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Summary of Contents for PV-50

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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...

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