# STC SA02625CH

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: SRS Aviation LLC, United States
- Description: Installation of corrugated aluminum elevator skins in place of corrugated magnesium elevator skins.
- Applied: September 24, 2008
- Status date: September 24, 2008
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS 3A16](https://openairdocs.org/tcds/3A16), [TCDS 5A3](https://openairdocs.org/tcds/5A3)
- Certificate PDF: https://openairdocs.org/files/sha256/43/aa/43aa170296e17d332eb137a3617423aeea7054c461d3c622f9ea3b10973e4b16
- Approved model list and other attachments: [STCSA02625CH.pdf](https://openairdocs.org/files/sha256/b6/da/b6da9d0ac32691ddd3402d5f7b1d9334176f787732544366a5bc26dbf71469a6)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/44CD6A2A671AA319862574E8007EB800.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02625CH

## ADs that name it (0)

None.

## Approved models (28)

- Hawker Beechcraft Corporation 35-33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation 35-A33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation 35-B33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation 35-C33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation 35-C33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation 45 (Military YT-34) ([TCDS 5A3](https://openairdocs.org/tcds/5A3))
- Hawker Beechcraft Corporation 95 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 95-55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 95-A55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 95-B55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 95-B55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation A36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation A45 (Military T-34A; B-45) ([TCDS 5A3](https://openairdocs.org/tcds/5A3))
- Hawker Beechcraft Corporation B36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation B95 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation B95A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation D45 (Military T-34B) ([TCDS 5A3](https://openairdocs.org/tcds/5A3))
- Hawker Beechcraft Corporation D95A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation E33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation E33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation E33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation F33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation F33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation F33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation G33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation G36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

## 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.

Page 1 of 1 FAA APPROVED MODEL LIST (AML) NO. SA02625CH SRS Aviation LLC

**INSTALLATION OF ALUMINUM ELEVATOR SKINS**

ISSUE DATE: September /24/08

**INSTALLATION**

**INSTRUCTIONS**

**ITEM**

**AIRCRAFT MAKE**

**AIRCRAFT MODEL**

**ORIGINAL TYPE**

**CERTIFICATE NUMBER**

**CERTIFICATION BASIS FOR**

**ALTERATION**

**NUMBER REVISION NO. & DATE**

ICA

**SUPPLEMENT**

**NUMBER/DATE**

AML

AMENDMENT DATE 1 Hawker Beechcraft B95, B95A, D95A (TD-534 through TD-

559), 95-55, 95-A55, 95-B55 (TC 502 through TC-547), 95-B55A (TC 502 through TC-547) 3A16 CAR 3 and amendments listed in TCDS 3A16 ICA Supplemental Doc. No.

SRS-33-36-95-55 Appendix B Revision B SRS-33-36-95-55 Rev. C 8/8/08

2 Hawker Beechcraft 95 3A16 CAR 3 and amendments listed in TCDS 3A16 ICA Supplemental Doc. No.

SRS-33-36-95-55 Appendix A Revision A SRS-33-36-95-55 Rev. C 8/8/08

3 Hawker Beechcraft 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33,E33A,E33C,F33,F33A,F33C,G33, 36,A36,A36TC,B36TC,G36 3A15 CAR 3 and amendments listed in TCDS 3A15 ICA Supplemental Doc. No.

SRS-33-36-95-55 Appendix A Revision A SRS-33-36-95-55 Rev. C 8/8/08

4 Hawker Beechcraft 45(YT-34) A45(T-34A,B-45) D45(T-34B) 5A3 CAR 3 and amendments listed in TCDS 5A3 ICA Supplemental Doc. No.

SRS-33-36-95-55 Appendix A Revision A SRS-33-36-95-55 Rev. C 8/8/08

Original Signed By:

F A A A P P R O V E D : _ _ Gregory J. Michalik for M a r y E l l e n A . S c h u t t M a n a g e r , A i r f r a m e & A d m i n i s t r a t i v e B r a n c h C h i c a g o A i r c r a f t C e r t i f i c a t i o n O f f i c e A m e n d e d : -

### STCSA02625CH.pdf

United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate

_____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

_____________________________________________________________________________________________________________________________________ FAA FORM 8110-2(10-68) PAGE 1 of 2 PAGES T his certificate may be transferred in accordance with FAR 21.47.

Number SA02625CH This certificate issued to

certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part * of the Civil Aviation Regulations.

Original Product--Type Certificate Number :

Description of Type Design Change:

Installation of corrugated aluminum elevator skins in place of corrugated magnesium elevator skins in accordance with SRS Aviation LLC “Aluminum Elevator kit Assembly Manual Doc. No.SRS-33-36-95-55-1, Revision C., dated August 8, 2008, or “Aluminum Elevator kit Assembly Manual Doc. No.SRS-33-36-95-55-2, Revision C., dated August 8, 2008 or later FAA approved revision.

Limitations and Conditions:

1) Compatibility of this design change with previously appr oved modifications must be determined by the installer.

2) 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 basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

SRS Aviation LLC 8529 Ridgewood Ln.

Savage, MN 55378 * See attached FAA Approved Model List (AML) No.

SA02625CH for list of approved airplane models and Applicable airworthiness regulations Make : * Model : *

Date of application : August 16, 2007

Date of issuance :September 24, 2008

Date reissued :

Date amended :

By direction of the Administrator

_______________________________________________________ ( Signature) Mary Ellen A. Schutt, Manager Airframe & Administrative Branch Chicago Aircraft Certification Office _______________________________________________________ ( Title)

## Every issue (1)

- September 24, 2008: Issued, Current. [certificate](https://openairdocs.org/files/sha256/43/aa/43aa170296e17d332eb137a3617423aeea7054c461d3c622f9ea3b10973e4b16), [STCSA02625CH.pdf](https://openairdocs.org/files/sha256/b6/da/b6da9d0ac32691ddd3402d5f7b1d9334176f787732544366a5bc26dbf71469a6)

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