DG Flugzeugbau DG-1001M Flight Manual page 111

The following lines will be displayed:
1. RES. TRIP COUNTER: Push the selector knob, N (no) is pre-selected,
rotate the selector knob Y (yes) will be displayed, push the selector knob
to reset the time to zero.
2. RES. MAINT. TIMER: Push the selector knob, N (no) is pre-selected,
rotate the selector knob Y (yes) will be displayed, push the selector knob
to reset the time to the service-interval (25 hours).
3. FLIGHTLOG  PC: Push the selector knob, N (no) is pre-selected, rotate
the selector knob Y (yes) will be displayed, push the selector knob to start
the download of the recorded data. The PC must be connected to the serial
interface (socket close to the radio). Flight log and service data will be
downloaded (see section 7.4.6).
4. SET TIME: Set up time (HH:MM)
5. SET DATE: Set up date (DD.MM.YYYY)
6. STALL FACTOR: With this factor the start of the stall warning will be
set (warning via a buzzer).
Adjustment may be made by flying level and gently stalling the glider to
determine the stalling speed, then fly approx. 5% faster, note the
displayed stall factor (upper centre display) and change the factor in the
set up menu to this value. You have to make the adjustment for one
operating condition only. The sensors for the stall warning make a quasi
angle of attack measurement and thus the stall warning will work in other
operating conditions too (different wing loading, turning flight, airbrakes
extended etc.).
Caution: If the stall factor is set to 0.89 the stall warning is switched off
completely. This setting is only allowed to eliminate a permanent stall
warning in case a sensor fails. Send the DEI for repair to the manufacturer as
soon as possible.
7. CALIBRATE FUEL G(auge): Calibration of the fuel gauge with empty
tank. Push the selector knob, N is pre-selected, rotate the selector knob, Y
will be displayed. Push the selector knob to execute the calibration.
8. SYSTEM SETUP ****: PIN- secured menu. Only for service by the
manufacturer.
9. FREEZE WARNING: Activation (Y) or deactivation (N) of the warning
message. You may deactivate this warning in case no watertanks are
installed. When deactivated the OAT screen will still blink at
temperatures lower than +2°C.
Deactivation and activation see above.
10. AUDIO ALARM: Activation (Y) or deactivation (N) of the alarm tone,
except for the stall warning tone which can't be deactivated. Deactivation
and activation see above.
Note: The signal for the stall warning will not be deactivated.
Issued: October 2010
Copyright DG Flugzeugbau GmbH - any copy or publishing prohibited
Flight Manual DG-1000M
7.14