172S99999Eligibility Chart
Cessna F172DF172DS/N F172-0001 – F172-0018F172-0018Eligibility Chart
Cessna F172EF172ES/N F172-0019 – F172-0085F172-0085Eligibility Chart
Cessna F172FF172FS/N F172-0086 – F172-0179F172-0179Eligibility Chart
Cessna F172GF172GS/N F172-0180 – F172-0319F172-0319Eligibility Chart
Cessna F172HF172HS/N F17200655 – F17200754F17200754Eligibility Chart
Cessna F172HF172HS/N F172-0320 – F172-0654F172-0654Eligibility Chart
Cessna F172KF172KS/N F17200755 – F17200804F17200804Eligibility Chart
Cessna F172LF172LS/N F17200805 – F17200904F17200904Eligibility Chart
Cessna F172MF172MS/N F17200905 – F17201234F17201234Eligibility Chart
Cessna F172MF172MS/N F17201235 – F17201514F17201514Eligibility Chart
Cessna F172NF172NS/N F17201515 – F17202039F17202039Eligibility Chart
Cessna F172PF172PS/N F17202040 – F17202254F17202254Eligibility Chart
Cessna FP172FP172S/N FP172-0001 – FP172-0003FP172-0003Eligibility Chart
Cessna FR172EFR172ES/N FR17200001 – FR17200060FR17200060Eligibility Chart
Cessna FR172FFR172FS/N FR17200061 – FR17200145FR17200145Eligibility Chart
Cessna FR172GFR172GS/N FR17200146 – FR17200225FR17200225Eligibility Chart
Cessna FR172HFR172HS/N FR17200226 – FR17200350FR17200350Eligibility Chart
Cessna FR172JFR172JS/N FR17200351 – FR17200590FR17200590Eligibility Chart
Cessna FR172KFR172KS/N FR17200591 – FR17200675FR17200675Eligibility Chart
Cessna P172DP172DS/N P17257120 – P17257188P17257188Eligibility Chart
Cessna R172KR172KS/N R1722000 – R1723454R1723454Eligibility Chart
Cessna 177177S/N 17700001 – 1770116417701164Eligibility Chart
Cessna 177A177AS/N 17701165 – 1770137017701370Eligibility Chart
Cessna 177B177BS/N 17701371 – 1770275217702752Eligibility Chart
Cross Reference

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

  • S1823-3
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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