STC SA02439SE

Supplemental type certificate · Fidelitad, Inc.

Holder
Fidelitad, Inc. · United States
Status
Current · Amended
Status date
January 3, 2018
Applied
August 5, 2013
Product
Aircraft · Small Airplane
Certification basis
Part 3, Part 21
Data sheet
TCDS3A13

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

What it approves

Structural provisions for carrying external load attached to the wing strut/fuselage interface

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.

Un ited S tates of Am erica Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number SA02439SE

This certificate, issued to Fidelitad, Inc.

801 Panorama Court P.O. Box 688 White Salmon, WA 98672

Part 3 of the Civil Air Regulations.

Original ProductType Certificate Number: 3A13 Make: Textron Aviation Inc.

Model: 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M

Description of the Type Design Change: Structural provisions for carrying external load attached to the wing strut/fuselage interface in accordance with Fidelitad, Inc. Master Drawing List Document DM1319-3, Revision IR, dated August 5, 2014, or later Federal Aviation Administration (FAA) approved revision. This modification must be operated in accordance with Fidelitad, Inc. Flight Manual Supplement FCL182-FMS-001, Revision B, dated April 5, 2015, or later FAA-approved revision. This modification must be maintained in accordance with Fidelitad, Inc. Instructions for Continued Airworthiness (ICA) Report FCL182-ICA-001, Revision IR, dated April 5, 2015, or later FAA-approved revision.

Limitations and Conditions: This provisions-only approval does not authorize any equipment installation on the mounting bracket. Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of this model series unless the installer determines that the relationship between this change and any other previously incorporated approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate and ICA must be maintained as part of the permanent records for the modified aircraft.

Date of application: August 5, 2013 Date reissued:

Date of issuance: May 29, 2015 Date amended: January 3, 2018

FAA FORM 8110-2 (5/14) PAGE 1 OF 2 PAGES

(Signature)

Manager, Seattle ACO Branch (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 · 8

MakeModelData sheet
Cessna Aircraft Company182E3A13
Cessna Aircraft Company182F3A13
Cessna Aircraft Company182G3A13
Cessna Aircraft Company182H3A13
Cessna Aircraft Company182J3A13
Cessna Aircraft Company182K3A13
Cessna Aircraft Company182L3A13
Cessna Aircraft Company182M3A13

Every issue · 2

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

DateStatusFiles
January 3, 2018Amended, currentCertificate
May 29, 2015Issued, earlier issueCertificate