Flygas F.050 Installation And Maintenance Manual Download Page 19

 

19 

 

Draft and possible run out of gasoline 

 

 

Operation  with  low  fuel  in  the  tank  or  other  operation  that  generates  a  air  draft 
from the injection pump (ex. caused by the shaking of the vehicle and then by the 
oscillation  of  fuel  in  the  tanks)  leads  to  a  sudden  deterioration  of  the  fuel  pump 
and  the  wear  of  the  engine  with  the  risk  of  possible  breakage.  In  fact,  the  air 
bubbles sucked do not come back in good percentage to the tank, but they must 
be expelled through the injectors. (In a case of E.F.I. engine) 

 

 

 

The disassembly and assembly of the mechanical fuel pumps MUST BE DONE 
ONLY FROM FLYGAS. A disassembly of the pump without written authorization 
from Flygas, lifts Flygas from any responsibility. 

 

 

 

 

It  is  suggested  to  insert  between  tank  and  fuel 

pump  a  "Gascolator”  (filter  and 

water  decanter)  with  appropriately  sized  sections  to  separate  presence  of 
moisture or water in gasoline and retain dirt in order to avoid the clog of  the inlet 
pumps  filter. 

 

 

 

  

Inspect  frequently  the  cleanliness  of  the  filter,  considering  that  its  eventual 
blockage (because of the small total surface and the filtering fine pattern it may 
happen), would reduce the passage of  gasoline  causing the wear of the engine 
with the potential risk of breakage of the Oldham Joint and sudden turn off. 

 
 

From the fuel pressure regulator to the tank 

 

The  fuel  pressure  regulator    has  an  exit  hole  that  returns  to  the  tank  to  constantly  dispose  the 
amount  of  exceeding  gasoline.  The  connection  pipe  will  have  an  internal  section  not  less  than  6 
mm of diameter, if the length does not exceed 2 meters, otherwise we must increase the diameter 
according to the increased length to re-establish the proper flow.  
Use pipe and fittings of aircraft type (Aeroquip) resistant to 10 bar pressure and gasoline so called 
" Green”, taking care that the connectors are mounted to the heads of the tubes in the correct way, 
as indicated by manufacturer Aeroquip. 

 
 

 

The return of the fuel must have a low resistance to the flow. From the pressure 
regulator to the tanks the maximum tolerated pressure drop is 0.1 bar  

  
 

 

Long  periods  of  fuel  pump    inactivity  or    fuel  pressure  regulator  can  lead  to  a 
deterioration  of  these  elements  and  of  their  components.  The  downtime  should 
not  exceed  30  consecutive  days.  The  presence  of  water,  even  in  very  small 
quantities, could irreparably damage the components compromising the function 
of the complete system. 

 

 

Summary of Contents for F.050

Page 1: ...perimental All the information the technical data and the specific drawings reported in this manual are owned by FLYGAS and they cannot be reproduced neither entirely nor partially without previous ag...

Page 2: ...Experimenter 2 Index 1 FOREWORD 4 2 KIT FUEL PUMP FOR ROTAX DESCRIPTION OF THE PARTS 8 3 TECHNICAL DATA 8 4 INSTALLATION 9 5 INSTALLATION ON ROTAX 914 10 6 OPERATION 16 7 FUEL SYSTEM 17 8 FIRST START...

Page 3: ...nstallation of this system In this case Flygas reserves to repay the full amount paid equal to the invoice and collect all the material as long as it is intact in all its parts not altered or defaced...

Page 4: ...ontains information which are useful for you safety Please observe carefully the indication contained and perform the recommended procedures which if not properly observed could result in damage of th...

Page 5: ...could cause personal injury Regular inspections and careful maintenance will ensure you a safe and proper usage of this kit Read this manual carefully and completely before operating this kit Do not a...

Page 6: ...perational and reliable Make sure that they can be reached in case of emergency Before starting the engine with propeller installed the pilot must ensure that the surrounding area is clear of obstacle...

Page 7: ...uel Pump can cancel the guarantees issued by the engines manufacturer In addition to compliance of the instructions contained in our manual and that of the engine manufacturer all the general measures...

Page 8: ...minium support plate N 3 Allen screw M5 length 12mm N 3 Allen screw M5 length 16mm N 3 Allen screw M6 length 16mm N 1 Diameter 6mm pin L14mm N 2 Diameter 4mm pin L16mm 3 TECHNICAL DATA Total weight in...

Page 9: ...nformation listed below will allow proper installation operation and maintenance At least ONE ELECTRICAL FUEL PUMP MUST BE INSTALLED for emergency and safety reasons This electrical fuel pump must be...

Page 10: ...ening caused by vibration expansion etc The presence of particles of dirt may damage the various and important mechanical seals causing the premature wear by abrasion Therefore avoid that parts of pro...

Page 11: ...11 1 Install the Driving Joint with Loctite 243 2 Tight the Driving Joint with torque aprox 30Nm 3 Insert N 2 pin 4mm diameter in Rotax case...

Page 12: ...m That temporary operations is necessary to find a right Axial Alignment between Fuel Pump and Crank Shaft 6 Install the Fuel Pump and Bell and screw with Loctite 243 the N 3 Allen Screw M5 after neve...

Page 13: ...holes on not properly protected sheets do not lean them on sharp edges or on any other cutting element The thermal expansion of materials and their vibrations during operation of the engine can cause...

Page 14: ...at may cut it If necessary insert a anti pulsations This will avoid excessive stress to the gauge the carburattors the injector and all elements could be deteriorate if pressure is not linear and cons...

Page 15: ...15 10 Install again the Plate The Belt and Fuel Pump and tight N 3 Allen Screw M6 at 10Nm...

Page 16: ...Pressure Fuel Flow Draft Depth Fuel Level 2000 2500 Fuel Temperature 3000 3500 Hour Km 4000 4500 Data 5000 5500 5800 Never carry out the steps during the flight only for testing Perform tests on the g...

Page 17: ...regulator Fuel pressure Electronics Fuel injection system Maximum 3Bar Minimum Flow 100Lt Hour Measured with the pump 15 C Fuel temperature The fuel lines must be designed according to the latest sta...

Page 18: ...nd of impurity especially during installation and then make sure you have made all the connections necessary to provide proper function Example of installation scheme work together electrical fuel pum...

Page 19: ...ing fine pattern it may happen would reduce the passage of gasoline causing the wear of the engine with the potential risk of breakage of the Oldham Joint and sudden turn off From the fuel pressure re...

Page 20: ...arting without propeller and with fly wheel instead of propeller with closed accelerator in an open and proper place away from people especially if not employees Whenever you turn the engine on withou...

Page 21: ...s it might occur for many reasons a leak that could be small at the beginning but it may increase over time This loss would lead to a leakage of gas which inevitably reduces the estimated autonomy of...

Page 22: ...a possible break partial or total or a failure of any component within the system may occur The engine therefore could suddenly shut down or malfunction due to changes in injection timing that are go...

Page 23: ...works on the tanks Every 250 hours Every 250 hours of use make all the scheduled maintenance checks indicated by the engine manufacturer including the above mentioned descriptions Jut for this test k...

Page 24: ...24...

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