P/N: 45-521212-607R
Category: Flight Controls
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 45-521212-607R is a flap actuator assembly that converts hydraulic or electric power into linear motion to position trailing-edge flaps. This component controls flap extension and retraction during takeoff, landing, and cruise phases of flight. The actuator interfaces with the flap drive system, synchronized across wing stations to maintain even deployment.
Installation requires verification against your aircraft's Illustrated Parts Catalog and rigging per the Aircraft Maintenance Manual. Designed for FAA-approved aviation service and overhaul practices.
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 45-521212-607R is a flap actuator assembly that converts hydraulic or electric power into linear motion to position trailing-edge flaps. This component controls flap extension and retraction during takeoff, landing, and cruise phases of flight.
The ACTUATOR ASSY FLAP may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: As Removed. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the ACTUATOR ASSY FLAP. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 45-521212-607R.