Pipistrel ALPHA Trainer
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1 Pipistrel ALPHA Trainer Operators Manual for the LX Instrument Suite Fitted to the Pipistrel ALPHA Trainer with Air Data, Engine Monitoring and AHRS Revision 3 Page 1 of 5
2 ALPHA Trainer Panel Layout EMSIS AHRS IAS Indicator Altimeter Variometer Tachometer Engine Data Display Revision 3 Page 2 of 5
3 System description The LX Navigation Instrument system consists of following instruments: EMSIS AHRS - 80 mm (3⅛ ) unit with artificial horizon and air data source; DAQU engine monitoring box (mounted behind instrument panel); LX Cluster engine data display; IAS indicator - 80 mm (3⅛ ); Altimeter - 80 mm (3⅛ ); Variometer - 57 mm (2¼ ); RPM and hour meter - 57 mm (2¼ ). All instruments are electronic devices connected to the main system electrical bus. They have a familiar needle display recognized immediately by older pilots as well as large digital numbers which are easy to read in all conditions. The only unit which is connected to the airplane pitot and static source is EMSIS AHRS. 1 EMSIS AHRS The EMSIS AHRS is a 80 mm (3⅛ ) instrument and is the central part of the LX instrument system; it and the other instruments turn on immediately after main power is applied. The display is divided into three parts, the upper part displays your track heading (derived from inbuilt GPS) the larger middle section is an artificial horizon indicator and the lower part shows IAS, altitude and QNH. QNH always matches the value which is set on the altimeter. The altimeter has the QNH adjustment knob which is shared between both instruments. Description of commands: Long press on pitch zeroing; Short press on increasing of backlight; Short press on decreasing of backlight; Micro SD slot for future updates. Safety Instructions! Keep the unit powered during flight, otherwise engine data and air data Will be lost from the displays until power is re-applied. Revision 3 Page 3 of 5
4 2 IAS Indicator The IAS instrument is a 80 mm (3⅛ ) unit which consists of a familiar mechanical needle and a large OLED digital display. Both the needle display and the digital indicator show the indicated airspeed in knots. Green, yellow and white bars indicate the different airspeed limitations. Never exceed (VNE) which is clearly marked with the red line. 3 Altimeter The altimeter is a 80 mm (3⅛ ) unit which shows aircraft altitude based on QNH. The altimeter consists of familiar mechanical needle which shows the altitude from zero up to feet. The large OLED digital display shows altitude in feet, FL (flight level) and QNH in InHg. The QNH is adjusted by rotating the knob as shown in the picture. This knob also adjusts the QNH on the EMSIS instrument. 4 Variometer QNH adjustment knob The variometer is a 57 mm (2¼ ) unit and consists of a familiar needle and OLED digital display. The needle shows if the aircraft is climbing or descending. The scale is calibrated from 0 up to ± 2000 ft/min. The large OLED digital display shows: Flight time; UTC. Note: There are no adjustments on this instrument by the pilot. UTC time is obtained through GPS signal, flight time resets to zero after each flight. Revision 3 Page 4 of 5
5 5 LX Cluster Engine Data Display The LX Cluster Engine Data Display is used for monitoring the engine operating parameters. The only exception is fuel tank indicator which indicates fuel tank status in percentage fuel remaining ranging from - 0% (empty) up to 100% (full). Most indicators have multicolored bars to show the preferred operating temperature. The red bar defines the out of limit status and exceeds the Rotax recommended limitations. The LX engine data display shows most settings with colored bars and digital numbers. NOTE: The actual fuel consumption/flow and fuel quantity remaining are calculations based on engine rpm and manifold pressure. These settings are to be used as a guide only and are NOT to be relied upon for the safe operation of the aircraft. If in doubt confirm the fuel quantity remaining before flight. The LX Cluster Engine Data instrument displays the following readings. Oil pressure; Oil temperature; Water temperature; Manifold pressure; CHT 1 & 2; EGT 1, 2, 3 & 4; Fuel pressure; Instant fuel flow*; Fuel % remaining*; Bus voltage; Outside air temperature. NOTE: The actual fuel consumption/flow and fuel quantity remaining are calculations based on engine rpm and manifold pressure. These settings are to be used as a guide only and are NOT to be relied apon for the safe operation of the aircraft. If in doubt confirm the fuel quantity remaining before flight. 6 RPM Meter - Tacho The RPM indicator is a 57 mm (2¼ ) unit which displays the current engine revolutions with both a familiar mechanical needle as well as a large OLED digital display. Color arcs display the operating limitations of the Rotax 912 UL2 engine. The Tacho also includes the Hobbs Hour meter. End of Document Revision 3 Page 5 of 5
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