STC ST12076CH

Supplemental type certificate · Canard Aerospace Corporation

Holder
Canard Aerospace Corporation · United States
Status
Current · Issued
Status date
August 1, 2025
Applied
April 15, 2024
Product
Aircraft · Large Airplane
Certification basis
Part 25
Data sheet
TCDSA13NM

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

What it approves

Installation of FMS Software Upgrade and Solid State Data Transfer Unit Plus (SSDTU+)

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.

ST12076CH Canard Aerospace Corporation 1157 Valley Park Dr., Suite 115 Shakopee, MN 55379 Part 25 the Code of Federal Regulations A13NM De Havilland Aircraft of Canada Limited DHC-8-400 Series

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

April 15, 2024 August 1, 2025 Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Services 3 Installation of FMS Software Upgrade and Solid State Data Transfer Unit Plus (SSDTU+) in accordance with Canard Aerospace Corporation, Data Control Document No. 40226 Revision D, dated July 21, 2025, or later FAA approved revision.

(See Continuation sheet 3 of 3 for complete Description of Type Design Change) for:

ST12076CH 08/01/25 3

ST12076CH 08/01/25 Description of Type Design Change (Continued):

The aircraft must be maintained in accordance with Instructions for Continued Airworthiness, document number 34-3689-07 Revision NC, dated August 20, 2024 or later FAA accepted revision.

FAA Approved Airplane Flight Manual Supplement 34-3689-06 Revision NC, approved July 29, 2025, or later FAA approved revision is required on board the modified aircraft.

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 De Havilland DHC-8-400 Series aircraft is as follows:

a. The type certification basis for the De Havilland DHC-8-400 series aircraft is shown on TCDS A13NM for parts not changed or not affected by this change.

b. The certification basis for the parts changed or affected by this change since the reference date of application, April 15, 2024, is based on TCDS A13NM and the following:

14 CFR Part 25 Regulations at the amendment level:

§§ 25.29(b) [25-72], 25.1301 [25-0], 25.1307(c) [25-72], 25.1309(a)(b)(c)(d)(e)(f) [25-41],

25.1322 [25-38], 25.1351(a) [25-72], 25.1353(a)(b) [25-113], 25.1357(a)(c) [25-0],

25.1431 [25-113], 25.1529 [25-54], 25.1581(a) [25-72].

14 CFR Part 26 Regulations at the amendment level:

§ 26.11(c) [26-0]

Special Condition 25-876-SC, Canard Aerospace Corporation, De Havilland Model DHC-8-400 Series Airplane; Electronic System Security Protection From Unauthorized External Access

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Approved models · 1

MakeModelData sheet
De Havilland Aircraft of Canada LimitedDHC-8-400 SeriesA13NM