© Copyright 2010 GARMIN Ltd. or its subsidiaries All Rights Reserved Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express prior written consent of GARMIN.
GARMIN International, Inc Log of Revisions EASA Approved AIRPLANE FLIGHT MANUAL SUPPLEMENT G1000 Integrated Avionics System and GFC 700 AFCS In Hawker Beechcraft 200, 200C, B200 and B200C King Air Aircraft REV NO. PAGE NO(S) 1 ALL 190-00915-04 Rev.
This page intentionally left blank. Hawker Beechcraft 200, 200C, B200 and B200C King Air Page 4 of 7 190-00915-04 Rev.
Table of Contents Section 1 - General ........................................................................................................ 7 Section 2 - Limitations .................................................................................................. 7 Section 3 – Emergency Procedures ............................................................................ 7 Section 3A – Abnormal Procedures ............................................................................
This page intentionally left blank. Hawker Beechcraft 200, 200C, B200 and B200C King Air Page 6 of 7 190-00915-04 Rev.
Section 1 - General The information in this supplement is EASA-approved material and must be attached to the FAA Approved STC Airplane Flight Manual Supplement, p/n 190-00915-02, when the airplane has been modified by installation of the GARMIN G1000 Integrated Avionics System and GFC 700 AFCS in accordance with STC SA01535WI-D. This EASA approved Airplane Flight Manual Supplement is required in addition to the FAA approved Airplane Flight Manual Supplement, p/n 190-00915-02.
