MGL Avionics Stratomaster Maxi Single Flight II Скачать руководство пользователя страница 22

Please note that this kind of tubing is not advised for pressurized aircraft. In this case you would 
need to obtain aircraft grade tubing of suitable diameter. You would also have to use hose clamps 
to fasten the hose onto the Stratomaster pitot and static ports. 
 
The Flight II allows you to calibrate the airspeed reading. This is done in the “ASI Cal” menu item. 
The main reason for this is to be able to remove errors introduced due to the airflow around your 
aircraft which may have an effect of your pitot tube pressure. 
 

Rev counter pickup 

 
The above drawing shows a typical connection for a standard “old fashioned” contact breaker 
system. Most electronic ignition systems are very similar, the only difference is that the breaker 
has been replaced with a semiconductor switching device. Most electronic ignition modules have 
an output terminal intended for connection to a rev counter. 
This sample circuit suggests a 2200 ohm resistor (2K2) and a 20V zener diode. Note that the 
zener diode is a polarized device, install with the band marker as shown. This small circuit should 
be installed if older contact breaker ignition systems are used as it is possible for these systems 
to generate very high voltages over the contact breaker. This could potentially damage the 
instrument if no protection is used. The components can be obtained from any electronics parts 
shop and are very inexpensive. 
Most other sources of RPM pickup do not require any further protection. 
 
The Flight II RPM input is quite universally usable. For example, it is common to connect a hall-
effect sensor using the +5V line to supply the sensor. A small magnet it then mounted on a shaft 
(for example rotor shaft of a helicopter) and the hall effect sensor switches every time the magnet 
passes the sensor. 
 
The Flight II needs a typical voltage swing of about 4 to 5.5V minimum to operate and the input is 
A/C coupled for easy installation. This means that the voltage signal may have a DC voltage 
superimposed without affecting the instrument. For example, if you have a signal that varies in 
voltage from 5V to 10V with every pulse, it can be used with the Flight II. 
 
For installations such as with the Rotax DCDI two-stroke engines, the rev counter input is simply 
connected to the grey rev counter wire from the engine. These engines produce six pulses per 
rev (set this up in the relevant menu item). 
Please note that is appears very common that many Rotax engines require a ballast resistor on 
the grey rev counter pickup wire. Some of these engines produce a very noisy signal without this 
ballast that can result in very unstable RPM readings. We have found a resistor of about 220 
ohms to be a good value for most cases. Some engines may need as little as 100 ohms. This 
ballast resistor should in some cases also be used for the Rotax 912 engines. 
 
Most engines produce 0.5, 1 or 2 pulses per revolution. This needs to be setup in the “Calib” 
menu item. 
 

Please note: The 5V supply line is unprotected and intended only for the supply of hall-
effect, optical or geartooth sensors. Connecting any voltages (such as the 12V supply) to 
this line will destroy the instrument. 
The 5V line may supply currents of up to 30mA. Should your sensor require greater 
currents you must supply it from another source.  
 

Содержание Stratomaster Maxi Single Flight II

Страница 1: ...ny functions from Altimeter Airspeed to Fuel level flow Engine RPM and many secondary functions including an automatic flight log The Flight II s light weight small size and high level of functionalit...

Страница 2: ...ge programmable for different engine types 12 Engine Hobbs meter can be preset to any hour minute setting up to 9999 hours 13 Maintenance timer MPI Plug changes etc 14 Automatic flight log logs last 6...

Страница 3: ...formation display four display pages Local pressure setting QNH The menu key Press this key to enter the menu system Enter Select key Used in the menu system or to select one of four auxiliary informa...

Страница 4: ...l monitoring It is intended to be installed in a standard 3 5 instrument panel putout front installation 3 5 refers to the distance between the mounting holes The hole itself is usualy a 3 1 8 size Th...

Страница 5: ...the Menu key Items in the main menu Flight Start End Detect If instrument is setup for automatic flight detect then the word Detect appears In this case this menu function is disabled If your instrum...

Страница 6: ...ntering this function will allow you to view the entries in your flight log The instrument will maintain a log of your last 60 flights Each log entry contains date and time of your take off duration o...

Страница 7: ...will count down to zero when the engine is running A good use for this function is to set the hours until your next spark plug change or engine inspection Calibration This enters a menu system contai...

Страница 8: ...r hour knots According to this selection your airspeed will be indicated in mph km h or knots VSI Select if you would like the VSI to read in feet per minute ft min or in meters per second m s Temp Se...

Страница 9: ...vant function in the main menu Fuel flow Yes No Select if you have a fuel flow sender connected to the Flight II instrument Fuel Level Yes No Select if you have a fuel level sender connected to the Fl...

Страница 10: ...ction ASI low Enter the minimum flight speed indicated airspeed ASI below which you would like the instrument to issue an alarm The alarm is by means of flashing the ASI reading as well as activating...

Страница 11: ...tered here Should you have access to an accurate reference you may use this function to calibrate your altimeter Before you do this ensure that you have your local pressure set to coincide with a cali...

Страница 12: ...to 112 to cancel out the error Zero ASI VSI This setup allows your instrument to measure the zero airspeed reading of the airspeed sensor and set a calibration value internally for this This is equiva...

Страница 13: ...readings The initial accuracy of fuel flow readings is dependant on the viscosity or type of fuel you use added oils installation and finally the temperature of the fuel A good installation can achiev...

Страница 14: ...ender reading has stabilized You will see the sender reading at the top line This could take up to a minute so have patience ENSURE THAT THE FLOAT IS NOT SUBMERGED AND IS FLOATING ON TOP OF THE FUEL L...

Страница 15: ...tion e g moving the fuel level sender manually when it is not inserted in to the fuel tank Should you get a slope error message determine the cause of the error If you do not know the cause of your er...

Страница 16: ...2 pulses per revolution A typical Rotax DCDI two stroke engine would generate 6 pulses per revolution The well known Rotax 912 914 engines generate one pulse per revolution Temp Cal This function is i...

Страница 17: ...ur units of measure This to you in the Setup Units menu c Set your alarm limits This you do in the Setup Limits menu d Set your rev counter pulses per RPM setting in the calibration menu e Select your...

Страница 18: ...hipping costs are for the account of the purchaser Note for operation on supplies with inductive loads Any operation of electronic instrumentation on power supplies that are subject to high voltages c...

Страница 19: ...failure or malfunction Under no circumstances does the manufacturer condone usage of this instrument for IFR flights...

Страница 20: ...ender Fuel flow sender Red wire from flow senders Blue wire from flow sender Braid from flow sender Brown Yellow Green Red Blue Orange Green Cannon D 9 connector pin mapping and cable colors 1 ground...

Страница 21: ...o popular belief Pitot tubes are not carefully designed and calibrated but are simple orifices or tubes that get pointed in the direction that you are flying The forward movement of the aircraft cause...

Страница 22: ...is common to connect a hall effect sensor using the 5V line to supply the sensor A small magnet it then mounted on a shaft for example rotor shaft of a helicopter and the hall effect sensor switches...

Страница 23: ...f a gyro plane rotor speed indication The optical reflective pickup can provide a simple means of contactless RPM sensing in difficult installations RPM GROUND 5VDC RPM GROUND 5VDC RPM GROUND 5VDC RPM...

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