What it approves
Installation of Cleveland 40-28, 6.00 - 6 main wheel assemblies and Cleveland 30-18 brake assemblies
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
This Certificate issued to
Part 04* of the Civil Air Regulations.
*Complete certification basis is specified in Aircraft Specification No. A-754, Revision 8.
Description of Type Design Change: Installation of Cleveland 40-28, 6.00 - 6 main wheel assemblies and Cleveland 30-18 brake assemblies in accordance with Arctic Aircraft Company, Inc., Drawing No. A-C-5000, Revision B dated December 15, 1975, or later FAA approved revision, and Arctic Aircraft Company, Inc., document entitled "Parts List for Cleveland Wheel and Brake Conversion Kit", original issue dated March 31, 1976, or later FAA approved revision, and Arctic Aircraft Company, Inc., document entitled "Installation Procedure for Cleveland Wheel and Brake Conversion Kit", original issue dated March 31, 1976, or later FAA approved revision.
Limitations and Conditions: Compatibility of this design change with previously approved modifications must be determined by the installer.
The holder of this Certificate will provide each person it permits to use the Certificate to alter one or more airplanes with written evidence of that permission in a form acceptable to the Administrator.
14 CFR Part 43 is adequate to insure continued airworthiness of this modification.
STOL Aviation LLC c/o Tom Csatari 8 South Park Street Lebanon, N.H. 03766 754 Make: Interstate Model: S-1B1
Date reissued: June 2, 2000;
October 31, 2007
Date amended: June 2, 2000
( Signature) Gregory J. Holt Manager Anchorage Aircraft Certification Office
( Title) Date of application: July 16, 1974
Date of issuance: March 31, 1976
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.