MGL Avionics Stratomaster Maxi Single Flight II Скачать руководство пользователя страница 12

VSI cal 

 
This is a technical function that is used to calibrate your VSI to read exact rates of climb or 
decent. This function works as a percentage of initial reading. The default setting for this function 
is 100%. Increasing this value increases the VSI reading and decreasing the value decreases the 
reading. 
 
Suggested calibration method. 
After you have installed the instrument, perform a calibration flight. This should be done in very 
calm conditions. Turbulence and thermal activity will make accurate calibration impossible. Many 
areas have ideal conditions during early mornings or late afternoons. 
 
Place the instrument in “feet” units mode for ease of calibration. 
Take your aircraft to a few thousand feet above ground and start a glide with a low power setting. 
Take a stopwatch and when the glide is stable (stable VSI reading) start the stopwatch. Take 
note of your altimeter reading at the same time. 
Continue the stable glide for one minute exactly. After the minute has finished, take another 
reading of your altimeter. 
 
Example: 
VSI reading during stable glide: -400 ft/min 
Start altitude: 2500 ft. 
End altitude: 2050 ft. 
 
In the above example the VSI is under reading by about 12%. Set your VSI calibration 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 equivalent to some mechanical airspeed 
indicators that have an adjustment to set the needle to zero when the aircraft is not moving. 
You would use this function occasionally if you see an airspeed reading when the aircraft is at 
rest. This may be caused by aging of the built in pressure sensor or related electronics. 
When you perform this function, please make sure that no wind is blowing into the pitot tube as 
this would result in an incorrect internal calibration.  
This function also resets your VSI to zero. For maximum  accuracy this should be performed on a 
wind still day. 
You may find that it is difficult to zero the VSI accurately if you perform this inside an aircraft 
hanger if there is any wind outside. This is because the buildings internal pressure will vary 
greatly with the winds airflow. The VSI is a very sensitive instrument. 
 

KFactor 

 
The K-Factor is the number of pulses generated by the fuel flow sender for one liter of fuel. The 
dual range fuel flow sender supplied by MGL Avionics has a K-Factor of 7000 in the low flow 
mode (jet installed) and 1330 for the high flow mode (no jet installed). 
 
You can use the K-Factor to calibrate your fuel flow sender.  
The recommended procedure would be: 
 

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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