STC SA02266LA

Supplemental type certificate · Finnoff Aviation Products LLC

Holder
Finnoff Aviation Products LLC · United States
Status
Current · Reissued
Status date
April 14, 2023
Applied
April 1, 2008
Product
Aircraft · Small Airplane
Certification basis
Part 23
Data sheet
TCDSA78EU

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of a Pratt and Whitney PT6A-67P

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may 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&HUWLILFDWH1XPEHU 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\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\D ILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&¶VVXSSRUWLQJGRFXPHQWDWLRQ GUDZLQJVLQVWUXFWLRQV SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5  )$$)RUP  683(56('(635(9,286(',7,21 3DJH RIBBB 3

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

Date oI transfer:

$Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\D ILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&’s supporting documentation (drawings, instructions, SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5  )$$)RUP  683(56('(635(9,286(',7,21 3DJH RIBBB 3

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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ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 2

MakeModelData sheet
Pilatus Aircraft LimitedPC-12/45A78EU
Pilatus Aircraft LimitedPC-12/47A78EU

Every issue · 9

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
April 14, 2023Reissued, currentCertificate
January 19, 2022Reissued, earlier issueCertificate
February 1, 2019Reissued, earlier issueCertificate
July 16, 2018Reissued, earlier issueCertificate
June 27, 2018Reissued, earlier issueCertificate
December 19, 2013Reissued, earlier issueCertificate
May 7, 2012Reissued, earlier issueCertificate
April 11, 2012Amended, earlier issueCertificate
November 17, 2009Issued, earlier issueCertificate