STC SA1346GL

Supplemental type certificate · Shadin Avionics

Holder
Shadin Avionics · United States
Status
Current · Reissued
Status date
June 8, 2006
Applied
July 5, 1988
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23
Data sheet
TCDSA51EU

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of a Shadin Company Digital Fuel Flow Indicating 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 A51EU for complete certification basis.)

Installation of a Shadin Company Digital Fuel Flow Indicati ng System in accordance with Shadin Company Report Number 4108, revised August 29, 1988, or later FAA approved revision.

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 other previously approved modifications will introduce no adverse effect upon the airworthiness of the aircraft.

2) 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 A51EU Make : S.O.C.A.T.A Model : TB20, TB21

Date of application : July 5, 1988

Date of issuance : December 16, 1988

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 · 2

MakeModelData sheet
SOCATA - Groupe AerospatialeTB20A51EU
SOCATA - Groupe AerospatialeTB21A51EU