3010880 – Pratt and Whitney OEM Igniter Gasket
Available now on the Airparts.aero Marketplace.
Overview
The 3010880 is a genuine OEM, flight-critical igniter gasket, engineered by Pratt & Whitney Canada (P&WC) for the legendary PT6A series of turboprop engines. This is not a standard gasket; it is a precision-manufactured, single-use "crush" gasket designed to create a perfect, gas-tight seal between the turbine igniter plug and the engine's combustor case. Fabricated from a soft, high-temperature metal alloy, the 3010880 is essential for containing the immense pressures and temperatures of the combustion chamber, ensuring the safety and performance of the engine.
Key Features
- High-Pressure Combustion Seal: Its sole purpose is to create a perfect, leak-proof seal at the igniter boss. It is designed to contain the high-pressure, superheated gases within the combustion chamber, preventing dangerous leaks into the engine nacelle.
- Soft Metal "Crush" Design: Made from a soft, malleable, high-temperature metal alloy (such as nickel or a specialized alloy). When the igniter is torqued to specification, the gasket plastically deforms, or "crushes," filling the microscopic imperfections in both the igniter and the engine case to form a perfect metal-to-metal seal.
- Single-Use Component: Engineered as a mandatory single-use item. Once compressed, the gasket work-hardens and will not provide a reliable seal if reused. A new gasket is required for every igniter installation.
- Prevents Seizing: Acts as a barrier between the dissimilar metals of the igniter shell and the engine case, helping to prevent galling and seizing at extreme temperatures, which facilitates easier igniter removal during maintenance.
- Genuine OEM Part: As a genuine part specified by Textron Aviation and manufactured by Pratt & Whitney, it guarantees the correct material composition, annealing (softness), and dimensional tolerances required for a flight-critical seal.
Technical Specifications
- Part Number: 3010880
- Component Type: Igniter Plug Gasket / Crush Washer
- OEM Manufacturer: Pratt & Whitney Canada (P&WC)
- Material: High-Temperature, Annealed Metal Alloy
- Primary Function: Provides a gas-tight seal for the turbine engine igniter.
- Certification: FAA / TCCA Production Approval
Aircraft Compatibility
The 3010880 is the standard igniter gasket for an extremely wide range of aircraft powered by the ubiquitous Pratt & Whitney Canada PT6A engine.
- Primary Engine Models:
- Pratt & Whitney Canada PT6A Series (numerous variants)
- Common Textron Aviation Platforms:
- Beechcraft King Air: 90, 100, 200 Series
- Cessna: 208 Caravan
- Other Platforms:
- Pilatus: PC-12
- Daher (Socata): TBM Series
- De Havilland Canada: DHC-6 Twin Otter
Applications
The 3010880 is a fundamental component for engine ignition system maintenance:
- Igniter Installation: A new gasket is mandatory every time an igniter plug is installed or re-installed in the engine.
- Engine Overhaul & Hot Section Inspection: Always replaced during any maintenance action that requires the removal of the igniters.
- Preventing Combustion Leaks: The primary component responsible for preventing the escape of high-pressure, incandescent gases from the combustor.
Why Choose 3010880?
A leak from the igniter port on a turbine engine can have severe consequences, including damage to the engine case, ignition leads, and other firewall-forward components, and a significant risk of an in-flight fire. The 3010880 is the only gasket engineered and certified by the engine manufacturer to withstand this extreme environment. Using a genuine OEM part ensures the gasket is made from the correct alloy and is properly annealed to create a perfect seal. For a flight-critical seal, there is no substitute for a genuine, certified OEM part.
Order Your 3010880 Igniter Gaskets Now
Ensure the integrity of your turbine engine with genuine, factory-certified components. Visit Airparts.aero to order your Pratt & Whitney 3010880 igniter gaskets today.
The sealing principle of the 3010880 crush gasket relies on plastic deformation. The soft, annealed metal is designed to have a lower yield strength than the igniter body and the engine case. When the igniter is torqued to its specified value (e.g., 240-300 lb-in), the clamping force exceeds the gasket's yield strength. This causes the gasket material to flow like a very thick fluid into the microscopic valleys and tool marks on the mating surfaces of the igniter and the engine boss. This creates a perfect, void-free metal-to-metal interface that is impervious to the high-pressure gases of combustion. This is also why the gasket is single-use; the initial compression work-hardens the metal, significantly increasing its yield strength and preventing it from properly deforming a second time.
Note: This is a single-use, flight-critical engine component. It must be replaced every time an igniter is installed. Installation must be performed by a certified A&P or AME mechanic in strict accordance with the current Pratt & Whitney Canada maintenance manual. Ensure all sealing surfaces are meticulously clean before installation.
| Specifications | |
|---|---|
| Schedule B | 7419.80.5500 |
| ECCN / USML | 9A991.c |
| FAA Approval Code | TCCA |
| 8130-3 Eligible | NO |
| Hazmat(Y/N) | N |
| Country of origin | UNITED STATES |
| Dimensions | |
|---|---|
| Dimensions (W x H x D) | .75 x .75 x .07 IN |
| Weight | .002 LB |
