# STC SA02254AK

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Genesys Aerosystems Inc., United States
- Description: Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen"
- Applied: October 8, 2004
- Status date: June 16, 2022
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A17EU](https://openairdocs.org/tcds/A17EU), [TCDS A29EU](https://openairdocs.org/tcds/A29EU), [TCDS A7CE](https://openairdocs.org/tcds/A7CE), [TCDS A25CE](https://openairdocs.org/tcds/A25CE), [TCDS A28CE](https://openairdocs.org/tcds/A28CE), [TCDS A16EU](https://openairdocs.org/tcds/A16EU), [TCDS A14CE](https://openairdocs.org/tcds/A14CE), [TCDS A-684](https://openairdocs.org/tcds/A-684), [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS A-765](https://openairdocs.org/tcds/A-765), [TCDS 5A4](https://openairdocs.org/tcds/5A4), [TCDS A12CE](https://openairdocs.org/tcds/A12CE), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A31CE](https://openairdocs.org/tcds/A31CE), [TCDS 7A4](https://openairdocs.org/tcds/7A4), [TCDS A59EU](https://openairdocs.org/tcds/A59EU), [TCDS A78EU](https://openairdocs.org/tcds/A78EU), [TCDS 7A15](https://openairdocs.org/tcds/7A15), [TCDS A23SO](https://openairdocs.org/tcds/A23SO), [TCDS A56CE](https://openairdocs.org/tcds/A56CE) and 4 more
- Certificate PDF: https://openairdocs.org/files/sha256/cb/1d/cb1d31eb721c4d6c2559d9ed09e286c85bb601d74e1e5ba4cc7882ba6bd3c8e1
- Approved model list and other attachments: [SA02254AK AML.pdf](https://openairdocs.org/files/sha256/6b/9a/6b9a3ccca2983b06187cfdf5dacea0494f5600c56a712ceab5f36e0613112059)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FB80D8E79E503D5F8625886E004B22B3.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02254AK

## ADs that name it (0)

None.

## Approved models (203, first 50)

- B-N Group Ltd. BN-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-21 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-26 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-27 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-3 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-6 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-8 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-9 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-21 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-26 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-27 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2T ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2T-4R ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN2A MK. III ([TCDS A29EU](https://openairdocs.org/tcds/A29EU))
- B-N Group Ltd. BN2A MK. III-2 ([TCDS A29EU](https://openairdocs.org/tcds/A29EU))
- B-N Group Ltd. BN2A MK. III-3 ([TCDS A29EU](https://openairdocs.org/tcds/A29EU))
- Cessna Aircraft Company 401 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 401A ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 401B ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 402 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 402A ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 402B ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 402C ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 404 ([TCDS A25CE](https://openairdocs.org/tcds/A25CE))
- Cessna Aircraft Company 406 ([TCDS A25CE](https://openairdocs.org/tcds/A25CE))
- Cessna Aircraft Company 411 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 411A ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 414 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 414A ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 421 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 421A ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 421B ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 421C ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 425 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE))
- Cessna Aircraft Company 441 ([TCDS A28CE](https://openairdocs.org/tcds/A28CE))
- Dornier Luftfahrt GmbH Do 28 D ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Do 28 D-1 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-100 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-101 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-200 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-201 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Hawker Beechcraft Corporation 100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Hawker Beechcraft Corporation 18D ([TCDS A-684](https://openairdocs.org/tcds/A-684))
- 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))

All 203: https://openairdocs.org/stc/SA02254AK/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.

**14 CFR 21.120)**

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 1 OF 4

Number: SA02254AK This certificate issued to:

Configuration 1:

Installation of “Single Screen”, “2 or 3 Screen”, “Dual Screen”, or “4 or 6 screen”, FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV) configurations, in accordance with Chelton Flight Systems, Inc., System Installation Manual Commuter and Large Aircraft, Document Number 150-045057, Revision M, dated August 13, 2014 or later FAA approved revision.

(Description of Type Design Change continued on Page 3)

Genesys Aerosystems, Inc.

4001 Old International Airport Road, Unit 10 Anchorage, Alaska 99502 Original Product Type Certificate Number: *

Make: * Model: * See attached FAA Approved Model List (AML) No. SA02254AK, dated October 17, 2008 or later FAA approved revision, for a list of approved airplane models and applicable airworthiness regulations

Date of application: October 8, 2004

Date of issuance: September 21, 2005 Date reissued: January 11, 2010

Date amended: May 3, 2006; October 17, 2008;

November 6, 2011; May 1, 2017; June 16, 2022 By direction of the Administrator

August A. Asay Title: Manager, Anchorage ACO Branch

Part 23 of Federal Aviation Regulations.

**14 CFR 21.120)**

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 2 OF 4

Number: SA02254AK

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA02254AK

**14 CFR 21.120)**

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 3 OF 4

(Continuation Sheet) Number: SA02254AK Date of application: October 8, 2004 Date of issuance: September 21, 2005 Date reissued: January 11, 2010 Date amended: May 3, 2006; October 17, 2008; November 6, 2011;

May 1, 2017; June 16, 2022

Configuration 2:

Installation of “Single Screen”, “2 or 3 Screen”, “Dual Screen”, or “4 or 6 screen”, FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV) configurations, in accordance with Chelton Flight Systems, Inc., System Installation Manual Commuter and Large Aircraft, Document Number 64-000062, Revision E, dated August 13, 2014 or later FAA approved revision.

Configuration 3:

Installation of Genesys Aerosystems, Inc. Electronic Flight Information System (EFIS), in accordance with Genesys Aerosystems IDU-450 Installation Manual 9.0A, Document number 64-000124-090A, Revision A, dated April 26, 2021, or later FAA approved revision.

1. Compatibility of the design change with previously approved modifications must be determined by the installer.

2. For Configuration 1:

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 150-045054, Revision E, dated May 1, 2017, or later FAA approved revision is required for “Single Screen” or “2 or 3 Screen” installations as part of this installation.

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 150-045084, Revision D, dated May 1, 2017, or later FAA approved revision is required for “Dual Screen” or “4 or 6 Screen” installations as part of this installation.

(Limitations and Conditions continued on Page 4)

**14 CFR 21.120)**

FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 4 OF 4

(Continuation Sheet) Number: SA02254AK Date of application: October 8, 2004 Date of issuance: September 21, 2005 Date reissued: January 11, 2010 Date amended: May 3, 2006; October 17, 2008; November 6, 2011;

May 1, 2017; June 16, 2022

3. For Configuration 2:

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 13-254FMS-07E2, Revision B, dated May 1, 2017 or later FAA approved revision is required for “Single Screen” or “2 or 3 Screen” installations as part of this installation.

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 13-254FMS-07E4, Revision B, dated May 1, 2017, or later FAA approved revision is required for “Dual Screen” or “4 or 6 Screen” installations as part of this installation.

4. For Configuration 3:

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 13-254FMS-90A2, Revision A, dated March 31, 2022 or later FAA approved revision, is required for “Single Screen” or “2 or 3 Screen” installations as part of this installation.

FAA approved Airplane Flight Manual Supplement or Supplemental Airplane Flight Manual, Document Number 13-254FMS-90A4, Revision A, dated March 31, 2022 or later FAA approved revision, is required for “Dual Screen” or “4 or 6 Screen” installations as part of this installation.

5. For Configuration 1 or Configuration 2 Instructions for Continued Airworthiness, refer to Document Number 150-045055, Revision M, dated January 15, 2017, or later FAA approved revision. For Configuration 3 Instructions for Continued Airworthiness, refer to Document Number 13-254011, Revision A, dated November 11, 2021 or later FAA approved revision.

### SA02254AK AML.pdf

**FAA APPROVED MODEL LIST (AML) STC SA02254AK FOR**

**CHELTON FLIGHT SYSTEMS**

STC Reissued Date: March 27, 2006 STC Amended date : May 3, 2006 STC Amended date: October 17, 2008 Revision B Type Certificate Number Model Certification Basis

FAA Approved Page 1 of 5 Date: October 17, 2008 Twin Commander Models 560-F, 680, 680E, 680F, 720, 2A4, Rev. 46, 4/03/00 680FL, 680FL(P), 680T, 680V, 680W, 681, 690, 685, 690A, 690B, 690C, 690D, 695, 695A, 695B Certification Basis: CAR 3

Beechcraft Models 65 (L-23F), A65, A-65-8200, 65-80, 3A20, Rev. 67, 07/08/08 65-A80, 65-A80-8800, 65-B80, 65-88, 65-90, 65-A90, 70, B90, C90, C90A, C90GT, E90, H90 (T-44A), 65-A90-1, 65-A90-2, 65-A90-3, 65-A90-4 Certification Basis: CAR 3

Beechcraft Models 50 (L-23A), B50 (L-23B), C50, 5A4, Rev. 61, 3/26/07 D50 (L-23E), D50A, D50B, D50C, D50E, D50E-5990, E50 (L-23D, RL-23D), F50, G50, H50, J50 Certification Basis: CAR 3

ParisJet Models M.S. 760 (Paris I), M.S. 760 B (Paris II), 7A3, Rev. 4, 3/02/07 M.S. 760 A (Paris IA) Certification Basis: CAR 3

Piaggio Models P.166, P.166B, P.166C, P.166DL3 7A4, Rev. 7, 10/31/78 Certification Basis: CAR 3

**FAA APPROVED MODEL LIST (AML) STC SA02254AK FOR**

**CHELTON FLIGHT SYSTEMS**

STC Reissued Date: March 27, 2006 STC Amended date : May 3, 2006 STC Amended date: October 17, 2008 Revision B Type Certificate Number Model Certification Basis

FAA Approved Page 2 of 5 Date: October 17, 2008 Pilatus Models PC-6, PC-6-H1, PC-6-H2, PC-6/350, 7A15, Rev. 13, 5/01/07 PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, PC-6/C1-H2 Certification Basis: CAR 3

Beechcraft Models 18D, A18A, A18D, S18D, A-684, Rev. 3, 3/26/07 SA18A, SA18D Certification Basis: AB-7A

Beechcraft Models 3N, 3NM, 3TM, JRB-6, D18C, D18S, A-765, Rev. 75, 3/26/07 E18S, RC-45J (SNB-5P), E18S-9700, G18S, H18, C-45G, TC-45G, C-45H, TC-45H, TC-45J, UC-45J (SNB-5) Certification Basis: CAR 3

Cessna Models 401, 401A, 401B, 402, 402A, 402B, 402C, A7CE, Rev. 47, 3/27/07 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425 Certification Basis: CAR 3, 14 CFR Part 23

De Havilland Models DHC-6-1, DHC-6-100, A9EA, Rev. 13, 10/03/07 DHC-6-200, DHC-6-300 Certification Basis: CAR 3

**FAA APPROVED MODEL LIST (AML) STC SA02254AK FOR**

**CHELTON FLIGHT SYSTEMS**

STC Reissued Date: March 27, 2006 STC Amended date : May 3, 2006 STC Amended date: October 17, 2008 Revision B Type Certificate Number Model Certification Basis

FAA Approved Page 3 of 5 Date: October 17, 2008 Beechcraft Models 60, A60, B60 A12CE, Rev. 24, 3/26/07 Certification Basis: 14 CFR Part 23

Beechcraft Models 99, 99A, 99A (FACH), A99, A99A, A14CE, Rev. 37, 3/26/07 B99, C99, 100, A100 (U-21F), A100A, B100 Certification Basis: 14 CFR Part 23

Shorts Models SC-7 Series 2, SC-7 Series 3 A15EU, Rev. 10, 3/1/07 Certification Basis: 14 CFR Part 23

Dornier Models Do 28 D, Do 28 D-1, Dornier 228-100, A16EU, Rev. 9, 3/2/07 Dornier 228-101, Dornier 228-200, Dornier 228-201 Certification Basis: 14 CFR Part 23

Britten-Norman Models BN-2, BN-2A, BN-2A-6, A17EU, Rev. 17, 3/02/07 BN-2A-8, BN-2A-2, BN-2A-9, BN-2A-3, BN-2A-20, BN-2T-4R, BN-2A-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN-2T Certification Basis: 14 CFR Part 23

Piper Aircraft Models PA-42, PA-42-720, PA-42-1000 A23SO, Rev. 18, 8/07/06 Certification Basis: 14 CFR Part 23

**FAA APPROVED MODEL LIST (AML) STC SA02254AK FOR**

**CHELTON FLIGHT SYSTEMS**

STC Reissued Date: March 27, 2006 STC Amended date : May 3, 2006 STC Amended date: October 17, 2008 Revision B Type Certificate Number Model Certification Basis

FAA Approved Page 4 of 5 Date: October 17, 2008 Beechcraft Models 200, 200C, 200CT, 200T, B200, A24CE, Rev. 97, 5/15/08 B200C, B200CT, B200T, 300, 300LW, B300, B300C, A100-1 (U-21J), A200 (C-12A), A200 (C-12C), 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) Certification Basis: 14 CFR Part 23

Cessna Models 404, 406 A25CE, Rev. 11, 6/15/95 Certification Basis: 14 CFR Part 23

Cessna Model 441 A28C E, Rev. 12, 9/22/03 Certification Basis: 14 CFR Part 23

Britten-Norman Models BN2A MK. III, A29EU, Rev. 5, 3/02/07 BN2A MK. III-2, BN2A MK. III-3 Certification Basis: 14 CFR Part 23

Beechcraft Model F90 A 31CE, Rev. 8, 3/26/07 Certification Basis: 14 CFR Part 23

**FAA APPROVED MODEL LIST (AML) STC SA02254AK FOR**

**CHELTON FLIGHT SYSTEMS**

STC Reissued Date: March 27, 2006 STC Amended date : May 3, 2006 STC Amended date: October 17, 2008 Revision B Type Certificate Number Model Certification Basis

FAA Approved Page 5 of 5 Date: October 17, 2008 Piaggio Model P-180 A59E U, Rev. 17, 4/15/08 Certification Basis: 14 CFR Part 23

Pilatus Models PC-12, PC-12/45 A78EU, Rev. 18, 11/15/07 Certification Basis: 14 CFR Part 23

Polskie Zaklady Lotnicze Model PZL M28 05 A56CE, Rev. 1, 3/16/07 Certification Basis: 14 CFR Part 23

FAA APPROVED:_______________________________ Manager, Anchorage Aircraft Certification Office Federal Aviation Administration Anchorage, Alaska

## Every issue (8)

- June 16, 2022: Amended, Current. [certificate](https://openairdocs.org/files/sha256/cb/1d/cb1d31eb721c4d6c2559d9ed09e286c85bb601d74e1e5ba4cc7882ba6bd3c8e1), [SA02254AK AML.pdf](https://openairdocs.org/files/sha256/6b/9a/6b9a3ccca2983b06187cfdf5dacea0494f5600c56a712ceab5f36e0613112059)
- November 7, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/ce/4a/ce4a76441ee173be9108ba19602b5ba1f4039e3d4e6719ee7ab84a31d49fdea7), [SA02254AK AML.pdf](https://openairdocs.org/files/sha256/6b/9a/6b9a3ccca2983b06187cfdf5dacea0494f5600c56a712ceab5f36e0613112059)
- January 11, 2010: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/dd/6c/dd6c305017bd002c8cd95643fc41c555bb876e7af891f18f67c619e41f8460d8), [SA02254AK_Reissue_Jan2010_.pdf](https://openairdocs.org/files/sha256/ec/ad/ecadfb70d0e43446ef18db40b3257b97874bf2b7d190bb881fbc8615a3967f63)
- January 11, 2010: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/dd/6c/dd6c305017bd002c8cd95643fc41c555bb876e7af891f18f67c619e41f8460d8), [SA02254AK_Reissue_Jan2010_.pdf](https://openairdocs.org/files/sha256/ec/ad/ecadfb70d0e43446ef18db40b3257b97874bf2b7d190bb881fbc8615a3967f63)
- March 27, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/8a/34/8a346c7af8fff1bb88b4d41a58eaf5d75d4c72fefa06feea7fb27b690d4f0379), [SA02254AKaml.pdf](https://openairdocs.org/files/sha256/dd/6c/dd6c305017bd002c8cd95643fc41c555bb876e7af891f18f67c619e41f8460d8)
- March 27, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/8a/34/8a346c7af8fff1bb88b4d41a58eaf5d75d4c72fefa06feea7fb27b690d4f0379), [SA02254AKaml.pdf](https://openairdocs.org/files/sha256/dd/6c/dd6c305017bd002c8cd95643fc41c555bb876e7af891f18f67c619e41f8460d8)
- September 21, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/65/d9/65d99858bfff44d1bf3b82885999b727acdfe11f644d846682717cdf12dd63da), [SA02254AKAML.pdf](https://openairdocs.org/files/sha256/91/a6/91a616f669c859521dfb0f5e645f2dd96b0f571ced4905d4d02b2bc7d1cd0ee2)
- September 20, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/65/d9/65d99858bfff44d1bf3b82885999b727acdfe11f644d846682717cdf12dd63da), [SA02254AKAML.pdf](https://openairdocs.org/files/sha256/91/a6/91a616f669c859521dfb0f5e645f2dd96b0f571ced4905d4d02b2bc7d1cd0ee2)

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