STC ST11840WI

Supplemental type certificate · Duncan Aviation Inc.

Holder
Duncan Aviation Inc. · United States
Status
Current · Issued
Status date
December 11, 2024
Applied
August 12, 2024
Product
Aircraft · Large Airplane
Certification basis
Part 25
Data sheet
TCDST00003NY

From FAA DRS, with our copy of the certificate PDF. DRS record last changed August 24, 2026.

What it approves

Change to Layout of Passenger Accommodations (LOPA)

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 Number This certificate issued to:

ST11840WI Duncan Aviation, Inc.

3701 Aviation Road Lincoln, NE 68524 Part 25* Federal Aviation Regulations (* see Page 3) T00003NY Bombardier Inc.

BD-700-1A10 The installer must determine whether this design change is compatible with previously approved modifications. (Limitations and Conditions continued on Page 3) 08/12/2024 12/11/2024 Dain J. Christensen ODA STC administrator, ODA-501013-CE 3 Change to Layout of Passenger Accommodations (LOPA) in accordance with Duncan Aviation, Inc. STC Master Document List, Doc. No. CERTDOC-025191, Rev. A, dated December 11, 2024 or later FAA approved revisions.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number

Date o transfer:

ST11840WI 12/11/2024 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number ST11840WI 12/11/2024 Limitations and Conditions (continued):

You cannot use descriptive data from this design change to duplicate other products. This approval is limited to only the installation made in Bombardier Inc. BD-700-1A10, Serial Number 9125. This STC does not permit manufacturing of parts for multiple installations.

Certification Basis:

The certification basis for parts changed or affected by this design change is the 14 CFR Part 25 requirements defined in TCDS T00003NY, Revision 23 for the Bombardier Inc. BD-700-1A10.

Exemptions:

FAA Exemption No. 7120C from 25.785(b) for Side-Facing Divans, (per Note 9 of the TCDS).

In addition, the applicant has voluntarily complied with the following 14 CFR Part 25 regulation, effective February 1, 1965, as amended by the amendment stated:

14 CFR 25.613(a)(b)(c)(f) [Amdt. 25-112].

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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.BD-700-1A10T00003NY