# STC SA01696LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Securaplane Technologies, United States
- Description: Installation of Hawker PN 9750W0370 or 9750W0370-8 Series 24V/43AH Sealed Lead Acid Battery.
- Applied: April 30, 2004
- Status date: March 31, 2014
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A14CE](https://openairdocs.org/tcds/A14CE), [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A31CE](https://openairdocs.org/tcds/A31CE)
- Certificate PDF: https://openairdocs.org/files/sha256/a4/a1/a4a17e2376d6df388ce60de61360c7a066990c60333d11e203de44f8273fc43d
- Approved model list and other attachments: [SA01696LA_AML.pdf](https://openairdocs.org/files/sha256/9b/f0/9bf033f22d76ab5d78f6b022a8f7432168f2437f1932e5eac390f4df32266742)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EA645ECF7F0B307A86257CB5004FC93D.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01696LA

## ADs that name it (0)

None.

## Approved models (26)

- Beechcraft Corporation 100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Beechcraft Corporation A100A ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Beechcraft Corporation A200 (C-12A) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200 (C-12C) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200C (UC-12B) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (C-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (FWC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12G) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12H) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12K) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12P) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation A200CT (RC-12Q) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200C (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200C (C-12R) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200C (UC-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B200C (UC-12M) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation B90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Beechcraft Corporation C90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Beechcraft Corporation E90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Beechcraft Corporation F90 ([TCDS A31CE](https://openairdocs.org/tcds/A31CE))

## 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.

Number SA01696LA

This Certificate issued to Securaplane Technologies Inc.

12350 N. Vistoso Park Road, Oro Valley, AZ 85755

Part 23 of the Federal Aviation Regulations.

Description of Type Design Change: Installation of Hawker PN 9750W0370 or 9750W0370-8 Series 24V/43AH Sealed Lead Acid Battery in accordance with the Installation Instructions as listed on AML SA01696LA, Revision “ORIG“ dated November 09, 2004 or later FAA approved revision.

Limitations and Conditions: The approval of this installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. 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 that permission.

SA01696LA for list of approved model types

Date reissued: March 31, 2014

(Signature) Manager, Systems & Equipment Branch Los Angeles Aircraft Certification Office

Date of application: April 30, 2004

Date of issuance: November 10, 2004

The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental type certificate.

The FAA will reissue the certificate in the name of the transferee and forward it to him.

Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (2)

- March 31, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a4/a1/a4a17e2376d6df388ce60de61360c7a066990c60333d11e203de44f8273fc43d), [SA01696LA_AML.pdf](https://openairdocs.org/files/sha256/9b/f0/9bf033f22d76ab5d78f6b022a8f7432168f2437f1932e5eac390f4df32266742)
- November 10, 2004: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/23/91/2391f0021c0d580473ba95877d76b8f401f5e5a7c6cf5d454d97473a08a6974b)

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