STC SA940EA

Supplemental type certificate · PC6-AU23 Spares LLC

Holder
PC6-AU23 Spares LLC · United States
Status
Current · Reissued
Status date
October 25, 2023
Applied
August 24, 1972
Product
Aircraft · Single-Engine
Data sheet
TCDS7A15

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Left Wing 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.

SA940EA 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/C-H2,

1. 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.

2. Compatibility of this design change with previously approved modifications must be determined by the installer.

08/24/1972 10/18/1988 06/27/2003 12/21/1972 10/25/2023 Christina M. Underwood Manager, East Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 2 Left Wing Reinforcement in accordance with Section L of Fairchild Hiller Engineering Report No.

RPC6-237, dated May 2, 1972, revisied November 11, 1972, "ECP Descriptions and Drawing Lists".

06/30/1994

SA940EA 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.

No AD in this release names this STC

Approved models · 3

MakeModelData sheet
Pilatus Aircraft LimitedPC-6/B-H27A15
Pilatus Aircraft LimitedPC-6/B1-H27A15
Pilatus Aircraft LimitedPC-6/C-H27A15