# STC SA5262NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Otto E. Bartoe Jr., United States
- Description: Installation of the Skyote Gap Flap System.
- Applied: August 12, 1991
- Status date: October 26, 2011
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A24](https://openairdocs.org/tcds/3A24)
- Certificate PDF: https://openairdocs.org/files/sha256/0e/42/0e424e045ad95f2855588be58a4118ea0011b77aa64b7a7d6605bb0bc4de4325
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8A0F27C7E4562F2A8625793E00670DA4.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5262NM

## ADs that name it (0)

None.

## Approved models (7)

- Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185A ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185B ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185C ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company 185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company A185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- Cessna Aircraft Company A185F ([TCDS 3A24](https://openairdocs.org/tcds/3A24))

## 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.

This certificate issued to: Otto E. Bartoe Jr.

57980 CR 62 Clark, CO 80428

Part 3 of the Civil Air Regulations.

Original Product - Type Certificate Number : 3A24 Make : Cessna Model : 185, 185A, 185B, 185C, 185E, A185E, A185F

Installation of the Skyote Gap Flap System in accordance with Skyote Aeromarine Top Drawing No. 9100, Rev. D, dated August 31, 1992, and Installation Instructions Report No. 001, Rev. N/C, dated August 31, 1992, or later FAA approved revisions.

1. FAA Approved Skyote Aeromarine Airplane Flight Manual Supplement No. FMS-01, dated September 1, 1992, or later FAA Approved revision is a required part of this STC.

2. This approval should not be exte nded to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship 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.

Date of application : August 12, 1991 Date of issuance : September 1, 1992 Date reissued : October 26, 2011

Date amended : April 4, 1994

( Signature) Todd Dixon Manager, Denver Aircraft Certification Office (Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

## Every issue (2)

- October 26, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0e/42/0e424e045ad95f2855588be58a4118ea0011b77aa64b7a7d6605bb0bc4de4325)
- April 4, 1994: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/7e/68/7e6890860bb1daa5e6384a098361096d85f1213012e3442322b41e6112763cba)

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