# STC SA811WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: TALCO Aviation, United States
- Description: Installation of turbocharged Lycoming IO-540-C1B5 or -C1C5 engine.
- Applied: July 23, 1964
- Status date: August 31, 2023
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS 1A15](https://openairdocs.org/tcds/1A15)
- Certificate PDF: https://openairdocs.org/files/sha256/55/29/5529883d48850808e0d2c0949d72e1685626059c74c08464d4d4ff1fadabdbc1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124825096220231129144157.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA811WE

## ADs that name it (3)

- [AD 2002-19-03](https://openairdocs.org/ad/2002-19-03): Crankshaft · Lycoming Engines IO-540-A1A5, IO-540-AA1A5, IO-540-AA1B5 and 81 more. Effective Sep 20, 2002. Named in the applicability
- [AD 81-19-04](https://openairdocs.org/ad/81-19-04): Hose Assembly · Rajay Hose Assemblies, 500A, 500B and 87 more. Effective Sep 17, 1981. Cited in the text
- [AD 65-02-03](https://openairdocs.org/ad/65-02-03): Turbochargers · Rajay Turbochargers with STC SA529WE or 6 others. Named in the applicability

## Approved models (1)

- The New Piper Aircraft Inc. PA-24-250 ([TCDS 1A15](https://openairdocs.org/tcds/1A15))

## 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.

SA811WE TALCO Aviation 3015 E. New York St, STE A2-270 Aurora, IL 60504 Part 3 the Civil Air Regulations 1A15 Piper PA-24-250 Installation of turbocharged Lycoming IO-540-C1B5 or -C1C5 engine in accordance with FAA Sealed Roto-Master (Rajay) drawing List No. RJ0700 or later FAA approved revision.

(See continuation sheet 3 of 3) July 22, 1964 January 14, 1969; February 10, 1982; October 30, 1987; September 22, 1995; December 19, 2003;

June 26, 2006; March 16, 2007; March 5, 2018; February 2, 2021; August 31, 2023 October 20, 1964 March 21, 1985 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3

SA811WE 3

SA811WE Date of Issuance: October 20, 1964 Date Amended: March 21, 1985 Date of Reissuance: August 31, 2023

The engine must be previously modified to incorporate turbochargers in accordance with STC No. SE6WE. This approval of change in type design applies to the basic Piper PA-24-250 aircraft only. The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. FAA approved Roto-Master (Rajay) Airplane Flight Manual Supplement dated October 20, 1964 or later FAA approved revision is required with this installation.

-END- 3 3

## Every issue (3)

- August 31, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/55/29/5529883d48850808e0d2c0949d72e1685626059c74c08464d4d4ff1fadabdbc1)
- March 5, 2018: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a5/24/a524afd3e1870baeb6fd3e3c897d72b4a2d854d72595f39d1f1290110d5351af)
- June 26, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/22/fb/22fb4528efc6713bc73cb44701e5c2a05131eb9c8bb39456d504a873f4f4ffe0)

---
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.