# STC SA03527NY - Type: Supplemental type certificate - Status: Current, Issued - Holder: Avionik Straubing GmbH, Germany - Description: Installation of Universal Avionics UNS-1Lw Flight Management System (FMS) and Bendix/King KGP 560-02 Enhanced Ground Proximity Warning System (EGPWS). - Applied: November 10, 2014 - Status date: May 1, 2015 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A31CE](https://openairdocs.org/tcds/A31CE) - Certificate PDF: https://openairdocs.org/files/sha256/a5/6f/a56f8a59ddc837604ad8ec76e7cffc4d4cedaffef685d803fd020a56e94f2609 - Approved model list and other attachments: [AML_SA03527NY.pdf](https://openairdocs.org/files/sha256/f4/8c/f48c83897c78eeebbd79f3f2fe1febaad603e498e8d3db120cf8a99d314fd9dc) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/242792F0BFE7DE2D86257EFC005BFE70.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA03527NY ## ADs that name it (0) None. ## Approved models (7) - Beechcraft Corporation B90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation C90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation C90A ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation C90GT ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation C90GTi ([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. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. FAA Form 8110-2 (5/14) Page 1 of This certificate issued to: Part of the Signature Title SA03527NY Avionik Straubing GmbH Flugplatzstrasse 5 94348 Atting Germany Civil/Federal Aviation Regulations.3/23 1. Installation of Universal Avionics UNS-1Lw Flight Management System (FMS) and Bendix/King KGP 560-02 Enhanced Ground Proximity Warning System (EGPWS) in accordance with Avionik Straubing Instructions for Installation as listed on AML No. SA03527NY, or later EASA-approved revisions. 2. Aircraft is to be maintained in accordance with Avionik Straubing Instructions for Continued Airworthiness as listed on AML No. SA03527NY, or later EASA-accepted revisions to these documents. (See Description of Type Design Change continued on Page 3 of 3) 1. Operation is subject to the limitations set forth in the Avionik Straubing Approved Flight Manual Supplements as listed on AML No. SA03527NY, or later EASA-approved revisions to these documents. 2. The installer must determine whether this design change is compatible with previously approved modifications. 3. If the holder agrees to permit another person to use the certificate to alter the product, the holder must give the other person written evidence of that permission. Gaetano Sciortino Manager New York Aircraft Certification Office See attached FAA Approved Model List See attached FAA Approved Model List November 10, 2014 May 1, 2015 IMPORT See attached FAA Approved Model List (AML) No. SA03527NY for list of approved airplane models and applicable airworthiness regulations. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. FAA Form 8110-2 (5/14) Page 2 of To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): 3 SA03527NY This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. FAA Form 8110-2 (5/14) Page 3 of 3 Date of Issuance: May 1, 2015 Description of Type Design Change (continued): 3. The installation of the Universal Avionics LP/LPV Monitor is optional. Certification Basis: The certification basis for this type design change is as shown on the attached FAA Approved Model List (AML) No. SA03527NY. -----END----- SA03527NY ### AML_SA03527NY.pdf FAA APPROVED MODEL LIST (AML) NO. SA03527NY AVIONIK STRAUBING GmbH FOR INSTALLATION OF UNS-1Lw FMS AND BENDIX/KING KGP 560-02 EGPWS Page 1 of 2 Original Issue Date: May 1, 2015 **ITEM** **AIRCRAFT MAKE** AIRCRAFT MODEL TCDS CERTIFICATION BASIS INSTRUCTION FOR INSTALLATION * FLIGHT MANUAL SUPPLEMENT* INSTRUCTIONS FOR CONTINUED AIRWORTHINESS** AML AMDT DATE 1 Beechcraft Corporation B90, C90, C90A, C90GT, C90GTi, E90 3A20 CAR 3 (Note 1) ASR-2009-031-IFI-10- 02, Revision 2 dated April 17, 2015 UNS-1Lw FMS ASR-2009-031-FMS-05.1-00, dated September 09, 2009 KGP 560-02 EGPWS ASR-2009-031-FMS-05.2-00, dated July 14, 2009 UNS-1Lw FMS ASR-2009-031-ICA-11.1-03, dated April 17, 2015 KGP 560-02 EGPWS ASR-2009-031-ICA-11.2-03, dated April 17, 2015 2 Beechcraft Corporation F90 A31CE 14 CFR Part 23 Amendment 23-16 (Note 1) ASR-2009-031-IFI-10- 02, Revision 2 dated April 17, 2015 UNS-1Lw FMS ASR-2009-031-FMS-05.1-00, dated September 09, 2009 KGP 560-02 EGPWS ASR-2009-031-FMS-05.2-00, dated July 14, 2009 UNS-1Lw FMS ASR-2009-031-ICA-11.1-03, dated April 17, 2015 KGP 560-02 EGPWS ASR-2009-031-ICA-11.2-03, dated April 17, 2015 * or later EASA-approved revisions ** or later EASA-accepted revisions Note 1: See “Certification Basis for Alteration” section of this AML. FAA Approved: _______________________________ Gaetano Sciortino Manager New York Aircraft Certification Office FAA APPROVED MODEL LIST (AML) NO. SA03527NY AVIONIK STRAUBING GmbH FOR INSTALLATION OF UNS-1Lw FMS AND BENDIX/KING KGP 560-02 EGPWS Page 2 of 2 Certification Basis for Alteration: Note 1: Based on 14 CFR 21.115 and 21.101, and FAA Order 8110.48, the type certification basis is as shown on the aircraft TCDS for parts changed or affected by the change, with compliance shown to the following sections of 14 CFR Part 23 at the latest amendment level through Amendment 23-57: 23.301(a), 23.303, 23.305(a), 23.307(a), 23.365(a)(b)(d), 23.561(a )(b), 23.571(a)(b)(c), 23.575, 23.603(a)(b), 23.605, 23.607, 23.609(a), 23.611, 23.613, 23.671(a)(b), 23.771(a), 23.773(a), 23.843(b), 23.863, 23.867, 23.1301(a)(b)(c)(d ), 23.1309(a)(b)(c)(d)(e), 23.1321(a)(c), 23.1322(a)(b)(c)(d), 23.1323(a), 23.1325(a), 23.1327(a)(b), 23.1329(h), 23.1351(a)(b), 23.1353(h), 23.1357(a)(c), 23.1359(a)(b )(c), 23.1365(a)(b)(c)(d), 23.1367(a)(b)(c)(d), 23.1431(a)(b)(c)(d), 23.1529, 23.1581(a)(f), 23.1583(h), and 23.1585(a) ## Every issue (1) - May 1, 2015: Issued, Current. [certificate](https://openairdocs.org/files/sha256/a5/6f/a56f8a59ddc837604ad8ec76e7cffc4d4cedaffef685d803fd020a56e94f2609), [AML_SA03527NY.pdf](https://openairdocs.org/files/sha256/f4/8c/f48c83897c78eeebbd79f3f2fe1febaad603e498e8d3db120cf8a99d314fd9dc) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.