What it approves
Installation of the wing forward spar fuselage attachment assembly reinforcement.
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.
FAA Form 8110-2 (5/14) Page 1 of 2
Number: SA01154AT
This certificate issued to: Aerial Banners Mods LLC 601 SW 77th Way Pembroke Pines, FL 33023
Part 3of the Civil Air Regulations for Normal Category aircraft and of Part 8 of the Civil Aeronautics Manual for Restricted Category aircraft.
Original Product – Type Certificate Number: 2A8 (Normal Category) and 2A10 (Restricted Category) Make: Piper Model: PA-25 -235 and PA-25-260
Installation of the wing forward spar fuselage attachment assembly reinforcement in accordance with The STC Solutions, Inc. Installation Instructions, Document Number ST1911AT-A-INST, Revision A, dated August 4, 1996, or later FAA approved revision.
The STC Solutions, Inc., Maintenance Instructions, Document Number ST1911AT-A-MT, Revision A, dated August 7, 1996, 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 airplane.
Date of Application: January 29, 1996 Date Reissued: May 20, 2014 Date of Issuance: September 17, 1996 Date Amended:
Signature
Title Melvin D. Taylor Manager, ACE-115A Atlanta Aircraft Certification Office
FAA Form 8110-2 (5/14) Page 3 of
To (Name and address of transferee)
From (Name and address of grantor)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.