# STC SA02266LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Finnoff Aviation Products LLC, United States
- Description: Installation of a Pratt and Whitney PT6A-67P
- Applied: April 1, 2008
- Status date: April 14, 2023
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU)
- Certificate PDF: https://openairdocs.org/files/sha256/e2/b7/e2b748141052582a24981d5aeda543b5de7ad9ed14e51c5af99985de347d41cf
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119058294720230417185518.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA02266LA

## ADs that name it (0)

None.

## Approved models (2)

- Pilatus Aircraft Limited PC-12/45 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))
- Pilatus Aircraft Limited PC-12/47 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))

## 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 SA02266LANumber:

This certificate issued to: Finnoff Aviation Products, LLC 11914 Corporate Way Broomfield, CO 80021 BB__.

Make:Original Product A78EU Pilatus Aircraft LTD 7\SH&HUWLILFDWH1XPEHU PC-12/45, PC-12/47 Model:

Installation of a Pratt and Whitney PT6A-67P engine. Data required:

1. Finnoff Aviation Products Master Drawing List (MDL) No. 0201-00100, Rev. M, dated October 7, 2021, or later FAA approved revision, and

2. FAA approved Airplane Flight Manual Supplement (AFMS) No. FTA-FIN-001022, Rev. K, dated August 24, 2021 or 3S Certification AFMS No. 3S18-013-7101 or No. 3S18-013-7102, both at Rev. IR and dated October 8, 2021, or later FAA approved revision. (continued on page 3) Limitations and Conditions:

1) Compatibility of this design change with previously approved modifications must be determined by the installer.

2) 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. (continued on page 3)

5/7/2012, 12/19/2013, 6/27/2018, 7/16/2018, April 1, 2008 Date of Application: Date Reissued: 2/1/2019, 11/20/2020, 1/19/2022, 4/14/2023 4/11/2012, 2/19/2021, 10/8/2021 November 17, 2009 Date of Issuance: Date Amended:

Ben Tyson Program Manager, AIR-767 Title: Central Certification Branch $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\D ILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&¶VVXSSRUWLQJGRFXPHQWDWLRQ GUDZLQJVLQVWUXFWLRQV SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5  )$$)RUP  683(56('(635(9,286(',7,21 3DJH RIBBB 3

I o United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate SA02266LANumber:

Date oI transfer:

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United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA02266LA Reissued Date: 4/14/2023 Type Design Change (continued):

4. Finnoff Aviation Products Instructions for Continued Airworthiness (ICA), No. FTA-FIN-001014, Rev.

K, dated September 28, 2021, or later FAA accepted revision.

Limitations and Conditions (continued)

3) Approval of this change in type design applies to the model of aircraft shown on this STC.

4) A copy of this certificate, the ICA, and the AFMS(s) shall be maintained as part of the permanent records for the modified aircraft.

5) STC SA00564DE is required to be installed for the installation of the Generator 2, Second NACA Inlet Duct Option (0201-00500-7), installation of the Generator 2 Cooling System Option (300SGL116Q-7 Generator) (0201-00500-9), installation of the Generator 2 Cooling System Option (300SGL116Q-1 Generator) (0201-00500-11).

6) This STC is applicable to all serial numbers of Pilatus Aircraft models PC-12/45 and PC-12/47, with STC SA00564DE installed.

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## Every issue (9)

- April 14, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e2/b7/e2b748141052582a24981d5aeda543b5de7ad9ed14e51c5af99985de347d41cf)
- January 19, 2022: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/76/5a/765a90db12c8ee98f6c4e6635dcad3dd94edca0b4d4b1f70f1d42cd9b0d39a5b)
- February 1, 2019: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/0a/09/0a099b2dc74f1c3661f801356bb5ec59cf683fbd8701fd7b9928762fd567a454)
- July 16, 2018: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a0/8a/a08a956ef3a22a21a09fe1227fe1cbf4a0f81c11244859cf342c002b21828389)
- June 27, 2018: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/6f/3e/6f3e00bf81a04c2eb96781f41da3afc87126793f8c07f49ee03a5eaa35f39f39)
- December 19, 2013: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/63/f8/63f80bb754e64075db6e8266885cec4fe9c11eea0fdb952f3b9e3a09a71d1e9f)
- May 7, 2012: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/d4/50/d4501c461e456ef0229f7c54198a1a2688943a03a3ad7f85dd690876bfcda5eb)
- April 11, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/55/94/559416beaf12677ba3212ea52f74e5fecb33093ae3e4db01e5e59160ecab3a49)
- November 17, 2009: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/59/8a/598aa2d59eee746fa3526c6bb72150ec94c63de36bd08a6f7c6ec36ab2aa27f6)

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