Flytec – Flytec 4030 * User Manual
Page 20

Setting a GPS NMEA 183 interface
Baud rate:
4,800 baud
Interface:
Input no, output yes
- Garmin: NEMA 183 version 1.5
- Magellan: NMEA 183b
For the final approach computer, a destination co-ordinate must be entered and activated
with the GOTO or ROUTE function.
Normal flight according to MacCready
Theory:
Introduction
In order to reach the highest possible cruising speed, the pilot must fly according to MacCrea-
dy for cruise-optimized desired flight. Assuming that the pilot crosses a valley and expects a
thermal with a climb rate of 2 m/s on the other side, he must select his cruising speed so that
the bar of the MacCready display appears at 2 m/s during the glide phase.
If the bar only displays 1 m/s, he is flying too slowly and wasting precious time. If the pilot now
notices that - at the speed selected - he is coming too close to the ground, he must fly more
slowly. In an extreme case, at the speed for the best glide (that is to say with a MacCready dis-
play of 0 m/s), but never more slowly, as otherwise precious altitude is wasted!
Abbreviations
E:
Glide ratio
Emax:
Maximum glide ratio attainable
VH:
Horizontal speed (relative to the air: true airspeed)
VVE:
Own descent
VVL:
Vertical velocity of the air
VFM:
Speed displayed by the airspeed indicator
VW:
Wind speed
VSi:
Total descent (VVE + VVL)
VSt:
Effective rate of ascent in the thermal
VR:
Cruising speed
The polar and its interpretation
In still air, the polar states the vertical speed of descent V
VE
belonging to the specific horizon-
tal speed V
H
of a craft. V
VE
is a negative value as it represents a downward movement. In the
illustration: polar with and without a head wind
(Polar with head wind: shaded co-ordinate
system)
shows an example of a polar.
Flytec
Operating Instructions FLYTEC 4030
19