STC SA4108SW

Supplemental type certificate · Swick Aircraft

Holder
Swick Aircraft · United States
Status
Current · Issued
Status date
March 31, 1980
Applied
October 31, 1979
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA-696

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Use of Piper metal spars to replace original wood spars.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Unittd States or Zlmtrica Bepartment of ^transportation— federal 2ltnation administration Supplemental TCgpe Certificate iSl&aMta/i&n&.

SA4108SW Swick Aircraft Route 1, Box 128B McKlnney, Texas 75069 Project A4614SW-S ,<^^^xz4^ 04 J&o Civil Air Taylorcraft BC12-D of plper mtal §parg to raplace original wood sp«r» according to Drawings No. 53 dat*d 10/19/79; No. 54 dated 10/19/79, Rev. 3/27/80; No. 55 dated 10/19/79, Rev. 3/21/80; No. 56 dated 10/31/79, Rev. 3/27/80; No. 57 dated 10/19/79, Rev. 3/27/80; No. 58 dated 10/36/79.

Rev. 3/27/80; No. 59 dated 11/9/79, Rev. 3/27/80, or later FAA approved revision* Compatibility of this modification with other previously approved modifications must be determined by the installer.

October 31, 1979 March 31, 1980 _> *f& pftAAjtss/:

—X atf jttttfftfi**/.' .^4^>er//^/ tSyA^/t/tlu:,, sZ7 (Signature ) Don P. WatsonChief, Engineering and Manufacturing Branch (Title) ~~~~~~~~

FAA FOIM 6110-2(10-68)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
Taylorcraft 2000 LLCBC12-DA-696