DA 62 AFM
Normal Operating
Procedures
b) ILS
1. Navigation source . . . . . . . . . . . . . . . . . . . . . select LOC using CDI button on
PFD
2. Course bearing pointer . . . . . . . . . . . . . . . . . set using course knob
3. Intercept heading . . . . . . . . . . . . . . . . . . . . . . establish in HDG or ROL mode (if
required)
4. Mode controller . . . . . . . . . . . . . . . . . . . . . . . select APR on mode controller
5. Green or white LOC and GS annunciation . . note on PFD
6. Vertical mode and reference . . . . . . . . . . . . select on mode controller
NOTE
When the selected navigation source is a valid ILS, glideslope
coupling is automatically armed when tracking the localizer.
The glideslope cannot be captured until the localizer is
captured. The autopilot can capture the glideslope from
above or below the glideslope.
END OF CHECKLIST
Doc. No. 11.01.05-E
Rev. 0
11-Jan-2019
Page 4A - 57
Summary of Contents for DA 62
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Page 36: ...DA 62 AFM General 1 7 THREE VIEW DRAWING Doc No 11 01 05 E Rev 0 11 Jan 2019 Page 1 19 ...
Page 363: ...Performance DA 62 AFM Intentionally left blank Page 5 92 Rev 0 11 Jan 2019 Doc No 11 01 05 E ...
Page 438: ...Airplane Description DA 62 AFM Page 7 46 Rev 0 11 Jan 2019 Doc No 11 01 05 E ...
Page 496: ...Handling Care Maintenance DA 62 AFM Page 8 10 Rev 0 11 Jan 2019 Doc No 11 01 05 E 1 4 5 2 3 ...