STC SA00068SE

Supplemental type certificate · Electronics International Inc.

Holder
Electronics International Inc. · United States
Status
Current · Amended
Status date
October 20, 2010
Applied
November 1, 1993
Product
Aircraft · Single-Engine
Certification basis
Part 11, Part 21

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

What it approves

Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1)

What the certificate saysOCR

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Book Supplemental Type Certificate sent to Connie Duplicate Original to replace lost STC Number: SA00068SE This certificate issued to: Electronics International, Inc.

63296 Powell Butte Highway Bend, OR 97701 Part * of the * Regulations.

Original Product -Type Certificate Number: *See attached FAA Approved Model List (AML) Make: No. SA00068SE for a list of approved airplane Model: models and applicable airworthiness regulations.

Description of Type Design Change: Electronics International fuel flow/pressure instrument manufactured and installed in accordance with the drawings and installation instructions specified on the FAA AML of this STC, or later FAA approved revision.

NOTE: The instrument approved by this STC is to be used as a secondary instrument only. This approval does not allow the removal of any original equipment instrumentation. See the continuation sheet for required placards Limitations and Conditions: Approval of this change in type design applies to the airplanes and factory installed or ST'd float combinations listed on the AML only. 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 relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate, Continuation Sheet, and AML must be maintained as part of the permanent records for the modified aircraft.

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.

Date of Application: November 1, 1993 Date Reissued: October 15, 2002 Date of Issuance: March 31, 1994 Date Amended: October 15, 2002 FEDERAL AVIATION tion of the Administrator (Signature) TOMINSTRATION Acting Manager, Seattle Aircraft Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00068SE Electronics International, Inc.

Reissued: October 15, 2002 Amended: October 15, 2002 Limitations and Conditions: (cont 'd/ The following placards must be located on the instrument panel adjacent to the Electronics International fuel flow/pressure instrument approved by this STC:

For all aircraft models:

"DO NOT RELY ON FUEL FLOW INSTRUMENT TO DETERMINE FUEL LEVELS IN TANKS" For aircraft originally equipped with fuel flow and/or pressure instruments:

"REFER TO ORIGNAL FUEL FLOW/PRESSURE

- END - 47 FAA FORM 8110-2(10-68) Page 3 of 3 Pages

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 · 1,042

MakeModelData sheet
Aermacchi S.p.A.F.260A10EU
Aermacchi S.p.A.F.260BA10EU
Aermacchi S.p.A.F.260CA10EU
See all 1,042 models

Every issue · 3

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
October 20, 2010Amended, currentCertificateApproved model list
October 19, 2010Amended, currentCertificateApproved model list
October 15, 2002Reissued, earlier issueCertificate