STC SA02282CH

Supplemental type certificate · Rosemount Aerospace Inc

Holder
Rosemount Aerospace Inc · United States
Status
Current · Issued
Status date
May 31, 2006
Applied
August 24, 2005
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23
Data sheet
TCDSA37CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of Rosemount Aerospace Advisory Ice Detector System

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Part 23 of the Federal Aviation Regulations. (See Page 3 of 3 for complete certification basis.)

Installation of Rosemount Aerospace Advisory Ice Detector System in accordance with Rosemount Aerospace Master Data List, Doc. No. D06400453, Revision A, dated May 26, 2006, or later FAA approved revision.

1) Compatibility of this design change with previously approved modifications must be determined by the installer.

2) FAA Approved Airplane Flight Manual Supplement, Rosemount Aerospace Doc. No. FMS367002, Revision 2, dated February 22, 2006, approved May 30, 2006, or later FAA approved revision, is required on board the modified aircraft.

3) 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.

Rosemount Aerospace, Inc.

14300 Judicial Road Burnsville, MN 55306-4898 A37CE Make : Cessna Model : 208B Date of application : August 24, 2005

Date of issuance : May 31, 2006

( Signature) Charles L. Smalley Manager, Systems and Flight Test Branch Chicago Aircraft Certification Office

( Title)

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Number SA02282CH

Date of issuance : May 30, 2006

Certification Basis:

The certification basis for the changed Cessna 208B as described in this certificate is as follows:

a. The type certification basis for the Cessna 208B is shown on TCDS A37CE for parts not changed or not affected by this change.

b. The certification basis for the parts changed or affected by this change since the reference date of application, August 24, 2005, is shown on TCDS A37CE. In addition, the applicant has voluntarily complied with 14 CFR Part 23 as amended through Amendment 23-55.

Regulations at the latest amendment 23-0 through 23-55

23.1301(a)-(d); 23.1309(a), (b), (d), (g); 23.1321(c), (e); 23.1322(b), (d), (e); 23.1351(a); 23.1357(a), (c), (e); 23.1365(a)-(f);

23.1381(a)-(c); 23.1431(a)-(b).

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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
Cessna Aircraft Company208BA37CE