# STC SA01072SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: PAVCO Aircraft Systems Engineering LLC, United States
- Description: Installation of standby battery system to facilitate compliance with 14 CFR Part 135.163(f)(2)
- Applied: February 3, 2002
- Status date: May 5, 2002
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 23, Part 135
- Data sheets: [TCDS A4CE](https://openairdocs.org/tcds/A4CE)
- Certificate PDF: https://openairdocs.org/files/sha256/1a/de/1ade118ec7eff3f38a0276bb9e1ec3053b46364fd61935723d77c2906d50cc5e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DF223DBAEC643CB2862576E000595BD9.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01072SE

## ADs that name it (0)

None.

## Approved models (2)

- Cessna Aircraft Company 206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company T206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))

## 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 SA01072SE This certificate, issued to PAVCO Aircraft Systems Engineering, LLC 1110 26 th Ave. NW P.O. Box 615 Gig Harbor, WA 98335 certifies that the change in the type design for the follo wing product with the limitations and conditions therefor as specified hereon meets the airw orthiness requirements of Part 23 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: A4CE Make: Cessna Model: 206H, T206H

Description of the Type Design Change: Installation of standby battery system to facilitate compliance with 14 CFR Part 135.163(f)(2) in accordance with Olympic Aero Services, Inc. Master Drawing List OAS-30-206-001, Revision C, dated April 1, 2002, or later FAA approved revision. This system shall be maintained in accordance with Instructions for Continued Airworthiness document, OAS-30-23.1529, Revision A, dated March 27, 2002, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate and FAA approved Flight Manual Supplement OAS-30-23.1581, Revision A, dated April 5, 2002, or later FAA approved revision, must be maintained as part of the permanent records for the modified 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.

This certificate and the supporting data which is the ba sis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is ot herwise established by the Administrator of the Federal Aviation Administration.

Date of application: February 3, 2002 Date reissued:

Date of issuance: April 5, 2002 Date amended:

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- May 5, 2002: Issued, Current. [certificate](https://openairdocs.org/files/sha256/1a/de/1ade118ec7eff3f38a0276bb9e1ec3053b46364fd61935723d77c2906d50cc5e)

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