# STC SA02676CH

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: SRS Aviation LLC, United States
- Description: Installation of left and right hand fuselage external doublers per attached FAA Approved Model List (AML) No SA02676CH, issued June 8, 2011, or later FAA approved revision.
- Applied: November 21, 2008
- Status date: June 8, 2011
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS 5A4](https://openairdocs.org/tcds/5A4), [TCDS A14CE](https://openairdocs.org/tcds/A14CE), [TCDS A23CE](https://openairdocs.org/tcds/A23CE), [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/a8/ea/a8eafd6339b5fae61d6de05e5730c36e51f6307ab462e4ebc94db8727a22aaa5
- Approved model list and other attachments: [SA02676CHR1_AML.pdf](https://openairdocs.org/files/sha256/ed/9a/ed9ae1bc2cbd11f1094ffba243cae6bc6872ed02e9d622d9ba5bcda7f52bd8e2)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1D82422222C4D485862578ED0061D720.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02676CH

## ADs that name it (0)

None.

## Approved models (94, first 50)

- Hawker Beechcraft Corporation 100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Hawker Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 58A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 58P ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Hawker Beechcraft Corporation 58PA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Hawker Beechcraft Corporation 58TC ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Hawker Beechcraft Corporation 58TCA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Hawker Beechcraft Corporation 65 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-80 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-88 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-A80 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-A80-8800 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-A90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-A90-1 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-A90-2 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-A90-3 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-A90-4 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 65-B80 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- Hawker Beechcraft Corporation 70 ([TCDS 3A20](https://openairdocs.org/tcds/3A20))
- 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 95-B55B ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 95-C55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 95-C55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation A100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Hawker Beechcraft Corporation A100-1 (U-21J) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A100A ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Hawker Beechcraft Corporation A100C ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Hawker Beechcraft Corporation A200 (C-12A) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200 (C-12C) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200C (UC-12B) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (C-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (FWC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (RC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (RC-12G) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (RC-12H) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (RC-12K) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation A200CT (RC-12P) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

All 94: https://openairdocs.org/stc/SA02676CH/models.md

## 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.

Part * of the *Regulations.

Installation of left and right hand fuselage external doublers per attached FAA Approved Model List (AML) No SA02676CH, issued June 8, 2011, or later FAA approved revision.

1) This modification is intended to serve as a cosmetic, non-structural ice shield. This modification has been certified as noninterference Supplement Type Certificate and has not been evaluated to verify its intended function.

2) The installer must determine whether this design cha nge is compatible with previously approved modifications.

3) If the holder agrees to permit another pe rson to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

SRS Aviation LLC 8529 Ridgewood Ln.

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

SA02676CH for list of approved airplane models and Applicable airworthiness regulations Make : * Model : *

Date of application : November 21, 2008

Date of issuance :January 30, 2009

Date amended : June 8, 2011

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

( Title)

Original signed by:

Gregory J. Michalik

### SA02676CHR1_AML.pdf

**FAA APPROVED MODEL LIST (AML) NO. SA02676CH SRS AVIATION, LLC INC.**

FOR

INSTALLING NON-STRUCTURAL ICE SHIELDS ISSUE DATE: June 08, 2011

**ITEM**

**AIRCRAFT**

**AIRCRAFT**

**ORIGINAL TYPE**

**CERTIFICATION BASIS**

**INSTALLATION**

**INSTRUCTIONS**

AFM

AML

**MAKE MODEL CERTIFICATE NUMBER FOR**

**ALTERATION**

**NUMBER**

**REVISION NO. & DATE**

**SUPPLEMENT**

**NUMBER/DATE**

**AMENDMENT DATE**

Page 1 of 2 1 Hawker Beechcraft 58, 58A, G58 3A16 CAR 3 and amendments listed in TCDS 3A16

002-41SRS6 (FOR KIT # 002-41SRS6-100) Revision A, 15 Mar 11 N/A 2 Hawker Beechcraft 58P, 58PA, 58TC, 58TCA A23CE 14 CFR 23 and amendments listed in TCDS A23CE

002-41SRS6 (FOR KIT # 002-41SRS-100) Revision A, 15 Mar 11 N/A 3 Hawker Beechcraft 95, B95, B95A, D95A, E95,95-55, 95-A55, 95-B55, 95-B55A , 95-B55B(T-42), 95-C55, 95-C55A, D55A, E55, E55A, 56TC

3A16 CAR 3 and amendments listed in TCDS 3A16

002-41SRS6A (FOR KIT # 002-41SRS6-101) Revision INT., 15 Mar 11 N/A 4 Hawker Beechcraft 50(L-23A), B50(L-23B), C50, D50A, D50B, D50C, D50E, D50E-5990, E50(L-23D, RL-23D), F50, G50, H50, J50

5A4 CAR 3 and amendments listed in TCDS 5A4

99-41SRS6 (FOR KIT # 99-41SRS6-100) Revision INT., 15 Mar 11 N/A 5 Hawker Beechcraft 65(L-23F), A65, A-65-8200, 65-80, 65-A80, 65-A80-8800, 65- B80, 65-88, 65-90, 65-A90, 70, B90, C90, C90A, C90GT, E90, H90 (T-44A), C90GTi, 65-A90-1(JU-21A)(U- 21A)(RU-21A)(RU- 21D)(U-21G)(RU-21H), 65-A90-2(RU-21B), 65-A90-3(RU-21C), 65-A90-4(RU-21E)(RU- 21H)

3A20 CAR 3 and amendments listed in TCDS 3A20

99-41SRS6 (FOR KIT # 99-41SRS6-100) Revision INT., 15 Mar 11 N/A

**FAA APPROVED MODEL LIST (AML) NO. SA02676CH SRS AVIATION, LLC INC.**

FOR

INSTALLING NON-STRUCTURAL ICE SHIELDS ISSUE DATE: June 08, 2011

**ITEM**

**AIRCRAFT**

**AIRCRAFT**

**ORIGINAL TYPE**

**CERTIFICATION BASIS**

**INSTALLATION**

**INSTRUCTIONS**

AFM

AML

**MAKE MODEL CERTIFICATE NUMBER FOR**

**ALTERATION**

**NUMBER**

**REVISION NO. & DATE**

**SUPPLEMENT**

**NUMBER/DATE**

**AMENDMENT DATE**

Page 2 of 2 6 Hawker Beechcraft 100, A100 (U-21F), A100A, A100C, B100

A14CE 14 CFR 23 and amendments listed in TCDS A14CE

99-41SRS6 (FOR KIT # 99-41SRS-100) Revision INT., 15 Mar 11 N/A 7 Hawker Beechcraft A100-1(U-21J) A24CE CA R 3 and amendments listed in TCDS 3A16

99-41SRS6 (FOR KIT # 99-41SRS-100) Revision INT., 15 Mar 11 N/A 8 Hawker Beechcraft 200, 200C, 200CT, 200T, B200, B200C, B200CT, B200T, 300, 300LW, B300, B300C(C-12W), A200(C-12A)(C12C), A200C(UC-12B), A200CT(C-12D), A200CT(FWC-12D), A200CT(C-12F), A200CT(RC-12D), A200CT(RC-12G), A200CT(RC-12H), A200CT(RC-12K), A200CT(RC-12P), A200CT(RC-12Q), B200C(C-12F), B200C(UC-12M), B200C(C-12R), B200C(UC-12F), B200GT, B200CGT

A24CE 14 CFR 23 and amendments listed in TCDS A24CE 102-41SRS6 (FOR KIT # 102-41SRS6-100) Revision INT., 15 Mar 11 N/A

FAA APPROVED:

Mary Ellen A. Schutt, Manager, Airframe & Administrative Branch Chicago Aircraft Certification Office

Original signed by:

Gregory J. Michalik

## Every issue (2)

- June 8, 2011: Amended, Current. [certificate](https://openairdocs.org/files/sha256/a8/ea/a8eafd6339b5fae61d6de05e5730c36e51f6307ab462e4ebc94db8727a22aaa5), [SA02676CHR1_AML.pdf](https://openairdocs.org/files/sha256/ed/9a/ed9ae1bc2cbd11f1094ffba243cae6bc6872ed02e9d622d9ba5bcda7f52bd8e2)
- January 30, 2009: Issued, Current. [certificate](https://openairdocs.org/files/sha256/df/43/df43c10f49f2890802b62c1a4a24dd0382fedf26142e1cd9ddd9ef93dc6afb47)

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