Page
110
Max EGT-Inc
N/U [ 0 ]
Maximum Increase in EGT from the Lean Point. This alarm
is active while lean point is active. This alarm will often
generate a false alarm when the load on the engine
significantly reduced during descent. To avoid this false
alarm, reset the Lean Point. (Selecting “Set Lean Page” and
“Yes” activates alarm; “Reset” de-activates alarm.)
Set limit based on experience. A
small value will allow sensitive
detection of EGT increases,
which is useful for detection of
intermittent problems. Normal
operation may require a larger
setting to prevent false alarms
due to normal EGT fluctuation
caused by turbulence or other
small power/load fluctuations.
Max EGT-Dec
N/U [ 0 ]
Maximum Decrease in EGT from the Lean Point. See also
Max EGT-Inc description.
Set limit based on experience.
You may find that this limit is
significantly different from the
Max EGT-Inc. See also Max
EGT-Inc description.
Max Crate
N/U [ 0 ]
Maximum Cooling Rate for CHT – The alarm is provided in
degrees/minute, and corresponds to the maximum rate of
decrease in CHT. No limit applies to the maximum rate of
increase. All cylinders are checked for this limit.
Set limit based on engine
manufacturer’s recommendation.
If no limit is provided, establish a
limit based on experience.
Max CHT
[ 275 F ]
Maximum Cylinder Head Temperature. Often engines will
normally operate significantly lower than the engine
manufacturer’s limit. Consider setting this limit lower than
the maximum to get early warning of abnormal CHTs.
Set according to engine
manufacturer’s recommendation.
Min CHT
[ 150 F ]
Minimum Cylinder Head Temperature. Intended for engine
troubleshooting problems. Also useful as an “engine not
warmed up yet” reminder.
Set limit based on experience or
to zero if not used.
Display
[ 1 ]
Define which page number is your favorite. The instrument
will select this page at power-up, or when leaving the set
pages, after all alarms (if any) are acknowledged. This page
is also selected by double clicking the “Display” button. See
figure 2 for page numbering. This is a very useful feature. Be
sure to use it!
Set the your favorite page
number.
*
Contrast
– The contrast of the LCD display is set on this page. Four levels of contrast may be
selected, 0-3, with the lower settings best for higher ambient temperatures, and the higher settings best
for normal and cooler temperatures. Make your selection to achieve the most desirable appearance of
the display. It may be necessary to change it in response to large ambient temperature changes,
although this is rare. The contrast setting will automatically reset to level 2 at power-up if it is set
below level 2.
5.
INSTALLATION
5.1
Mounting the Instrument – Position and other considerations
The first step in mounting the instrument is selection of a suitable location in the aircraft. The location
must be selected such that it is not exposed to water or fuel, and preferably away from other devices
that generate heat. The instrument does not generate electrical noise that will interfere with radios, nor
is it affected by transmissions from radios or engine ignition systems. It is not likely to affect a
magnetic compass.
The excellent readability making in non-critical as to where the instrument is mounted with respect to
the pilots eyes. The instrument uses an anti-glare window to minimize reflections. Of course the
instrument should be positioned to allow easy access to its front panel buttons.
Summary of Contents for 912 Dragonfly
Page 3: ...Page 2 ...
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Page 25: ...Page 24 Drawing 1 ...
Page 27: ...Page 26 Drawing 2 ...
Page 29: ...Page 28 Drawing 3 ...
Page 31: ...Page 30 Drawing 4 ...
Page 33: ...Page 32 Drawing 5 ...
Page 35: ...Page 34 Drawing 6 ...
Page 37: ...Page 36 Note for Hydraulic Brakes see Appendix B Drawing 7 ...
Page 39: ...Page 38 Drawing 8 ...
Page 41: ...Page 40 Drawing 9 ...
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Page 45: ...Page 44 Drawing 11 ...
Page 47: ...Page 46 Drawings 12A 12B ...
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Page 73: ...Page 72 Drawing 25 ...
Page 75: ...Page 74 Drawing 26 ...
Page 77: ...Page 76 Drawing 27 ...
Page 79: ...Page 78 Wiring1 jpg Drawing 28a ...
Page 80: ...Page 79 Wiring2 jpg Drawing 28b ...
Page 81: ...Page 80 elecLights jpg Drawing 28c ...
Page 83: ...Page 82 Drawing 29 ...
Page 85: ...Page 84 Drawing 30 ...
Page 92: ...Page 91 Appendix B Brakes Manual for BX1320 BX1000 Appendix B Page 1 ...
Page 93: ...Page 92 Appendix B Page 2 ...
Page 94: ...Page 93 Appendix B Page 3 ...
Page 96: ...Page 95 Appendix B Page 5 ...
Page 97: ...Page 96 Appendix B Page 6 ...
Page 98: ...Page 97 Appendix B Page 7 ...
Page 104: ...Page 103 Figure 1a Description of Display Pages ...
Page 105: ...Page 104 Figure 1b Description of Display Pages ...
Page 138: ...Page 137 Appendix C EIS 4000 912 914 ...
Page 139: ...Page 138 Appendix C EIS 4000 912 914 ...
Page 140: ...Page 139 Appendix C EIS 4000 912 914 ...
Page 141: ...Page 140 Appendix C EIS 4000 912 914 End Appendix C ...
Page 155: ...Page 154 Appendix E2 Powerfin Prop Page 2 ...
Page 156: ...Page 155 Appendix E2 Powerfin Prop Page 3 ...
Page 157: ...Page 156 Appendix E2 Powerfin Prop Page 4 ...
Page 158: ...Page 157 Appendix E2 Powerfin Prop Page 5 ...
Page 159: ...Page 158 Appendix E2 Powerfin Prop Page 6 ...
Page 160: ...Page 159 Appendix E2 Powerfin Prop Page 7 ...
Page 161: ...Page 160 Appendix E2 Powerfin Prop Page 8 ...
Page 162: ...Page 161 Appendix E2 Powerfin Prop Page 9 ...
Page 163: ...Page 162 Appendix E2 Powerfin Prop Page 10 ...
Page 164: ...Page 163 Appendix E2 Powerfin Prop Page 11 End of Appendix E2 ...
Page 187: ...Page 186 By Memphis Soaring FIGURE 3 Common Signals ...