P/N: ca36200-1b
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 |
|---|---|
| Serviceable | 4 Available |
The CA36200-1B is a linear flap actuator for aircraft wing high-lift systems. This component converts hydraulic input into controlled extension and retraction of wing flaps during low-speed flight operations. Mounted within the flap drive assembly, it synchronizes flap position across both wings to maintain lift and control.
Installation and rigging must follow the aircraft Maintenance Manual (ATA 27 Flight Controls) and applicable FAA-accepted procedures. The actuator interfaces with flap control units and drive shafts to position surfaces at commanded angles during takeoff, landing, and approach phases.
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 CA36200-1B is a linear flap actuator for aircraft wing high-lift systems. This component converts hydraulic input into controlled extension and retraction of wing flaps during low-speed flight operations.
The ACTUATOR, 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: Serviceable. 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, 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 ca36200-1b.