# STC SA01968SE-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Corporate Aircraft Inc, United States
- Description: Certification of Reduced Vertical Separation Minimum (RVSM) Equipment Installation using a single or dual Garmin G600 system in accordance with Master Data List document CA600-100, Revision IR, dated 08 April 2011 or later FAA-approved revisions.
- Applied: October 21, 2010
- Status date: April 11, 2011
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A28CE](https://openairdocs.org/tcds/A28CE)
- Certificate PDF: https://openairdocs.org/files/sha256/f2/2c/f22cb66c6e76dd65f2d7fd12a66a814f6a0170218ea34b462b4eebaa2a20e5c9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7CEC64103B7ED9E08625788B0048146A.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01968SE-D

## ADs that name it (0)

None.

## Approved models (1)

- Cessna Aircraft Company 441 ([TCDS A28CE](https://openairdocs.org/tcds/A28CE))

## 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.

United States of America Department of Transportation – Federal Aviation Administration Supplemental Type Certificate Number SA01968SE-D This Certificate issued to: Corporate Aircraft 4885 E. Shields Fresno, CA 93726 Part 23 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: A28CE Make: Cessna Model: 441 Description of Type Design Change:

Certification of Reduced Vertical Separation Minimum (RVSM) Equipment Installation using a single or dual Garmin G600 system in accordance with Master Data List document CA600-100, Revision IR, dated 08 April 2011 or later FAA-approved revisions.

1. The installer must determine whether this desi gn change is compatible with previously approved modifications.

2. Previously approved installation of a single Ga rmin G600 with GDC 74B air data computer or a dual Garmin G600 with two GDC 74B air data computers is a prerequisite for this certification.

3. This certification is only applicable to Cess na Model 441 aircraft with the Cessna 1000 Autopilot system.

4. The Instructions for Continued Airworthiness document CA600-103, Revision A, dated 24 March 2011 or later FAA-accepted revision is required for this certification.

5. A copy of the FAA-approved Airplane Fli ght Manual Supplement (AFMS), document CA600-104, Revision IR, dated April 8, 2011, or later FAA-approved revision for the single Garmin G600 or document CA600-106, Revision IR, dated April 8, 2011, or later FAA-approved revision for the dual Garmin G600 is required on board for operation of the aircraft.

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.

Date of application: October 21, 2010 Date reissued:

Date of issuance: April 11, 2011 Date amended:

(Signature) ODA Administrator (Title)

United States of America Department of Transportation – Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA01968SE-D

Certification Basis:

The certification basis for the changed Cessna Model 441 as described in this certificate is as follows:

a. The type certification basis for the Cessna Model 441 aircraft is shown on TCDS A28CE for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by this change since the reference date of application, 21 October 2010, is based on 14 CFR part 23 as amended by Amendment 23-59.

-------------------------------END-------------------------------

FAA Form 8110-2.1(10-69) Page 3 of 3

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## Every issue (1)

- April 11, 2011: Issued, Current. [certificate](https://openairdocs.org/files/sha256/f2/2c/f22cb66c6e76dd65f2d7fd12a66a814f6a0170218ea34b462b4eebaa2a20e5c9)

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