STC SR02999NY

Supplemental type certificate · VIH Aerospace Inc

Holder
VIH Aerospace Inc · Canada
Status
Current · Issued
Status date
July 6, 2011
Applied
March 1, 2011
Product
Aircraft · Rotorcraft
Certification basis
Part 21
Data sheet
TCDS1H15

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

What it approves

Installation of Auxiliary External Torque Gauge and External Load Meter in accordance with VIH Aerospace Inc., Master Document List VS61-0715J-MDL, Revision A, Dated January 24, 2011, approved by Transport Canada Civil Aviation (TCAA) on February 15, 2011, or later TCCA approved revisions.

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

Part 7 of the Civil Aviation Regulations.

Installation of Auxiliary External Torque Gauge and External Load Meter in accordance with VIH Aerospace Inc., Master Document List VS61-0715J-MDL, Revision A, Dated January 24, 2011, approved by Transport Canada Civil Aviation (TCAA) on February 15, 2011, or later TCCA approved revisions.

1. The Instructions for Continued Airworthiness (ICA) VS61-0715J-ICA, Revision B, dated January 28, 2011 accepted by TCAA on January 28, 2011 or later TCCA accepted revisions must be used to maintain the airworthiness of the modified aircraft.

VIH Aerospace Inc.

1962 Canso Road North Saanich, British Columbia V8L 5V5 Canada 1H15 Sikorsky Aircraft S61N Date of application: March 01, 2011

Date of issuance: July 6, 2011

( Signature) Anthony Socias Manager New York Aircraft Certification Office

(Title)

FAA Form 8110-2-1(10-69) Page 2 of 2

Number SR02999NY Date of Issuance: July 6, 2011

2. Operations must be in accordance with VIH Aerospace In c. Rotorcraft Flight Manual Supplement VS61-0715J-FMS, Dated December 13, 2010, approved by TCCA on February 15, 2011 or later TCCA approved revisions.

3. STC SR00681SE for the Fabrication of Onboard Systems Model 200-243-00 Cargo Hook Load Weigh System is a prerequisite with this Installation.

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

5. If the holder agrees to permit another person to use the certificate to alter a product, the holder must give the other pe rson written evidence of that permission.

…………..END…………

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 · 1

MakeModelData sheet
Sikorsky Aircraft CorporationS-61N1H15