Home

Warning: Flyers should be aware of the risks to which

1. FD00307012 Modifica centraggio FD02753001 FD06157003 FD04543004 MC02000015 FD00257002 MC06040001 MC02000003 FD02127002 EC15000004 FD06127001 MC06040002 FD02123001 MC02000007 FD06223003 FD40053001 FD05263001 FD04463001 FD01638001 MC22000001 MC02000013 MCO02000051 FD07223006 MC02000018 FD02707002 MCO02000011 MC20000040 MC02000016 Denominazione CANOTTO PORTAPALA O RING mm 55 GHIERA DI SERRAGGIO 2003 GRANO M5X6 INOX CUSCINETTO GUSCIO DI CONTENIMENTO CHIAVETTA BOCCOLA MOZZO TRIPALA ROTAX 2003 GHIERA BLOCC INOX SUPP CHIOCC NEW CHIOCCIOLA TRIP PASSO 2 NEW VITE M4x16 DIN912 INOX VITE PASSO 2 NEW CUSCINETTO VITE M3X10 DIN912 INOX SUPPORTO 2003 MOTORE HP 11342642 GUSCIO DI RINFORZO CUSCINETTO TAPPO CARICO VITE VITE M6X25 DIN912 INOX SUPPORTO ALBERO MIDWEST ALBERO SUPPORTO RONDELLE BOCCOLA PORTASPAZZOLA SPAZZOLE SEEGER 10DIN492 TSEI M6X20 INOX LAMIERINO BLOCCAGGIO 2003 VITE M4X10 DIN912 INOX GHIERA DI FISSAGGIO PALA VITE M8X50 TCEI RONDELLA 8 DIN125 Denomination SUPPORT O RING mm 55 STOP RING NUT 2003 SOCKET SET SCREW BALL BEARING SUPPORT KEY BUSHING FLANGE SUPPORT ROTAX 2003 ADJUSTING NUT INOX SCROLL SUPPORT NEW SCROLL 2 NEW SCREW M4x16 DIN912 SCREW 2 NEW BALL BEARING SCREW 10 DIN912 INOX SUPPORT 2003 MOTOR HP SUPPORT BALL BEARING ADJUSTING NUT SCREW M6x25 DIN912
2. Preventive maintenance Error messages Emergency procedures Manual FL Y Pitch Control Flyspeed Gv 7 1 Inspections Maintenance Repairs Inspections and Maintenance Repairs Shipping and Storing Special tools and materials Electrical flyspeed diagrams Spare parts manual Exploded Drawing Torque values 1 General Information 1 1 Definition of Components Duration 1 1 1 Overhaul Overhaul occurs periodically and involves disassembly components inspection components maintenance replacement and reassembly The overhaul interval is determined by flight hours or calendar days whichever comes first During overhaul the hub must be completely disassembled and closely inspected for cracks excessive wear corrosion or any other anomaly Certain parts must be rebuilt or replaced as specified Overhaul must be performed in accordance with specifications set forth in the overhaul manual E P O M 1 The overhaul service interval is specified in the service bulletin B S 1 No overhaul is required on the F y and Flyspeed GV control units 1 1 2 Repairs Repairs are understood to be correction of minor problems occurring during normal use Any repair does not include and therefore preclude the normal overhaul schedule The type and severity of any damage will determine whether a full overhaul is necessary or not For example damage to a blade due to a ground strike will always require an overhaul 1 1 3 Components duration Expect
3. SUPPORT MIDWEST SHAFT WASHER BUSHING BRUSH HOLDER BRUSH LOCK RING 10DIN492 SCREW M6X20 INOX PLATE 2003 SCREW M4X10 DIN912 INOX STOP RING NUT BLADE SCREW M8x50 DIN912 WASHER 8DIN125 D nomination SUPPORT O RING mm 55 BAGUE ARRET 2003 VIS SANS TETE ROULEMENT SUPPORT CLAVETTE BAGUE SUPPORT A FLASQUE ROTAX 2003 EMBOUT INOX SUPPORT VIS MERE NEW VIS MERE 2 NEW VIS M4x16 DIN912 VIS 2 NEW ROULEMENT VIS M3X10 DIN912 INOX SUPPORT 2003 MOTEUR HP SUPPORT ROULEMENT EMBOUT VIS M6x25 DIN912 SUPPORT MIDWEST ARBRE RONDELLE BAGUE PORTE BROSSE BROSSE ANNEAU ELASTIQUE 10DIN492 VIS M6X20 INOX PLAQUE 2003 VIS M4X10 DIN912 INOX BAGUE ARRET PALE VIS M8x50 DIN912 RONDELLE 8 DIN125 Bezeichnung Qt TRAGER O RING mm 55 BLOCKIERGRIFF 2003 GEWINDESTIFT KUGELLAGER TRAGER PASSFEDER BUCHSE FLANSCH ROTAX 2003 EINSTELLMUTTER INOX GABELKLEMMSTUCK NEW MITNEHMERBUCHSE 2 NEW SCHRAUBE M4x16 DIN912 SCHRAUBE 2 NEW KUGELLAGER SCHRAUBE M3X10 DIN912 INOX TRAGER 2003 MOTOR HP TRAGER KUGELLAGER EINSTELLMUTTER SCHRAUBE M6x25 DIN912 TRAGER MIDWEST BOLZEN SCHEIBE BUCHSE BURSTENHALTER BURSTE SEEGERRING 10DIN492 SCHRAUBE M6X20 INOX PLATTE 2003 SCHRAUBE M4X10 DIN912 INOX BLOCKIERGRIFF SCHRAUBE M8x50 DIN912 SCHEIBE 8DIN125 44 Codice Coda Denominazione Denomination D nomination Bezeichnun Qt FD04703006 MC02000017 F
4. threshold DMP RPM matrix modification and others We recommend you do not make modifications to Default settings without first receiving approval from the manufacturer More Options Flyspeed GV will function with full feathering and reversing hubs High Performance fast pitch change hubs are also compatible High Performance propellers can be used in landing in braking effect 21 Diagnostics and Error Resolution By connecting Flyspeed GV to a PC via serial port you can access and download RPM DMP and electrical current data This is helpful when optimizing motor control and prop pitch parameters System Components Electronic Control and Display Units HALL type solid state RPM sensor with plastic bracket All necessary wiring for hub motor battery and sensors Neodymium magneto for use with the HALL magnetic sensor Optional Installation and Diagnostic Accessories PC Interface Cable serial DB9 Diagnostic and Data Collection Software Additional Options Available Soon 3 Axis Accelerometer for vibration measurement Flyspeed GV Installation Instrument Dial diameter 3 500 mm 88 9 Dashboard Hole diameter 3 125 mm 79 4 Depth 4 00 mm 101 6 Approximate weight 0 5 Ib gr 250 5 7 2 Regulating minimum pitch using the Flyspeed Gv Caution Before starting the engine remove the spinner so as to simplify later adjustments To ensure safety and reduce incidents choose a location which is free and
5. wear or loose connections Verify electric motor functionality and blade pitch change on the ground engine off Visually inspect each prop blade check for cracks dings and any other damage Pay particular attention to the root area EVERY 10 HOURS Remove the spinner and check for cracks corrosion excess wear damage verify that all the seals are intact and that the paint markers for on the bolt nut connections are correct Also perform the before every flight check ONLY AFTER THE FIRST 25 HOURS Grease the bearing sets of the blades the central screw and the bronze scroll and key Perform the 10 hour check ONLY AFTER THE FIRST 50 HOURS Grease the bearing sets of the blades the central screw and the bronze scroll and key Perform the 10 hour check EVERY 100 HOURS Grease the bearing sets of the blades the central screw and the bronze scroll and key In case of salt air conditions or of high temperature variations increase this interval to every 50 hours or three months whichever comes first Using a torque wrench verify the proper setting of the six bolts connecting the hub set to the engine mount also check the aluminum blade sleeves Perform the 10 hour check EVERY 335 HOURS Replace the brushes and brush mountings AT 500 HOURS Remove the blades and disassemble their mountings carefully clean all parts with a mild detergent Grease everything a new as at 100 hours repeat 10 hour and pre flight checks AT 1000 HOURS Com
6. Caution Before manually rotating the propeller ensure that both L amp R magnetos are in the OFF position in order to avoid inadvertently starting the engine 23 5 7 3 2 Hubs with the Slip Ring mounted on the propeller gearbox The magnet is already in place on the aluminum support on the slip ring The HALL sensor has a DB9 type plug which plugs into the back of the Flyspeed GV guide the wire through the firewall and bring it to the prop gearbox Normally the sensor mounting pylon is already assembled and in place In any case it is still necessary to tighten it using a gripping agent such as Loctite 222 Caution It is essential that you do not pass the Flyspeed GV wiring near Magneto wiring or Spark Plug wiring this is to avoid a potential electrical disturbance which could affect the Flyspeed GV s proper interpretation of engine RPM and consequent incorrect functionality The magnetic sensor needs to be carefully positioned above the magnet for proper reading to occur The ideal distance between the magnet and the sensor tip is 1 to 3 mm Set at 1 5 mm Next tighten the support pylon with a torque wrench being careful not to move the sensor positioning Also tighten the plastic support frame using a gripping agent such as Loctite 222 To verify correct magnet positioning connect Flyspeed GV to a 12V power source and then move the propeller manually back and forth so that the magnet passes in front of the sensor Proper positioning will r
7. Drive blades are between 42in and 72in e All weight values are achieved using 64in blade diameters Blade length will affect overall weight Warning e Manufacturer approval is required to install on engines other than those listed above e Acrobatic semi acrobatic and extreme maneuvers are not allowed 5 Installation instructions 5 1 Preparation In order to avoid problems relating to the improper installation and consequently improper functioning of your new propeller we strongly recommend you perform the following check on your aircraft Verify proper carburation jetting Verify carburator balancing syncronization Verify proper gearbox functionality on Rotax engines carefully verify spring preload The gearbox must be equipped with internal clutch as are all certified Rotax engines Besure that the air ducts and airbox are not wholly or partially obstructed Verify that full RPM and full Manifold Pressure are achieved at max throttle setting Carefully clean all surfaces of the engine flange mount with a mild solvent Verify that the flange has not been previuosly damaged by a blade ground strike by having the run out from the centering point and the axial run out inspected by a certified mechanic ensuring they are within the tolerance limits as set by the engine manufacturer Also ensure that there are no visible deformations or cracks which will prevent a perfect contact between the hub and engine flanges This inspect
8. IDLE select ENTER Pitch will transition to LANDING PITCH 96 and MOV LA will be displayed when proper pitch angle is achieved Flyspeed GV will display T OFF and will be ready for landing or go around In the case of landing it will be necessary to execute a PROP CYCLE before take off Flyspeed GV landing pitch will be imposed Following are possible manual settings a After PROP CYCLE pitch angle is determined by the TAKE OFF PITCH parameter value b Selecting IDLE and ENTER will determine pitch angle in accordance with LANDING PITCH parameter value TO land with DMP CONTROL set to OFF reduce power and select LAND manually on 35 c Simultaneously pressing the Y keys will result in LANDING PITCH parameter value Please check for operational modality based on hub type d Selecting IDLE and will freeze pitch angle 5 8 4 Configuration setting and details Flyspeed GV can manage multiple modes full feathering reverse high performance as well as standard a b C d Standard Hub Cannot be employed in Full Feathering Reverse or High Performance modes because of standard pitch angle change velocity Full Feathering Hub Cannot simultaneously handle Reverse and High Performance modes Reverse Hub Cannot simultaneously handle Full Feathering and High Performance modes High Performance hub Cannot simultaneously handle reverse e full feathering 5 8 5 Trouble s
9. Magnet Support Pylon installation 5 7 3 1 Hubs with flange mounted pre assembled Slip Ring Mount the support pylon beneath one of the six bolts fastening the hub set to the engine flange make sure the magnet is facing the brush mounting bracket The HALL sensor has a DB9 type plug which plugs into the back of the Flyspeed GV guide the wire through the firewall and bring it to the brush mounting bracket At this point mount the HALL sensor on the plastic frame and then mount the plastic frame onto the brush mounting bracket Caution It is essential that you do not pass the Flyspeed GV wiring near Magneto wiring or Spark Plug wiring this is to avoid a potential electrical disturbance which could affect the Flyspeed GV s proper interpretation of engine RPM and consequent incorrect functionality The magnetic sensor needs to be carefully positioned perpendicular to the magnet for proper reading to occur The ideal distance between the magnet and the sensor tip is 1 to 3 mm Set at 1 5 mm Next tighten the support pylon with a torque wrench being careful not to move the sensor positioning Also tighten the plastic support frame using a gripping agent such as Loctite 222 To verify correct magnet positioning connect Flyspeed GV to a 12V power source and then move the propeller manually back and forth so that the magnet passes in front of the sensor Proper positioning will result in an RPM reading between 100 and 1000 on Flyspeed GV s display
10. electric hubs the standard version achieves ca 2 sec in continuous motion therefore doubling typical electric hub performance On certain special settings like reverse full feathering and High Performance blade pitch variation occurs at ca 3 5 sec in continuous motion Another unique characteristic of Quinti Avio s props is that they employ mechanical slide limiters rather than electrical ones This is made possible by precision engineering and an innovative electronic constant speed control system Flyspeed GV Flyspeed GV is an evolution of normal constant speed variable pitch electric governors and can be thought of as programmed power and constant speed by automatically selecting more than 10 pre set power settings from a slow descent to a fast climb Flyspeed GV uses a differential sensor to monitor Manifold Air Pressure MAP Intake manifold pressure is constantly compared to atmospheric pressure yielding a value which is used to elaborate throttle setting The DMP setting constantly visible on the Flyspeed GV display stands for Differential Manifold Pressure and is achieved subtracting the pressure differential from 30 0 inches Hence DMP corresponds to MAP only when the ambient pressure is 30 0 inches At full throttle and all altitudes DMP will be between 29 2 and 29 5 inches With a throttle setting below 30 power DMP will be beneath 20 0 inches Flyspeed GV works based on existing conditions and pilot intentio
11. manufacturer 3or2 Identifies se the hub as 3 bladed or 2 bladed WD Identifies the blade manufacturer Warp Drive 001 Identifies the manufacturing batch 001 RorS Identifies the type of hub drilling for Rotax or SAE no 1 001 Identifies version standard hi performance extension for Rotax engines with or without vacuum pump IT0001 Identifies the hub s serial number IT ITALY US USA etc 3 2 Numbering the blades up to 120 HP and HPT HIGH POWER TYPE up to 160 HP The blade s serial number is assigned by the blade s manufacturer Warp Drive by way of an adhesive plate on only one of the blades composing the set The number identifies the type T C or N and the set s number ex T8118 This alphanumeric value is repeated at the hub side base of the blades along with the other alphanumeric values 2BL or 3BL 66 68 70 72 which identify the number of blades and their length Example C8018 3BL 66 C TorN Identifies the blade type C standard blade rectangular end T tapered blade N standard blade nickel leading edge In the case a tapered blade has a nickel leading edge T 8018 Identifies the progressive set numbering assigned by Warp Drive 2BLo3BL Identifies the set as 2 bladed or 3 bladed 66 Identifies the propeller length in inches 4 Hub Technical Specifications 4 1 Rotax Hubs available for 912 9125 914T Hubs with Rotax type mou
12. particular hub motors and will be further explored in later sections of this manual Safety System overload protection is guaranteed in two ways In the case of a malfunction due to an external electrical discharge or system anomaly non responsive to off on cycling a specific emergency channel can be activated which bypasses the entire system Flyspeed GV continuously monitors and limits current according to the limits as specified by the user Additional protection for all modes of operation is provided by two solid state fuses one for Flyspeed GV s general electronic protection and the other for the emergency control channel Simplicity of Use After completing a Prop Cycle CYCLE PROP standard starting procedure pre flight with DMP functionality on DMP ON the F yspeed GV can be utilized simply through normal manipulation of the throttle as when using a fixed pitch propeller Alternatively after CYCLE PROP with DMP functionality off DMP OFF the Y A buttons can be used to select pre programmed pitch settings for takeoff climb cruise medium cruise economic cruise and landing while maintaining constant speed functionality In MANUAL mode the V A buttons increase and decrease blade pitch Do not use in DMP OFF Customizing your Flyspeed GV A Personal Identification Code allows you to access additional functionality specifically to modify configuration parameters such as response control initial pitch setting short circuit
13. pitch setting is in the range of normal flight you may proceed with caution Throttle input should be applied as if employing a fixed pitch propeller Caution The pilot must verify low speed performance on the current pitch setting before initiating landing maneuvers This in order to know what behavior to expect in the case a go around becomes necessary Caution In the event that the blade pitch is frozen at an extremely high or low setting and performance is affected negatively to the point that it is not safe to continue flying it is imperative to land immediately In these cases the engine should be stopped at soon as possible to ensure better glide performance 38 7 0 Inspections Maintenance Repairs LOG BOOK download from web site 7 1 Inspections and Maintenance When environmental conditions are characterized by high humidity levels exposure to corrosive or acidic substances the owner operator must protect the external parts of the hub with an anti corrosive agent such as CRC Regularly scheduled maintenance consists of the following BEFORE EVERY FLIGHT Check the brushes their mountings and the slip ring for wear or damage Also verify that the brushes are positioned correctly Visually inspect all bolts nuts and screws Inspect the spinner and spinner plate Note any grease leaks Check for excessive prop blade play up to 2 pitch play allowed no axial or radial play is allowed Check all wiring for damage
14. the reverse hub type NEVER press the Y A keys simultaneously The subsequent pitch transition to Full Fine could slow the aircraft dramatically and create the conditions of imminent stall 33 5 8 3 OPERATIONAL GUIDELINES TAKE OFF 1 Initiate CYCLE PROP with engine off in order to reach minimum pitch setting If AUTO PROP CYCLE is ON this event will occur after start up During the pitch cycling the Flyspeed GV display will show current level and time and at the completion of the cycle will display T OFF If an error occurs it will default to MANUAL mode 2 Start the engine for warm up taxi and take off 3 Apply full power and when max RPM are reached release the brakes 4 After take off CLIMB mode will automatically be engaged Adjust throttle position for optimal DMP setting If DMP CONTROL is ON F yspeed GV will automatically optimise RPM according to DMP as established through throttle position Take off from high altitude fields while in Automatic Pitch Control If taking off from a higher altitude field than normal it is recommended that you employ a different procedure than normal after the PROP CYCLE sequence has been completed This is to avoid a potential overspeed event which could occur due to the lower air density found at higher elevations Execute a normal PROP CYCLE sequence Start the engine Enter MANUAL mode through the SEL key Re enter PRE SET mode through SEL key and ENTER to confirm At this point D
15. ANDING PITCH while the Flyspeed GV will display MOV LA once the correct pitch is attained T OFF will be displayed and landing or go around are both options In case of a landing it will be necessary to perform PROP CYCLE Caution Do not preset LANDING PITCH value much lower than TAKE OFF PITCH value despite the hub s rapid pitch change rate it may not be able to transit the pitch angle quickly enough to disallow an overspeed in the case of full power re application Caution Employ this operational mode only at safe approach altitudes as the braking effect it generates can quickly slow the aircraft to near stall speed As a consequence of the breaking effect a steeper glide path will be required Caution This functionality is to employed exclusively with hub prop sets specifically designed and tested for high performance use SAFETY CONSIDERATONS In order to avoid engine damage never exceed allowed RPM Flyspeed GV manages maximum power on take off while avoiding RPM overspeed An electrical malfunction could potentially freeze the propeller at a high or low pitch setting In this event the engine may not be able generate sufficient power for take off or climb Inthe event of severe turbulence it may be difficult to manage theF yspeed GV control keys as it may be difficult to operate in an efficient constant speed manner In such cases we recommended employing MANUAL mode Caution While in flight and with
16. CANIL OO SRL CONSTANT SPEED PROPELLERS MADE IN ITALY IN FLIGHT ADUSTABLE PITCH HUB KIT TYPE QA3WDOO5 S N XXXXX_ BLD XXXXXXXX CONTROLLER TYPE XXXXXXX MANUAL WARNING THE HUB DEVICE KIT IS NOT CERTIFIED AND IS NOT APPROVED BY FAA BY PFA OR BY OTHERS AUTHORITIES IT HAS NOT RECEIVED ANY SAFETY OR DURABILITY TESTING APPROVAL AND DOES NOT CONFORMS TO NO AIRCRAFT STANDARDS ITS USE IN STANDARD CATEGORY AIRCRAFT IS PROHIBITED IT IS INTENDED FOR USE IN EXPERIMENTAL UNCERTIFICATED AIRCRAFT IN WHICH AN HUB PROPELLER FAILURE OR BREAKAGE WILL NOT COMPROMISE SAFETY USER ASSUMES ALL RISK OF USE AND ACKNOWLEDGES BY HIS USE THAT HE KNOWS THE STATED LIMITS TEL 0575 842129 FAX 0575 842374 E MAIL QUINTI SISTED IT WWW QUINTIAVIO COM brevettato AREZZO ITALY Warning Flyers should be aware of the risks to which they expose themselves It is good practice to take every and all safety precautions to minimize risk while knowing that it cannot be eliminated altogether A propeller malfunction could be cause for an emergency landing or create vibrations severe enough to damage the aircraft Propellers are constantly subject to vibrations deriving from the motor and aerodynamic forces in addition they are subject to further stress from centrifugal forces Because of this it is essential that the propeller be maintained in accordance with the guidelines set forth in this manual and that it be in
17. D05523005 MC02000041 FD07223004 MC02000019 MC02000020 MC02000023 MC02000024 MC02000002 FD02253003 MC02000050 MC00000049 FD02253002 MC02000048 FD02253001 MC02000045 MC02000047 MC02000043 MC02000046 FD05453001 MC02000039 MC07015003 FD12203001 FD12203002 MC02000056 EC15000009 OPTIONAL COLONNETTA ROTAX NEW EXTENSION VITE M5X10 DIN7991 INOX SLIP RING MIDWEST VITE SPEC 3 8 24x30 ADATTATORE INGRASSATORE RONDELLA 5 IN125 INOX GRANO 5 50 INOX DADO M5 AUTOBL INOX LINGUETTA PER FILO BATTUTA 26 VITE M4X25 DIN912 GRANO M5X25 INOX BATTUTA VITE GRANO M4X4 INOX RONDELLA RITEGNO SPACCO SU VITE GRANO M4X25 INOX RONDELLA 4 IN125 INOX DADO M4 AUTOBL INOX GRANO M4X15 INOX BOCCOLA VITE M5X25 DIN912 INOX O RING mm 82 CHIAVE PER GHIERE CHIAVE CON SPINE ELICOIL M8 FILO TRASMISSIONE DRIVE LUG SCREW M5X10 DIN7991 FINAL DISK MIDWEST SCREW ADAPTER GREASER WASHER 5 IN125 INOX SOCKET SET SCREW NUT M5 INOX LOCK WIRE BUSHING SCREW M4x25 SOCKET SET SCREW BUSHING SOCKET SET SCREW WASHER SOCKET SET SCREW WASHER 4 IN125 INOX NUT M4 INOX SOCKET SET SCREW BUSHING SCREW M5x25 DIN912 INOX O RING mm 82 RINGS TOOL PINS TOOL ELICOIL M8 VIS M5X10 DIN7991 DISQUE FINAL MIDWEST VIS ADAPTEUR GRASSEUR RONDELLE 5 IN125 INOX VIS SANS TETE ECROU M5 INOX BAGUE VIS M4x25 VIS SANS TETE BAGUE VIS SANS TETE RONDELLE VIS SANS TETE R
18. MP control will take over RPM management Max allowable RPM will be a determined by the CLIMB parameter OM DON Caution This procedure will avoid an overspeed event The pilot must recognize that max RPM will be lower than normal and less quickly attained This is important to determining the safety of the take off maneuver Take off from high altitude fields while in Manual Pitch Control If taking off from a higher altitude field than normal it is recommended that you employ a different procedure than normal after the PROP CYCLE sequence has been completed This is to avoid a potential overspeed event which could occur due to the lower air density found at higher elevations Execute a normal PROP CYCLE sequence Start the engine Enter MANUAL mode through the SEL key Increase blade pitch sufficiently to avoid an overspeed At a safe altitude re enter PRE SET mode through SEL key and ENTER to confirm At this point DMP control will take over RPM management pu E NI Caution When in MANUAL mode because of the lower wind resistance after rotation RPM will tend to increase The pilot must consider this tendency and take the appropriate steps to avoid an overspeed event during this initial phase of flight 34 CRUISE With DMP CONTROL ON and flying at high altitude or in non standard temperature humidity conditions the preset RPM DMP settings may require some intervention as MAP will deviate substantially from DM
19. OMY CRUISE for maximum fuel efficiency If fewer than nine cruise settings are preferable they can be reconfigured and reduced through parameter customization If you choose to do so be careful to maintain a linear progression through the range of settings you define While descending or preparing to land blade pitch must revert to an angle close to that used for take off LAND mode achieves that It is engaged by the combination of RPM and DMP values requiring a reduced pitch setting Further reduction in power beneath the minimum DMP setting for LAND will result in IDLE mode and blade pitch will remain fixed no longer constant speed Adding power however will re initiate automatic selection of the appropriate mode from CLIMB to LAND without the necessity of Pilot interaction with Flyspeed GV alternative landing approach is as follows Reduce power until the Flyspeed GV displays IDLE Press ENTER below NO MOVE RPM and minimum DMP value Flyspeed GV will select the correct blade pitch specified by LANDING PITCH This will allow the application of full power for take off If LANDINGPITCH is not defined Flyspeed GV can achieve the proper pitch by returning to the minimum allowed When this is occurring MOV_LA is displayed and when the transition is complete TAKE OFF will be displayed confirming that the desired pitch setting has been attained During this relatively short timeframe it is important to be careful not to exceed RPM al
20. ONDELLE 4 IN125 INOX ECROU M4 INOX VIS SANS TETE BAGUE VIS M5x25 DIN912 INOX O RING mm 82 ELICOIL M8 SCHRAUBE M5X10 DIN7991 ENDSCHEIBE MIDWEST SCHRAUBE SCHEIBE 5 IN125 INOX GEWINDESTIFT MUTTER M5 INOX BUCHSE SCHRAUBE M4x25 GEWINDESTIFT BUCHSE GEWINDESTIFT SCHEIBE GEWINDESTIFT SCHEIBE 4 IN125 INOX MUTTER M4 INOX GEWINDESTIFT BUCHSE SCHRAUBE M5x25 DIN912 INOX O RING mm 82 ELICOIL M8 45 12 0 Exploded drawing CHIAVI TOOLS T 8 port 31 enlarged 46 13 0 Torque values Posfteil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil Pos teil number number number number number number number number number number number number number number number number number number number 36 48 42 25 if6mm 25 if5 27 if8mm 27 if 6 mm 39 44 if 8 mm 44 if3 8 50 4 3 n about 37 id about 24 about 34 57 use light glue on 54 61 Posfteil in spare parts manual usare solo chiavi speciali 8 Nm 13 Nm 13 Nm 15 Nm 13 Nm 25 Nm 15 Nm 25 Nm 25 Nm 35 Nm 8 Nm 10 Nm 15 Nm 87 Nm 2 Nm 5 Nm 5 Nm 8 Nm 5 Nm 5 84 9 5 9 5 10 96 9 5 18 27 10 96 18 27 18 27 25 55 5 9 7 3 10 95 64 11 1 45 3 65 3 65 5 84 3 65 N B il costruttore si riserva la facolt di apportare m
21. P because of the lower atmospheric pressure Use the Y keys for the following effect DMP Setting Standard RPM Down once Up once Up twice T OFF 5800 5800 5500 5400 CLIMB 5500 5800 5400 5300 CRUISE 7 5400 5500 5300 5200 CRUISE 6 5300 5400 5200 5100 CRUISE 5 5200 5300 5100 4900 4 5100 5200 4900 4700 CROISE 3 4900 5100 4700 4500 CRUISE 2 4700 4900 4500 4300 CRUISE 1 4500 4700 4300 4100 CRUISE 0 4300 4500 4100 3800 ECON CRUISE 4100 4300 3800 3800 LAND 3800 4100 3800 3800 If you have significantly deviated from standard pre set PRESET functionality and chose to re engage it a new press SEL bottom when in PRESET press ENTER bottom Pitch control will revert to standard DMP control LANDING 1 With DMP CONTROL enabled reduce power until LAND is displayed the correct descent landing pitch will automatically be selected If additional power reduction is necessary Flyspeed GV will freeze blade pitch and 2 display IDLE Transitioning from LAND to IDLE or IDLE to LAND is automatic Applying full power for a go around will not redline however as Flyspeed GV will achieve maximum continuous RPM with TAKE OFF TIME set ON or maximum RPM with TAKE OFF LIMIT set OFF You can achieve reduced pitch for landing in another manner as well to confirm 3 landing intention while the prop is spinning beneath NO MOVE RPM and Flyspeed GV displays
22. T is displayed then confirm with ENTER Constant speed logic will be resumed according to DMP governance Caution Use this functionality exclusively with hubs prop sets predisposed for full feathering functionality Caution This option should be employed only at a sufficient altitude to guarantee a safe power off landing in case of failure to restart the engine Caution Flyspeed GV and full feathering necessitate HIGH PERFORMANCE to be switched OFF Also the LANDING PITCH parameter value must be greater than the TAKE OFF PITCH parameter value this is to avoid the possibility of an overspeed as power is re applied 2 Selecting Reverse This option may be used when the propeller is turning at a speed below NO MOVE RPM and IDLE appears on the display Pressing Y will make REVERSE lt gt available as an option Selecting ENTER will initiate the propeller s transition to full fine which corresponds to reverse and Flyspeed GV will enter MANUAL mode At this point manipulate pitch as necessary with the Y A keys To exit REVERSE mode scroll with SEL and select PRE SE with ENTER You will enter IDLE mode now press and release Y A simultaneously LANDING PITCH 96 will be achieved and the display will show T OFF Allowing you to reapply power as necessary Caution Always use minimum power settings to avoid redlining Caution This functionality is to employed exclusively with hub prop sets specifically designed and tested for reve
23. V In this case do not tighten the one bolt hosting the mounting pylon as it will need to be positioned and tightened only after the brush installation has occurred 5 5 Blade Assembly Installation Once the hub set is mounted to the engine flange ensure the blade mounting cavities specifically the threading the bearing contact surfaces and the o ring slots All must be in perfect condition Repeat for each blade sleeve housing Ensure that the blade steel mounting support that already has a bearing mounted resists pressure and has no superficial cracks or dings which could slow or block its rotation once mounted into the hub housing Each hub housing is identified by a number corresponding the blade which it will host The blade has the corresponding number on the aluminum sleeve Vertically position one of the hub blade housings Insert the bronze key provided with the kit greased into the steel spine of the hubs internal support structure carefully sending it full run positioning it horizontally and parallel to the blade s mounting flange Insert the o ring from the kit greased in the specific notch at the end of the hub s blade housing next to the threading Install the ball bearing unit from the kit greased in the specific notch at the bottom of the hub s threaded housing cavity Grease the entire blade housing cavity including the threading which will host the blade itself Take the blade with your left hand near t
24. and confirming with ENTER If ON maintains TAKE OFF RPM for number of seconds specified in MAX TAKE OFF TIME At timeframe end it enters CLIMB mode automatically precluding the possibility to revert to take off mode If OFF take off mode can be re engaged OFF A will increase pitch reverse engine rotation ON A will increase pitch software direction control ALWAYS USE IN OFF MODE ON For special hubs with fast pitch variation control OFF in all other cases ON For hubs compatible with Full Feathering and or reverse in all other cases 27 F_FEATH REVERSE MAX PROP RPM FC NO MOVE RPM T OFF RPM CLIMB RPM CRUISE 7 RPM CRUISE 0 RPM EC CRUISE RPM LAND RPM T OFF DMP CLIMB DMP CRUISE 7 DMP CRUISE 0 DMP ECONCRUISE DMP LAND DMP COARSE PULSE DUR COARSE PULSE DLY COARSE HYST RPM Active only with EXTENDED PITCH set ON ON reverse OFF full feathering Defines RPM value above which no pitch control will occur Defines RPM value beneath which PROP CYLE can occur before full feathering or reverse can take place or High Performance mode can initiate on special hubs Defines RPM for take off climb fast cruise slow cruise economy cruise landing pattern Defines minimum DMP for take off climb fast cruise slow cruise economy cruise landing pattern Beneath this DMP value further automatic pitch control is not possible while DMP CONTROL is ON defines the duration of
25. avoid a PROP CYCLE from initiating while in flight should Flyspeed GV be inadvertently disconnected from the power supply and immediately reconnected again Once the prop has correctly completed the cycle the Flyspeed GV will default to PRESET mode and RPM TAKE OFF and DMP will be displayed on the screen Caution It is mandatory to conduct the Flyspeed GV PROP CYCLE sequence with engine off before each flight The sequence runs a series of internal and system checks During the max min cycle the display will Show hub motor electrical draw and the time employed to reach the mechanical end runs Both the electrical draw and time values are important indicators of the system s health A high draw value or unusually long time can be indicatory of a potential malfunction within the hub Flyspeed GV will automatically go to MANUAL mode in the case of the instance described above Please see Operational Guidelines for additional information 5 7 5 Preset Parameters and Customization Modifying preset parameters should only be attempted once in possession of extreme operational familiarity with Flyspeed GV and under the guidence of the manufacturer Flyspeed GV is delivered with preset parameters based on the engine type in use 26 In order to manipulate preset parameters turn on Flyspeed GV and immediately press ENTER for two seconds and release From this point until shutdown ACCESS CODE will appear as a menu choice you can reach by scrolling w
26. bolts on the hub s rim tighten with washers and self blocking lug nuts The bolt on the aluminum sleeve does not require a self blocking lug nut Repeat the procedure for each blade Caution Once the propeller installation is complete check aircraft weight and balance parameters to ensure that you have not exceeded the parameters as set forth in the aircraft user manual 5 5 1 Propeller Balancing Balancing the propeller is required in order to avoid the possible waving of warranty coverage We recommend the use of the most accurate instruments available to identify the extent and location of any imbalance Once identified and addressed the remaining imbalance must be equal to or less than 0 20 IPS inches per second If the initial imbalance value is 1 20 IPS or greater the propeller must be removed from the aircraft and balanced statically before being re balanced dynamically We recommend weight placement in a radial patter on the spinner plate 17 5 6 Installing the FLY manual governor non constant speed 5 6 1 General Information The FLY manual control unit consists of a double polarity switch which sends electric current of opposite polarity depending on the switch position UP DOWN which activates the electric motor in a clockwise or counter clockwise direction resulting in an increase or decrease of blade pitch angle This controller doses current to the electric motor through a resistance unit to avoid damage to
27. ccident or misuse are to be performed exclusively by Quinti Avio srl Quinti Avio srl should be notified in every case of accident or inoperability diagnosed through inspection or maintenance The manufacturer or dealer will recommend repair pro cedures or if necessary that the damaged components be returned for factory repair 8 0 Shipping and Storing If the propeller needs to be stored for an extended period of time use the original packaging or similar Store only at temperatures between 20 C and 35 C Centigrade and 1096 and 75 relative humidity Avoid high humidity extreme temperatures and rapid temperature changes All metal components need to be coated with an anti corrosion substance which can be easily removed Most lubricants will be acceptable provided they do not damage other parts If the components will travel by sea or be stored near the sea salt air fog all metal parts should be coated with a thick layer of light grade motor oil 9 0 Special tools and materials With the hub kit is supplied two special keys to use for maintenance Key for 3 in spare parts manual Key for part 24 in spare parts manual We suggest to use LOCTITE 222 for light lock LOCTITE 243 for medium lock LOCTITE 262 for strong lock About greasing operation for Hub maintenance we suggest to use NICO GREASE GN 22 G 395 KLUBER GREASE ISOFLEX LDS 18 SPECIAL A AEROSHELL GREASE 22 MOBILGREASE 28 40 10 0 Electrical flysp
28. ch in time could compromise the transfer of current and consequently blade pitch control Before final tightening of the brush mounting be sure that the brush slide exclusively along the slip ring s metal tracks by manually rotating the propeller Repeat until correctly positioned Once the positioning is correct tighten the brush support via the M6x25 screw once again using a gripping agent like Loctite222 or similar Caution Before manually rotating the propeller ensure that both L amp R magnetos are in the OFF position in order to avoid inadvertently starting the engine Is it absolutely unacceptable for the brush mountings to make contact outside of the metallic tracks Caution If necessary cut the engine cowling to ensure there is no physical contact between it and the brush set We recommend leaving as much space as possible to allow for natural engine oscillation Be sure that when making modifications to the engine cowling you do not inadvertently create openings or gaps outside of the spinner s aerodynamic shadow 5 4 Hub Set Installation Instructions 5 4 1 Rotax Hub Set Remove the six original engine flange tightening bolts and replace with the six tightening bolts provided in the kit Ensure a proper seal is regained when tightening space between any parts is not allowed Carefully clean all contact surfaces engine flange and propeller flange Mount the Hub Set first without the blades or the spinner ensure the
29. clear of objects obstacles and people Also ensure that the area is devoid of gravel sand and other materials which could be sucked into the path of the propeller potentially damaging it and or causing injury to you and others participating in the process Verify max take off RPM with full brakes and chocked wheels progressively apply full throttle To avoid potentially going past red line we recommend starting with a moderate high pitch setting Max take off RPM should be set using the FLY switch at approx 50 propeller RPM beneath max take off RPM as specified in the aircraft operating manual or the engine operating manual Once the correct RPM value is achieved throttle back gently and switch the engine off Regulate the three adjustment points surrounding the electric motor by carefully and uniformly sliding them to touch the support within the hub this sets the physical end run limits Then tighten the adjustment points using the three self blocking lug nuts do this carefully while keeping the adjustment points immobile with a Hallen wrench In case of any doubts regarding the hub installation or the electric pitch control system we ask that you contact the manufacturer or an authorized technician 22 Caution If the adjustment points are not properly registered damage could occur as the rotating asymmetry will result in greater current loads greater friction of the movable parts damage to the adjustment points themselves and dif
30. complete extent to which Quinti Avio srl is held responsible relative to the client Including all expressed and implicit guarantees and all other obligations and any responsibility on the part of Quinti Avio srl relative to contractual and civil obligations The warranty is specific to the owner and non transferable In case the original owner sells or otherwise disposes of the parts and or accessories to a third party the owner must notify the third party that Quinti Avio Srl will make a separate accord of warranty with the third party in the form here represented The owner assumes all responsibility concerning installation procedures proper installation operation maintenance inspection repair and upgrades of the propeller and any accessories As a function of customer service not a warranty service Quinti Avio s personnel and representatives of Quinti Avio are available to answer any questions regarding individual use applications All questions should be accompanied by client address propeller model and serial number Total Time and any other relevant details This manual will be periodically upgraded on web You will find on the web too all the information regarding mandatory upgrades to the products The customer will pawn his self to make upgrade to proper products Parts for upgrade will be in charge to the costumer 3 Nomenclature Part Identification 3 1 Hub Nomenclature Example QA3WDO001R001 QA Identifies the
31. ed parts lifetime is expressed in hours of use Total Time TT and in hours since overhaul Time Since Overhaul TSO Both values are important to determining component duration Certain components may have a limited lifetime meaning they must be replaced after a specified time in use All limited life components are listed on the overhaul manual E P O M 1 An overhaul will bring all parts to zero hours TSO time since overhaul Total Time TT Jis unaffected by an overhaul 1 2 Introduction Quinti Avio s propellers have been designed to maximize performance in all phases of flight take off climb cruise max leveled speed descent and landing Currently carbon blades produced by the US based Warp Drive are used Pitch increase and decrease is produced along the blade s longitudinal axis by an electric motor rotating a main screw at the center of the hub The rotating screw moves a mechanism at the base of each blade which enacts the pitch variation Compared to most propellers on the market Quinti Avio props boast quick pitch control movement Such movement approaches that achieved by hydraulically controlled variable pitch hubs which allow for constant propeller speed regardless of engine RPM Typically electric hubs achieve relatively low pitch variation speeds of ca 1 sec which translates to a performance loss compared to hydraulic hubs Quinti Avio props distinguish themselves by approaching hydraulic hub performance with
32. eed diagrams FLYSPEED GV INSTALLATION rev 2 1 Febr 2002 slow blow user provided current 18A slow blow user provided High current c i m TS E di TEEF e af px p ge x Mote P N M z NC t N SQ Pd ieee shield Re zn DB9 DD N FEMALE MALE permanent magnet Connector Connector Wal 4 po Pressure Inlet Hall effect sensor PANEL CONNECTOR DB9 Female 16 AWG 105 C Nec SHIELDED CABLE 1 Hall effect sens 22AWG 150 C INSTRUMENT BACK VIEW 41 4 PULSE asa R6 TXRS232 Eme 3 Tg C3 C4 a ae ET E eL TT han bibi d C13 100uF 10V tp 1 tp R1 p Mot Curent 7 UP TO 314 2001 0 03 Ohm tp5 BEGINNING 2002 R1 0 4 Ohm Aa E Uu asc char tp4 a A D4 R7 MOT2 7 MOT 1 7 gt g TXRS232 Sw2 6 UP AUTO E DOWN EMERG u 2 rS E UP TOGGLE CCW MIDDLE FREE DOWN TOGGLE CW i SENSOR EE C 5 out a 102 ede 1 4 FrEE 4 GND FLYSPEED GV HC GND 12 Febr 2002 pl POWER BOARD 42 FLYSPEED HC POWER BOARD SIDE A oooo Polyswitch nmooo t nee ip4 P3 qup SIDE B 12 Feb 2002 Rev 2 0 43 11 0 Spare parts manual Codice Code Code Kennziffer FD02507001 MC07015002 FD02727002 MC07005001 MC06035001 FD02507003 FD01343002 FD04433002
33. electric motor impulse insistence in case RPM error margin exceeds that defined by COARSE HYST RPM defines the time interval delay between two consecutive COARSE PULSE DUR impulses defines error margin for electric motor management during broad RPM control events 28 FINE PULSE DUR FINE PAUSE DLY FINE HYST RPM ENG PROP RATIO T OFF PITCH LANDING PITCH MAX DMP RATE LONG PITCH INCR MAX T OFF TIME MIN PROP CYCLE MAX PROP CYCLE DMP OFFSET DMP GAIN DMP WINDOW MAX CYCLE CURRENT MAX MOT CURRENT MED MOT CURRENT MIN MOT CURRENT HI CURRENT DLY SHUNT RESISTOR defines the duration of electric motor impulse insistence in case RPM error margin exceeds that defined by FINE HYST RPM defines the time interval delay between two consecutive FINE PULSE DUR impulses defines error margin for electric motor management during precise RPM control events RPM propeller RPM ratio based on PSRU ratio if applicable take off pitch setting landing pitch setting DMP rate change when it is exceeded pitch increase will occur for the number of seconds as specified in LONG PITCH INCR Only on special High performance hubs see MAX DMP RATE defines time in seconds after which TAKE OFF RPM transitions to CLIMB RPM minimum time to perform CYCLE PROP maximum time to perform CYCLE PROP pre set to 30 0 inches DMP sensibility adjustment calibration defines control window for DMP sensibility define
34. ential readings Flyspeed GV is delivered already tuned complete tuning guidelines can be found however in the service manual 30 5 8 Operational Guidelines 5 8 1 General concepts for Flyspeed GV use with standard hubs and DMP control Take off maximum power is delivered to the propeller while not exceeding the time allowed at the full power setting With speed increase there is a corresponding load decrease on the propeller creating a condition where applied full power could lead to excessive RPM as defined by the engine manufacturer Flyspeed GV will automatically increase blade pitch maintaining constant speed and avoiding red lining or overspeed Once you reach a safe altitude power must be throttled back to the maximum continuous setting as defined by the manufacturer Flyspeed GV will automatically transition to CLIMB mode based on pre programmed parameters where the minimum DMP value for CLIMB will correspond to maximum continuous power The automatic transition to CLIMB occurs after the number of seconds as specified by MAX TAKE OFF TIME If MAX TAKE OFF TIME is OFF the reduction in power setting must occur by throttling back and bringing the DMP value beneath the minimum required by TAKE OFF RPM Current DMP value is constantly visible on the display screen Atcruise altitude any of the many Flyspeed GV cruise settings can be engaged through throttle action There are nine cruise settings CRUISE 7 to CRUISE 0 and ECON
35. esult in an RPM reading between 100 and 1000 on Flyspeed GV s display Caution Before manually rotating the propeller ensure that both L amp R magnetos are in the OFF position in order to avoid inadvertently starting the engine 24 5 7 4 Installing Flyspeed GV on the instrument panel 5 7 4 1 General Information We recommend installing your Flyspeed GV near the engine instruments in a position optimized for pilot visibility and access Avoid placing it near instruments with high electromagnetic emissions or improper shielding Complete all wiring and manifold tube connections before fixing the instrument into place 5 7 4 2 Technical Specifications Input 9 16 V Draw motor excluded lt 0 1A Motor Current 0 1 15A RPM 600 20000 Pressure sensor 10 45 inches Hg Short circuit protection 2 15 A Polyswitch check label for installed version The hub s electric motor is responsible for most of the current draw Flyspeed GV itself only draws approx 0 1A Keeping in mind maximum electric motor draw we recommend installing a 10A breaker only in case of electrical stop system installed use a 15A breaker Caution Before Installing Flyspeed GV ensure that the cabling connecting the battery to the engine starter is sufficiently stout In certain cases on Rotax engines during engine start high current draws were observed approx 170A at peak which resulted in a drop of current to the instrument panel master to below the minimum necessa
36. ferences in pitch between the propeller blades Caution The use of variable pitch propellers requires the presence of a Manifold Pressure Gauge Consult the aircraft operating manual for maximum RPM and Manifold Pressure combinations Pay special attention to RPM settings that are permissible only for limited time periods We recommend using red tape to identify on the RPM gauge directly RPM settings that are to be avoided for extended periods of time In addition the RPM gauge must be registered on an annual basis and the accuracy should be within 50 RPM consistent inaccuracy is cause to replace or repair the instrument Caution In case of any doubts regarding the hub installation or the electric pitch control system we ask that you contact the manufacturer or an authorized technician Caution Never apply direct current to the hub s electric motor Do so only through a Quinti Avio controller Do not attempt to modify pitch without the blade being mounted the end runs could be damaged Never use a battery charger to power the control unit only use professional lab quality stabilized power units that guarantee constant current output of 12 13 8V Caution During the first installation and during overhaul it is possible for a small quantity of grease to leak from the hub onto the spinner and blades use a mild detergent to remove the grease in such cases Any grease loss should end within 15 to 20 hours of operation 5 7 3 RPM Sensor and
37. guide notches are well matched up between the hub and the engine flange With the slip ring mounted behind the gearbox connect the hub wires with the slip ring wires passing them through the center of the engine mounting flange Ensure the hub is properly aligned with the principal axis and is matched up completely with all parts touching Caution In the case of hub installations described in section 5 3 2 exercise caution while sliding the various parts into position Ensure that all wires are carefully wound and completely inside the engine flange cavity to ensure they are not accidentally damaged while positioning the parts Next install six washers and M8 self blocking lug nuts to the six fastening bolts tightening carefully and lightly in an x pattern until the hub and engine flanges are completely in adherence Finally tighten the lug nuts employing a torque wrench being careful to avoid excessive tightening which could result in thread damage to the hub which could result in a general weakening of the part Caution If you are installing a hub with directly mounted slip ring you must install the included magnet mounting pylon beneath one of the six M8 mounting bolts only when using the Flyspeed GV In this case do not tighten the one bolt hosting the mounting pylon as it will need to be positioned and tightened only after the brush installation has occurred In all other cases the mounting pylon will not be necessary as it is incor
38. h Set for Slip Ring equipped hubs for gearbox installation on SUBARU 5 4 Set Installation Instructions 5 4 1 Rotax Hub Set 5 4 2 Instructions for Subaru Eggenfeller Hub Type Installation 5 5 Blade Assembly Installation 5 5 1 Propeller Balancing 5 6 Installing the FLY manual governor non constant speed 5 6 1 General Information 5 6 2 Installing the FLY control unit on the dashboard using a std 2 1 4 diameter hole 5 6 3 Regulating minimum pitch using the manual switch 5 7 Installing Flyspeed GV on the instrument panel 5 7 1 General information 5 7 2 Regulating minimum pitch using the manual switch 5 7 3 RPM Sensor and Magnet Support Pylon installation 5 7 3 1 Hubs with flange mounted pre assembled Slip Ring 5 7 3 2 Hubs with the Slip Ring mounted on the propeller gearbox 5 7 4 Installing Flyspeed GV on the instrument panel 5 7 4 1 General Information 5 7 4 2 Technical Specifications 5 7 4 3 Connecting Flyspeed GV to the Hub s electric motor 5 7 4 4 Connecting the intake manifold pressure tube DMP 5 7 4 5 Initial Flyspeed GV power up 5 5 5 8 5 8 1 5 8 2 5 8 3 5 8 4 5 8 5 5 8 6 5 8 7 6 0 6 1 6 2 7 0 7 1 7 2 8 0 Preset Parameters and Customization Operational Guidelines General concepts for Flyspeed GV use with standard hubs and DMP control General concepts for Flyspeed GV use with special hubs and DMP control OPERATIONAL GUIDELINES Configuration setting and details Trouble shooting
39. he base with the right hand take the aluminum sleeve Ensure that the fitting at the base of the blade matches up with the bronze key you previously installed in the hub Begin to screw in the aluminum sleeve perpendicularly to the housing Continue screwing the blade into place until you are 2 or 3 threads from completion at this point you should guide the bronze key into place by applying downward pressure on the blade while simultaneously rotating it back and forth You ll be sure of having fitted the key into place properly once the blade descends further into place and can no longer move at an angle At this point finish screwing the aluminum sleeve into place Caution The aluminum blade sleeve cannot extend out of the hub housing if it does this is an indication that the blade is not properly hosted in the hub and the installation procedure needs to be repeated Throughout the installation make sure that the o ring remains in place With the particular wrench included in the kit tighten the aluminum blade sleeve using a torque wrench We recommend 2 or 3 tightening loosening cycles in order to expel all the excess grease from the hub blade housing and the blade itself Once that has occurred tighten for the last time at the recommended torque setting Caution Axial play between coupled parts is not allowable Install the provided safety lock which will prevent inadvertent blade sleeve separation Place the lock by lining up at the
40. hooting 1 2 3 If the RPM display shows Flyspeed GV is not receiving RPM data This may be an issue of extremely low RPM or of sensor non connectivity Check the following a Check all Flyspeed GV connections b Verify magnet sensor proximity and magnet polarity c Ensure secure magnet sensor fastening d Damaged or inoperable magnet sensor gt If the problem persists contact an authorized service provider or the manufacturer No DMP variation with different throttle settings a Disconnect Flyspeed GV pressure sensing tube from engine placement Blow into tube lightly Flyspeed GV should register and display a 5 10 pressure increase b Verify that the tubes connected to the carburetors for MAP reading are intact and that all seals are tight so as to rule out the possibility of air leaks gt If the problem persists contact an authorized service provider or the manufacturer Hub motor is inactive a Verify proper Flyspeed GV display function and no error messaging b Set Flyspeed GV to EMERGENCY mode and connect DVM Digital Voltmeter through the slip ring Move selector switch UP and DOWN and verify 12 and 12 Volts With voltage reaching the slip ring ensure motor functionality In voltage absence check all components for functionality including wiring brushes brush mountings etc c The LED will illuminate when the hub motor is turning If that is not occuring be sure the AUTO EMERGENCY switch is
41. imum safety It evolves from typical electric constant speed governors and can be considered to be power programmed at constant speed with the automatic selection of more than 10 pre programmed cruise settings What separates the Flyspeed GV from other normal governors is that it will choose the ideal RPM setting based upon an interpretation of throttle setting while normal governors will require the pilot to make that decision The F yspeed GV uses a differential sensor to monitor Manifold Air Pressure MAP Intake manifold pressure is constantly compared to atmospheric pressure yielding a value that is used to elaborate throttle setting The DMP setting constantly visible on the Flyspeed GV display stands for Differential Manifold Pressure and is achieved subtracting the pressure differential from 30 0 inches Hence DMP corresponds to MAP only when the ambient pressure is 30 0 inches At full throttle and all altitudes DMP will be between 29 2 and 29 5 inches With a throttle setting below 30 power DMP will be beneath 20 0 inches Flyspeed GV works based on existing conditions and pilot intentions The primary pilot intentions are 1 Intention to take off 2 Intention to land 3 Sure to land 4 Intention to abort landing 1 After completing a Prop Cycle Blade pitch automatically settles on the TAKE OFF setting T OFF Automatic pitch control will not occur until RPM values reach the set range as established by T OFF Examp
42. ion should also be performed on new engines Performing all of the above requisites will set us on the right course to achieving a correct propeller installation 5 2 Installation Procedures Before beginning the installation carefully check the materials as you remove them from the original packaging Check the spinner plate the spinner the electrical group the electric motor the prop speed governor the connecting flange the blade mounts and the blades The propeller kit arrives to the client divided into 4 groups Brush Set Hub Set Blade Set Fly or Flyspeed GV 10 53 Installing Brush Set 5 3 1 Brush Set for hubs with slip ring pre installed on hub ROTAX This Brush Set will be installed on the right front side of the gearbox seeing the gearbox from the side of the engine flange mount using the two M8 machined holes Bolt the Brush Set using M8x25 screws along with Loctite 222 gripping agent Place the brush holders and brushes on the slip ring directly above the metal tracks make them touch making sure they are centered Pre load the brushes on the slip ring rotating the center cam apply medium tension to allow for standard brush wear Pre loading excessively will result in faster wear Insufficient pre load will result in increasingly lighter contact pressure as wear reduces the brushes thickness a condition which in time could compromise the transfer of current and consequently blade pitch control Bef
43. ircraft operating manual for maximum RPM and Manifold Pressure combinations Pay special attention to RPM settings that are permissible only for limited time periods We recommend using red tape to identify on the RPM gauge directly RPM settings that are to be avoided for extended periods of time In addition the RPM gauge must be registered on an annual basis and the accuracy should be within 50 RPM consistent inaccuracy is cause to replace or repair the instrument Caution In case of any doubts regarding the hub installation or the electric pitch control system we ask that you contact the manufacturer or an authorized technician Caution Never apply direct current to the hub s electric motor Do so only through a Quinti Avio controller Do not attempt to modify pitch without the blade being mounted the end runs could be damaged Never use a battery charger to power the control unit only use professional lab quality stabilized power units that guarantee constant current output of 12 13 8V Caution During the first installation and during overhaul it is possible for a small quantity of grease to leak from the hub onto the spinner and blades use a mild detergent to remove the grease in such cases Any grease loss should end within 15 to 20 hours of operation 5 7 Installing the Flyspeed GV constant speed governor 5 7 1 General Information The Flyspeed GV constant speed governor is designed to optimize propeller performance in max
44. ith SEL Selecting ACCESS CODE with ENTER will allow you to enter one of the codes described below to gain access to the parameters lists Scrolling through individual parameters is achieved with the SEL key Once a parameter is visible on screen its value can be modified using the Y A UP DOWN keys keeping in mind that the value change will be effective only after confirming with the ENTER key at this point the text STORED will confirm your change System version 7 1 functionality MANUAL PRE SET CYCLE PROP ACCESS CODE DMP CONTROL AUTO PROP CYCLE T OFF TIME LIMIT PROP PITCH DOWN HIGH PERFORMANCE EXTENDED PITCH Pressing the up down arrow keys Y you increase decrease pitch not constant speed functionality Conferm with ENTER key It engages the preset parameter constant speed mode After power up it check cycles the prop from Max Pitch to Min Pitch and their respective mechanical stops Once complete it settles on TAKE OFF mode pitch setting See also AUTO PROP CYCLE After power up press ENTER for two seconds INSERT CODE appears Hit ENTER again and the sequence Y Y Enable DMP Differential Manifold Pressure to manage pitch control ON DMP selects pitch based on DMP RPM correct use OFF RPM is controlled by Y A keys do not use on OFF If ON prop cycle sequence CYCLE PROP is executed automatically If OFF CYCLE PROP needs to be executed manually by selecting with SEL
45. le if Flyspeed GV T OFF RPM are set at 5800 and the broad range set by COARSE HYST RPM is set at 300 RPM it will be necessary to achieve a minimum of 5501 RPM 5800 300 5500 to initiate automatic pitch control In this case after a pre established time interval normally 20 seconds as established by TAKE OFF TIME parameter the CLIMB setting will automatically be inserted to avoid an excessive time period at 100 power setting Ex Rotax 20 2 LAND DMP selects a low pitch setting very close to T OFF thereby yielding moderate thrust while allowing a smooth descent This setting can be used for landing By applying power this flight condition can be exited in order to extend a landing pattern or to remain in a holding pattern 3 A more pronounced descent can be achieved by reducing power until IDLE appears on the F yspeed GV display If the pilot applies full throttle the increase in RPM to near T OFF levels alerts the Flyspeed GV to an aborted landing In this case the CLIMB preset will be engaged which will allow maximum continuous power 4 Comments Unfortunately DMP cannot optimize all flight conditions We could additional sensors such as altitude temperature and humidity measurement but this would result in excess complexity It is however possible to obtain a programmed RPM shift relative to DMP Flyspeed GV will support constant speed even without DMP control but this is possible only with
46. lowances The pitch angle attained in this manner will be slightly higher than that attained on the ground prior to take off the reason being that the motion through the air lightens the load on the blades slightly compared to when the aircraft is stationary on the ground Flyspeed GV during all operational activity constantly monitors the pitch variation mechanisms to ensure that it is functioning properly and efficiently This is achieved by constantly checking the electric current levels High current levels might indicate abnormal mechanical friction Low current levels indicate and electrical anomaly or an increase in resistance at the slip ring or at the brushes 31 5 8 2 General concepts for Flyspeed GV use with special hubs and DMP control 1 Selecting Full Feathering This option may be used when the propeller is turning at a speed below NO MOVE RPM and IDLE appears on the display To engage press V FULL FT lt gt will appear Shut the engine off and press ENTER the propeller will move to full coarse and display MANUAL when it is achieved Flyspeed GV must remain on Before restarting the engine you must press Y A simultaneously and release The prop will transit to LANDING PITCH and Flyspeed GV will display T OFF at this point the engine can be restarted Normal flight can resume in one of two ways 1 Initiate a gentle climb as if in TAKE OFF adding power gently to avoid an overspeed event 2 Press SEL until PRE SE
47. lyspeed Gv 7 1 The following symptoms of incorrect functionality must be addressed immediately Steep Engine and Propeller RPM variation especially when sudden and not co relational to correct pitch control functionality Not to be mistaken for the normal RPM changes that occur when in DMP CONTROL between one parameter setting and another and which can be easily stabilized by tweaking the throttle setting up or down which clears us from the transitional parameter setting determined by DMP WINDOW usually pre set with range of 0 4 inch DMP The Flyspeed Gv display no longer gives any indications In this case and in all other cases where pitch control is lost due to Flyspeed Gv malfunction the following steps should be taken Throttle back if engine speed is high and an overspeed event may be imminent Select EMERGENCY mode with the appropriate switch and modify pitch as necessary using the switch on the left Use short pitch movement inputs to maximize accuracy Caution A long input on the pitch control switch while in EMERGENCY mode can quickly attain a pitch setting which may be in excess of that which was intended A long input could also trip the resetable switch designed to protect the EMERGENCY circuitry which will then make further pitch settings unavailable until it has reset approximately 20 30 seconds Caution If the EMERGENCY mode cannot be called up blade pitch will remain on the most recent setting If the
48. ngine can cause this or the unit may be malfunctioning See footnote 3 under DOUBT RESOLUTION 3 PROP UNDER CURR The hub motor is drawing less current as set by MIN MOT CURR See footnote 3 under DOUBT RESOLUTION 4 PROP OVER CURR The hub motor is drawing more current as set by MIN MOT CURR The motor is absorbing excess amperage Likely causes are increased mechanical resistance due to damage or dirt or a damaged electric motor 5 INVALID PRESET The selected value is outside of the range of available choices Review the manual for acceptable values or contact the manufacturer or dealer 6 NOT PRESET LOADED Flyspeed GV has not yet been pre configured for use See INVALID PRESET above 37 6 0 Emergency procedures Following are potential malfunction sequences which could adversely affect the propeller hub system s operation 6 1 Manual FLY Pitch Control In the case that the FLY manual control is not enacting pitch change it is imperative to determine whether the flight can be safely continued with the pitch angle currently set It is recommended however that you land as soon as possible to avoid the possibility of entering into unsafe flying conditions If the pitch angle is set to fine low pitch exercise caution in order to avoid redlining If the pitch angle is extremely high and developing sufficient power to maintain safe flight is difficult it will become necessary to prepare for an emergency landing A 6 2 F
49. not set to EMERG and that there is not an issue of excess current draw d See error message Footnote 2 gt If the Flyspeed GV s display is operating normally but voltage is still abnormal contact an authorized service provider or the manufacturer Opening the instrument casing will void warranty coverage 36 5 8 6 Preventive maintenance Regularly inspect the brushes and the slip ring Dirty contact patches can be cause of electrical arcing which will reduce component service life and cna cause static noise within the aircraft and may eventually damage Flyspeed GV We recommend periodic wiring inspections be looking for cracked frayed wires loose connections and severe bends folds Also look for leaks crimps cracks and any other damage due to aging and wear to the tubes collecting intake manifold pressure data 5 8 8 Error messages 1 SHORT CYCLE ERR The time employed to cycle the propeller was under MIN CYCLE TIME This can mean that the hub motor required an excess of current or that MAX CYCLE CURRENT is set too low Inspect the hub prop for any mechanical obstructions anomalies 2 LONG CYCLE ERR The time employed to cycle the propeller was over MAX CYCLE TIME This can mean that the hub motor required less current than normal or that MAX CYCLE CURRENT is set too high Check that the AUTO EMERGENCY switch is set to AUTO and that the LED is illuminating An open circuit somewhere between the Flyspeed GV and the e
50. ns The primary pilot intentions are 1 Intention to take off 2 Intention to land 3 Sure to land 4 Intention to abort landing 2 Product Warranty Conditions Te warranty period is All parts composing new propellers supplied by Quinti Avio srl are warranted for a period of 24 months from the date of shipment or 200 hours of operation whichever comes first All accessories supplied by Quinti Avio srl are warranted for a period of three months from the date of shipment or 50 hours of operation whichever comes first Warranty benefits are subject to the following terms and conditions All parts and or accessories must be installed and used in accordance with the guidelines in the operating manuals and under normal operating conditions Parts and or accessories are not to be repaired or modified outside of direct supervision by Quinti Avio srl Parts and or accessories cannot have been damaged as a result of excessive wear improper use negligence accident or in speed conditions in excess of the guidelines set forth by the manufacturer Damaged parts and or accessories should be returned to Quinti Avio srl via pre paid courier Quinti Avio srl s obligations under this warranty do not extend to the labor costs associated with substituting parts making repairs making adjustments or any other work on any propeller The client accepts that the rights and benefits as expressed in this warranty represent the
51. nting flange no 6 holes for 13mm pins set on a diameter of 4 in 101 6 mm and a centering hole of 47 mm Max power applicable only with engines equipped with gearbox Type no of blades max kW max max RPM pitch range Kg Ibs Degrees Std Rev feath QA2WD R 2 60 80 2800 20 55 80 8 4 18 50 QA3WD R 3 90 120 2800 20 55 80 10 7 23 54 42 SAE no 1 type hubs available for Subaru 25 Eggenfellner rated at 160 HP SAE 1 type mounting flange no 6 holes 5 8 in pins 15 87 mm set on a diameter of 4 in 111 125 mm and a centering hole of 2 74 in 57 15 mm Max power applicable only with engines equipped with gearbox and high power blades Type no of blades max kW max max RPM pitch range Kg Ibs Degrees Std Rev feath QA3WD S 3 120 160 2800 20 55 80 11 3 24 90 4 3 SAEno 2type hubs available for Subaru H6 Eggenfellner rated at 200 HP SAE 2 type mounting flange no 6 holes 5 8 in pins 15 87 mm set on a diameter of 4 6 8 in 120 65 mm and a centering hole of 2 74 in 57 15 mm Max power applicable only with engines equipped with gearbox and high power blades no of blades max kW max max RPM pitch range Kg Ibs Degrees Std Rev feath QA4WD S 4 150 200 2800 20 55 80 15 5 34 15 e All weight values are without spinner plate and spinner which typically is ca 1Kg e Propeller diameters mounting Warp
52. odifiche al prodotto in qualsiasi momento e senza preavviso Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft Ibs ft 47
53. ore final tightening of the brushes mounting be sure that the brushes slide exclusively along the slip ring s metal tracks by manually rotating the propeller Repeat until correctly positioned Once the positioning is correct tighten the brushes support via the M6x25 screw once again using a gripping agent like Loctite222 or similar Caution Before manually rotating the propeller ensure that both L amp R magnetos are in the OFF position in order to avoid inadvertently starting the engine Is it absolutely unacceptable for the brushes to make contact outside of the metallic tracks Caution If necessary cut the engine cowling to ensure there is no physical contact between it and the brush set We recommend leaving as much space as possible to allow for natural engine oscillation Be sure that when making modifications to the engine cowling you do not inadvertently create openings or gaps outside of the spinner s aerodynamic shadow 5 3 2 Brush Set for hubs with slip ring to be installed on engine gearbox ROTAX Insert the slip ring wires from the back side of the gearbox through the engine block flange passing hole until the slip ring reaches and engages the appropriate notch in the engine block flange Install the M4 screw bolt on the top side of the gearbox mounting after having passed the slip ring wires through the appropriate holes on the mounting bracket At the same time ensure the M4 anchoring bolt passes through to the opp
54. osite side of the gearbox Tighten the anchoring bolt by adding a washer and self tightening M4 lug nut to the opposite side ensure the gearbox is properly tightened Add two fasteners to the wire ends Install the brush mounting bracket on the back side of the gearbox using the two M6 screw bolt mounting holes and M6x25 bolts apply a gripping agent such as Loctite 222 Ensure that the brushes match up with the metal tracks on the slip ring Caution Before manually rotating the propeller ensure that both L amp R magnetos are in the OFF position in order to avoid inadvertently starting the engine Is it absolutely unacceptable for the brushes to make contact outside of the metallic tracks 5 3 3 Brush Set for Slip Ring equipped hubs for gearbox installation on SUBARU engines This sensor group will be installed on the front right side of the gearbox seeing the gearbox from the engine flange side using the two screw holes on the aluminum plate of the gearbox Mount the brush mounting bracket with the appropriate screws and using a gripping agent such as Loctite 222 Place the brush arms on the slip ring carefully lining them up with the tracks Pre load the brushes on the slip ring rotating the center cam apply medium tension to allow for standard brush wear Pre loading excessively will result in faster wear Insufficient pre load will result in increasingly lighter contact pressure as wear reduces the brush thickness a condition whi
55. plete overhaul to be performed by the manufacturer Overhaul intervals are specified by operational hours and calendar time in months since manufacture An overhaul must be performed after a maximum of 72 months from installation if no more than 24 months have passed since manufacture overhaul when properly stored This means that the calendar time TBO Time Before Overhaul can be a maximum of 96 months Caution In case of an overspeed event up to 11096 of maximum engine RPM a 100 hour inspection will be necessary Between 111 and 120 a manufacturer overhaul will be required In the case greater than 12096 further propeller use is not allowable Consistent overspeed events can result in structural damage to the propeller which are extremely dangerous 39 7 2 Repairs All internal hub components are coated with a special protective lubricant when assembled It is recommended that you protect hub components using diluted motor oil or other corrosion inhibitor Spinner and spinner plate repairs are not allowed when damaged those components must be replaced In the case of electrical system malfunction components must be replaced as they cannot be repaired Repairs must be performed at an authorized service center and or by authorized service personnel all components will be shipped at the owner s expense Repairs required by damage resulting from accident or misuse are not covered by warranty coverage repair of damages resulting from a
56. porated into the slip ring 5 4 2 Instructions for Subaru Eggenfeller Hub Type Installation Subaru Eggenfeller engine mounts do not have mounting bolts rather they have cavities for 5 8 inch bolts If you have said bolts they should be removed Ensure that the hub has the slip ring pre installed and the six 5 8 bolts are already inserted These bolts have reduced diameter on a portion to allow them to properly lodge within the engine flange Ensure during installation that you use the correct parts Carefully clean all contact surfaces engine flange propeller flange slip ring flange Mount the hub gearbox spinner plate assembly without the blades yet mounted on the engine flange being careful to properly line up the mounting bolts and their holes Slide the hub carefully into position Ensure the hub is properly aligned with the principal axis and is matched up completely with all parts touching Next install six washers and 3 8 24 self blocking lug nuts to the six fastening bolts tightening carefully and lightly in an x pattern until the hub and engine flanges are completely in adherence Finally tighten the lug nuts employing a torque wrench being careful to avoid excessive tightening which could result in thread damage to the hub which could result in a general weakening of the part Caution you must install the included magnet mounting pylon beneath one of the six 3 8 24 mounting bolts only when using the Flyspeed G
57. rse use Caution Reverse functionality is for exclusive use with hydroplanes or amphibious aircraft after a water landing for taxiing purposes Caution Flyspeed GV and reverse necessitate HIGH PERFORMANCE to be switched OFF Also the LANDING PITCH parameter value must be equal to the TAKE OFF PITCH parameter value this will allow take off to be performed once the Y A keys have been simultaneously engaged and released Caution A water landing must be executed in automatic mode without confirm landing intention with ENTER Doing so would bring create a situation of likely overspeed as the LANDING PITCH and TAKE OFF values are equal in REVERSE mode 32 3 High performance This mode should be used in high performance aircraft in which the propeller can serve as a braking device upon landing In standard operational mode redlining becomes a real possibility in case power needs to be reapplied quickly In such cases the sudden DMP increase in excess of MAX DMP RATE will initiate rapid within mechanical limits transition from the very low landing pitch angle to a broader pitch angle suitable for reapplying power The preset value for this pitch angle transition is determined by LONG PITCH INCREMENT Subsequent to which normal take off mode will be employed This option may be used when the propeller is turning at a speed below NO MOVE RPM and IDLE appears on the display Selecting ENTER will initiate the propeller s transition to L
58. ry of 9V In such cases Flyspeed GV goes into tilt and will not operate in a standard manner or it will enact a complete re set Flyspeed GV has two separate internal circuits one for automatic operational mode and one for emergency mode The automatic constant speed circuit can be used with or without DMP control Manual mode is also available non constant speed This circuit is protected by an internal solid state Polyswitch with automatic reset You can activate the emergency circuit from the instrument panel The switch can handle currents up to 6A The circuit includes a resetting breaker 30 second reset interval When in emergency mode for best results manipulate propeller pitch in small increments Caution In emergency mode the aforementioned protection limits excessive torque to the pitch adjusting mechanism Ensure that the electric motor is operating in ranges far from the end runs 5 7 4 3 Connecting F yspeed GV to the Hub s electric motor Keeping in mind that wire length dictates wire thickness in cases of current transmission we recommend the use of type 16AWG or 1 38mm 2 cross section wires To properly connect the wires to the to the brush mounting will require you to Place the Flyspeed GV Emergency Auto switch in the Emergency position 25 The wires connecting the brush mounting must be connected so that acting on the UP arrow will result in blade pitch increase Switch the Emergency Au
59. s maximum electric current use during CYCLE PROP defines maximum electric current used in constant speed mode defines maximum electric current used in manual mode Also when using special hubs in full feathering reverse and High Performance modes defines minimum electrical current for the hub motor defines time delay in reading electrical current values 0 05 equal to 50 milliseconds defines the unit s resistance thresholds Current model is 0 10 ohm Check the label for additional info 2000 and 2001 models LC 0 22 ohm HC 0 03 ohm 29 PROP TEST CYCLE automatic propeller self test Only for use during in shop maintenance It should be off during normal flight operations BASIC MODE constant speed functionality disabled Pitch control can be achieved only through manual intervention This function displays the electrical current value and its direction while overload protected FACTORY PRESETS manufacturer s preset parameters Select tables to modify TABLES Table 0 Table 1 Table 2 Table 3 Table 4 Table 5 Table 6 Table 7 Table 8 using ENTER Cycle Flyspeed GV off then on in order change parameter values reserved The user can add change data keeping count of engine characteristics and propeller use Rotax 912 80 HP Rotax 9125 100HP Rotax 914 Turbo Midwest Rotare 105 HP Alfa Romeo avionic conversion Continental C85 non gearboxed Lycoming Subaru 1 82 gearbox Tuning intake pressure differ
60. spected regularly in order to identify any minor issues which if left ignored could become larger problems Any grease escape new vibration or any deviance in typical functioning must be investigated as it could be an indication of something serious which must be resolved We recommend a thorough read through of this manual as it contains all information relevant to your new propeller We especially request a careful reading of the sections dedicated to inspections and controls Thank you for choosing a Quinti Avio propeller If properly inspected and maintained it will grant you safe and reliable service General Index General Information Definition of Components Duration 1 Overhaul 2 Repairs 3 Components duration Introduction RAE A oR MS x N a 2 Product Warranty Conditions 3 Nomenclature Part Identification 3 1 Hub Nomenclature 3 2 Numbering the blades up to 120 HP and HPT HIGH POWER TYPE up to 160 HP 4 Hub Technical Specifications 4 1 X Rotax Hubs available for 912 9125 914T 4 2 SAE no 1 type hubs available for Subaru EJ25 Eggenfellner rated at 160 HP 4 3 SAE no 2 type hubs available for Subaru H6 Eggenfellner rated at 200 HP 5 Installation instructions 5 1 Preparation 52 Installation Procedures 5 3 Installing Brush Set 5 3 1 Brush Set for hubs with slip ring pre installed on hub ROTAX 5 3 2 Brush Set for hubs with slip ring to be installed on engine gearbox ROTAX 5 3 3 Brus
61. tentially damaging it and or causing injury to you and others participating in the process Verify max take off RPM with full brakes and chocked wheels progressively apply full throttle To avoid potentially going past red line we recommend starting with a moderate high pitch setting Max take off RPM should be set using the FLY switch at approx 50 100 propeller RPM beneath max take off RPM as specified in the aircraft operating manual or the engine operating manual Once the correct RPM value is achieved throttle back gently and switch the engine off Regulate the three adjustment points surrounding the electric motor by carefully and uniformly sliding them to touch the support within the hub this sets the physical end run limits Then tighten the adjustment points using the three self blocking lug nuts do this carefully while keeping the adjustment points immobile with a Hallen wrench In case of any doubts regarding the hub installation or the electric pitch control system we ask that you contact the manufacturer or an authorized technician Caution If the adjustment points are not properly registered damage could occur as the rotating assimetry will result in greater current loads greater friction of the movable parts damage to the adjustment points themselves and differences in pitch between the propeller blades Caution The use of variable pitch propellers requires the presence of a Manifold Pressure Gauge Consult the a
62. the motor when the blades reach the end of their pitch range 5 6 2 Installing the FLY control unit on the dashboard using a std 2 1 4 diameter hole Verify proper blade movement on the ground with the engine off when the FLY switch is held in the down fine pitch position the blades reduce pitch angle and the amber ed illuminates when the switch is held in the up coarse pitch position the blades increase pitch angle and the green led illuminates When you reach maximum minimum pitch angles the red led illuminates If you verify exact opposite functionality the wires connecting to the brush must have their positioning inverted Caution Avoid maintaining pressure on the switch once the red led is illuminated it is warning you that you have reached the end run and any insistence will unnecessarily deliver excessive current levels to the electric motor We recommend to never allow the red led to be illuminated for more than 3 5 seconds MANUAL CHANGER PITCH SYSTEM 9 LONG t MECC FN y MP END k z FINE PITCH 18 5 6 3 Regulating minimum pitch using the manual switch Caution Before starting the engine remove the spinner so as to simplify later aqjustments To ensure safety and reduce incidents choose a location which is free and clear of objects obstacles and people Also ensure that the area is devoid of gravel sand and other materials which could be sucked into the path of the propeller po
63. to switch back to Auto Activate MANUAL mode by pressing the SEL key Press the A UP key and verify blade pitch increase Caution Different pitch variation between Automatic and Emergency modes is not acceptable 5 7 4 4 Connecting the intake manifold pressure tube DMP Employ a 5 6mm fuel tube of the same quality and for the same fuel type used by the engine Attach the tube to the appropriate connection on the back of the Flyspeed GV and then connect the other end to the intake pressure outlet of the engine Alternatively connect the tube to a standard MAP instrument using a Y or T connection Ensure proper fastening at all points in order to avoid accidental disconnections 5 7 4 5 Initial Flyspeed GV power up For the first two seconds the screen will display the manufacturer name and product version then Flyspeed GV will enter the PROP CYCLE mode If you select AUTO PROP CYCLE the propeller will automatically complete a cycle from maximum to minimum pitch and then settle to preset take off pitch If AUTO PROP CYCLE is not active the Flyspeed GV screen will display MANUAL Scrolling through the menu you can choose PRESET or CYCLE PROP Before starting the engine it will be necessary to select CYCLE PROP and then ENTER to complete the max min pitch cycle described above The PROP CYCLE function will not occur in any case where propeller revolutions exceed the preset value set by NO MOVE RPM This is to

Warning: Flyers should be aware of the risks to which

Contents

Download Pdf Manuals

Related Search

Related Contents