STC SE1206GL

Supplemental type certificate · Shadin Avionics

Holder
Shadin Avionics · United States
Status
Current · Reissued
Status date
June 8, 2006
Applied
March 18, 1986
Product
Engine
Certification basis
Part 21
Data sheet
TCDSTC 5E-14

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 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.

FAA Specification 5E-14 .

(See Type Certificate Data Sheet 5E-14 for complete certification basis.)

Installation of a Shadin Company Fuel Flow Transducer in accordance with Shadin Company report number 4099, dated March 18, 1986, or later FAA approved revision.

1) 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 modifications will introduce no adverse effect on the airworthiness of these engines.

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 5E-14 Make : Wright Model : Military Cyclone R-1300-1A, -1B, -3, -3A, -3B, -3C, -3D Date of application : March 18, 1986

Date of issuance : July 17, 1987

Date reissued : June 8, 2006

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

( Title)

ADs that name this STC · 0

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No AD in this release names this STC

Approved models · 1

MakeModelData sheet
Wright Aeronautical Division Curtiss-Wright CorporationMilitary Cyclone R-1300 SeriesTC 5E-14