GI 275 Part 23 AML STC
190-02446-12 Rev. 4
Airplane Flight Manual Supplement
Page 63 of 70
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An annunciator located in the upper right corner of all
configured pages on ADI, HSI and MFD units provides text
annunciations of alert conditions.
For all GI 275 configurations which provide alerts and all
configurations where the GI 275 is interfaced to a GTN with TAWS-B
enabled:
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If a terrain alert occurs and the MFD is not selected to the
dedicated terrain page, then a terrain “popup window” is
provided, which depicts the obstruction generating the alert
with controls provided to either go to the dedicated terrain
page, inhibit the terrain alert, or close the popup window. On a
primary ADI GI 275, if a terrain alert occurs, an annunciation
will illuminate in the top right corner of the display.
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The terrain page and map page, if the terrain overlay is
enabled, will depict the area or obstruction causing the alert as
an area of color corresponding to the alert severity and
encircling the obstruction.
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If Synthetic Vision depiction is turned on, an area
corresponding to the alert area on the map/terrain page is
shaded in the corresponding color for terrain alerts. Obstacle
alerts will cause the relevant obstacle to be depicted in the
alert color in SVT. Powerline alerts do not have a
corresponding indication in SVT.
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In Dual ADI installations, GI 275 generated alert audio is only
provided by the Pilot side GDU. If the Pilot side GDU
becomes inoperative, the Co-Pilot side GDU visual
annunciations may still function, but the aural alerts will not be
heard.
Controls are provided for terrain, obstacle, and wire alerts as follows:
For all GI 275 configurations in which the GI 275 system provides
alerts:
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Controls are provided in the Terrain Page menu. A “Terrain
Inhibit” button inhibits terrain, obstacle, and powerline alerts
when pressed. An annunciation is provided on all configured
pages to indicate that alerts are inhibited. A “Terrain Test”
button initiates a self-test sequence which results in aural and
visual self-test annunciations.
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...
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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...
Page 102: ...SECTION V PERFORMANCE MOONEY MODEL M20M 5 26 ISSUED 3 90...
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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