# STC SA01243NY

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Viking Air Limited, Canada
- Description: Installation of a Flutter Prevention Modification.
- Applied: July 18, 2000
- Status date: October 27, 2008
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 3, Part 21, Part 23
- Data sheets: [TCDS A-815](https://openairdocs.org/tcds/A-815)
- Certificate PDF: https://openairdocs.org/files/sha256/2e/de/2ede7a98fec353dfa968c405c936a8e4787c3d271be3b430596a0c87e9c33e97
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E9CD771C63E440188625756F00731800.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01243NY

## ADs that name it (1)

- [AD 2004-24-01](https://openairdocs.org/ad/2004-24-01): Elevator servo tab assembly · Viking Air DHC-3. Effective Dec 28, 2004. Cited in the text

## Approved models (1)

- Bombardier Inc. DHC-3 ([TCDS A-815](https://openairdocs.org/tcds/A-815))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Part 3 of the Civil Air Regulations.

Installation of a Flutter Prevention Modification to be completed in accordance with Viking Air Ltd. Master Document Index No.

V3MK1148, Issue 3, dated February 13, 2002 or later Transport Canada approved revision.

Certification Basis:

1. For the areas unaffected by this modification, the certification basis is as defined in TCDS A-815.

2. For the areas affected by this modification, the certification basis is as defined in TCDS A-815, plus 14 CFR §23.629 at Amendment 23-23, October 30, 1978 and 14 CFR §23.659 at Amendment 23-23, October 30, 1978.

1. Repair Manual Supplement PSM1-3-3 “Control Surface Trim and Servo Tab Balancing Procedure, Viking Air Flutter Prevention Kit”, dated January 31, 2002, or later Transport Canada accepted revision is required with this STC.

2. Maintenance must be performed in accordance with Maintenance Manual Supplement V3MK1148-2, “Installation of Viking Air Limited V3MK1148 Flutter Prevention Kit”, Issue 2, dated February 10, 2002 or later Transport Canada accepted revision.

3. STC SA01243NY supersedes ST01243NY.

Viking Air Limited 9574 Hampden Road Sidney, British Columbia V8L SVS Canada A-815 Make: Viking Air Limited Model: DHC-3 Date of application: July 18, 2000

Date of issuance: September 26, 2000 Date reissued: March 18, 2002, February 27, 2004 October 27, 2008

Date amended: March 18, 2002, October 06, 2004 January 21, 2009

( Signature) Anthony Socias Manager New York Aircraft Certification Office

( Title)

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

Number SA01243NY Date of Amendment: January 21, 2009

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 this certificate to alter a product, the holder must give the other person written permission of that permission.

**APPROVED CONFIGURATION LIST**

Configuration 1 2 3 4 5 Engine Pratt and Whitney S3H1-G, S1H1-G, R- 1340-59 or R-1340- 61 Pezetel PZL ASZ-621R-M18 Pratt and Whitney PT6A-135, PT6A- 135A, PT6A-34 Honeywell (Garrett) TPE331-10/-12JR Walter M601E-11 Propeller Hamilton Standard 3D40-6511A-9X, 6529A-9X or 6631A- 9 (3 bladed) Pezetel AW-2-30 (4 bladed) Hartzell HC-B3TN- 3DY/T10282/T1028 2 +4 (3 bladed) Hartzell HC-B4TN- 5NL/LT10890N (4 bladed) AVIA V508E-AG (3 bladed) Method of Approval

TCDS A-815 (A-27, Canadian) STC SA327NE (SA83-18) STC SA3777NM (SA89-32) STC SA09866SC (SA02-15) STC SA09857SC (SA01-11)

…END…

## Every issue (1)

- October 27, 2008: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/2e/de/2ede7a98fec353dfa968c405c936a8e4787c3d271be3b430596a0c87e9c33e97)

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