# STC SA02076CH-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: Standard Aero, United States - Description: Installation of a Rockwell Collins IDS-3000 Integrated Display System in accordance with Garrett Aviation Services Drawing List #1003286, Revision B, dated May 10, 2005 or later FAA approved revision. - Applied: August 11, 2004 - Status date: January 8, 2009 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS A27CE](https://openairdocs.org/tcds/A27CE) - Certificate PDF: https://openairdocs.org/files/sha256/59/f0/59f0abb34f0e4fcfa25dfbe324b0e701ec86c7d12485e15aa6eefa6ded8c445d - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/33997BC9541EE57186257632004DBFB5.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02076CH-D ## ADs that name it (0) None. ## Approved models (1) - The Cessna Aircraft Company 501 ([TCDS A27CE](https://openairdocs.org/tcds/A27CE)) ## 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: SA02076CH-D This certificate issued to: Standard Aero 1200 North Airport Drive Springfield, IL 62707 Part 23 of the Federal Aviation Pegulations. See Type Certificate Data Sheet A27CE as amended by Special Condition No. 25-286-SC, dated February 16, 2005, Docket No. NM302 for complete certification basis. Original Product Type Fertificate Number: A27CE Make: Cessna Aircraft Company Model: 501 Description of Type Design Change: Installation of a Rockwell Collins IDS-3000 Integrated Display System in accordance with Standard Aero Master Data List #1003286, Revision "I", dated December 31, 2008 or later FAA approved revision. Limitations and Conditions: FAR140 1. Compatibility of this design change with previously approved modifications must be determined by the installer. 2. FAA Approved Airplane Flight Manual Supplement document #1003290 revision "B" dated July 26, 2005, or later FAA approved revision is a required part of this modification for configuration 01 with single AHRS 1000S. 3. FAA Approved Airplane Flight Manual Supplement document #1009274 revision "A" dated December 25, 2005, or later FAA approved revision is a required part of this modification for configuration 02 4. FAA Approved Airplane Flight Manual Supplement document #1008624 revision "A" dated May 19, 2005, or later FAA approved revision is a required part of this modification for aircraft incorporating the optional IFIS-5000 installation. 5. FAA Approved Airplane Flight Manual Supplement document #1016257 revision "A" dated January 07, 2009, or later FAA approved revision is a required part of this modification for configuration 01 with dual AHRS 3000S. 6. FAA Approved Airworthiness Limitations document #1008334 revision "B" dated December 25, 2005, or later FAA approved revision is a required part of this modification. 7. 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. Limitations and Conditions: continued on page 3 of 3) suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of Application: August 11, 2004 Date Reissued: March 13, 2008 Date of Issuance: May 19, 2005 Date Amended: December 25, 2005, March 14, 2008, January 8, 2009 FEDERAL AVIATION By Direction of the Administrator (Signature) for Tim Winiesdorffer, DAS Administrator TOMINISTRATO Standard Aero, Springfield, IL DAS-100079-CE (Title) tion of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. sportation - Federal Aviation A: nistration Supplemental Type Certificate (Continuation Sheet) Supplemental Type Certificate Number: SA2076CH-D Date of Issuance: May 19, 2005 Dale of amendment: January 8, 2009 Date of reissue: March 13, 2008 Certification Basis: Based on 14 CFR ยงยง 21.15, 21.101 and the FAA policy for significant/non-significant changes in FAA Order 8110.48, the certification basis for the Cessna Aircraft Company, 501, installation of the Rockwell Collins IDS-3000 Integrated Display System is as follows: a. The type certification basis for Cessna Aircraft Company 501 shown on TCDS A27CE for parts changed or affected and for parts not changed or not affected by the change. Regulations at the amendment level in TCDS A27CE applicable to this installation, amendment 23-1 through 23-16, and specific regulations of Part 25, amendment 25-1 through 25-37 23.1, 23.29(a, b), 23.301(a, b), 23.303, 23.305(a, b), 23.307(a), 23.603(a, b), 23.605, 23.609(a, b), 23.611, 23.613(a-c), 23.615(a), 23.619, 23.625(a), 23.1301(a1, a2, a3, a4, b), 23.1307(b, b3), 23.1309(a, a2, b), 23.1327(a, b), 23.1329(e, f), 23.1351(a, b1), 23.1357(a-d), 23.1365(a, b), 23.1367(a, c, d), 23.1431, 23.1501(b), 23.1529(a-k), 23.1541(a-d), 25.1581(a-c), 25.1585(a, b). END ## Every issue (3) - January 8, 2009: Amended, Current. [certificate](https://openairdocs.org/files/sha256/59/f0/59f0abb34f0e4fcfa25dfbe324b0e701ec86c7d12485e15aa6eefa6ded8c445d) - March 13, 2008: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/e1/53/e1534da4e66fe6b5b19c24d96891095173f3d90e8359173d327fb84ff7efb679) - May 19, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/fd/c5/fdc58cbb3b386059564e799ec912ff5a60ebc6c2ade8439ca90e5bc087448221) --- 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.