What it approves
Installation of a Rockwell Collins TCAS 4000 Traffic Alert and Collision Avoidance System (TCAS II) in accordance with Elliott Aviation Master Data List, No. 2026-576DL, Revision 8, dated January 6, 2011, or later FAA approved revision.
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.
Part 23 of the Federal Aviation Regulations.
Installation of a Rockwell Collins TCAS 4000 Traffic Alert and Collision Avoidance System (TCAS II) in accordance with Elliott Aviation Master Data List, No. 2026-576DL, Revision 8, dated January 6, 2011, or later FAA approved revision.
1) Compatibility of this design change with previously appr oved modifications must be determined by the installer.
2) FAA Approved Airplane Flight Manual Supplement, Elliott Aviation Doc. No. TCAS4000FMS, Revision 0, approved December 4, 2000, or TCAS4000MFD-85CFMS, Revision 0, approved December 4, 2000, as appropriate for the installed configuration, or later FAA approved revision, is required on board the aircraft modified per Configuration 1.
3) FAA Approved Airplane Flight Manual Supplement, Elliott Aviation Doc. No. FS2026-576, Revision 2, approved December 6, 2010, or later FAA approved revision, is required on board the aircraft modified per Configuration 2.
Elliott Aviation Technical Products, Inc.
PO Box 100 Quad City Airport Moline, IL 61266-0100 A24CE Make : Raytheon Aircraft Company (Beech) Model : 200; 200C; 200CT; 200T; B200; B200C; B200CT;
B200T; 300; B300; 300LW; B300C, B200GT, B200CGT
Date of application : March 30, 2000
Date of issuance : December 4, 2000
Date amended : October 27, 2004; January 6, 2011
( Signature) Steven L. Lardinois Manager, Systems and Flight Test Branch Chicago Aircraft Certification Office
( Title)
FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES
Number SA01352CH
Date Amended: January 6, 2011
Limitations and Conditions : (Continued from Page 1 of 3)
4) FAA approved Airplane Flight Manual Supplement, Elliott Aviation Doc. No. FS2026-344, Revision 0, approved October 26, 2004, or later FAA approved revision, is required on the aircraft modified per Configuration 3.
5) FAA Approved Instructions for Continued Airworthiness, Chapter 10 – Airworthiness Limitations, Elliott Aviation Report No.
CA2026-576, Revision 5, FAA approved January 6, 2011, or later FAA approved revision, is required for this modification.
6) 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.
- END -
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 18
| Make | Model | Data sheet |
|---|---|---|
| Hawker Beechcraft Corporation | 200 | A24CE |
| Hawker Beechcraft Corporation | 200C | A24CE |
| Hawker Beechcraft Corporation | 200CT | A24CE |