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MS29513-034 - Aerospace Applications O-Ring 2.114 In ID 2-1/4 in OD 1/16 in Thick
MS29513-034 - Aerospace Applications O-Ring 2.114 In ID 2-1/4 in OD 1/16 in Thick
2,14
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MS29513-211 - Aircraft Engine O-Ring 0.796 In ID 1-1/16 in OD 1/8 In Thick
MS29513-211 - Aircraft Engine O-Ring 0.796 In ID 1-1/16 in OD 1/8 In Thick
0,88
0,88

MS29513-114 - Aircraft Engine O-Ring 0.612 in ID, 13/16 in OD, 3/32 In Thickness

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MS29513-114 – Aircraft Engine High-Temperature O-Ring

Available now through the AirParts Aero marketplace.

Overview Section

The MS29513-114 is a specialized, fuel-resistant Aviation O-Ring specifically designed for aircraft engine applications.1 Manufactured to the Military Standard (MS) 29513, this O-ring is engineered to provide a high-integrity seal in environments characterized by high temperatures and constant exposure to petroleum-based fluids.

While it shares dimensions with standard industrial O-rings, the MS29513 series is distinguished by its material chemistry—a medium-to-high nitrile (Buna-N) compound specifically optimized for fuel system service. It is the primary choice for sealing interfaces in carburetors, fuel injection systems, and oil lines where failure-free performance is a flight-safety requirement.

Key Features Section

  • Fuel & Oil Optimization: Specifically formulated to resist swelling and degradation when in constant contact with 100LL Avgas, Jet-A, and mineral-based engine oils.

  • High-Heat Tolerance: Capable of maintaining its sealing "memory" in engine compartment temperatures ranging from -40°F to +250°F.

  • Precision -114 Sizing: Manufactured to the AS568 standard dash size -114, ensuring a perfect "void-to-volume" fill in standard aerospace glands.

  • Low Compression Set: Engineered to resist "flattening" over time, ensuring a persistent seal against mating surfaces even during long periods of engine inactivity.

  • 70 Durometer (Shore A): Provides the ideal medium hardness to seal irregular surfaces while remaining stiff enough to resist extrusion under moderate pressures.

  • MS-Certified Reliability: Meets the strict quality control standards for tensile strength and elongation required for FAA-certified engines.

Technical Specifications Section

SpecificationDetail
StandardMS29513 (Supersedes AN6227 series)
Dash Size-114
MaterialAcrylonitrile Butadiene (Nitrile / Buna-N)
Inside Diameter (ID)0.612 in (15.54 mm)
Outside Diameter (OD)0.812 in (20.62 mm)
Cross-Section (W)0.103 in (2.62 mm)
Hardness70 Shore A
ColorBlack

Aircraft Compatibility Section

The MS29513-114 is a critical seal for both legacy and modern reciprocating engines:

  • Lycoming & Continental Engines: Frequently used in oil cooler bypass valves, fuel injector manifolds, and pushrod housing seals.

  • Precision Airmotive (Bendix) Carburetors: Found in the fuel inlet fittings and mixture control shafts of the MA-series carburetors.

  • Cessna & Piper Fuel Systems: Used in fuel selector valves and fuel strainer (gascolator) assemblies.

  • General Aviation Accessories: Often utilized in engine-driven vacuum pumps and oil temperature bulb adapters.

Technical Applications & Safety

In aircraft engines, the MS29513-114 creates a seal by being "squeezed" between two metal surfaces. Because engine vibration is constant, the O-ring must maintain its elasticity to prevent "weeping."

Safety Warning: Do not substitute with standard industrial Nitrile O-rings. While a hardware-store O-ring may share the -114 dimensions, its rubber compound is not certified for high-octane aviation fuel. It may swell or dissolve, leading to fuel leaks or engine-stoppage due to debris in the fuel lines. Additionally, check the Cure Date (shelf life) on the packaging; Nitrile O-rings typically have a 15-year shelf life.3 Expired seals become brittle and can crack upon installation.4

  1. Avoid Spiral Failure: When installing the O-ring over a long shaft, use a small amount of clean engine oil or Parker O-Lube to ensure it slides without twisting.

  2. Tooling: Use a plastic O-ring pick to remove the old seal. Scratches on the aluminum gland caused by metal screwdrivers are a primary cause of persistent leaks.

  3. Visual Check: Ensure the O-ring is seated flat in the groove before tightening the mating part. A "pinched" O-ring will fail immediately upon the application of fuel pressure.