STC SE765GL

Supplemental type certificate · Shadin Avionics

Holder
Shadin Avionics · United States
Status
Current · Reissued
Status date
June 8, 2006
Applied
May 8, 1984
Product
Engine
Certification basis
Part 21, Part 33
Data sheet
TCDSE19EA

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

What it approves

Installation of a fuel flow transducer.

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.

This certificate issued to

Part 33 of the Federal Aviation Regulations. (See Type Certificate Data Sheet E19EA for complete certification basis.)

Description of Type Design hange:

Installation of a Fuel Flow Transducer in accordance with Shadin Report 4061, revised March 30, 1984, or subsequent FAA approved revision.

Limitations and Conditions: This approval should not be extended to other engines of this model that incorporate any other previously approved modification, unless it is determined that the interrelationship between this change and any other previously approved modification will introduce no adverse effect upon the airworthiness of these engines.

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.

Shadin Avionics 6831 Oxford Street St. Louis Park, MN 55426 E19EA Make : AVCO Lycoming Model : TIGO-541-E1A

Date of application : January 3, 1984

Date of issuance : May 8, 1984

Date reissued : June 8, 2006

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

( Title)

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
Textron Lycoming AVCO CorporationTIGO-541-E1AE19EA