Flytec 5020 v1.18 * - Manual (Page 6)

Flytec 5020 technical manual
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Audio threshold Fine tuning of climbing tone max
20 cm 2 cm/sec
Sink tone thres. Activation point of sink tone 0,8 m/s (ft/m)
L.thermal thres Threshold for the last thermal 0.5 to 3.0 m/s
Vario/Spd delay Response time delay for Analogue
Vario and Speed 12 ( » 1,2 sec)
Best L/D Best glide ratio with according
speed
Stallspeed Use of stall alarm and altitude limit 0 km/h (mph)
Spd corr. vane Windwheel 70 ... 150 %
correction 100 %
Units Meter or feet; Km/h or mph or
knots Temp.: In Grd C or Grd F m ; km/h ; Grd C
Coordinate Format * dd°mm,mmm or dd,ddddd or
dd°mm’ss” UTM ; Suisse Grid #
dd,mm,mmm
Time Date Year Time difference to UTC Present
Pilotname Pilot name entry; max 25 letters not set
Glider type Name of glider for OLC not set
Glider ID Glider registration for OLC not set
Del all records Deletion of flight memory (all
records) no
Del all WP& Rts Deletion of all WPs and Routes no
Init EEPROM Back to factory settings No
Init CTRs Reorganization of the memory
Attention: The deletion of waypoints, routes or records needs a few seconds to perform.
Please wait until the confirmation shows up.
1.8 User selectable fields
The main screen as well as the final approach screen can show up to three pages with user
selectable fields. The pages can be selected with the ► key and the page number is
displayed under the battery status as P1 to P3.
Alt a. BG
Safety height above the best glide path* (Not available in first
SW release 1.10 and 1.11)
FL (ft) Flight Level not adjustable by the user
Airspeed Speed measured with the vane wheel, true air speed or calculated
airspeed
Alt a. Gl Calculated height above goal, calculated for a route, including
Windspeed an direction*
Dist Gl Distance to goal calculated along a route*
WindSpd Wind strength*
Vario The digital vario as userfield for the final glide screen
A1 The altitude A1 as userfield for the final glide screen
Dst Toff Distannce to start or flight recognition (acceptance)
Dist Cyl Distance to the radius of a waypoint cylinder in case of a competition route
Dist to WP Distance to chosen destination (waypoint)*
Fl.Time Flight time since take off
GND speed ground speed*(=GS)
Time Time
Bearing Direction to chosen destination*
Wind Spd The calculated windspeed, derived from a circle.
Spd-Diff Wind component (ground speed minus true airspeed)*
Track Flight direction (course)*
Temp Internal temperature