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Aircraft structures

STC SA871WE

FAA DRS lists SA871WE as Current · Reissued, held by Evans & Bailey Holdings LLC, for Piper Aircraft PA-24-250, Piper Aircraft PA-24-260, and Piper Aircraft PA-24-400, and 3 more aircraft configurations. Recorded change: Installation of fiberglass wing tips. Snapshot dated June 30, 2026.

FAA-listed holder
Evans & Bailey Holdings LLC
Aircraft configurations
6
FAA revision date
FAA status
Current · Reissued

Recorded modification

What the FAA record covers

Installation of fiberglass wing tips.

SA871WE identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.

Applicability

Aircraft named in FAA DRS

Named aircraft: Piper Aircraft PA-24-250, Piper Aircraft PA-24-260, and Piper Aircraft PA-24-400, and 3 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Piper Aircraft PA-24-2501A15Piper Aircraft PA-24-2601A15Piper Aircraft PA-24-4001A15Piper Aircraft PA-241A15Piper Aircraft PA-30A1EAPiper Aircraft PA-39A1EA

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact Piper Aircraft PA-24-250 and Piper Aircraft PA-24-260, and 4 more aircraft configurations model, serial range, and configuration?
  2. 02Which configuration, loads, materials, inspections, and damage limits apply?
  3. 03Who can legally supply the design data, kit, instructions, and ICAs?
  4. 04What parts, labor, conformity, and return-to-service work are excluded?

Related aircraft structures STCs

SA6073NMAircraft structures

Installation of fatigue sensor and structural life extension of wing spar in accordance with FAA approved SIE Master Drawing List 91000, Revision A, dated September 23, 1993, or later FAA approved revision, and FAA approved Airplane Flight Manual Supplement Report No. SIE-12-601, Revision N/C, dated October 19, 1993 or later FAA approved Airplane Flight Manual Supplement, and Report No. SIE-12-602, Revision N/C, dated December 21, 1993, or later FAA approved Revision. (SIE-12-601 is for model C99 only, and SIE-12-602 is for the remaining models, 99, 99A, A99A, and B99.).

FAA holder: Structural Integrity Engineering

View record