# STC SA1004CE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Williams Robert or Barbara, United States
- Description: Install STOL kit.
- Status date: August 28, 1985
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 5A6](https://openairdocs.org/tcds/5A6)
- Certificate PDF: https://openairdocs.org/files/sha256/f3/5b/f35b4eac93ac7cd9f6ac29bc577c81875c461293d35d27f0e82a78408fd82201
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/34310757DDDFE62E85256CC10080DC04.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1004CE

## ADs that name it (0)

None.

## Approved models (11)

- The Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180G ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- The Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6))

## What the certificate says

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

Anita State of alone Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number I SA1004CE This certificate issued to: Bob or Barbara Williams P. 0. Box 608 Udall, Kansas 67146 lary Regulations SA6 Make i Cessna Madel 180, 180A, B, C, D. E, F, G. & H Lesortion flype Desig lahange Install STOL Kit (wing leading edge cuffs, wing tipso upper surrace flow. ences and al eron gap seals in accordance with and data called out on FAA approved copy of martin Machining Drawing List No. 180.

Similaliens and Conditimis This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the anterrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworth ness ofithat airplaned Parts manufactured under this STC may have been produced without an FAA approved quality control procedure Prior to installation, such parts must be inspected for conformity and airworthiness in accordance with FAR's ?l and 43.

This certificate and the supportiny da lie ches the base fir apiperivă un in ofeil antil sur rendered, suspended, verned, in a te rise established by the Adiminis triker of the Fileral Shiralin SIdenistralum Datarapplications January 25, 1973 Sal resid April 24, 1979 Saty emanc March 19, 1974 Dalend September 9. 1974 FEDERAL STATIO By gricken of the Eldenistrter Laurence A Messn (Signufure) TASTER NO A BARRY D. CLEMENTS Chief. Vichita Engr. & mfor District Office A Title) bl exceeding 3 yeers, or both This certificate may be transferred in accordance with FAR 21.97 FAA FOR 8110-2 (10-651

## Every issue (1)

- September 9, 1974: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/f3/5b/f35b4eac93ac7cd9f6ac29bc577c81875c461293d35d27f0e82a78408fd82201)

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