Ir al contenido
MS29513-114 - Aircraft Engine O-Ring 0.612 in ID, 13/16 in OD, 3/32 In Thickness
MS29513-114 - Aircraft Engine O-Ring 0.612 in ID, 13/16 in OD, 3/32 In Thickness
0,97
0,97
MS29513-238 - Military Standards Oil Filter Housing O-Ring
MS29513-238 - Military Standards Oil Filter Housing O-Ring
3,23
3,23

MS29513-211 - Aircraft Engine O-Ring 0.796 In ID 1-1/16 in OD 1/8 In Thick

https://airparts.aero/web/image/product.template/21013/image_1920?unique=2672e5e
(0 reseña)

  • Condition Code

This combination does not exist.


Terms and Conditions
Same day shipping on in-stock items.
Cutoff time is 8:30 PM EST.

Sell On Airparts

MS29513-211 – Aircraft Engine Fuel & Oil Resistant O-Ring

Available now through the AirParts Aero marketplace.

Overview Section

The MS29513-211 is a high-performance Aviation O-Ring specifically designed for use in aircraft engine fuel and lubrication systems. Manufactured from a medium-to-high Nitrile (Buna-N) compound, this O-ring is engineered to withstand the chemically aggressive environment of high-octane aviation gasoline and synthetic engine oils.

The MS29513 series is the primary standard for reciprocating engine seals, particularly where components are subject to significant thermal cycling and vibration. As a -211 dash size, it features a robust 1/8-inch cross-section, providing a substantial sealing surface for larger fluid ports, filter housings, and engine accessory drive interfaces.

Key Features Section

  • Aromatic Hydrocarbon Resistance: Formulated to resist swelling and degradation when in constant contact with 100LL Avgas and Jet-A fuels.

  • Engine Compartment Durability: Maintains its sealing properties and elasticity in temperatures ranging from -40°F to +250°F.

  • Precision -211 Sizing: Manufactured to the AS568 standard dash size -211, ensuring a consistent and reliable "squeeze" in standard aerospace glands.

  • Vibration Dampening: The thicker 0.139-inch cross-section helps absorb mechanical harmonics between engine components, preventing "weeping" leaks.

  • Low Compression Set: Engineered to resist permanent flattening, ensuring the seal remains effective during long periods of engine inactivity.

  • Certified Traceability: Meets all Military Standard (MS) requirements for tensile strength, elongation, and material purity required for flight-certified hardware.

Technical Specifications Section

SpecificationDetail
StandardMS29513 (Supersedes AN6227 series)
Dash Size-211
MaterialAcrylonitrile Butadiene (Nitrile / Buna-N)
Inside Diameter (ID)0.796 in (20.22 mm)
Outside Diameter (OD)1.074 in (27.28 mm)
Cross-Section (W)0.139 in (3.53 mm)
Hardness70 Shore A
ColorBlack

Aircraft Compatibility Section

The MS29513-211 is a foundational seal for a variety of aircraft systems:

  • Lycoming & Continental Engines: Frequently used in oil filter adapter housings, oil cooler fittings, and large-diameter fuel injection manifolds.

  • Radial Engines: Found in pushrod housing seals and accessory drive mounting pads for Pratt & Whitney and Curtiss-Wright powerplants.

  • Fuel Systems: Standard seal for larger gascolator (fuel strainer) bowls and main fuel selector valve ports.

  • Hydraulic Systems: Used in low-pressure return lines and reservoir caps where fuel/oil resistance is required.

Technical Applications & Safety

The MS29513-211 creates a seal through mechanical deformation within a "gland." Because of its 1/8-inch thickness, it is particularly effective at sealing surfaces that may have slight thermal expansion variances.

Safety Warning: Do not substitute with industrial-grade O-rings. While a standard Nitrile O-ring from a hardware store may share the -211 dimensions, the elastomer is not certified for aviation fuel. Standard Nitrile can leach plasticizers into the fuel system, causing the O-ring to shrink, crack, and fail prematurely. Additionally, always verify the Cure Date (shelf life). MS29513 seals typically have a 15-year shelf life; an expired O-ring may feel soft but can fail instantly under the pressure spikes of an engine-driven pump.

Technical Engineering Insight

The engineering value of the MS29513-211 lies in its Volumetric Fill and Gland Design compatibility. Aerospace engineering manuals (such as MIL-HDBK-695) specify that the O-ring should occupy approximately 70–90% of the gland's volume. The -211 size, with its specific 0.139-inch cross-section, is optimized to allow for the thermal expansion of Nitrile without over-filling the groove. If an O-ring fills 100% of the groove during operation, it can act as a solid and crack the aluminum housing or shear the mounting bolts. Sourcing a genuine MS-standard part ensures the volumetric expansion coefficients remain within the engine manufacturer's safety limits.

Installation & Maintenance Addendum

  1. Gland Preparation: Ensure the mounting groove is free of carbon deposits or old "baked-on" rubber. Use only a plastic or brass pick for cleaning to avoid scratching the seating surface.

  2. Lubrication: Lightly coat the O-ring with clean engine oil or Parker O-Lube before installation. This prevents "spiral failure," where the O-ring twists during the assembly of a threaded housing.

  3. Stretch Limits: Avoid stretching the O-ring more than 50% of its diameter during installation, as this can lead to microscopic surface tearing in the Nitrile compound.