# STC ST10001SC-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Duncan Aviation Inc, United States
- Description: Installation of the Honeywell Solid State Flight Data Recorder with interface to Collins Proline 21
- Applied: November 9, 2001
- Status date: August 24, 2021
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25, Part 135
- Data sheets: [TCDS A3EU](https://openairdocs.org/tcds/A3EU)
- Certificate PDF: https://openairdocs.org/files/sha256/3d/0f/3d0f50c47c78441d33b74bb36a5a541ced2a9c51141c98cef9a46d58d02f6438
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BEB9AF09E957CC3186258752004CEF9B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST10001SC-D

## ADs that name it (0)

None.

## Approved models (4)

- Beechcraft Corporation Hawker 750 ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))
- Beechcraft Corporation Hawker 800XP ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))
- Beechcraft Corporation Hawker 850XP ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))
- Beechcraft Corporation Hawker 900XP ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))

## 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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST10001SC-D This certificate issued to: Duncan Aviation, Inc.

3701 Aviation Road Lincoln, NE 68524 Part * of the (see continuation sheet 3 of 3) Original Product – Type Certificate Number: Make: Textron Aviation (Beechcraft) Model:

800XP, 850XP, 900XP, 750A3EU Description of Type Design Change:

Installation of the Honeywell Solid State Flight Data Recorder with interface to Collins Proline 21 in accordance with the Hawker Beechcraft Master Drawing List No. 800-199, Revision AJ, dated October 28, 2010, or later FAA approved revision.

For Hawker 800XP, installation is limited to aircraft equipped with Collins Pro Line 21 Avionics. The installer must determine whether this design change is compatible with previously approved modifications. 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.

The Flight Data Recorder system installed by this STC has NOT been shown to meet the requirements of 14 CFR 135.152.

Date of Application: November 9, 2001 Date Reissued: 5/9/07, 7/31/07, 8/26/13, 11/16/16, 8/24/21 Date of Issuance: June 26, 2002 Date Amended: 9/18/02, 6/8/06, 12/3/07, 4/17/08, 10/29/10 By Direction of the Administrator Signature Title Grant Youngdahl Program Manager Wichita, ACO Branch This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

FAA Form 8110-2 (5/14) Page 1 of 3

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

FAA Form 8110-2 (5/14) Page 2 of 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST10001SC-D Date Reissued: 8/24/2021 Description of Type Design Change (continued):

Models: 800XP, 850XP, 750. -101, -105, -107 Installations:

FAA approved Flight Manual Supplement No. 800-304, Revision R4, dated April 17, 2008, or later FAA approved revision.

Model: 900XP. -109, -111, -113, -115 Installations:

FAA approved Flight Manual Supplement No. 230-3004, Revision R1, dated December 3, 2007, or later FAA approved revision.

Certification Basis:

4b of the Civil Air Regulations and Part 25 of the Federal Aviation Regulations.

The type certification basis of this STC is shown on TCDS A3EU for parts not changed or not affected by the change.

The type certification basis of this STC for parts affected by this change are:

For -101, -103, -105, -107, -109 Installations: TCDS A3EU For -111, -113, -115 Installations:

CAR 4b 4b.104 4b.302 4b.605(e) 4b.200 4b.303 4b.606(a)(b) 4b.201 4b.304(a)(b) 4b.621 4b.202(a)(b) 4b.305 4b.624(a)(c) 4b.210 4b.306 4b.625(a)(b)(c) 4b.230 4b.307(c) 4b.630(a)(b)(c) 4b.260 4b.320(a) 4b.650(a)(c) 4b.270 4b.329 4b.730 4b.300 4b.600 4b.301 4b.601 FAR 25, Amendment in Square Brackets

25.571(a)(b)(c) [25-54] 25.1301(a)(b)(c)(d) [Basic] 25.1353(a) [2 5-42]

25.613(a) [25-46] 25.1309(a)(b)(d) [25-41] 25.1431( a)(c) [Basic

25.615(a) [25-23] 25.1322(b) [25-38] 25.1459(a)(b)(c)(d) [25-124]

25.981(a)(3)(b) [25-102] -- END -- This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

FAA Form 8110-2 (5/14) Page 3 of 3

## Every issue (4)

- August 24, 2021: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3d/0f/3d0f50c47c78441d33b74bb36a5a541ced2a9c51141c98cef9a46d58d02f6438)
- August 26, 2013: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/05/de/05dec79e5863ae84851408b2b1ab2cf2179ba70fd1e88c720e8ee24069fa209c)
- October 29, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/53/94/53945bc2fc37cdc46384b1065916d5c9f888f34d2f5952d8517720d9339d509d)
- July 31, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/7f/a8/7fa8beaa9b0e6164516942b70a0654869413ba9b526eae75dd1944f10d03d70e)

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