STC SA09862SC

Supplemental type certificate · Canada Turbine Conversions Inc.

Holder
Canada Turbine Conversions Inc. · Canada
Status
Current · Reissued
Status date
March 21, 2003
Applied
October 15, 1998
Product
Aircraft · Single-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDSA-815

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of the AVIA Hamilton Standard VJ8.510 propeller

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 Air Regulations.

Installation of the AVIA Hamilton Standard VJ8.510 propeller in accordance with AVIA Hamilton Standard “Operator’s Installation and Maintenance Manual, V510 Propeller”, dated 1994. FAA approved Flight Manual Supplement dated May 31, 2001, or later FAA approved revision is required.

Compatibility of design change with previously approved modifications must be determined by the installer. If 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. Limited to airplanes with STC SA09857SC (Walter M601E-11 engine) and propeller electronic speed limiter unit.

Canada Turbine Conversions, Inc.

Lot 16 RM of Alexander 105081 Highway 11 Pine Falls, MB ROE 1MO CANADA A-815 Make : Bombardier Inc.

Model : DHC-3 Otter Date of application : October 15, 1998

Date of issuance : May 31, 2001

Date reissued : March 21, 2003

( Signature) S. Frances Cox, Manager Special Certification Office, Southwest Region

( Title)

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

MakeModelData sheet
Bombardier Inc.DHC-3A-815