# STC SA01101DE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aviation Fabricators Inc., United States
- Description: Installation of Gogo AVANCE L5/LX5 System
- Applied: September 21, 2022
- Status date: November 14, 2024
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/15/b0/15b00eefc841cbe87e73330988735d2ab02ac1087d20dec6f237365e7c8887d2
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126075729820250305133500.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01101DE

## ADs that name it (0)

None.

## Approved models (2)

- Textron Aviation Inc. B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. B300C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## 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 Number 

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

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805 North Fourth Street Clinton, MO 64735 23 Title 14 Code of Federal Regulations.

A24CE Textron Aviation, Inc B300, B300C Installation of Aviation Fabricators Interior in accordance with Master Data List, Doc no. AF-655, revision D, dated 03-01-23 or later FAA approved revision. Instructions for Continued Airworthiness (ICA), Document No. AF-665, Revision IR dated 1/18/2023, FAA accepted 5/11/2023, or later FAA accepted revision is required to be made available at installation. No Flight Manual Supplement is required for this installation.

1. This STC is applicable to all serial numbers for this Textron Aviation Inc B300 and B300C.

Continued Page 3 of 3 9/21/22 11/14/24 5/11/23 Kreg R. Voorhies, ODA Lead administrator Cert Works, LLC ODA ODA No. ODA(AIR)883887-NM 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number  (IIHFWLYH'DWH I Transferr Endorsementt Transfer the ownership of Supplemental Type Certificate Number:

Too (Name and address of transferee):

Date oI transfer:

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(Continuation Sheet) Number  (IIHFWLYH'DWH  $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOH E\D ILQH RIQRW H[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ \HDUVRUERWK7KLVFHUWLILFDWH PD\ EHWUDQVIHUUHGRUPDGH DYDLODEOHWR WKLUGSHUVRQVE\OLFHQVLQJDJ UHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQ RIWKLV6XSSOHPHQWDO7\SH &HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH 67&KROGHUGR HVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWD QRUWRDOWHUDQ DLUFU DIW DLUFUDIWHQJLQH KROGHU$Q 67&KROGHUZKRDOORZVDSHUVRQWRXVHWKH67&WRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHUPXVWSURYLGH WKDWSHUVRQZLWKZULWWHQ SHUPLVVLRQ DFFHSWDEOHWR WKH)$$ 5HI &)5  )$$  3DJH BBBRI BBB SA01101DE Limitations and Conditions Continued:

2. The installer must determine whether this design change is compatible with previously approved modifications.

3. 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.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the installation of the Drink Rail and Tables System is as follows:

a. The type certification basis for the Textron Aviation Inc B300 and B300C for parts not changed or not affected by the change are shown on TCDS A24CE.

b. The certification basis for parts changed or affected by the change since the reference date of application, 9/21/2022, is based upon 14 CFR Part 23 with amendment 23-1 through 23-34. Based on 14 CFR §§ 21.115 and

21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment; None Regulations at an intermediate amendment; None Regulations at the Original Aircraft Certification Basis amendment level per TCDS A24CE;

14 CFR Sections: 23.301(a,b) Amdt. 23-28; 23.303 Amdt. - ; 23.305 Amdt. - ; 23.307(a) Amdt. - ; 23.337(a,b) Amdt. 23-48; 23.341 Amdt. 23-34; 23.561(a,b,e) Amdt. 23-34; 23.601 Amdt. - ; 23.603 Amdt. 23-23; 23.605(a) Amdt. 23-23; 23.607 Amdt. 23-17; 23.609 Amdt. - ; 23.611 Amdt. 23-7; 23.613 Amdt. 23-23; 23.619 Amdt. 23-7;

23.625(a-c) Amdt. 23-7; 23.785(j) Amdt. 23-34; 23.807(a)(1),(b)(1) Amdt. 23-34; 23.807(b)(3) Amdt. 23-34;

23.815 Amdt. 23-34; 23.853(a)(d)(3)(i,ii,iv,v) Amdt. 23-34; 23.1301(a-c) Amdt. 23-20; 23.1301(d) Amdt. 23-20;

23.1309(b) Amdt. 23-34; 23.1541(a)(2)(b) Amdt. 23-21; 23.1557(d) Amdt. 23-23

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - END- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 33 11/14/24

## Every issue (1)

- November 14, 2024: Issued, Current. [certificate](https://openairdocs.org/files/sha256/15/b0/15b00eefc841cbe87e73330988735d2ab02ac1087d20dec6f237365e7c8887d2)

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