# STC SA1043SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Quantum Swiss LLC, United States
- Description: Installation of Lycoming O-360-A1A or O-360-A3A engine and Hartzell Constant-Speed Propeller Model HC-C2YK-1B/7666A-2.
- Applied: November 15, 1968
- Status date: July 12, 2022
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A13CE](https://openairdocs.org/tcds/A13CE)
- Certificate PDF: https://openairdocs.org/files/sha256/80/98/809876b346604ae58f289cd6d63248599d1fc94515cb680beca50e40fb3fb566
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/62D65048BF2201918625887E0042B6E2.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1043SW

## ADs that name it (0)

None.

## Approved models (1)

- Cessna Aircraft Company 177 ([TCDS A13CE](https://openairdocs.org/tcds/A13CE))

## 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.

$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 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

BB__.

Original Product 7\SH&HUWLILFDWH1XPEHU Make:

SA1043SW Quantum Swiss LLC 1000 Brickell Avenue, Suite 201 Miami, FL 33131 Part 23* the Federal Aviation Regulations A13CE Cessna 177 Installation of Lycoming O-360-A1A, O-360-A3A, O-360-A1F, O-360-A1F6 and Hartzell Constant Propeller Model HC-C2YK-1B/7666A-2 in accordance with Air Mod Engineering Drawing 68020CS (21 pages).

See continuation sheet on page 3 of 3.

November 15, 1968 May 16, 1989; March 24, 1999; July 15, 2009; July 12, 2022 March 17, 1969 January 26, 2010 Luke Walker Acting Manager, Denver ACO Branch Compliance and Airworthiness Division 3

$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&’s supporting documentation (drawings, instructions, 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 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Too (Name and address of transferee):

Date oI transfer:

SA1043SW 3

$Q\DOWHUDWLRQRIWKLVFHUWLILFDWHDQGRUWKH7\SH&HUWLILFDWH'DWD6KHHWLVSXQLVKDEOHE\DILQHQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ \HDUVRUERWK7KLV FHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGHDYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK7LWOHRIWKH&RGHRI)HGHUDO5HJXODWLRQVSDUWVHFWLRQ &)5 $WUDQVIHUPXVWEHHQGRUVHGDVSURYLGHGRQWKHUHYHUVHKHUHRI$7\SH&HUWLILFDWHKROGHUZKRDOORZVDSHUVRQWRXVHWKH7\SH&HUWLILFDWHWRPDQXIDFWXUHD QHZDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKDZULWWHQOLFHQVLQJDJUHHPHQWDFFHSWDEOHWRWKH)$$ 5HI&)5  )$$)RUP  683(56('(635(9,286(',7,21 3DJHBBBRIBBB United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1043SW * Certification Basis is set forth in Type Certificate Data Sheet A13CE ----------------------------------------------------------END--------------------------------------------------- Limitations and Conditions:

1. The following placards are required:

a. Avoid continuous operation between 2000 and 2250 RPM

b. Minimum octane fuel 100/130

2. FAA approved Airplane Flight Manual Supplement, Document AU-AFMS-02, Revision Original, dated January 15, 2010, or later FAA approved revision is required after January 26, 2010.

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

4. 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 permission.

----------------------------------------------------------END--------------------------------------------------- Date reissued, July 12, 2022 33

## Every issue (3)

- July 12, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/80/98/809876b346604ae58f289cd6d63248599d1fc94515cb680beca50e40fb3fb566)
- January 26, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/bf/26/bf26722e78f9909e316b98fff969aff6169b6fd1f8a535401453bb203a27fe5a)
- July 15, 2009: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b4/35/b4357c42fe30409a27e65eb6eda8383c6d53d03dd9aff2599731250627e7928a)

---
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.
