# STC SA09905SC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Hawker Beechcraft Services Inc., United States
- Description: Installation of a 110 VAC Inverter with a maximum of four (4) 110 VAC outlets in the cabin.  Modifications.
- Applied: August 8, 2001
- Status date: April 24, 2007
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/55/60/55606f2075730501c874faca4fb3e5c6d793effb56db1f80db38e892578f81de
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E4E1066803A2FA9D862572DE00689A6F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA09905SC

## ADs that name it (0)

None.

## Approved models (12)

- Hawker Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 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.

Part 23 of the Federal Aviation Regulations.

Installation of a 110 VAC Inverter with a maximum of four (4) 110 VAC outlets in the cabin. Modifications in accordance with the FAA Approved Master Data List, RAS25-340129-MDL, Revision “IR” dated October 16, 2001, or later FAA Approved Revisions. Airplane Flight Manual Supplement RAS25-340126-AFMS, Revision IR, dated October 28, 2001, or later FAA Approved Revision, is required.

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

Hawker Beechcraft Services, Inc.

10440 John Cape Road San Antonio, TX 78216 A24CE Make : Raytheon (Beech) Model : 200; 200C; 200CT; 200T; B200; B200C;

B200CT; B200T; 300; 300LW; B300; B300C Date of application : August 08, 2001

Date of issuance : October 31, 2001

Date reissued : April 24, 2007

( Signature) S. Frances Cox, Manager Special Certification Office, Southwest Region

( Title)

FAA Form 8110-2-1(10-69) Page 2 of 2

## Every issue (1)

- April 24, 2007: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/55/60/55606f2075730501c874faca4fb3e5c6d793effb56db1f80db38e892578f81de)

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