Rvsm Checks; Figure 7-10, Static Port Measurement - Garmin G1000 System Maintenance Manual

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.
HARDWARE
DESCRIPTION
ITEM
1 GIA 63W IAU #1
2
GIA 63W IAU #2
3
GDU 1040A PFD
4 GDU 1040A PFD
5 GDU 1500 MFD
GDC 7400 AIR DATA
6
COMPUTER
GDC 7400 AIR DATA
7
COMPUTER
GTX 33 /33D
*
TRANSPONDER
8
(IF INSTALLED)
GTX 33/33D
*
TRANSPONDER
9
(IF INSTALLED)
* Any other transponder that meets or exceeds the requirements of TSO-C74c (Mode C) or
TSO-C112 (Class 2a; Mode S) may be installed.
Page 7-46
Revision 1
OK
PART NUMBER
MAIN SUB-SYSTEM
GPS/WAAS ENGINE
COMMUNICATION
CERTIFICATION GAINS
MAIN SUB-SYSTEM
GPS/WAAS ENGINE
COMMUNICATION
CERTIFICATION GAINS

Figure 7-10, Static Port Measurement

G1000 / GFC 700 System Maintenance Manual - 300/B300 Series King Air
SOFTWARE
DESCRIPTION PART NUMBER
AUDIO
NAVIGATION
NAV FPGA
AUDIO
NAVIGATION
NAV FPGA
SYSTEM
FPGA
SYSTEM
FPGA
SYSTEM
FPGA
SYSTEM
FPGA
SYSTEM
FPGA
GTX 33 SYSTEM
GTX 33 SYSTEM
SYSTEM STATUS
OK
REPORT
VER
GIA1
GIA1 AUDIO
GPS1
COM1
NAV1
NAV1 FPGA
GFC CERT GIA 1
GIA2
GIA2 AUDIO
GPS2
COM2
NAV2
NAV2 FPGA
GFC CERT GIA 2
PFD1
PFD1 FPGA
PFD2
PFD2 FPGA
MFD1
MFD FPGA
GDC1
GDC1 FPGA
GDC2
GDC2 FPGA
GTX1
GTX2
190-00716-01