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G1000/GFC 700 Post Installation Checkout Procedure – Hawker / Beechcraft King Air C90
Revision 5
190-00682-00
6
Final System Checkout
6-1
1.
GPS Failure Test................................................................................................................................ 6-1
6.1
GIA Failure Test ................................................................................................................................. 6-2
6.2
Display Failure Test............................................................................................................................ 6-3
6.3
Cooling Fan Failure Annunciations .................................................................................................... 6-5
6.4
Standby Electrical Power Checks ...................................................................................................... 6-5
6.5
G1000 Backup Path Tests ................................................................................................................. 6-7
7
GFC 700 GROUND CHECKS
7-1
7.1
Pre-Flight Test.................................................................................................................................... 7-1
7.2
AFCS Switch Checks ......................................................................................................................... 7-2
7.3
Autopilot Clutch Overpower Check .................................................................................................... 7-3
7.4
Manual Electric Pitch Trim Speed Check........................................................................................... 7-3
7.5
Autopilot Operation Checks ............................................................................................................... 7-3
8
GFC 700, TAWS and POST MODIFICATION FLIGHT TEST PROCEDURE
8-1
8.1
Before Take-Off.................................................................................................................................. 8-1
8.2
Initial Engagement.............................................................................................................................. 8-1
8.3
Vertical Speed (VS) Mode.................................................................................................................. 8-1
8.4
Pitch Mode (PIT) & Altitude Alerting................................................................................................... 8-2
8.5
Flight Level Change (FLC) Mode & Altitude Capture......................................................................... 8-2
8.6
Altitude Hold (ALT) Mode & Heading Select (HDG) Mode ................................................................ 8-3
8.7
Overspeed Protection Mode .............................................................................................................. 8-3
8.8
NAV Modes ........................................................................................................................................ 8-3
8.9
TAWS ‘FIVE HUNDRED’ Call-out...................................................................................................... 8-5
9
SIGNATURES
9-1
LIST OF ILLUSTRATIONS
LIST OF TABLES
Figure 1-1. G1000 & GFC 700 in King Air C90A/C90GT..........................................................................1-4
Figure 2-1. Software/Configuration Overview ...........................................................................................2-2
Figure 3-1. MFD Power Up Page............................................................................................................3-10
Figure 3-2. PFD Power-up System Annunciations .................................................................................3-11
Figure 3-3. 4th AUX Page .......................................................................................................................3-13
Figure 3-4. Marker Beacon Symbology ..................................................................................................3-15
Figure 5-1. Pitch/Roll Offset ......................................................................................................................5-1
Figure 5-2. G1000 Engine/Airframe Indicators .........................................................................................5-2
Figure 5-3. AHRS Information Valid..........................................................................................................5-7
Figure 5-4. Magnetometer Interference Test ............................................................................................5-8
Figure 7-1. Pre-Flight Test ........................................................................................................................7-1
Table 1-1. Referenced Documentation .....................................................................................................1-2
Table 5-1. Magnetometer Interference Test Sequence ............................................................................5-9
