STC SA03094NY

Supplemental type certificate · Beringer Aero

Holder
Beringer Aero · France
Status
Current · Issued
Status date
May 14, 2012
Applied
January 14, 2011
Product
Aircraft · Small Airplane
Certification basis
Part 3, Part 21
Data sheet
TCDS7A15

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

What it approves

Installation of Beringer Aero s Wheel and Brake 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.

Part 3 of the Civil Aviation Regulations.

Installation of Beringer Aero’s Wheel and Brake System is in accordance with their Maintenance and Overhaul Manual, MM-STC- 002, Revision 2, dated April 5, 2012.

The following documents are required with this installation:

Instruction for Continued Airworthiness found in Beringer Aero document MC-STC-002, “Time Limits / Maintenance Checks”, dated April 5, 2012.

Maintenance must be conducted in accordance with Beringer Aero document MM-STC-002, “and Overhaul Manual”, dated April 5, 2012.

1. The installer must determine whether this design change is compatible with previously approved modifications.

2. If the holder agrees to permit another person to use this certification to alter a product, the holder must give the other person written evidence of this permission.

Beringer Aero Aeropole 05130 Tallard France

7A15 Pilatus Aircraft Ltd.

PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4 series aircraft Date reissued:

( Signature) Gaetano Sciortino Acting Manager New York Aircraft Certification Office

( Title) Date of application: January 14, 2011

Date of issuance: May 14, 2012

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/B1-H27A15
Pilatus Aircraft LimitedPC-6/B2-H27A15
Pilatus Aircraft LimitedPC-6/B2-H47A15