What it approves
Installation of horizontal/stabilizer 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.
the Civil Air Regulations.
SA910EA PC6-AU23 Spares, LLC 37 Styles Way Lagrangeville, NY 12540 Part 3
7A15 Pilatus Aircraft Works, Ltd.
PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/C-H2
1. This installation is also eligible on those aircraft incorporating STC SA545EA.
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.
3. Compatibility of this design change with previously approved modifications must be determined by the installer.
03/16/1972 04/04/1974 06/30/1994 05/03/1972 06/27/2003 04/04/1974 10/25/2023 Christina M. Underwood Manager, East Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 2 lnstallation of horizontal/ stabilizer reinforcement in accordance with data listed in:
Configuration A: "ECP-200'' as shown in Porter Drawing List, RPC6-151, Rcvision Q, dated Scptember 15, 1975, effective on aircraft serial numbers 2001 through 2072.
OR Configuration B: Same as Configurution A, except that drawing 6300.10, Revision A, is replaced by drawing 6300.6010, Revision (-) and EAI-1, dated July 22, 1975, effective on aircraft serial number 2073 and up.
10/18/1988 10/31/1975
SA910EA 10/25/2023 2
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.