# STC SA880WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Evans & Bailey Holdings LLC, United States
- Description: Installation of a new design fiberglass wing tip.
- Applied: December 30, 1964
- Status date: February 23, 2017
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13)
- Certificate PDF: https://openairdocs.org/files/sha256/a2/57/a257385f3b27dc9b4720eb449c01c45c3c601b3a3a066cf1e70609ab3dc78b78
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/03B24CF902EE662C862580D00060951C.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA880WE

## ADs that name it (0)

None.

## Approved models (6)

- Piper Aircraft Inc. PA-28-140 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-150 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-200 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))

## 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 *Refer to T.C. Data Sheet 2A13 for a complete statement of the certification basis.

Original Product Type Certificate Number Make :

2A13 Piper PA28 -140, -150, -160, -180, -28R-180, 28R-200 Description of Type Design Change: Installation of a new design fiberglass wing tip in accordance with Met-Co-Aire FAA sealed Installation Instruction No. SD 1023, dated December 31, 1964; Revision of October 25, 1982.

Manufacture of the tips is controlled by Met-Co-Aire Drawing No. 11051, dated December 31, 1964, or later FAA approved revision.

Limitations and Conditions: This approval should not be extended to other specific aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect on the airworthiness of that aircraft. 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 30, 1964

Date of issuance : March 1, 1965

Date reissued : September 20, 1995;

February 23, 2017

Date amended : January 4, 1983

(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 (2)

- February 23, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a2/57/a257385f3b27dc9b4720eb449c01c45c3c601b3a3a066cf1e70609ab3dc78b78)
- September 20, 1995: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b2/5b/b25b1e4417d3f1248bca7b986c0742bd84608fcd651ea891b5404047230d160b)

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