Garmin Software Version 0458.01 Uživatelská příručka Strana 47

  • Stažení
  • Přidat do mých příruček
  • Tisk
  • Strana
    / 116
  • Tabulka s obsahem
  • KNIHY
  • Hodnocené. / 5. Na základě hodnocení zákazníků
Zobrazit stránku 46
Garmin G1000 Cockpit Reference Guide for the Beechcraft A36/G36
SECTION 6 – AUTOMATIC
FLIGHT CONTROL
6-7
Flight Level Change Mode (FLC)
1. Select the desired altitude by turning the
ALT
knob to set the altitude in the Altitude Select
box.
2. Press the
FLC
key. The flight director is acti-
vated (if not already active) and ‘FLC’ is now
displayed in green in the Active Mode field and
the Airspeed Bug will appear on the Airspeed
Indicator. Pitch and roll commands are given
to manually maintain airspeed. Press the
AP
key to engage the autopilot for maintaining
the current airspeed.
Altitude Hold mode is automatically armed with
ALT’ displayed white in the Armed Mode field
to the right of the ‘FLC’ annunciation.
3. If the autopilot is engaged, the Airspeed
Bug can be adjusted in 1 knot increments by
pressing the
NOSE UP/NOSE DN
keys to set the
desired airspeed. The airspeed setting will be
displayed in the Selected Airspeed box above
Figure 6-15 Flight Level Change Mode
Altitude Hold mode is armed
Airspeed Reference
Selected Airspeed
Airspeed Reference
Bug
Flight Level Change mode is active
Selected Altitude
the Airspeed Indicator and in the Airspeed
Reference field in the AFCS Status Bar.
4. Airspeed may also be changed by pressing and
holding the
CWS
button to manually establish
the desired airspeed using the control wheel.
When the
CWS
button is released, the current
airspeed will be maintained. This method must
be used when using only the flight director.
5. Adjust engine power to allow the autopilot
to fly the aircraft at a pitch attitude which
corresponds to the selected airspeed and the
desired flight profile (descent or climb).
6. With Altitude Hold mode armed, as the selected
altitude is reached, ALT’ will ash in green
for 10 seconds in the Active Mode field, after
which the annunciation stops flashing. This
signals the altitude capture is complete and
the selected altitude will be maintained at the
selected airspeed. If only the flight director is
engaged, pitch and roll commands are given
to manually maintain the selected altitude.
Zobrazit stránku 46
1 2 ... 42 43 44 45 46 47 48 49 50 51 52 ... 115 116

Komentáře k této Příručce

Žádné komentáře