FLAP (P/N my20162-17) - As Removed

The my20162-17 is a trailing-edge wing flap that increases lift during low-speed flight operations. This high-lift device lowers stall speed during approach and landing by changing the wing's aerodynamic profile. Deployed from the wing trailing edge, the flap works in coordination with other control surfaces to enhance aircraft maneuverability at reduced airspeeds.

Installation follows your aircraft's maintenance manual specifications. Verify compatibility with your aircraft's Illustrated Parts Catalog before installation to ensure proper fit and operational performance.

What is the FLAP (P/N my20162-17)?

The my20162-17 is a trailing-edge wing flap that increases lift during low-speed flight operations. This high-lift device lowers stall speed during approach and landing by changing the wing's aerodynamic profile.

Is the my20162-17 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 my20162-17 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 my20162-17 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 my20162-17.