FLAP (P/N 0752715-2) - As Removed

The 0752715-2 is a wing flap assembly that increases lift during takeoff and landing by changing the wing's camber. Installed at the trailing edge, this high-lift component reduces approach speed and improves aircraft handling at low speeds. The flap operates through the aircraft's control system, extending and retracting via hydraulic or mechanical actuation.

Installation and rigging must follow the aircraft maintenance manual and verified against the Illustrated Parts Catalog for your specific airframe. Inspect per FAA AC 43.13-1B acceptable practices.

What is the FLAP (P/N 0752715-2)?

The 0752715-2 is a wing flap assembly that increases lift during takeoff and landing by changing the wing's camber. Installed at the trailing edge, this high-lift component reduces approach speed and improves aircraft handling at low speeds.

Is the 0752715-2 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 0752715-2 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 0752715-2 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 0752715-2.