Citation Encore 560 Spécifications télécharger pdf (Page 178)

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SECTION III

INSTRUMENTATION AND AVIONICS

MODEL 560

COMPARISON MONITOR

Selected pilot and copilot input data are compared in the symbol generator. If the difference between

the data exceeds predetermined levels, the out-of-tolerance symbol will be displayed in amber. A list of the

compared signals and the displayed cautionary symbols is given below. When the compared pitch and roll

attitude or glideslope and localizer signals are out of tolerance, a combined level (ATT or ILS) will be

displayed.

Compared Parameter Annunciation Triggering Difference

1. Pitch Attitude “PIT” 5°

2. Roll Attitude “ROL” 6°

3. Heading “HDG”

12°

4. Localizer “LOC”

Approximately dot

5. Glideslope “GS”** Approximately dot

6. Pitch and Roll Attitude “ATT” 5° & 6° respectively

7. Localizer and Glideslope “ILS”

** & dot respectively

8. Indicated Airspeed “IAS”

***

5 Knots

9. Altitude “ALT”

***

200 Feet

If the compared heading sources are not the same (both MAG or TRU) the comparison

monitor is disabled.

These comparisons are only active during flight director, localizer, and glideslope

capture with both NAV receivers tuned to a LOC frequency.

***

Airspeed and altitude displays will flash for ten seconds and then go steady.

3-60 Configuration AA 56OMB-01

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Citation Encore 560 Spécifications Page 178

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