# STC SA00159MC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Sierra Nevada Company LLC, United States
- Description: Outer Mold Line (OML) modification to include aircraft survivability equipment provisions, structural
provisions for a new mission antenna suite and relocation of existing antenna
- Applied: August 17, 2016
- Status date: July 9, 2024
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/11/8d/118d471a2e3c2f3dcd8a253d6861cc1e8a2b2ce20ec6642be1c434bd52071a85
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189172450020240716184710.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00159MC

## 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.

SA00159MC Sierra Nevada Company, LLC 18632 Jarkey Drive Hagerstown, MD 21742, United States 23 Chapter 14 CFR A24CE Textron Aviation Inc.

Models B300, B300C Outer Mold Line (OML) modification to include aircraft survivability equipment provisions, structural provisions for a new mission antenna suite and relocation of existing antenna in accordance with

1) Sierra Nevada Company Master Data List, Document Number 03120000, Revision A, dated August 27, 2018, FAA Approved November 13, 2018, or later FAA approved revision continued on page 3

1) A prerequisite to this installation are the installation of the Sierra Nevada Company STC SA03349NY, configuration 1, and Sierra Nevada Company STC SA03087NY.

continued on page 3 August 17, 2016 11/19/2018; 07/05/2019; 07/09/2024 November 13, 2018 William Eckler ODA administrator, ODA-833355-CE 3

SA00159MC 3

SA00159MC Description, continued from page 1

2) Instruction for Continued Airworthiness, Document Number 03120102, Revision B, dated June 14, 2018, FAA accepted November 13, 2018, or later FAA accepted revision

3) Airplane Flight Manual Supplement, Document Number 03120103, Revision A, dated October 15, 2018, or later FAA approved revision

Limitations, continued from page 1

2) A prerequisite to this installation is the modification per Hawker Beechcraft drawing 130M000030 or kit drawing 130-4014 for increased gross weights and increased fuel capacity, or modification per Hawker Beechcraft drawing 130M000009 or kit drawing 130-4030 for increased gross weights.

3) The FAA has not certified the equipment for which these provisions are intended.

You must get additional FAA approval to install this equipment. The FAA must evaluate the installation to ensure it complies with the applicable airworthiness standards.

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.

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

## Every issue (4)

- July 9, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/11/8d/118d471a2e3c2f3dcd8a253d6861cc1e8a2b2ce20ec6642be1c434bd52071a85)
- July 5, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/4f/cb/4fcb1e141e5130574e63c831c3e5ca8df531057f9a23a5138651ee91ec818344)
- November 19, 2018: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/d9/c7/d9c7c6f1619a79da324e9c2529c6151e5342e414891077fe13c4197c2bbbfb32)
- November 13, 2018: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/54/a1/54a19d99acd4b385d6474d9cbc743dadc4562029ca084f11aef8ff0e5c30186e)

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