What it approves
Installation of the Collins Pro Line 21 Avionics System
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.
FAA Form 8110-2 (5/14) Page 1 of
Part of the
Signature
Title *and additional requirements in TCDS 3A20, Special Conditions 23-108-SC, and Equivalent Level of Safety ACE-07-06.
SA01447WI-D Textron Aviation Inc.
One Cessna Boulevard Wichita, KS 67215 3 Civil Air Regulations * Hawker Beechcraft Corporation C90GT Installation of the Collins Pro Line 21 Avionics System in accordance with:
1. Collins Master Drawing List, AAC-0488-001, Revision --, dated July 23, 2007;
2. Hawker Beechcraft Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement, 90-590024-179, Revision 0, dated December 17, 2007;
3. Collins Maintenance Manual Supplement, AAC-0459, Revision --, dated August 31, 2007; or later FAA approved revision to 1, 2, or 3.
3 3A20
1. Compatibility of this design change with previously approved modifications must be determined by the installer.
2. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
September 24, 2007; December 12, 2016 September 20, 2007; December 20, 2007 October 6, 2006 August 31, 2007 Mark Fuller STC ODA administrator ODA-100129-CE
FAA Form 8110-2 (5/14) Page 2 of
To (Name and address of transferee)
From (Name and address of grantor)
FAA Form 8110-2 (5/14) Page 3 of
Date of Issuance: August 31, 2007 Date Reissued: December 12, 2016 Date Amended: December 20, 2007
3. In addition to the TCDS requirements, Rockwell Collins, Inc. has voluntarily complied with the following additional Part 23 Federal Aviation Regulations:
§23.901(e)(1) (Amdt. 23-53); §23.1301(a)(b)(c)(d) (Amdt. 23-20); §23.1305(a)(2)(3)(c)(1)(2)(5)(e)(1) (Amdt. 23-52);
§23.1309(a)(b)(c)(d)(e) (Amdt. 23-49); §23.1311(a)(b)(c) (Amdt. 23-49); §23.1321(a)(b)(c)(d)(e) (Amdt. 23-49);
§23.1322(a)(b)(c)(d) (Amdt. 23-43); §23.1329(a)(b)(d)(e)(f) (Amdt. 23-49); §23.1335 (Amdt. 23-20); §23.1357 (Amdt. 23-43);
§23.1359(c) (Amdt. 23-49); §23.1365(a)(b)(c)(d)(e) (Amdt. 23-49); §23.1367(a)(b)(c)(d) (Amdt. 23-Orig.);
§23.1381(a)(b)(c) (Amdt. 23-Orig.); §23.1431(a)(b)(c) (Amdt. 23-Orig.); §23.1457(a)(c) (Amdt. 23-35); §23.1501(a) (Amdt. 23-21);
§23.1521(b)(c) (Amdt. 23-50); §23.1529 (Amdt. 23-26); §23.1543(c) (Amdt. 23-50); §23.1545(a)(b)(c) (Amdt. 23-50);
§23.1549 (Amdt. 23-45); and §23.1555(a) (Amdt. 23-50).
-- END -- SA01447WI-D 3
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Hawker Beechcraft Corporation | C90GT | 3A20 |
Every issue · 3
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| December 12, 2016 | Reissued, current | Certificate |
| December 1, 2016 | Reissued, earlier issue | Certificate |
| September 24, 2007 | Reissued, earlier issue | Certificate |