FLAP (P/N 2-1800-1) - As Removed

The 2-1800-1 is a trailing-edge wing flap that increases lift and reduces stall speed during takeoff and landing. This high-lift control surface deploys from the wing's trailing edge to augment aerodynamic performance in short-field operations. Installation and rigging must follow the aircraft maintenance manual or FAA AC 43.13-1B acceptable methods.

Verify compatibility with your aircraft's illustrated parts catalog before installation. Proper flap operation is critical for safe takeoff and landing performance.

What is the FLAP (P/N 2-1800-1)?

The 2-1800-1 is a trailing-edge wing flap that increases lift and reduces stall speed during takeoff and landing. This high-lift control surface deploys from the wing's trailing edge to augment aerodynamic performance in short-field operations.

Is the 2-1800-1 a PMA or OEM part?

The 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.

Does the 2-1800-1 include installation hardware?

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 FLAP. We stock related hardware and can help identify companion parts.

Can the 2-1800-1 be shipped internationally?

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 2-1800-1.