# STC SA02381LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Alexandeer R Dubose, United States
- Description: Removal of Lycoming IO-360-B1A engines and installation of Lycoming IO-360-B1B engines in accordance with FAA Approved Installation Instruction, Revision N/C, dated August 26, 2011, or later FAA approved revisions to this document.  FAA Approved William Crowder Airplane Flight Manual Supplement dated November 9, 2011, or later FAA approved revisions is required.
- Applied: August 26, 2011
- Status date: February 7, 2018
- Product: Aircraft
- Certification basis: Part 21
- Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16)
- Certificate PDF: https://openairdocs.org/files/sha256/9e/37/9e370020df169de3a4d907c37e854a1774109d6fd3c9ade65f53f3ea492ae152
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/32B9E1E45CC6040786258232004C15AD.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02381LA

## ADs that name it (0)

None.

## Approved models (1)

- Hawker Beechcraft Corporation B95A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA02381LA This certificate issued to: ALEXANDEER R. DUBOSE 1720 NORD AVENUE CHICO, CA 95926 Part 3 of the Civil Abir Regulations. as amended to May 15, 1956. See Type Certificate Data Sheet No. 3A16.

Original Product Type Certificate Number : 3A16 Make: Hawker Beechcraft Corporation Model:

B95A, S/N TD-458 one only Description of Type Design Change: Removal of Lycoming 10-360-B1A engines and installation of Lycoming IO-360-B1B engines in accordance with FAA Approved Installation Instruction, Revision N/C, dated August 26, 2011, or later FAA approved revisions to this document. FAA Approved William Crowder Airplane Flight Manual Supplement dated November 9, 2011, or later FAA approved revisions is required.

Limitations and Conditions: Data pertaining to this modification are considered to be inadequate for duplication on other aircraft. This change in type design is approved for installation on Beech B95A, S/N TD-458 only. A copy of this certificate must be maintained as a part of the permanent records for this modified aircraft.

Date of Application: August 26, 2011 Date Reissued: February 1, 2018 Date of Issuance: November 18, 2011 Date Amended:

EDERAL AVIATION By Direction of the Administrator (Signature) Manager, Technical & Administrative Support TOMINSTRATO Section Los Angeles ACO Branch (Title)

FAA Form 8110-2(10-68) Pade 1 of 2

## Every issue (2)

- February 7, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/9e/37/9e370020df169de3a4d907c37e854a1774109d6fd3c9ade65f53f3ea492ae152)
- November 18, 2011: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/f6/1d/f61d907efdb7cbe4f035231a2a5ac94ff6bb0d13215e717cc0382f42875f69ab)

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