# STC SA10465SC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Corporate Aircraft Inc, United States
- Description: Installation of dual Thommen, model AD32E, air data display units (ADDU).
- Applied: October 25, 2004
- Status date: February 20, 2007
- 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/c1/9c/c19c8e6705d28d2407d307db166038552341e8a6addc462a07dcaeeb6b657557
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/55E161376537B5AC8625733D00500573.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA10465SC

## 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.

This Certificate issued to Ross Fresno LLC d/b/a Corporate Aircraft 4885 East Shields Fresno, California 93726 Part 23* of the Federal Aviation Regulations. *Certification basis is set forth in Type Certificate Data Sheet A28CE Original Product Type Certificate Number :

A28CE

Cessna Aircraft Company

441 Series Description of Type Design Change: Installation of dual Thommen, Model AD32E, Air Data Display Units (ADDU) in accordance with -01 and -02 configurations or single Shadin ADC-6000L and single Thommen, Model AD32E, Air Data Display Unit (ADDU) in accordance with -03 configuration of Corporate Aircraft Inc., “Master Data List for Installation of Improved Altimeter Systems in Cessna Model 441 Aircraft”, Document Number PAD569-002, DOC, Revisi on L, dated October 16, 2006, or later FAA approved Airplane Flight Manual S upplement (AFMS) Document Number PAD 569-013 DOC, Revision A, dated April 27, 2006, or later FAA approved revision is required. For -03 configuration FAA Approved AFMS Document Number CA569-030 DOC, Revision IR, dated December 6, 2006, or later FAA approved revision is required.

Limitations and Conditions: This approval should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. 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 25, 2004

Date of issuance : October 3, 2005

Date reissued : December 14, 2005, February 20, 2007

Date amended : December 20, 2006

( Signature) Manager, Technical and Administrative Support Los Angeles Aircraft Certification Office ( Title)

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

Number

## Every issue (3)

- February 20, 2007: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c1/9c/c19c8e6705d28d2407d307db166038552341e8a6addc462a07dcaeeb6b657557)
- December 14, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/aa/25/aa255a67ebf156f5b821ba9b4b5a16d82acd0614a42bec5536dccc398758330c)
- October 3, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/99/49/99496141c1f5875997640593812d67befaacb736cce44cd3e8226a6dd03d9b11)

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