# STC SE135SO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: TALCO Aviation
- Description: Installation of two (2) Rajay turbochargers Model 315A10.
- Status date: August 31, 2023
- Data sheets: E-275
- Certificate PDF: https://openairdocs.org/files/sha256/68/05/6805f3018e5e49d134598fe3c4e56c8c7cd9b40758f6213f27ff0cf821c5f228
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181507317920231114182422.0001
- Page: https://openairdocs.org/stc/SE135SO

## ADs that name it

None.

## Approved models (1)

- Textron Lycoming AVCO Corporation GO-480-D1A (TCDS E-275)

## 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.

SE135SO TALCO Aviation 3015 E. New York St, STE A2-270 Aurora, IL 60504 Part * the Federal Aviation Regulations E-275 Lycoming GO-480-D1A Installation of two (2) Rajay turbochargers Model 315A10.

(See continuation sheet 3 of 3) October 13, 1964 7/15/66, 1/14/69, 10/23/87, 12/24/03, 6/16/05, 6/26/06, 3/16/07, 3/12/18, 2/2/2021; 8/31/2023 June 9, 1965 11/1/65, 2/17/67, 7/30/68, 2/20/69, 2/10/82, 2/14/85 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 3

SE135SO 3

SE135SO Date of Issuance: June 9, 1965 Date Amended: February 14, 1985 Date of Reissuance: August 31, 2023

*CAR 13 effective 3.5.52 and amendments 13-1 and 13-2.

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.

This approval covers engine-turbocharger compatibility only. For power limitations with this installation refer to FAA approved Riley Drawing R00523. The approval of the change in type design applied basically to GO-480-D1A engines only. This determination should include consideration of significant weight distribution such as an increase in the fixed disposable weight in the fuselage.

-END- 3 3

## Every issue (4)

- August 31, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/68/05/6805f3018e5e49d134598fe3c4e56c8c7cd9b40758f6213f27ff0cf821c5f228)
- March 5, 2018: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/6d/72/6d72753ad829524bd2b4858f86ee69b62ac8ac58f859685142f9eaea4782ef2e)
- June 26, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/02/c4/02c48b00344532c2907482d1d1ce2f1031cf4fa80e4a6aa22724387b3dd0b396)
- June 16, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/21/d6/21d68aedbde11d10e1ae08bd2445683135dc6feccfcf9051291206eff7009a06)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.