What it approves
Installation of fiberglass wing tips.
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 Aircraft Innovations, LLC PO Box 110164 Anchorage, AK 99511
Part 3 of the Civil Air Regulations.
Original Product — Type Certificate Number: 1A1 Make: Piper Model: PA-16, PA-16S
Description of Type Design Change: Installation of fiberglass wing tips as described on D&R Industries “Hot Tip” wing tip installation drawing number 1-0 revised March 23, 1972, or later FAA approved revision, when installed in accordance with D&R Industries Wing Tip Installation Instructions, pages 1 through 6 dated July 23, 1971, or later FAA approved revision.
1. The approval of this change in type design applies basically to Piper PA-16’s only. Compatibility of this design change with previously approved modifications must be determined by the installer. This determination should include consideration of significant changes in weight distribution, such as an increase in the fixed disposable weight in the fuselage.
2. 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.
Date of application: December 9, 1971 Date reissued : January 17, 1975; May 7, 1979;
September 11, 2009
Date of issuance: May 2, 1972 Date amended: September 11, 2009
( Signature) David D. Swartz Acting Manager, Anchorage 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 · 2
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| September 11, 2009 | Reissued, current | Certificate |
| May 7, 1979 | Reissued, earlier issue | Certificate |