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MCS2323-10 (mcs2323-5--mas.jpg)
Part Number MCS2323-10

MCS2323-10, WIRE CLAMP, Bolt

Part # MCS2323-10

WIRE CLAMP, Bolt


$24.35 Retail Price: $157.33
In Stock

Product Details

Specifications

Approval
FAA PMA
Condition
New
Manufacturer
McFarlane Aviation
Dimensions
L: 0.59 x W: 0.38 x H: 0.38 in
Weight
0.01 lbs
Unit of Measure
Each
McFarlane Part Number
MCS2323-10

Product Description

Bolt Style Wire Clamps for Solid Wire Controls

The best for less!
  • Many applications: carb heat, cabin air, defrost controls, oxygen control and more
  • Unique design to reduce wire stress
  • Heat treated stainless steel for wear and corrosion resistance

Wire Clamp Diagram

Wire Clamp IPC

Part Number A - Bolt Dia. (in) B - Wrench Size (in) C - Thick (in) D - Grip Length (in) E - Hole Position (in) F - Shank Length (in) G - Hole Dia. (in) T - Thread Application

MCS2323-1

0.188

3/8

0.125

0.250

0.183

0.653

0.073

0-32

Carb heat, starter, mixture, cabin heat, fuel shutoff, strainer drain, defrost, shutter, wastegate, oxygen control, de-ice, heater, airbox, alternate air, flap/elevator, pressure air dump, heat exchanger

MCS2323-2

0.250

7/16

0.156

0.312

0.325

0.781

0.073

1/4-28

Cabin heat, mixture, defrost, cabin heat

MCS2323-3

0.250

7/16

0.156

0.188

0.199

0.539

0.073

1/4-28

Strainer drain, cowl flaps, carb heat, alternate air

MCS2323-4

0.250

7/16

0.156

0.313

0.312

0.781

0.073

1/4-28

Mixture, flap indicator, flap guide, fuel shut-off

MCS2323-5

0.188

3/8

0.125

0.125

0.188

0.531

0.073

10-32

Cabin air, carb heat, starter, airbox, defrost, flap, shutter, oxygen

MCS2323-6

0.250

7/16

0.156

0.188

0.355

0.656

0.073

1/4-28

Mixture, hopper, induction

MCS2323-7

0.188

3/8

0.125

0.250

0.192

0.656

0.076

10-32

Fuel shut-off, alternate air, flap elevator trim

MCS2323-8

0.188

3/8

0.125

0.250

0.202

0.656

0.096

10-32

Fuel shut-off oxygen control

MCS2323-9

0.250

7/16

0.156

0.438

0.343

0.906

0.129

1/4-28

Flap control, flap guide

MCS2323-10

0.188

3/8

0.125

0.125

0.204

0.477

0.079

10-32

Fuel shut-off, heat exchanger

MCS2323-11

0.188

3/8

0.125

0.250

0.266

0.656

0.076

10-32

Mixture, bleed air, fuel selector, flap/elevator

MCS2323-12

0.250

7/16

0.156

0.188

0.357

0.656

0.073

1/4-28

Mixture, cabin heat, pressurization

MCS2323-13

0.250

7/16

0.156

0.313

0.271

0.781

0.073

1/4-28

Mixture, alternate air, bleed air

MCS2323-14

0.188

3/8

0.125

0.125

0.132

0.531

0.082

10-32

Cabin heat, cabin air

MCS2323-19

0.188

3/8

0.125

0.125

0.200

0.531

0.094

10-32

Defroster

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 210N210NS/N 21064536 – 2106489721064897Quantity Per Aircraft 1Location fuel shut-offEligibility Chart 6189
Cessna 210R210RS/N 21064898 – 2106500921065009Quantity Per Aircraft 1Location fuel shut-offEligibility Chart 6189
Cessna P210NP210NS/N P21000761 – P21000834P21000834Quantity Per Aircraft 1Location fuel shutoffEligibility Chart 6189
Cessna P210RP210RS/N P21000835 – P21000874P21000874Quantity Per Aircraft 1Location fuel shutoffEligibility Chart 6189
Cessna T210NT210NS/N 21064536 – 2106489721064897Quantity Per Aircraft 1Location fuel shut-offEligibility Chart 6189
Cessna T210RT210RS/N 21064898 – 2106500921065009Quantity Per Aircraft 1Location fuel shut-offEligibility Chart 6189
Cessna FT337GP (FP337)FT337GP (FP337)S/N FP3370001 – FP3370022FP3370022Quantity Per Aircraft 1Location rear heat exchangerEligibility Chart 6189
Cessna FT337GP (FP337)FT337GP (FP337)S/N FP3370016 – FP3370022FP3370022Quantity Per Aircraft 1Location front heat exchangerEligibility Chart 6189
Cessna FT337HP (FP337H)FT337HP (FP337H)S/N FP3370023 – FP3370023FP3370023Quantity Per Aircraft 1Location rear heat exchangerEligibility Chart 6189
Cessna FT337HP (FP337H)FT337HP (FP337H)S/N FP3370023 – FP3370023FP3370023Quantity Per Aircraft 1Location front heat exchangerEligibility Chart 6189
Cessna P337HP337HS/N P3370293 – P3370356P3370356Quantity Per Aircraft 1Location rear heat exchangerEligibility Chart 6189
Cessna P337HP337HS/N P3370293 – P3370356P3370356Quantity Per Aircraft 1Location front heat exchangerEligibility Chart 6189
Cessna T337GT337GS/N P3370001 – P3370292P3370292Quantity Per Aircraft 1Location rear heat exchangerEligibility Chart 6189
Cessna T337GT337GS/N P3370226 – P3370292P3370292Quantity Per Aircraft 1Location front heat exchangerEligibility Chart 6189
Cessna T337H-SPT337H-SPS/N 33701920 – 3370195533701955Quantity Per Aircraft 1Location rear heat exchangerEligibility Chart 6189
Cessna T337H-SPT337H-SPS/N 33701920 – 3370195533701955Quantity Per Aircraft 1Location front heat exchangerEligibility Chart 6189
Cross Reference

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

  • 0450311-10
  • S2323-10
FAQs

How do I keep contaminants out of my fuel system?

The fuel selector valve works in unscreened fuel. Contaminated fuel can cause selector valve seal damage. When fueling from possibly contaminated fuel sources McFarlane recommends the use of a fuel filter, such as Mr. Funnel or another filtering device, to reduce trash in the fuel system.

What pressure is used to test the fuel selector valves after repairs?

We pressure test our repaired valves to a minimum of 5 psi using precision controlled air pressure and a calibrated low pressure indicator. This pressure is above the normal fuel pressure on the valve and below the limits of the springs in the valve. Each valve is submerged in Stoddard solvent while the air pressure is applied to the valve. The valves are then tested in each position to assure that there are no inter-port or external leaks. Leaks are detected by looking for air bubbles escaping from the valve.

How do I know when to replace or service my fuel selector valve?

The most common indication of external fuel valve leaks is the smell of avgas in the cabin. Most valves are located under the cabin floor. Fuel stain on the valve and drain plug or drain valve or on the belly of the aircraft can also indicate external leakage. External leaks are generally around the actuation valve stem. Internal leaks are detected when the fuel is turned off and fuel continues to drip during fuel system maintenance. Inner port leakage will allow fuel from one tank to leak into another fuel tank. This type leak is difficult to detect. Fuel transfer from one tank to another with the fuel valve selected to one tank only will indicate inner-port leakage. An extended period of time is needed to detect fuel transfer from one tank to another. Generally if internal leakage is detected when servicing the fuel system, it is likely there is also inner-port leakage. 

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