Supplemental type certificate · Standard Aero

Holder
Standard Aero · United States
Status
Current · Amended
Status date
January 8, 2009
Applied
August 11, 2004
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21
Data sheet
TCDSA27CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

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.

What the certificate saysOCR

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 §§ 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

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
The Cessna Aircraft Company501A27CE

Every issue · 3

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
January 8, 2009Amended, currentCertificate
March 13, 2008Reissued, earlier issueCertificate
May 19, 2005Issued, earlier issueCertificate