STC SA3274WE

Supplemental type certificate · G and S Industries

Holder
G and S Industries · United States
Status
Current · Issued
Status date
September 17, 1976
Applied
March 2, 1976
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDS3A21

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of flap gap seal

What the certificate saysOCR

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA327LNE This certificate issued to: G and S Industries Certifies that the change in the type design for the filleming praduct with the limitations and conditions therefor as specified heren meets the airer thiness requirements f Purt 3 of the CiviT Air Regulativni, effective May 15, 1956.

Original Product - Type tertificates kumber: 3A21 Make: Cessna Model: 210, 210A Description of Type Design Change:

Installation of flap gap seal in accordance with sealed G and S Industries Report No. 03-76 dated April 1, 1976.

Jimitutim andtundilund: The approval of this change in type desien applies to the basic aircraft of the specified models that are otherwise unmodified.

approval should not be extended to other aircraft of these models 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 will introduce no adverse effect upon the airworthiness of that aircraft.

Sales$ upplicatin: March 2, 1976 Date Reissued:

I ate ef issuence: SEP 1 7 1376 Date Amended:

FEDERAL AVIATION •Dy direction «f the Staministrater Henan (Signature ) TOHINISTRATO Chief, Aircraft Modification Branch (Title ) 04 R0078

1. NAME AND ADDRESS OF APPLICANT 2. APPLICATION MADE FOR: 3. PRODUCT INVOLVED G and S Industries 3243 Airport Dr. TYPE CERTIFICATE AIRCRAFT Torrance, Calif. 90505 PRODUCTION CERTIFICATE ENGIN E SUPPLEMENTAL T. C. PROPELLER

4. COMPLETE THE FOLLOWING FOR TYPE CERTIFICATE A. MODEL DESIGNATION (S) (All models listed are to be completely described in the required technical data, including drawings, material, specifications, construction, and performance of the Aircraft, Aircraft Engine, Propeller which is the subject of ghis

5. COMPLETE THE FOLLOWING FOR PRODUCTION CERTIFICATE (With this for submit, in manual form, one copy of quality control data or changes thereto covering new products, as required by applicable FAR.)

A. FACTORY ADDRESS (If different from 1 above) B. APPLICATION IS FOR: NEW P.C. _ ADDITIONS TO P.C. NO..

C. APPLICANT IS HOLDER OF OR A LICENSEE UNDER T. C. OR S.T.C. NO. (attach evidence of licensing agreement)

6. COMPLETE THE FOLLOWING FOR SUPPLEMENTAL TYPE CERTIFICATE A. MAKE AND MODEL DESIGNATION OF PRODUCT TO BE MODIFIED Cessna 210, 210A Installation Wing Flap Gap Heals B. DESCRIPTION OF MODIFICATION C. WILL DATA BE AVAILABLE FOR SALE OR RELEASE TO OTHER PERSONS?

• YES ENO D. WILL PARTS BE MANUFACTURED FOR SALE? (Ref. FAR 21.303) _ NO

CERTIFICATION

CERTIFY THAT THE ABOVE STATEMENTS ARE TRUE

SIGNATUR CERTIFYING OFFICIAL 3/2/76 DATE Co Owner TITLE FAA FOrm 8110-12 (5-69) FORMERLY FAA FORM 312.

GPO 875. 056 C FAA AC 73-8284

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 · 2

MakeModelData sheet
Cessna Aircraft Company2103A21
Cessna Aircraft Company210A3A21