STC SA608GL

Supplemental type certificate · Shadin Avionics

Holder
Shadin Avionics · United States
Status
Current · Reissued
Status date
June 8, 2006
Applied
November 14, 1981
Product
Aircraft · Small Multi-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDS1A10

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

What it approves

Installation of a Shadin Co. 910502 or 910504 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 3 of the Civil Air Regulations.

(See Type Certificate Data Sheet 1A10 for complete certification basis.)

Installation of a Shadin Company 910502 or 910504 Fuel Flow Indicating System in accordance with Shadin Company Report Number 4030 revised February 2, 1982, or subsequent FAA approved revision.

1) This approval should not be extended to other airplanes 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 on the airworthiness of these airplanes.

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 1A10 Make : Piper Aircraft, Inc.

Model : PA-23-250, PA-E23-250, Serial Numbers 27-2000 and up

Date of application : November 14, 1981 Date of issuance : May 13, 1982

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
Piper Aircraft Inc.PA-23-250 (Navy UO-1)1A10
Piper Aircraft Inc.PA-E23-2501A10