STC ST04449NY

Supplemental type certificate · Voyageur Aerotech Inc

Holder
Voyageur Aerotech Inc · Canada
Status
Current · Issued
Status date
March 6, 2020
Applied
May 23, 2017
Product
Aircraft · Large Airplane
Certification basis
Part 21, Part 25, Part 26
Data sheet
TCDSA13NM

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

What it approves

Conversion of DHC-8-102/-103/-106 from passenger carrying aircraft into Package Freighter with a Class E Cargo Compartment

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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate FAA Form 8110-2 (5/14) Page 1 of 4

1500 Airport Road

IMPORT Number: ST04449NY This certificate issued to: Voyageur Aerotech, Inc.

North Bay, Ontario, Canada P1B 8G2

Part 25 of the Federal Aviation Regulations.

A13NM Make: Bombardier Model: DHC-8-102 DHC-8-103 DHC-8-106

1. Conversion of DHC-8-102/-103/-106 from passenger carrying aircraft into Package Freighter with a Class E Cargo Compartment in accordance with Voyageur Aerotech, Inc. installation document DCS 15-2700, Rev. B, "DHC-8-100 Package Freighter," dated December 16, 2019, or later TCCA approved revision.

2. Voyageur Aerotech, Inc. Aircraft Flight Manual Supplement AFMS 15-2700, Rev. C, TCCA approved December 12, 2019, or later TCCA approved revision, is required as part of this installation.

3. The aircraft must be maintained in accordance with Voyageur Aerotech, Inc. Maintenance Manual Supplement, MMS 15-2700, Rev. A, dated April 24, 2017, or later TCCA accepted revision.

1. Airworthiness Limitation Tasks must be performed in accordance with Voyageur Aerotech, Inc. Maintenance Manual Supplement MMS 15-2700, Rev A, Chapter 4-00-00, TCCA approved May 10, 2017 or later TCCA approved revision.

2. Operation must be in accordance with Voyageur Aerotech, Inc. Aircraft Flight Manual Supplement AFMS 15-2700, Rev. C, TCCA approved December 12, 2019, or later TCCA approved revision.

(See Limitations and Conditions Continued on Page 3 of 4)

Date of Application: May 23, 2017 Date Reissued:

Date of Issuance: March 6, 2020 Date Amended:

Signature Anthony E. Gallo Title Acting Manager New York ACO Branch

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate FAA Form 8110-2 (5/14) Page 2 of 4

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: ST04449NY

To (Name and address of transferee)

From (Name and address of grantor)

This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST04449NY FAA Form 8110-2 (5/14) Page 3 of 4

Date of Issuance: March 6, 2020

3. The aircraft is limited to cargo operations.

4. Cargo must be loaded and secured in accordance with Voyageur Aerotech, Inc. Cargo Loading Manual Supplement CLMS 15-2700, Rev. A, dated May 1, 2017 or later TCCA accepted revision.

5. Prior to completion of this modification, the aircraft must have the following additional installations incorporated:

a) 825SO08063-2; "2 Baggage Divider Nets and Post (Standard Bulkhead)" (Bombardier/Factory Option)

b) 835CH00077-2 (SB8-35-10); "Oxygen-Increased Capacity of Crew Member's Fixed Oxygen Cylinder and Onboard Recharging Capability - Change Request 835CH00077-2" (Bombardier/Factory Option)

c) STC No. ST01872SE; "Installation of Lightweight Window Plug" issued to LiteAir Aviation Products, Inc.

d) EO 17-3079; "Installation of insulation blankets at plugged window locations" developed by Voyageur Aerotech, Inc.

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

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

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the modified Bombardier DHC-8-102/-103/-106 is as follows:

(a) For parts not changed or not affected by the change: The existing type certification basis for the aircraft model as shown on the FAA Type Certificate Data Sheet A13NM.

(b) For parts changed or affected by the change as shown below:

(See Certification Basis Continued on Page 4 of 4)

This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST04449NY FAA Form 8110-2 (5/14) Page 4 of 4

Date of Issuance: March 6, 2020 Certification Basis (Continued):

i. Part 25 regulations:

Paragraph Amdt. Paragraph Amdt. Paragraph Amdt.

§25.1 25-0 §25.803 25-46 §25.1529 25-54 §25.29 25-42 §25.805 25-0 §25.1541 25-0 §25.301 25-23 §25.809 25-47 §25.1555 25-0 §25.303 25-23 §25.811 25-88 §25.1557 25-38 §25.305 25-23 §25.812 25-128 §25.1561 25-46 §25.307 25-23 §25.813 25-128 §25.1581 25-42 §25.365 25-0 §25.831 25-41 §25.1583 25-46 §25.561 25-91 §25.851 25-74 §25.1585 25-105 §25.571 25-45 §25.853 25-116 §25.1701 25-123 §25.601 25-0 §25.855 25-123 §25.1703 25-123 §25.603 25-46 §25.857 25-93 §25.1705 25-123 §25.605 25-46 §25.858 25-93 §25.1707 25-123 §25.607 25-23 §25.869 25-123 §25.1709 25-123 §25.609 25-0 §25.1301 25-0 §25.1711 25-123 §25.611 25-23 §25.1307 25-72 §25.1713 25-123 §25.613 25-112 §25.1309 25-41 §25.1715 25-123 §25.619 25-23 §25.1322 25-38 §25.1717 25-123 §25.625 25-23 §25.1351 25-41 §25.1719 25-123 §25.685 25-38 §25.1353 25-123 §25.1721 25-123 §25.771 25-4 §25.1357 25-0 §25.1723 25-123 §25.777 25-46 §25.1360 25-123 §25.1725 25-123 §25.783 25-23 §25.1381 25-72 §25.1727 25-123 §25.787 25-139 §25.1431 25-113 §25.1729 25-123 §25.789 25-46 §25.1439 25-115 §25.1731 25-123 §25.791 25-72 §25.1501 25-42 §25.1733 25-123 §25.793 25-51 §25.1525 25-0

ii. Part 26 regulations: 26.47 Amendment 26-1

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This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

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
De Havilland Aircraft of Canada LimitedDHC-8-102A13NM
De Havilland Aircraft of Canada LimitedDHC-8-103A13NM
De Havilland Aircraft of Canada LimitedDHC-8-106A13NM