P/N: CH34723
Category: Magnetos & Ignition
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New Surplus | 1 Available |
The CH34723 is a FAA-PMA turbine engine igniter plug designed for high-energy combustion initiation in Pratt & Whitney PW206/PW207 engines, including Airbus H135 applications. Installed in the combustor case, this igniter receives power from an exciter unit to generate spark for engine start and inflight relight capability. The ceramic-insulated plug withstands extreme combustor temperatures and pressures during ignition events.
Installation requires torque specifications and procedures per the engine maintenance manual and illustrated parts catalog.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The CH34723 is a FAA-PMA turbine engine igniter plug designed for high-energy combustion initiation in Pratt & Whitney PW206/PW207 engines, including Airbus H135 applications. Installed in the combustor case, this igniter receives power from an exciter unit to generate spark for engine start and inflight relight capability.
Depending on condition, the CH34723 may include an FAA 8130-3 Airworthiness Approval Tag, a yellow serviceable tag, or manufacturer documentation. Currently available in: New Surplus. Contact us for specific documentation details on the condition you need.
Yes, the IGNITER: IGNITION,ENGINE can be used in engine overhauls and maintenance events. Always verify part compatibility against your engine's Type Certificate Data Sheet (TCDS) and Illustrated Parts Catalog (IPC) before installation.
In-stock items ship same business day when ordered before 3 PM EST. We also offer 24/7 AOG (Aircraft on Ground) support at (904) 998-9101 for urgent engine part needs.