# STC SA871WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Evans & Bailey Holdings LLC, United States
- Description: Installation of fiberglass wing tips.
- Applied: December 9, 1965
- Status date: February 23, 2017
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 1A15](https://openairdocs.org/tcds/1A15), [TCDS A1EA](https://openairdocs.org/tcds/A1EA)
- Certificate PDF: https://openairdocs.org/files/sha256/a5/18/a5186892dbe0b5c8102c01e436db48cadb212524e14f68f1f0426bf001b01f5d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DA203916B777D819862580D00060855B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA871WE

## ADs that name it (0)

None.

## Approved models (6)

- Piper Aircraft Inc. PA-24 ([TCDS 1A15](https://openairdocs.org/tcds/1A15))
- Piper Aircraft Inc. PA-24-250 ([TCDS 1A15](https://openairdocs.org/tcds/1A15))
- Piper Aircraft Inc. PA-24-260 ([TCDS 1A15](https://openairdocs.org/tcds/1A15))
- Piper Aircraft Inc. PA-24-400 ([TCDS 1A15](https://openairdocs.org/tcds/1A15))
- Piper Aircraft Inc. PA-30 ([TCDS A1EA](https://openairdocs.org/tcds/A1EA))
- Piper Aircraft Inc. PA-39 ([TCDS A1EA](https://openairdocs.org/tcds/A1EA))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

This Certificate issued to Evans & Bailey Holdings LLC 709 Airport Road Burlington, WI 53105 Part 3 of the Civil Air Regulations Original Product Type Certificate Number Make :

1A15 (PA-24 Series); A1EA (PA-30, PA-39) Piper PA-24, PA-24-250, PA-24-260, PA-24-400, PA-30, PA-39 Description of Type Design Change: Installation of fiberglass wing tips in accordance with FAA approved sealed Met-Co-Aire Drawing No. 11050, Revision A, dated July 23, 1965, and Drawing No. SD 1022, revised September 23, 1976.

Limitations and Conditions: The approval of this change in type design applies basically to Models PA-24 series, PA-30, and PA-39 only. This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect on the airworthiness of that airplane. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of application : December 9, 1965

Date of issuance : February 2, 1965

Date reissued : September 20, 1995;

February 23, 2017

Date amended : June 23, 1965;

September 23, 1976; January 8, 1993

(Signature) Manager, Technical and Administrative Support Staff, ANM-103L (Title)

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

Number (STC No.)

## Every issue (1)

- February 23, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a5/18/a5186892dbe0b5c8102c01e436db48cadb212524e14f68f1f0426bf001b01f5d)

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