Overall dimensions, max:
Mounting frame - 196х430х33 mm;
Computing unit - 198х334х25,4 mm;
Computing unit on frame . 222 x 430 x 33 mm.
Computing unit . not more than 1.4 kg;
Computing unit on frame . not more than2.5 kg.
Supply voltage = 27+5-9V.
Power consumption - not more than 15 Wt.
ARINC 429 - 12 channels.
Potentiometric . 3 channels;
Direct current . 2 channels
Servo resolver signal - 5 channels.
Single command (SC):
SC 27W/case . 9 channels;
SK (27W/break)/ (case/break) . 18 channels.
ARINC 429 . 2 channels;
ARINC 708A . 1 channels (for graphical information output).
Audio - 1 channel (100 mWt per 600 Om).
SC 27W/case . 12 channels;
SC 27W/break . 2 channels.
Sinusoidal vibration - frequency span from 5 Hz to 2000 Hz.
Amplitude vibrant-acceleration to 5 g.
Load impact . to 6.0 g.
Linear acceleration . to 5 g.
Atmosphere pressure . from 12 . till 170 kPa.
High work temperature . 328K (55oC).
Low work temperature . 218K (minus 55oC).
Short-term high work temperature . 343K (70oC).
Extreme high temperature . 358K (85oC).
Extreme low temperature . 213K (минус 60oC).
Relative humidity . not more than 98% by temperature of environment.
Modes of warning
Mode 1 - warning about exceeding of the established limits of barometrical lowering speed.
Mode 2 - warning about exceeding of the established limits of ground approximation speed.
Mode 3 - warning about excessive loose of altitude by aircraft during takeoff or while going to the second round.
Mode 4 - warning about insufficient reserve of altitude over underlying surface, when aircraft is not in landing configuration.
Mode 5 - warning about inadmissible deviation of aircraft lower than approach descent.
Mode 6 - warning about inadmissible discrepancy between relative barometrical altitude and veritable altitude of aircraft, during the attempt to land by pressure (QFE).
Mode 7 - warning about lowering of aircraft to decision altitude (DA) or to altitude 150 m over underlying surface (runway threshold).
Mode 8 - warning about lowering of aircraft to predetermined altitudes (altitude counting).
mode 9 - warning about reaching the extreme meaning of angle of roll.
Mode TAW - Terrain Awareness and Warning (TAW) function: warning about presence of dangerous elements of relief of earth surface or artificial obstacles in flight direction of aircraft.
Mode TCF - Terrain Clearance Floor (TCF) function: warning about premature lowering of aircraft during the flight in airport area and on landing attempt.
System control options
Warning modes control:
- Prohibition of flap position analysis. During the effect of the prohibition the system will use the default value of the parameter "Position of flaps" equal to "Landing" for analysis of criteria of signalization actuation.
- Signalization prohibition in modes EWAE and WRA.
- Suppression of voice signalization in Mode 5 "Glide slope". Will be restored automatically as the airplane enters the area of hard signalization or on full exit from area of Mode 5 signalization actuation.
- Suppression of voice signalization in any mode. Will be restored automatically as the airplane enters to area of another Mode signalization or on full exit from area of actuation of that Mode, which signalization was depressed.
"Relative Altitudes" mode
Graphical information is output in this Mode, if in range of mapping, which corresponds to scale selected by pilot, is available at least one element of underlying surface, over which the excess of airplane is less than 600m. In Relative Altitudes Mode the image of longitudinal side view of underlying surface can be formed.
"Absolute Altitudes" Mode
Graphical information is output in this mode, if there is no elements of underlying surface or artificial obstacles in range of mapping, which corresponds to scale selected by pilot, over which the excess of airplane is less than 600m.
15/15, building 55, Vikentiy Khvoyka str., Kyiv, 04080, Ukraine,
tel. +380 (44) 4251525, e-mail: firstname.lastname@example.org