# STC SA3513WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: TALCO Aviation, United States
- Description: Installation of Roto-Master (Rajay) turbocharged Lycoming IO-540-K1G5D engine.
- Applied: July 7, 1966
- Status date: August 31, 2023
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS A3SO](https://openairdocs.org/tcds/A3SO)
- Certificate PDF: https://openairdocs.org/files/sha256/f0/2b/f02bbc96490269c80be00a28d26147e10badd5fb51c8cb54aa7790bbabb75195
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123802906920231117173509.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA3513WE

## ADs that name it (2)

- [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

## Approved models (1)

- The New Piper Aircraft Inc. PA-32R-300 ([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.

SA3513WE TALCO Aviation 3015 E. New York St, STE A2-270 Aurora, IL 60504 Part 3 the Civil Air Regulations A3SO Piper PA-32R-300 Installation of Roto-Master (Rajay) turbocharged Lycoming IO-540-K1G5D engine in accordance with FAA Sealed Roto-Master (Rajay) Drawing List No. RJ0850, dated October 26, 1977, or later FAA sealed revision.

(See continuation sheet 3 of 3) June 30, 1977 2/10/82; 10/23/87; 9/22/95; 12/19/03; 7/3/06; 3/16/07; 3/5/18; 2/2/2021;

8/31/2023 November 8, 1977 March 21, 1985 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3

SA3513WE 3

SA3513WE Date of Issuance: November 8, 1977 Date Amended: March 21, 1985 Date of Reissuance: August 31, 2023

The engine must be modified to incorporate turbochargers in accordance with Supplemental Type Certificate No. SE85WE. Roto-Master (Rajay) FAA-Approved Flight Manual Supplement dated November 8, 1977, or later FAA approved revision is required.

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.

-END- 3 3

## Every issue (4)

- August 31, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f0/2b/f02bbc96490269c80be00a28d26147e10badd5fb51c8cb54aa7790bbabb75195)
- March 5, 2018: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/dd/1d/dd1d83a94e67b3eb6d721a9cdb3a580282bba2e897cc831934878486b3dfebd3)
- July 3, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/3d/d5/3dd531dc3493f45fd6edb897f2e458a29718f35586e95940248697de06d92ab5)
- December 12, 2003: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/65/a2/65a2de8905bf03d1863cd7df56c6fc99509a6bf9999ccdf95c18bfbb04f92afb)

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