# STC SA02327CH-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: Rockwell Collins Inc, United States - Description: Installation of a Rockwell Collins, Inc. Pro Line 21 Integrated Display System (IDS). P-180 serial numbers prior 1105. - Applied: April 25, 2006 - Status date: February 9, 2010 - Product: Aircraft, Single-Engine - Certification basis: Part 21 - Data sheets: [TCDS A59EU](https://openairdocs.org/tcds/A59EU) - Certificate PDF: https://openairdocs.org/files/sha256/7c/bd/7cbd40f342118627ccdeaf20609d097f3f809668fbf2516fc0c4fc01c2ec4add - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6A1F9488C72710E8862576F600778017.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA02327CH-D ## ADs that name it (0) None. ## Approved models (1) - Piaggio Aero Industries S.p.A. P-180 ([TCDS A59EU](https://openairdocs.org/tcds/A59EU)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA02327CHD This certificate issued to: Rockwell Collins, Inc. 400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 furt 23 of the Federal Aviation Repututions. (see sheet 2 for complete certification basis) Original Product Type Certificate Vuter : A59E0 • Madr.: Piaggio Aero Industries S.p.A. Model: P-180 serial numbers prior to 1105 Description of Type Design Change: Installation of a Rockwell Collins, Inc. Pro Line 21 Integrated Display System (IDS) in accordance with Rockwell Collins, Inc. Master Data List JW2121A-3425-01, Revision B. dated October 15, 2006, or later FAA approved revision. (1) Installation of Jet Works Air Center STC, SA02326CH, (Installation of a dual Rockwell Collins, Inc. AHS-1000A Attitude Heading Reference Systems) is to be installed concurrent with this STC. (2) Compatibility of this design change with previously approved modifications must be determined by the installer. (3) FAA Approved Flight Manual Supplement, Rockwell Collins, Inc. Document JW2121A-3425-100, Revision A. dated November 2, 2006, or later FAA approved revision, is a required part of this STC. (4) FAA Approved Flight Manual Supplement, Rockwell Collins, Inc. Document JW2121A-3425-101, Revision -, dated September 21, 2006, or later FAA approved revision, is a required part of this STC when the optional Rockwell Collins, Inc. IFIS-5000 Integrated Flight Information System (IFIS) is installed (5) The aircraft must be maintained in accordance with Airworthiness Limitations contained in Rockwell Collins. Inc. document JW2121A-3425-200, Revision -, dated August 30, 2006, or later FAA approved revision, in addition to (6) 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 that permission. Late r/ appfication : April 25,2006 Lude prared January 4, 2007 Lute of insurre : September 22. 2006 Cafe chended: February February 2010 AVIATION By Direction of the Administrator Mean 15com TOMINSTRATO (Signature) Steven P. Brune Administrator, ODA-500864-CB (Title) or imprisonnent not exceeding 3 years, or both FAA PORA 8310-2(10-68) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA02327CH-D Certificatien Basis: Based on 14 CFR §$ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Piaggio Aero Industries S.p.A. Model P-180 is as follows: (1) The type certification basis for Piaggio Aero Industries S.p.A. Model P-180 is shown on TCDS A59EU for parts not changed or not affected by the change. (2) The certification basis for parts changed or affected by this change since the reference date of application, April 25, 2006, is as follows at the latest amendment 23-0 through 23-55: 14 CFR Part 14 CFR Part 14 CFR Part 23.301 (a)(b) 23.625 (a) 23.1357 (a)(b)(c)(d) 23.303 23.777 (a)(b) 23.1359 (b) 23.305 (a)(b) 23.867 (a)(b) 23.1365 23.307 (a) 23.1301 (a)(b)(c)(d) 23.1367 23.365 (a)(b)(c)(d) 23.1303 (a)(b)(c)(e)(1) 23.1381 23.561 (a)b)(e) 23.1307 23.1431 (a)(b)(e) 23.571 (c) 23.1309 (a)(b)(c)(d)(e)(f) 23.1501 23.573 (b) 23.1311 (a)(b) 23.1529 23.575 23.1321 (a)(c)(d)(e) 23.1541 (a)(b) 23.603 (a)(b) 23.1322 23.1543 (b) 23.605 (a) 23.1323 (a)(c) 23.1545 (a)(b) 23.607 (b) 23.1325 (6)(1) 23.1547 23:609 (a)(b) 23.1327 (a) 23.1581 23.611 23.1331 (a)(b) 23.1583 (m) 23.613 (a)(b)(d) 23.1335 23.1585 (a)u) 23.619 23.1351 (a) - - END--- PAA PORE 8110-2-1(10-69) PACE 2 Of 2 PAGES ## Every issue (1) - February 9, 2010: Amended, Current. [certificate](https://openairdocs.org/files/sha256/7c/bd/7cbd40f342118627ccdeaf20609d097f3f809668fbf2516fc0c4fc01c2ec4add) --- 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.