# STC SA01071LA - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Evans & Bailey Holdings LLC, United States - Description: Installation replacement tail cone fairing assembly. - Applied: June 29, 2000 - Status date: February 23, 2017 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS A3SO](https://openairdocs.org/tcds/A3SO) - Certificate PDF: https://openairdocs.org/files/sha256/00/d6/00d6664dd4f07771344e6adab1d6a2b74e4baac7e43042b5ec519ca294852d6f - Approved model list and other attachments: [SA01071LA_AML.pdf](https://openairdocs.org/files/sha256/c8/d4/c8d444810c61d2abe21bd525c43760340b2d9f7a6c90e8f8eb13026dc927e484) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DF3B684E0EA96A5F862580D000610632.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA01071LA ## ADs that name it (0) None. ## Approved models (15) - Piper Aircraft Inc. PA-28-140 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-151 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-161 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-181 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-235 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-236 ([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)) - Piper Aircraft Inc. PA-28R-201 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28R-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-32R-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32R-301 (HP) ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32R-301 (SP) ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32R-301T ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) ## 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 23* of the Federal Aviation Regulations Original Product Type Certificate Number Make : *See attached FAA Approved Model List (AML) No. SA01071LA for list of approved airplane models and applicable airworthiness regulations. Description of Type Design Change: Installation replacement tail cone fairing assembly in accordance with FAA approved Met-Co-Aire Controlled Drawing List, MA1-1-03, dated September 10, 2000, or later FAA approved revision. Limitations and Conditions: The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previous approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted airplane model series only. 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 : June 29, 2000 Date of issuance : October 6, 2000 Date reissued : February 23, 2017 (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.) ### SA01071LA_AML.pdf **FAA APPROVED MODEL LIST (AML)** Evans & Bailey Holdings LLC Number SA01071LA For Installation Replacement Tail Cone Fairing Assembly Issue Date: October 6, 2000 Page 1 of 1 Item Aircraft Make Aircraft Model Original Type Certificate Number Certification Basis for Alteration Installation Instruction Number Installation Instructions Revision No./Date AFM Supplement Number/Date AML Amendment Date 1 Piper PA-28-140, -150, -151, -160, -161, -180, -181, -201T, -235, -236 2A13 CFR 14 Part 23 Through Amendment 23-53 MA1-1-03 REV. NC, September 10, 2000 N/A 2/23/2017 2 Piper PA-28R-180, -200, -201, -201T 2A13 CFR 14 Part 23 Through Amendment 23-53 MA1-1-03 REV. NC, September 10, 2000 N/A 2/23/2017 3 Piper PA-32-260, -300, -301, -301T A3SO CFR 14 Part 23 Through Amendment 23-53 MA1-1-03 REV. NC, September 10, 2000 N/A 2/23/2017 4 Piper PA-32R-300, -301(SP), -301(HP), -301T A3SO CFR 14 Part 23 Through Amendment 23-53 MA1-1-03 REV. NC, September 10, 2000 N/A 2/23/2017 FAA Approved: _______________________________ Date: ____________________ Manager, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office ## Every issue (1) - February 23, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/00/d6/00d6664dd4f07771344e6adab1d6a2b74e4baac7e43042b5ec519ca294852d6f), [SA01071LA_AML.pdf](https://openairdocs.org/files/sha256/c8/d4/c8d444810c61d2abe21bd525c43760340b2d9f7a6c90e8f8eb13026dc927e484) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.