Page 7-46
G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
Revision 1
190-00716-01
7.25 RVSM
Checks
The following are required initial and continued airworthiness checks to verify proper configuration for
operation in RVSM airspace. RVSM operations are prohibited until the all of the RVSM checks are
completed successfully.
7.25.1
RVSM Required Avionics Check
With the PFD in configuration mode, select the System Status page using the small FMS knob. Press the
small FMS knob to activate the cursor. Highlight each of the following items in the LRU window and
verify that the required software part number and version matches the information in the General
Arrangement drawing listed in Table 1-2. By visual inspection of the units, verify hardware part number
matches the information in the General Arrangement drawing listed in Table 1-2. Record the results in
Figure 7-10.
DESCRIPTION
PART NUMBER
DESCRIPTION
PART NUMBER
VER
MAIN SUB-SYSTEM
GIA1
AUDIO
GIA1 AUDIO
GPS/WAAS ENGINE
GPS1
COMMUNICATION
COM1
NAVIGATION
NAV1
NAV FPGA
NAV1 FPGA
CERTIFICATION GAINS
GFC CERT GIA 1
MAIN SUB-SYSTEM
GIA2
AUDIO
GIA2 AUDIO
GPS/WAAS ENGINE
GPS2
COMMUNICATION
COM2
NAVIGATION
NAV2
NAV FPGA
NAV2 FPGA
CERTIFICATION GAINS
GFC CERT GIA 2
SYSTEM
PFD1
FPGA
PFD1 FPGA
SYSTEM
PFD2
FPGA
PFD2 FPGA
SYSTEM
MFD1
FPGA
MFD FPGA
SYSTEM
GDC1
FPGA
GDC1 FPGA
SYSTEM
GDC2
FPGA
GDC2 FPGA
8
*
GTX 33 /33D
TRANSPONDER
(IF INSTALLED)
GTX 33 SYSTEM
GTX1
9
*
GTX 33/33D
TRANSPONDER
(IF INSTALLED)
GTX 33 SYSTEM
GTX2
7
GDC 7400 AIR DATA
COMPUTER
GDU 1500 MFD
5
6
4
GDU 1040A PFD
GDC 7400 AIR DATA
COMPUTER
SYSTEM STATUS
REPORT
1
GIA 63W IAU #1
HARDWARE
ITEM
SOFTWARE
OK
OK
GDU 1040A PFD
2
GIA 63W IAU #2
3
Figure 7-10, Static Port Measurement
* Any other transponder that meets or exceeds the requirements of TSO-C74c (Mode C) or
TSO-C112 (Class 2a; Mode S) may be installed.
Summary of Contents for Cessna Caravan G1000
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