background image

Page 8 of 8              © 

Lyndhurst Touchdown Services Limited updated February 2007

 

Limit Switch Settings 

(based on Rotax 912 and 912S) 

 
For initial settings we suggest the following: 
 

For propellers fitted with standard ARPLAST controller 

 
Fine pitch limit set to give 5200 rpm at full throttle with aircraft tethered. 
 
Course pitch limit set to give 5200 rpm at full throttle in level flight at full course setting.  
 
 
 

For aircraft fitted with CSC1 Constant Speed controller 

 
Fine pitch limit set to give 5800 rpm (absolute max) at full throttle with aircraft tethered. 
It may be prudent to limit pitch such that max obtainable rpm is 5500 rpm or less. 
The lower the rpm the less likely the engine is to over-speed in the event of a pitch change failure. 
 
Course pitch limit set to give 5200 rpm at full throttle in level flight at full course setting.  

 
 
 

Spinner Clearance 

 
Always allow at least 3mm clearance between the propeller blades and spinner. This allows for slight 
movement of the blades during normal operation. Ensure this clearance is checked throughout the pitch 
range. 
 

Leadscrew Cleaning and lubrication 

 
The leadscrew should be periodically removed, cleaned, lubricated with a light grease and replaced. 
Remove the A/C spinner and slide the tube cover off the micro switch housing. 
 
 
Remove the three M4 cap head screws. Taking care not to 
damage the electrical wires allow the motor assembly to drop 
down.  
 

 
 
 
 
 
 
 
 
 
Using a flat screwdriver unscrew the leadscrew assembly. 
 
 

 
 
 
Remove the leadscrew assembly. Clean it with a solvent but 
do not wash the bearing. Inspect the leadscrew carefully and 
replace if wear is detected. Lubricate the screw with a light 
grease. Re-assemble and check proper operation. 
 
 
 

Summary of Contents for PV-50

Page 1: ......

Page 2: ......

Page 3: ......

Page 4: ......

Page 5: ......

Page 6: ......

Page 7: ......

Page 8: ......

Page 9: ......

Page 10: ......

Page 11: ......

Page 12: ......

Page 13: ......

Page 14: ......

Page 15: ......

Page 16: ......

Page 17: ......

Page 18: ......

Page 19: ......

Page 20: ......

Page 21: ......

Page 22: ......

Page 23: ......

Page 24: ......

Page 25: ......

Page 26: ......

Page 27: ......

Page 28: ......

Page 29: ......

Page 30: ......

Page 31: ......

Page 32: ......

Page 33: ......

Page 34: ......

Page 35: ......

Page 36: ......

Page 37: ......

Page 38: ......

Page 39: ......

Page 40: ......

Page 41: ......

Page 42: ......

Page 43: ......

Page 44: ......

Page 45: ......

Page 46: ......

Page 47: ......

Page 48: ......

Page 49: ......

Page 50: ......

Page 51: ......

Page 52: ......

Page 53: ...the blades are not in place can allow the swash plate to rotate damaging wires at the front of the lead screw TAKE CARE Electronic Control Unit models supplied after 2003 use a solid state controller...

Page 54: ...to earth out on the casing or on the hollow shaft The control rod must be placed directly in the centre of the hollow shaft Cables and other parts of the system should be kept clear of the control ro...

Page 55: ...the counterweights to fit the blades in the hub With all three blades placed in the hub carefully and slowly drive the swash plate back into its delivered position Rotate the counterweights so the oth...

Page 56: ...it will be necessary to replace three of the existing threaded collar nuts with three special ones provided If you intend to wire lock the propeller fixing blots recommended drill the heads at this s...

Page 57: ...the position of the tube that runs outside the lead screw Run the engine and adjust propeller pitch to give the maximum desired fine and coarse settings as determined by flight testing Measure the di...

Page 58: ...ired but we recommend fuses because they cause less voltage drop and are more reliable Schematic As Delivered Modified Digital Pitch Display Mount the display in the panel the displays currently requi...

Page 59: ...e Type Rotax Aircraft Type Maximum pitch measured at diameter Minimum pitch measured at diameter Maximum rpm at minimum pitch measured with the aircraft stationary tethered rpm Please provide as much...

Page 60: ...rse pitch limit set to give 5200 rpm at full throttle in level flight at full course setting Spinner Clearance Always allow at least 3mm clearance between the propeller blades and spinner This allows...

Reviews: