# STC SA00039BO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Ameriflight LLC, United States
- Description: Incorporation of cockpit panel modifications to support single pilot operations without an autopilot
- Applied: November 7, 1994
- Status date: December 22, 2025
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A21SO](https://openairdocs.org/tcds/A21SO)
- Certificate PDF: https://openairdocs.org/files/sha256/7a/05/7a0526c92e6d87e92fbc3c6ef59a2c90a392db792abf5b8bad00a1840b3b8e3f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132047361820260401150029.0001
- DRS record last changed: April 1, 2026
- Page: https://openairdocs.org/stc/SA00039BO

## ADs that name it (0)

None.

## Approved models (2)

- Embraer S.A. EMB-110P1 ([TCDS A21SO](https://openairdocs.org/tcds/A21SO))
- Embraer S.A. EMB-110P2 ([TCDS A21SO](https://openairdocs.org/tcds/A21SO))

## 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.

SA00039BO Applicant Name: Ameriflight LLC Street Address: 1515 W. 20th St City, ST Zip: DFW Airport, TX 75261 Part 23 Federal Aviation Regulations A21SO Embraer EMB-110P1, EMB-110P2

1. For installation of this STC after the amendment date December 07, 2007, conformance must be in accordance with Business Air Inc. Drawing No. 95-01A, dated April 09, 2007, Revision 5, or later FAA approved revision.

(continued on Page 3 of 3) 11/07/1994 05/16/2005 06/12/2014 12/22/2025 02/24/1995 07/03/1996 10/21/2000 12/07/2007 3 Incorporation of cockpit panel modifications to support single pilot operations without an autopilot in accordance with Avior Drawing No. 95-01, dated February 20, 1995, or later FAA approved revision or in accordance with Business Air Inc. Drawing No. 95-01A, dated April 09, 2007, Revision 5, or later FAA approved revision.

SA00039BO 12/22/2025 3

SA00039BO 12/22/2025 Limitations and Conditions: (continued from Page 1 of 3)

2. Operation must be in accordance with:

Avior Aircraft Flight Manual Supplement (AFMS) Revision C, FAA approved on January 09, 2001, or later FAA approved revision (for aircraft modified in accordance with Avior Drawing No. 95-01, dated February 20, 1995, or later FAA approved revision).

OR Business Air Inc. Aircraft Flight Manual Supplement (AFMS) Revision D, FAA approved on December 07, 2007, or later FAA approved revision (for aircraft modified in accordance with Business Air Inc. Drawing No. 95-01A, dated April 09, 2007, Revision 5, or later FAA approved revision).

The AFMS must be carried in the aircraft during all flights.

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

Certification Basis: Not documented.

-------------------------------------------------------END------------------------------------------------------- 3 3 Add Page

## Every issue (3)

- December 22, 2025: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/7a/05/7a0526c92e6d87e92fbc3c6ef59a2c90a392db792abf5b8bad00a1840b3b8e3f)
- June 12, 2014: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f4/40/f44004c778a82c98ff0dfb526fa261ed66c9d96862e05c42bb33e79d33cd68ac)
- May 16, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b8/47/b84780431e00d919a170c3b10929ae1271f684e69de35640e58de83a88add056)

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