# STC SA02439SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Fidelitad, Inc., United States - Description: Structural provisions for carrying external load attached to the wing strut/fuselage interface - Applied: August 5, 2013 - Status date: January 3, 2018 - Product: Aircraft, Small Airplane - Certification basis: Part 3, Part 21 - Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13) - Certificate PDF: https://openairdocs.org/files/sha256/75/c7/75c70bc7fcfecc574537e56f0de27193cc065f3e32a5d5eec1282c4dddd292cb - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/28208BF77F6A9BCE86258218004A97D6.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA02439SE ## ADs that name it (0) None. ## Approved models (8) - Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) - Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can 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) ## Every issue (2) - January 3, 2018: Amended, Current. [certificate](https://openairdocs.org/files/sha256/75/c7/75c70bc7fcfecc574537e56f0de27193cc065f3e32a5d5eec1282c4dddd292cb) - May 29, 2015: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/e9/57/e957b8988db72c4c98e65dc0885372d23d8e5ce61af3d6b7a17402c58d1c83b7) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.