P/N: eaedc8407-415
Category: Engine Parts
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 1 Available |
The eaedc8407-415 is an engine anti-icing unit that regulates hot bleed air from the turbine engine to the induction system inlet. This component prevents ice accumulation on the inlet and adjacent nacelle structures by maintaining stable airflow temperature during flight. Installed on turboprop and turbine-powered aircraft, the unit supports compliance with 14 CFR 33.68 and 25.1093 anti-icing requirements.
Installation and functional testing must follow the applicable Aircraft Maintenance Manual or Engine Maintenance Manual specifications for your airframe.
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 eaedc8407-415 is an engine anti-icing unit that regulates hot bleed air from the turbine engine to the induction system inlet. This component prevents ice accumulation on the inlet and adjacent nacelle structures by maintaining stable airflow temperature during flight.
Depending on condition, the eaedc8407-415 may include an FAA 8130-3 Airworthiness Approval Tag, a yellow serviceable tag, or manufacturer documentation. Currently available in: As Removed. Contact us for specific documentation details on the condition you need.
Yes, the ENGINE ANTI-ICING UNIT 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.