P/N: 25-8vf7-1
Category: Turbine 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 | 2 Available |
The 25-8vf7-1 is an engine bleed air valve that regulates hot, pressurized air from the engine compressor to aircraft pneumatic systems. Installed in the engine bleed-air manifold, this valve modulates or isolates flow based on flight deck commands. It supplies air for environmental control, cabin pressurization, anti-ice protection, and cross-start functions within the ATA 36 pneumatic architecture.
The valve responds to control signals to manage system pressure and temperature demands during various flight phases. Installation and rigging must follow the applicable aircraft maintenance manual and approved technical data.
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 25-8vf7-1 is an engine bleed air valve that regulates hot, pressurized air from the engine compressor to aircraft pneumatic systems. Installed in the engine bleed-air manifold, this valve modulates or isolates flow based on flight deck commands.
The 25-8vf7-1 is currently available in the following conditions: As Removed. Each condition reflects the part's maintenance history and certification status per FAA standards.
The 25-8vf7-1 requires a custom quote. Submit a Request for Quote (RFQ) through our website or call our sales team at (904) 998-9101 for immediate pricing assistance.
Yes, we offer same-day processing on in-stock items and provide 24/7 AOG (Aircraft on Ground) support for urgent needs. Standard, expedited, and overnight shipping options are available.