GI 275 Part 23 AML STC
190-02446-12 Rev. 4
Airplane Flight Manual Supplement
Page 57 of 70
navigation source is shown on the left side of the HSI or LDI. CDI source
selection can be synchronized across multiple GI 275 and G500 TXi’s if enabled
by the pilot.
7.14.7
HSI
The course pointer and deviation indicator are shown as a single, solid line for
GPS 1 and VLOC 1, and as an outline with no fill for GPS 2 and VLOC 2. GPS
and VLOC sources are further differentiated with color.
The selected course is displayed above and to the right of the HSI. The selected
course is set via touchscreen keyboard entry or dual-concentric knob.
In addition, the HSI can display two simultaneous bearing pointers sourced from
GPS or VHF NAV.
The bearing pointer display and navigation source are pilot controlled under the
Menu → HSI Options → Bearing sub menus.
The HSI Map includes an integral moving map within the HSI depiction. HSI
map data is a subset of the data on the MFD map page. Traffic, terrain, obstacle,
topographic, and weather overlays are also available for the HSI map. Flight
plan, runways, TAWS FLTAs, and TFRs are always displayed. Overlays are
controlled on the Menu → HSI Options → HSI Map Options → Map Options
menu.
7.14.8
Lateral Deviation Indicator (LDI)
A Lateral Deviation Indicator (LDI) is displayed on the ADI above the heading
display when selected in the Menu. This LDI shows course deviation, navigation
source, and VLOC station identifier or GPS phase of flight. The LDI uses the
same color convention as the HSI .
The LDI incorporates automatic reverse sensing correction into the deviation
display. When the difference between the heading and the selected course is
greater than 107°, the LDI will enable reverse sensing correction. Reverse
sensing correction inverts the course deviation needle and to/from indicator so
that they correctly indicate the direction of the course and waypoint. The course
deviation needle will be deflected in the direction of the desired course, and the
to/from indicator will point in the direction of the waypoint (similar to how the
HSI depiction inverts with heading changes).
Message, waypoint, phase of flight, LOI, and DR annunciations from a GTN or
GNS interfaced to the GI 275 are annunciated on the LDI.
7.14.9
Vertical Deviation Indication (VDI)
Vertical guidance is shown by a vertical deviation indicator (VDI) adjacent to
the altitude tape. The VDI displays glideslope (GS) information from an ILS
source, glidepath (GP) information for a GPS approach, or barometric VNAV
guidance from a GTN navigator.
Summary of Contents for M20M
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Page 10: ...INTRODUCTION MOONEY MODEL M20M BLANK ISSUED 3 90...
Page 12: ...SECTION I GENERAL MOONEY MODEL M20M FIGURE 1 1 THREE VIEW ISSUED 3 90...
Page 60: ...SECTION IV NORMAL PROCEDURES MOONEY MODEL M20M ISSUED 3 90...
Page 78: ...SECTION V PERFORMANCE MOONEY MODEL M20M ISSUED 3 90...
Page 82: ...SECTION V PERFORMANCE MOONEY MODEL M20M 5 6 ISSUED 3 90...
Page 89: ...SECTION V PERFORMANCE ISSUED 3 90 5 13...
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Page 91: ...MOONEY MODEL M20M SECTION V PERFORMANCE ISSUED 3 90 5 1 5...
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Page 97: ...RPM PEAK T I T...
Page 99: ...MOONEY SECTION V MODEL M20M PERFORMANCE ISSUED 3 90 5 23...
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Page 104: ...SECTION V PERFORMANCE MOONEY MODEL M20M 5 28 ISSUED 3 90...
Page 111: ...MOONEY MODEL M20M SECTION VI WEIGHT AND BALANCE M2OM WT BAL RECORD ISSUED 3 90 6 5...
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Page 114: ...SECTION VI WEIGHT AND BALANCE MOONEY MODEL M20M 6 8 ISSUED 3 90...
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Page 157: ...MOONEY M20M SECTION VII AIRPLANE AND SYSTEM DESCRIPTION ISSUED3 90 REV A 1 96 7 23...
Page 176: ...SECTION Vlll HANDLING SERVICE AND MAINTENANCE MOONEY MODEL M20M BLANK ISSUED 3 90...
Page 178: ...SECTION IX SUPPLEMENTAL DATA SUPPLEMENT INSERTED MOONEY MODEL M20M DATE ISSUED 3 90...
Page 180: ...SECTION IX SUPPLEMENTAL DATA MOONEY MODEL M20M BLANK ISSUED 3 90...
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