# STC SA00737DE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Pilatus Business Aircraft Ltd, United States - Description: Installation of Flight Display Cabin Entertainment System - Applied: October 28, 2011 - Status date: November 20, 2012 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU) - Certificate PDF: https://openairdocs.org/files/sha256/5f/ef/5fef023e98ce29465e637133355f073000324dcc361ecdb1382690f9693f723e - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DB9FE800D70535C0862580880076A2AC.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00737DE ## ADs that name it (0) None. ## Approved models (4) - 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)) - Pilatus Aircraft Limited PC-12/47E ([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. 11755 Airport Way Broomfield, Colorado 80021 Part 23* of the F ederal A viation R egulations. *See continuation Page 3 Original Product - Type Certificate N umber : A78EU M ake : Pilatus Aircraft Ltd. M odel : PC-12/47E Description of Type Design Change : Installation of Flight Display Cabin Entertainment System in accordance with Pilatus Business Aircraft Ltd. Master Drawing List, Report No. PBA.600.118, Revision I, dated 11/14/2012 or later FAA approved revision. A copy of this certificate and FAA Approved Airplane Flight Manual Supplement Document number PBA.323.032, Rev IR, dated 9/10/2012 or later FAA approved revision must be maintained as part of the aircraft permanent records. Instructions for Continued Airworthiness (ICA), Document No. PBA.323.031 Rev D, dated 8/2/2012 or later FAA accepted revision must be made available to the operator at the time of installation. 1. Compatibility of this design change with previously approved 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 the permission. 3. Approval of this change in type design applies to the above model of airplane only. Date of application: October 28,2011 Date reissued: Date of issuance: November 20,2012 Date amended : B y direction of the A dministrator (Signature) John May ODA Administrator ODA 636304-NM ASES, LLC d/b/a ARINC Aerospace (Title) TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number & street) (City, State, and ZIP code) Extent of Authority (if licensing agreement ) : Signature of grantor (In ink): N umber SA00737DE (Date of Issuance: November 20, 2012) Certification B asis: The certification basis for this modification is as follows: In accordance with Type Certificate Data Sheet, A78EU, Rev 20, dated September 14, 2010; For model PC-12/47E, certification basis is 14 CFR 23, Normal Category, effective February 4, 1991, including Amendments 23-1 through 23-42 and additional 14 CFR 23 paragraph and amendment levels. Regulation at the amendment level in TCDS A 78EU 23.29(a) [Amdt 23-21], 23.301 [Amdt 23-48], 23.303 [Amdt Original], 23.305(a) [Amdt 23- 45], 23.307(a) [Amdt Original], 23.601 [Amdt Original], 23.603 [Amdt 23-23], 23.605(a) [Amdt 23-23], 23.607(c) [Amdt 23-48], 23.609 [Amdt Original], 23.611 [Amdt 23-7],23.613 [Amdt 23-45], 23.625 [Amdt 23-7], 23.627 [Amdt Original], 23.1301(a) (b) (c) (d) [A mdt 23-20], 23. 1309(a) [Amdt 23-41], 23.1322(e) [Amdt 23-43], 23.1351(a) (d) [Amdt 23-34], 23.1357(b) (c) (d) [Amdt 23-20], 23.1357(a) [Amdt 23-43], 23.1359(c) [Amdt 23-49], 23.1365(a) [Amdt 23-14], 23.1365(b) (d) (e) [Amdt 23-49], 23.1367(a) (b) (c) (d) [Amdt Original], 23.1381 [Amdt Original], 23.1431(b) (d) (e) [Amdt 23-49], 23.1529 [Amdt 23-26], 23.1541(a) (b) [Amdt 23-21], 23.1581(a) (b) (d) [Amdt 23-34], 23.1585(a) [Amdt 23-34] Regulations at an intermediate amendment 23.571(c) [Amdt 23-48] Regulations at the latest amendment 23-0 through 23-62 23.305(b) [Amdt 23-45], 23.573(b) [Amdt 23-48], 23.575 [Amdt 23-48], 23.607(a)(b) [Amdt 23-48], 23. 1322(d) [Amdt 23-43] ----------------------------------------------------------------------END---------------------------------------------------------------------- ## Every issue (1) - November 20, 2012: Issued, Current. [certificate](https://openairdocs.org/files/sha256/5f/ef/5fef023e98ce29465e637133355f073000324dcc361ecdb1382690f9693f723e) --- 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.