# STC SA02255NY - Type: Supplemental type certificate - Status: Current, Amended - Holder: Innovative Solutions & Support Inc, United States - Description: Configuration A Dual 15 Flat Panel Display System (Pilot and Copilot Positions) Installation of Innovative Solutions & Support - (IS&S) Dual 15 Flat Panel Display System Configuration B 10 Flat Panel Display System (Pilot and Copilot/Pilot Side Only Installation) Installation of Innovative Solutions & Support - (IS&S) 10 Flat Panel Display System Configuration C 10 Flat Panel Display System (Pilot Side) and 15 Flat Panel Display System (Copilot Side) Installation) Installation of Innovative Solutions & Support - (IS&S) 10 Flat Panel Display System - Applied: November 17, 2005 - Status date: April 7, 2009 - Product: Aircraft, Single-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU) - Certificate PDF: https://openairdocs.org/files/sha256/69/bf/69bf87c2c118fd3192d05d72410a2c57a825c4047f46fb2e9e1223f0f6da8768 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E0A11F2B538F22B4862575C80079C6ED.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02255NY ## ADs that name it (0) None. ## Approved models (3) - Pilatus Aircraft Limited PC-12 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) - Pilatus Aircraft Limited PC-12/45 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) - Pilatus Aircraft Limited PC-12/47 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) ## 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 SA02255NY This certificate issued to Part 23 of the Federal Aviation Regulations. Configuration A – Dual 15” Flat Panel Display System (Pilot and Copilot Positions) Installation of Innovative Solutions & Support - (IS&S) Dual 15” Flat Panel Display System in accordance with IS&S Master Drawing List, 1D-06319 Revision 9, dated March 27, 2009. Configuration B – 10” Flat Panel Display System (Pilot and Copilot/Pilot Side Only Installation) Installation of Innovative Solutions & Support - (IS&S) 10” Flat Panel Display System in accordance with IS&S Master Drawing List, 1D-06718 Revision E, dated March 27, 2009. Configuration C – 10” Flat Panel Display System (Pilot Side) and 15” Flat Panel Display System (Copilot Side) Installation) Installation of Innovative Solutions & Support - (IS&S) (2x10” and 1x15”) Flat Panel Display System in accordance with IS&S Master Drawing List, 1D-07356 Revision 4, dated March 27, 2009. Innovative Solutions and Support 720 Pennsylvania Drive Exton, PA 19341 A78EU Make: Pilatus Aircraft Limited Model: PC-12, -12/45, -12/47 Series Date of application: November 17, 2005 Date of issuance: May 02, 2006 Date reissued: Date amended: September 13, 2006, June 19, 2007, April 07, 2009 ( Signature) Anthony Socias Manager New York Aircraft Certification Office ( Title) FAA Form 8110-2-1(10-69) Page 2 of 2 Number SA02255NY Date of Amendment: April 07, 2009 Configuration A – Dual 15” Flat Panel Display System (Pilot and Copilot Positions) 1. IS&S Airplane Flight Manual Supplement Document No. 1D-06314, Revision C, FAA Approved April 7, 2009 is required with this installation. 2. The aircraft must be maintained in accordance with IS&S Instructions for Continued Airworthiness, Flat Panel Display Installation, 1D-06313, Revision 7, dated January 29, 2009. 3. STC SA01933LA must be installed prior to using the GPS WAAS approach capabilities of this installation. 4. The Installer must determine whether this design change is compatible with previously approved modifications. 5. If the holder agrees to permit another person to use the certificate to alter a product, the holder must give the other person written evidence of that permission. Configuration B – 10” Flat Panel Display System (Pilot and Copilot/Pilot Side Only Installation) 1. IS&S Airplane Flight Manual Supplement Document No. 1D-06715, Revision C, FAA Approved April 7, 2009 is required with this installation. 2. The aircraft must be maintained in accordance with IS&S Instructions for Continued Airworthiness, Flat Panel Display Installation, 1D-06714, Revision 4, dated January 29, 2009. 3. STC SA01933LA must be installed prior to using the GPS WAAS approach capabilities of this installation. 4. The Installer must determine whether this design change is compatible with previously approved modifications. 5. If the holder agrees to permit another person to use the certificate to alter a product, the holder must give the other person written evidence of that permission. Configuration C – 10” Flat Panel Display System (Pilot Side) and 15” Flat Panel Display System (Copilot Side) Installation) 1. IS&S Airplane Flight Manual Supplement Document No. 1D-07357, Revision B, FAA Approved April 7, 2009 is required with this installation. 2. The aircraft must be maintained in accordance with IS&S Instructions for Continued Airworthiness, Flat Panel Display Installation, 1D-07358, Revision 3, dated January 29, 2009. 3. STC SA01933LA must be installed prior to using the GPS WAAS approach capabilities of this installation. 4. The Installer must determine whether this design change is compatible with previously approved modifications. 5. If the holder agrees to permit another person to use the certificate to alter a product, the holder must give the other person written evidence of that permission. Certification Basis: The Certification Basis for Configurations A, B and C are defined as: 1. The type certification basis for Pilatus PC-12 -12/45, -12/47 Series as shown on TCDS A78EU for parts not changed or not affected by the change. 2. Title 14 CFR Part 23, dated February 1, 1965, including Amendments 23-1 through 23-54 for the change and all areas affected by the change. The following lists the Federal Aviation Regulations complied with through Amendment Level 23-54. 23.301 23.303 23.305 23.307 23.321 23.331 23. 333 23.335 23.337 23.341 23.561 23.603 23.607 23.613 23.619 23.625 23.771 23.773 23.777 23.1301 23.1303 23.1309 23.1311 23.1321 23.1322 23.1323 23.1327 23.1331 23.1351 23.1353 23. 1357 23.1359 23.1361 23.1365 23.1367 23.1381 23.1431 23.1501 23.1523 23.1529 23.1541 23. 1543 23.1545 23.1555 23.1581 23.1583 23.1585 ---END--- ## Every issue (4) - April 7, 2009: Amended, Current. [certificate](https://openairdocs.org/files/sha256/69/bf/69bf87c2c118fd3192d05d72410a2c57a825c4047f46fb2e9e1223f0f6da8768) - June 19, 2007: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/e0/df/e0df9a004594746d334e7230780eab32f37bca6d30dd558deca9a43fb45d555c) - September 13, 2006: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/e2/57/e25761e146241d5030d6be8e93fbe1a3ad13da1a93d6f1a310b5cdf418997b7d) - May 2, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/d7/40/d7404ad4701c2cbcdec6feb7a0d74fdc289d19544c65f66535804a1c86e35a9c) --- 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.