What it approves
Modification of a Rockwell Collins, Inc. FGC-3000 Flight Guidance Computer Module.
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 Textron Aviation Inc.
One Cessna Boulevard Wichita, KS 67215 3 SA01566WI-D Federal Aviation Regulations.
23 A24CE B200/B200C/B200GT/B200CGT *See Sheet 3 for Certification Basis Modification of a Rockwell Collins, Inc. Flight Guidance System (FGS) installation in accordance with Rockwell Collins, Inc. Master Drawing List RCA-0241-001, Revision -, dated September 15, 2009, or later FAA approved revision.
Hawker Beechcraft Corporation
1. Prior FAA approved installation of a Rockwell Collins, Inc. FGC-3000 Flight Guidance Computer Module (CPN 822-1108-031) is a prerequisite to this STC.
2. Compatibility of this design change with previously approved modifications must be determined by the installer.
3. 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.
February 12, 2010; December 12, 2016 August 3, 2009 November 11, 2009 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: November 11, 2009 Date Reissued: December 12, 2016
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 Hawker Beechcraft Corporation Models B200/B200C/B200CGT is as follows:
1. The type certification basis for Hawker Beechcraft Corporation Models B200/B200C/B200CGT is shown on TCDS A24CE for parts not changed and not affected by the change.
2. The certification basis for parts changed or affected by this change since the referenced date of application, August 3, 2009, is as follows:
14 CFR Part Amendment
23.143(b) 50
23.671(a) Orig.
23.677(a) 49
23.867(a)(b)(c) 49
23.1301(a)(b)(c)(d) 20
23.1308(a)(b)(c)(d) 57
23.1309(a)(b)(c)(d)(e) 49
23.1329(e) 49
23.1335 20
23.1357(a)(c) 43
23.1431(a)(b) 49
23.1529 26
23.1581(a) 50
-- END -- SA01566WI-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 · 8
| Make | Model | Data sheet |
|---|---|---|
| Hawker Beechcraft Corporation | B200 | A24CE |
| Hawker Beechcraft Corporation | B200C | A24CE |
| Hawker Beechcraft Corporation | B200C (C-12F) | A24CE |
| Hawker Beechcraft Corporation | B200C (C-12R) | A24CE |
| Hawker Beechcraft Corporation | B200C (UC-12F) | A24CE |
| Hawker Beechcraft Corporation | B200C (UC-12M) | A24CE |
| Hawker Beechcraft Corporation | B200CGT | A24CE |
| Hawker Beechcraft Corporation | B200GT | A24CE |
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 |
| February 12, 2010 | Reissued, earlier issue | Certificate |
| November 11, 2009 | Issued, earlier issue | Certificate |