What it approves
Installation of Fin Tip Plates in accordance with Farrington Aircraft Drawing No. FAC-FIN-1011, Revision A , dated October 13, 1989, and removal of existing Side Slip Warning System.
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 6 of the Civil Air Regulations.
(See T.C. Data Sheet 1H17 for complete certification basis.)
Description of Type Design Change: Installation of Fin Tip Plates in accordance with Farrington Aircraft Drawing No. FAC-FIN-1011, Revision “A”, dated October 13, 1989, and removal of existing Side Slip Warning System.
Limitations and Conditions: The Rotorcraft Flight Manual Supplement, dated January 31, 1990, is a required part of this STC. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage.
If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
Heliplane Aircraft Corporation International 1821 North US Highway 1 Ft. Pierce, Florida 34946 1H17 Make : Air and Space Manufacturing, Inc.
Model : 18A Date of application : May 24, 1989
Date of issuance : January 31, 1990
Date reissued : July 22, 2011
( Signature) Melvin D. Taylor Manager, Atlanta Aircraft Certification Office
( Title)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Air & Space America Inc. | 18A | 1H17 |