# STC SA1762NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Sky Services Inc, United States - Description: Installation of a pressurized magneto system on the Continental turbocharged TSIO-360-C, F, and FB engines. - Applied: October 21, 1982 - Status date: March 14, 2006 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 3, Part 21, Part 23 - Data sheets: [TCDS A6CE](https://openairdocs.org/tcds/A6CE), [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS 2A3](https://openairdocs.org/tcds/2A3) - Certificate PDF: https://openairdocs.org/files/sha256/75/84/7584b874754f0a7b2e0cceea00ae2d0a5e9d57e1d0bc18a56711ef642bbce24a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C3863543A9091AB78625713400732C8A.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA1762NM ## ADs that name it (0) None. ## Approved models (5) - Mooney Aircraft Corporation M20K ([TCDS 2A3](https://openairdocs.org/tcds/2A3)) - The Cessna Aircraft Company T337G ([TCDS A6CE](https://openairdocs.org/tcds/A6CE)) - The New Piper Aircraft Inc. PA-28-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - The New Piper Aircraft Inc. PA-28R-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - The New Piper Aircraft Inc. PA-28RT-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) ## 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. United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate (This STC is a duplicate original to replace the original which was lost. Issued 3/14/06) Number SA1762NM This certificate, issued to: Sky Services, Inc. 1725 E Street N.E. Auburn, WA 98002 Part * of the Civil Air Regulations. * Part 3 * Part 23 * Part 3 Original Product⎯Type Certificate Number: 2A13 A6CE 2A3 Make: Piper Ce ssna Mooney Model: PA-28-201T, T337G M20K PA-28R-201T, and PA-28RT-201T Description of the Type Design Change: Installation of a pressurized magneto system on the Continental Turbocharger TSI0-360-C and –F and FB engines** in accordance with SGH, Inc. Installation Instructions No. SGH-3000-A. NOTE: ** Refer to STC SE1760NM. Limitations and Conditions: Approval of this change in type design applies basically to the above model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate dated January 16, 1984, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft. 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: October 21, 1982 Date reissued: December 7, 1987, March 14, 2006 Date of issuance: November 12, 1982 Date amended: October 28, 1983; January 16, 1984 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (1) - March 14, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/75/84/7584b874754f0a7b2e0cceea00ae2d0a5e9d57e1d0bc18a56711ef642bbce24a) --- 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.