STC SA83CH

Supplemental type certificate · Shadin Avionics

Holder
Shadin Avionics · United States
Status
Current · Reissued
Status date
June 8, 2006
Applied
April 9, 1993
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 6, 2025.

What it approves

Installation of a Shadin engine trend monitor 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 Type Certificate Data Sheet No. A37CE for complete certification basis.)

Installation of a Shadin Engine Trend Monitor System per Shadin Report 3258, dated March 24, 1993, or later FAA approved revisions.

1) This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft..

2) FAA Approved Airplane Flight Manual Supplement dated July 7, 1993, or later FAA Approved revision is required.

Shadin Avionics 6831 Oxford Street St. Louis Park, MN 55426 A37CE Make : Cessna Model : 208, 208A, 208B Date of application : April 9, 1993

Date of issuance : July 7, 1993

Date reissued : June 8, 2006

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

( Title)

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

Number SA83CH

Date of issuance : June 8, 2006

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.

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Approved models · 3

MakeModelData sheet
Cessna Aircraft Company208A37CE
Cessna Aircraft Company208AA37CE
Cessna Aircraft Company208BA37CE