# STC SA4-1484

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Everitt Robert B, United States
- Description: Modify wings using sheet metal in place of fabric
- Applied: April 7, 1960
- Status date: May 1, 1961
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A-767](https://openairdocs.org/tcds/A-767)
- Certificate PDF: https://openairdocs.org/files/sha256/f0/34/f03493216bbb0becbf83dcf90f29fd3a1640ff27e24bdae8a8d2606d3956f8ee
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E274C7FCCCFA9AEA86257D9B004E15B0.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA4-1484

## ADs that name it (0)

None.

## Approved models (1)

- Univair Aircraft Corporation 108 ([TCDS A-767](https://openairdocs.org/tcds/A-767))

## What the certificate says

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

FS -4102

FEDERAL AVIATION AGENCY Supplemental Type Certificate

1. NAME AND ADDRESS OF APPLICANT Robert B. Everitt 2134 Xavier Santa Clara, Calif.

**FORM APPROVED, BUDGET BUREAU NO. 04-R015**

**INSTRUCTIONS - SUBMIT IN TRI FLICATE TO LOCAL FAA FLIGHT STANDARDS INSPECTOR.**

**COPY WILL BE RETURNED TO APPLICANT UPON**

ISSUANCE Supplemental Type Certificate APPLIED FOR:

**AIRCRAFT ENGINE PROPELLER**

ORIGINAL MODEL DESIGNATION Stinson 108 NEW MODEL DESIGNATION (If desired)

3. DESCRIPTION OF CHANGE Modify wings using sheet metal in place of fabric, No change to existing structure. Ailerons we remain fabric covered. Recovering S-ce done according to setee ed drawings, #1001, sheet 1 through 8, Instruction Sheet, #1002, Sheet 1, 2 and 3, and C.A.A. Manual #18.

LIMTTATION OF APPLICABILITY% The approval of this change in type design applies basically to the standard Stinson 108 only. This approval should not be extended to other specific airplanes of this model on which other previously approved neteen the chroe energ of those other pretenty approdificatintionship between this change and any of of that airplane will introduce no adverse effect upon the airworthiness of that airplane/ *. WILL DATA BE AVAILABLE FOR SALE OR RELEASE TO OTHER PERSONS? YES NO

b. WILL PARTS BE MANUFACTURED FOR SALE (Ref. CAR 1.55)? YES NO

5. SIGNATURE AND TITLE OF APPLICANT Ковся В. Янію

SIGNATURE 4-7-60 Aircraft Parts Fabrication Date of Application: TITLE

6. To be Completed by FAA

NATURE AND LOCATION OF DATA Drawing 1001, Sheets 1 through 8, and Installation Instructions 1002, are on file at 2134 Xavier, Santa Clara, ¡California, and at FAA Fourth Region, Flight Standards Engineering and Manufacturing Branch.

Certification Basis: CAR 3 ORIGINAL TYPE CERTIFICATE NO. A-767 FAA APPROVAL Rocco L. Lippis Original signed by Supplemental Type Certificate NO.

SIGNATURE SA4-1484 Charles R. Hawks, Chief DATE OF APPROVAL Engineering and Manufacturing Branch May 1, 1961 Flight Standards Field Division TITLE * U.S. GOVERNMENT PRINTING OFFICE: 1959 0-509657 FORM FAA- 2417(5-59)

## Every issue (1)

- May 1, 1961: Issued, Current. [certificate](https://openairdocs.org/files/sha256/f0/34/f03493216bbb0becbf83dcf90f29fd3a1640ff27e24bdae8a8d2606d3956f8ee)

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