G1000/GFC 700 Post Installation Checkout Procedure - Hawker / Beechcraft King Air C90
Page 1-1
190-00682-00
Revision 5
1 INTRODUCTION
1.1
Scope
This document presents the post-installation procedures which are required to be performed after
installing the G1000 Integrated Cockpit System in the Hawker Beechcraft King Air C90 series aircraft.
This document and revision are effective for the following aircraft:
Aircraft Model
Model Name
G1000 System
Software Version
C90A / C90GT
King Air
Ref. General Arrangement, G1000/GFC 700 AFCS,
King Air C90A/GT (005-00375-22)
Refer to the General Arrangement, G1000/GFC 700 AFCS, King Air C90A/GT (005-00375-22) for details
on specific aircraft eligibility for this STC.
Additional STC documents are listed in the Master Drawing List, 005-00375-30.
1.2
Organization
Follow the procedures in this document to configure and test a newly-installed Garmin G1000 Integrated
Avionics System with GFC 700 Automatic Flight Control System in the Hawker Beechcraft King Air Model
C90A/GT. The person performing the configuration and testing should read through this entire document
prior to beginning any procedures.
Section 1:
Introduction, reference documents, system description and operation.
Section 2:
Software and system configuration loading procedures. Manual configuration items are also
addressed. At the end, all software versions and part numbers are verified against drawing 005-
00375-22 “General Arrangement, King Air C90A/GT”.
Section 3:
Ground checks include exercising and testing basic G1000 functions.
Section 4:
Ground checks of G1000 interfaced equipment including GWX 68, StormScope®, Traffic
System, DME and ADF.
Section 5:
AHRS alignment and calibration procedures.
Section 6:
Final systems checkout.
Section 7:
Detailed GFC 700 ground checks are given in this section.
Section 8:
Flight testing procedures are given where mode function checks are conducted, and final
autopilot and TAWS checks are made.
