G1000/GFC 700 Post Installation Checkout Procedure – Hawker / Beechcraft King Air C90
Page iii
190-00682-00
Revision 5
TABLE OF CONTENTS
1
INTRODUCTION
1-1
1.1
Scope ................................................................................................................................................. 1-1
1.2
Organization ....................................................................................................................................... 1-1
1.3
Reference Documents........................................................................................................................ 1-2
1.4
System Description ............................................................................................................................ 1-3
1.5
G1000 Control Interface ..................................................................................................................... 1-6
2
POST INSTALLATION PROCEDURES
2-1
2.1
Required Test Equipment................................................................................................................... 2-1
2.2
G1000 Hardware/Software Compatibility Check................................................................................ 2-1
2.3
G1000 Software/Configuration Procedure .........................................................................................2-2
2.4
Software Load Confirmation............................................................................................................... 2-5
2.5
King Air C90 Airframe Configuration .................................................................................................. 2-7
2.6
Traffic System Option Configuration ................................................................................................ 2-11
2.7
StormScope (WX-500) Option Configuration ................................................................................... 2-12
2.8
ADF – 60 Option Configuration ....................................................................................................... 2-15
2.9
DME 42 Option Configuration .......................................................................................................... 2-15
2.10
FliteCharts Configuration.................................................................................................................. 2-16
2.11
ChartView Configuration .................................................................................................................. 2-17
2.12
TAWS Configuration......................................................................................................................... 2-18
2.13
Aircraft Registration Number Entry .................................................................................................. 2-19
2.14
Terrain/Obstacle Database Loading ................................................................................................ 2-19
2.15
Aviation Database Loading .............................................................................................................. 2-20
2.16
Clearing Default User Settings ......................................................................................................... 2-20
2.17
Software/Configuration Troubleshooting.......................................................................................... 2-21
3
G1000 INITIAL SYSTEM TESTING
3-1
3.1
Electrical Power Distribution Testing.................................................................................................. 3-1
3.2
Electrical Load Test Procedures ........................................................................................................ 3-5
3.3
Display Testing................................................................................................................................. 3-10
3.4
GPS Signal Acquisiton ..................................................................................................................... 3-13
3.5
GMA 1347D Testing......................................................................................................................... 3-14
3.6
VHF COMM Operational Check ....................................................................................................... 3-15
3.7
Marker Beacon Test ......................................................................................................................... 3-15
3.8
VHF COM Interference Test ............................................................................................................ 3-15
3.9
VOR/LOC/GS Test ........................................................................................................................... 3-16
3.10
COM Antenna VSWR Checks.......................................................................................................... 3-16
3.11
GTX 33 Testing ................................................................................................................................ 3-17
3.12
Pitot Static System Leak Checks ..................................................................................................... 3-18
3.13
GDC 74B Testing ............................................................................................................................. 3-19
3.14
GDL 69A Functional Check.............................................................................................................. 3-22
3.15
GEA Functional Check ..................................................................................................................... 3-26
3.16
TAWS Functional Check .................................................................................................................. 3-27
3.17
FliteCharts Functional Check ........................................................................................................... 3-28
3.18
ChartView Functional Check ............................................................................................................ 3-29
3.19
SafeTaxi Functional Check .............................................................................................................. 3-30
3.20
Aircraft Weight Configuration Functional Check .............................................................................. 3-31
4
INTERFACE TESTING
4-1
4.1
GWX 68 Weather Radar Check ......................................................................................................... 4-1
4.2
Optional Stormscope Functional Check............................................................................................. 4-2
4.3
Optional Traffic System Functional Check ......................................................................................... 4-4
4.4
Optional DME Functional Check ........................................................................................................ 4-5
4.5
Optional ADF Functional Checks ....................................................................................................... 4-6
5
GRS 77/GMU 44 INITIAL ALIGNMENT and STBY COMPASS CALIBRATION
5-1
5.1
Procedure A: GRS 77 Pitch/Roll Offset Calibration .......................................................................... 5-1
5.2
Engine Start........................................................................................................................................ 5-2
5.3
Final GRS 77/GMU 44 Calibration Procedures.................................................................................. 5-3
