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AutoGyro RotorSport CALIDUS Pilot's Handbook Manual

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Copyright of RotorSport UK Ltd
Document number RSUK0060
Pilots Handbook
Gyroplane Type CALIDUS (UK spec only)
RotorSport UK Ltd
Poplar Farm
Prolley Moor
Wentnor
Bishops Castle
SY9 5EJ
Company Reg No 5486550
Phone: +44 (0) 1588 650769
Fax: +44 (0) 1588 650769
Email:
info@rotorsport.org
Approval number DAI/9917/06
Page 1 of 101
Page issue 4, dated 01.07.13

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  • Page 1 Copyright of RotorSport UK Ltd Document number RSUK0060 Pilots Handbook Gyroplane Type CALIDUS (UK spec only) RotorSport UK Ltd Poplar Farm Prolley Moor Wentnor Bishops Castle SY9 5EJ Company Reg No 5486550 Phone: +44 (0) 1588 650769 Fax: +44 (0) 1588 650769 Email: info@rotorsport.org Approval number DAI/9917/06...
  • Page 2 IVO-prop DL3-68 in-flight variable pitch propeller NOTE! This autogyro may be operated only under adherence to the operation limits and the information contained in this manual. The manual should be carried on board the aircraft. The manual is not a replacement for theoretical and practical training as to how to operate this machine.

  • Page 3: Table Of Contents

    Copyright of RotorSport UK Ltd Document number RSUK0060 Table of contents Page 1. GENERAL 1.1 Introduction 1.2 UK Authority for flight 1.3 Explanations and sensible safety measures 1.4 Aircraft description 1.5 Pictorial views 2. OPERATIONAL LIMITS 2.1 Introduction 2.2 Airspeed 2.3 Airspeed indicator marking 2.4 Rotor 2.5 Engine...
  • Page 4 Copyright of RotorSport UK Ltd Document number RSUK0060 6. DESCRIPTION 6.1 Structure 6.2 Controls 6.3 Instrument panel 6.4 Wheels and Tyres 6.5 Seats and belts 6.6 Engine 6.7 Fuel system 6.8 Electrical system 6.9 Pitot and static pressure 6.10 Avionics 6.11 Navigation lights 6.12 Options and Modifications 7.
  • Page 5 Copyright of RotorSport UK Ltd Document number RSUK0060 Amendments Control Page 1. Where & when necessary RotorSport UK Ltd (hereafter referred to as RSUK) will issue updates to this manual, and will notify known owners to review the changes via the RSUK website with changes appropriately identified by a strike in the margin.
  • Page 6 Copyright of RotorSport UK Ltd Document number RSUK0060 FFECTIVE AGES Page Issue Date Page Issue Date Page 1 01.07.13 Page 51 12.9.11 Page 2 12.04.16 Page 52 12.9.11 Page 3 12.04.16 Page 53 12.9.11 Page 4 12.04.16 Page 54 12.9.11 Page 5 12.04.16 Page 55...

  • Page 7: Introduction

    Pilots must make themselves familiar before flight with the special characteristics of this autogyro. Pilots are obliged to read both this pilots manual and the maintenance manual to ensure you are familiar with all equipment and aircraft structure/engine.
  • Page 8 Copyright of RotorSport UK Ltd Document number RSUK0060 PRECAUTIONARY & SENSIBLE SAFETY MEASURES Before flight pilots should familiarise themselves with the appropriate navigational, weather and safety information pertinent to their planned route. Flight in severe turbulence is prohibited. Flight near thunderstorms is prohibited Aerobatics and manoeuvres resulting in reduced “g”...

  • Page 9: Aircraft Description

    Copyright of RotorSport UK Ltd Document number RSUK0060 1.4 AIRCRAFT DESCRIPTION Characteristics:  Autogyro  Airframe manufactured from inert gas welded stainless steel tube  Front aircraft structure is a GRP/CRP monocoque bolted to the airframe.  Two-seat tandem configuration (monocoque design) ...

  • Page 10: Pictorial Views

    Copyright of RotorSport UK Ltd Document number RSUK0060 1.5 PICTORIAL VIEWS OF THE CALIDUS (figure 1, dimensions in mm) Page 10 of 101 Page issue 1, dated 14.01.11...
  • Page 11 Copyright of RotorSport UK Ltd Document number RSUK0060 Front quarter view Rear quarter view Page 11 of 101 Page issue 1, dated 14.01.11...
  • Page 12 Copyright of RotorSport UK Ltd Document number RSUK0060 View from the side Example cockpit view (Centre blank panel for customer GPS fitment) Page 12 of 101 Page issue 1, dated 14.01.11...
  • Page 13 Copyright of RotorSport UK Ltd Document number RSUK0060 Intentionally blank Page 13 of 101 Page issue 2, dated 12.9.11...

  • Page 14: Operational Limits

    2. OPERATIONAL LIMITS 2.1 INTRODUCTION This section defines the limit values for safe operation of the Calidus autogyro. It contains the operation limits established during flight testing, as well as limit values established by test or computation. The existing instrument placards are described.

  • Page 15: Airspeed

    Copyright of RotorSport UK Ltd Document number RSUK0060 Manoeuvre Limitations Aerobatic manoeuvres are prohibited. Manoeuvres involving a deliberate reduction in normal ‘g’ shall be avoided. Maximum bank angle 60 degrees from vertical This aircraft shall be flown by day and under Visual Flight Rules only CROSS-WIND The maximum cross-wind component for takeoff is 22kts.

  • Page 16: Engine

    Copyright of RotorSport UK Ltd Document number RSUK0060 2.5 ENGINE Manufacturer: Bombardier Rotax, Gunskirchen/A Type: Rotax 912 ULS or Rotax 914UL Take-off power: 100 HP/5800 rpm (for 5 minutes max operation), 115HP/5800 for the 914UL (for 5 minutes max operation) Continuous duty: 90 HP/5500 rpm 912ULS, 100 HP/5500rpm 914UL Cylinder head temperature: max.
  • Page 17 Copyright of RotorSport UK Ltd Document number RSUK0060 Evaluation recorded that the approved envelope extremes (with maximum 10kg baggage in the rear passenger footwell) are: Most Forward limit - 125pilot, 74Kg pass, min fuel – 485mm forward of mainwheel axle. Most Rearwards limit - 65Kg pilot, 82Kg passenger, max fuel –...

  • Page 18: Fuel

    Copyright of RotorSport UK Ltd Document number RSUK0060 2.8 FUEL The engine manufacturer recommends unleaded gas station premium fuel (EN228 MOGAS, as allowed under GC No 3 of CAP747, accessible via the CAA website). AVGAS 100LL can be used, although not recommended for long term operation, as the lead in the fuel causes excess plug fouling and problems with the slipper clutch –...
  • Page 19 Copyright of RotorSport UK Ltd Document number RSUK0060 Limitations if fitted with orange end-cap rotor system OPERATING LIMITATIONS Aerobatic Limitations Aerobatic manoeuvres are prohibited. Manoeuvres involving a deliberate reduction in normal ‘g’ shall be avoided. CG Range Limits (Gyroplane) – refer to Pilots Handbook data. Airspeed Limitations Maximum Indicated Airspeed (Vne): 90mph Other Limitations...
  • Page 20 Copyright of RotorSport UK Ltd Document number RSUK0060 Coolant header tank Engine oil tank Coolant Header Tank. Oil tank Filled with 50/50 Capacity 3 ltrs. water/antifreeze Use Shell VSX or equivalent Motorcycle oil SF or SG Fuel tank beside the filler neck (shows 39ltrs capacity if only one tank installed). Fuel capacity: 75 ltrs Preferred fuel: EN228 MOGAS super or super plus...
  • Page 21 Copyright of RotorSport UK Ltd Document number RSUK0060 Luggage lockers 2Kg max Baggage load 2Kg MAX Removable map bag Baggage load (where fitted) 1Kg max 1Kg MAX Static ports – ring around saying ‘Static Port – do not obstruct!’ Canopy handle ‘Ensure locked down before flight!’ On top of control stick (either type of stick grip) Trim, Brake Pre rotate, PTT...
  • Page 22 Copyright of RotorSport UK Ltd Document number RSUK0060 Instructor pack (where fitted). Brake placard only where brake is fitted. Ignition cut off BRAKE switches. ↓ ↑ To switch off, ENGAGE THROTTLE lift safety flaps and pull toggles backwards. - Other If the compass deviation is more than 5°...
  • Page 23 Copyright of RotorSport UK Ltd Document number RSUK0060 If an IVO-prop in-flight variable pitch propeller is fitted in combination with a 914UL turbocharged engine the following placard is fitted adjacent to the manifold pressure gauge or combined engine rpm/manifold pressure gauge, as applicable. Max manifold pressure (take off): 39.9in Hg Max continuous manifold pressure:...

  • Page 24: Emergency Procedure

    Copyright of RotorSport UK Ltd Document number RSUK0060 3. EMERGENCY PROCEDURE 3.1 INTRODUCTION The Calidus gyroplane uses an engine which is not certified to normal aviation standards. Whilst normally reliable, engine reliability cannot be guaranteed, so always bear this in mind.

  • Page 25: Engine Start In The Flight

    Copyright of RotorSport UK Ltd Document number RSUK0060 mast bushes, such that the limit stops are reached. The impact between the limit stops causes the rumble. It is not detrimental to flight operation. 3.3 ENGINE START IN THE FLIGHT The engine should not be deliberately stopped in flight except as part of forced landing training under the supervision of a competent Instructor.

  • Page 26: Gliding Flight & Forced Landings

    Land as soon as possible. After landing, if not already stopped, turn off engine. Turn off the keyswitch. Exit and abandon the autogyro, away from the fire. Call emergency services, use local fire fighting equipment if available & trained to do so.

  • Page 27: Loss Of Control

    Copyright of RotorSport UK Ltd Document number RSUK0060 3.8 LOSS OF CONTROL FUNCTION Loss of primary control systems could be 1. Engine power control. If jammed open, use ignition switches turned on/off to reduce power, and turn off when clear to land in a suitable place. If jammed closed, land as per engine off.

  • Page 28: Vibration

    Copyright of RotorSport UK Ltd Document number RSUK0060 normal manoeuvres, the rotor will quickly slow to a level to match the reduced load – and similarly speed up to match increased loads. If the load is reduced to a point where the centripetal load can no longer support the bending load, then the blades will fold up, and the aircraft will enter an uncontrolled terminal descent.

  • Page 29: Other Equipment Failure

    Copyright of RotorSport UK Ltd Document number RSUK0060 Flight in icing conditions may also lead to ice forming on the inner leading edge of the blade (see photo), leading to vibration and loss of lift performance. Flight in icing conditions is NOT allowed! Photo of rotor blade with significant icing built up.

  • Page 30: Canopy Open In Flight

    Copyright of RotorSport UK Ltd Document number RSUK0060 2. Oil pressure falls to zero, possible loss of pressure. Stop engine, make precautionary landing 3. Water temp gradually or suddenly rises above max temp. Possible loss of coolant. Stop engine, make precautionary landing 4.

  • Page 31: Normal Operational Procedures

    Copyright of RotorSport UK Ltd Document number RSUK0060 4. NORMAL OPERATIONAL PROCEDURE 4.1 INTRODUCTION Section 4. Contains check lists and procedures to be used for the normal operation. Procedures for additional equipment are in Section 8. 4.2 ROTOR RIGGING The aircraft are fitted with 8.4m (orange end caps) rotors or the 8.4m RotorSystem II with red end caps, or the 8.4m RotorSystem II TOPP variant with blue end caps.
  • Page 32 Copyright of RotorSport UK Ltd Document number RSUK0060 Other notable differences: the RotorSystem II hub bar is scalloped, with different lengths of blade to hub bar bolt, and is also heavier than the earlier rotor. Typical weight is 30.5kg (RSII) –...
  • Page 33 Copyright of RotorSport UK Ltd Document number RSUK0060 5. Tighten the nut to the required torque (hand tight, 1-2Nm, never tight), and fit a split pin through the nut, and secure the pin appropriately. 6. There must be minimal sideways free play of the rotor in the head. 7.
  • Page 34 Copyright of RotorSport UK Ltd Document number RSUK0060 Views of orange end-cap rotor system View of rotor bottom Page 34 of 101 Page issue 6, dated 12.04.16...
  • Page 35 Copyright of RotorSport UK Ltd Document number RSUK0060 View of orange cap rotor installed Top view of rotor installed Page 35 of 101 Page issue 6, dated 12.04.16...
  • Page 36 Copyright of RotorSport UK Ltd Document number RSUK0060 Match parts using dot marks on tower, spacer and hub (normally one dot or two dots) Rotor vibration damper A single damper may be located between the rotor head and the mast to dampen out any residual vibration between the rotor and the control stick.
  • Page 37 Copyright of RotorSport UK Ltd Document number RSUK0060 Additional views below show the differences between the original and RotorSystem II construction. Section view of rotor head with RotorSystem II parts shown. Page 37 of 101 Page issue 6, dated 12.04.16...
  • Page 38 Copyright of RotorSport UK Ltd Document number RSUK0060 Old rotor head assy Rotorsystem II head assy View of RotorSystem II fitted (rotor blades not installed). Page 38 of 101 Page issue 6, dated 12.04.16...
  • Page 39 Copyright of RotorSport UK Ltd Document number RSUK0060 WARNING - under MC-227 low-profile metal lock-nuts known as “Binx” nuts replace nyloc nuts for attachment of the teeter-block to the hub-bars. These two nut types must not be interchanged. For further information see AMM RSUK0061. Binx low-profile self-locking nuts Page 39 of 101 Page issue 6, dated...

  • Page 40: Daily Inspection

    Most, if not all, technical problems can be found with a conscientious and careful pre-flight inspection. In your own interest, take the necessary care and attention with your aircraft. The safety and integrity of an autogyro stands and falls with its regular, conscientious examination and maintenance. Use the full pre-flight checklist shown below.
  • Page 41 Copyright of RotorSport UK Ltd Document number RSUK0060 Task Aircraft area Task & task type Powerplant/ Inspect – coolant and oil radiator for condition, security and leakage cont Engine Inspect – all ‘loose’ cables around engine for correct attachment and connection Inspect all engine cowlings secure.

  • Page 42: Flight Operation

    Failure to take appropriate instruction can have fatal consequences. Before commencing flight operations, and before each flight, the pilot must complete a visual check of the autogyro. Expertise necessary to do this it is obtained during the pilot training.
  • Page 43 Copyright of RotorSport UK Ltd Document number RSUK0060 4. Fuel supply on 5. Altimeter adjusted 6. Rudder control effective 7. Wind direction known 8. Minimum equipment functioning. Minimum flight equipment is Compass, Altimeter, Airspeed indicator, slip indicator, Engine rpm gauge, rotor rpm gauge. 9.
  • Page 44 Copyright of RotorSport UK Ltd Document number RSUK0060 Check oil pressure. If not increasing correctly shutdown engine immediately and find the cause. When the engine able to run without the choke, open the choke. For starting a cold engine, have the choke fully closed, (lever pulled rearwards) and throttle closed, otherwise the choke does not work.
  • Page 45 Copyright of RotorSport UK Ltd Document number RSUK0060 about 1900 at 110 rotor rpm, and increasing the engine rpm prematurely will cause the clutch to slip. Normal pre spin is a rotor speed of 200 rpm (maximum Prerotator speed is 280 rpm).
  • Page 46 Copyright of RotorSport UK Ltd Document number RSUK0060 The most economical speed is between 70mph and 80mph. The permissible maximum speed (V ) is either 90 mph (orange cap rotor system) or 120mph (RotorSystemII with red end caps or TOPP variant with blue end caps. must not be exceeded.
  • Page 47 Copyright of RotorSport UK Ltd Document number RSUK0060 LANDING Before making the approach check all key equipment and functions. Ensure brakes are not locked on, and backup electric fuel pump turned on. The landing should take place into wind where practical/permissible. Maximum crosswind limitation is 15kts.

  • Page 48: Performance

    Copyright of RotorSport UK Ltd Document number RSUK0060 WARNING! FUEL MANAGEMENT! ALWAYS plan your fuel loading to suit your flight, with headwinds and alternate airfields in mind. ALWAYS make a safe precautionary landing to get more fuel, rather than wait for an unsafe emergency landing because you have run out of fuel! Check list after flight finish 1.
  • Page 49 70mph in still air, but this should be established by trial for each individual aircraft/loading condition NOISE DATA The Calidus meets the German BUT noise protection requirements for ultralight autogyro of 68dB(A) max. Typical reported result is 61bB(A). TYRE PRESSURE Main landing gear wheels 1.5 to 2.2 bar...
  • Page 50 Copyright of RotorSport UK Ltd Document number RSUK0060 5.3 Height speed diagram Height velocity diagram Speed in mph The height speed diagram indicates the minimum height for the flown speed (IAS), at which a safe landing is considered possible at max all up weight, 8.4m rotors following engine failure.

  • Page 51: Description

    6. DESCRIPTION 6.1 GENERAL STRUCTURE The airframe of the autogyro consists of an inert gas-welded high-grade stainless steel tubing framework, bolted to a composite monocoque occupant enclosure. The tail unit structure is manufactured in GRP (or CRP). The engine is attached via a steel tube carrier (motor mounting frame) at the rear of the mast.
  • Page 52 Copyright of RotorSport UK Ltd Document number RSUK0060 MC-162 introduces an alternative stick-grip, optimised for use with gloved hands (OEM stick grip). To ensure that operating clearances to instrument panel and seats are maintained the alternative installation is supplied as a pre-wired stick-grip assembly. Its placarding is the same in content but positioned differently.
  • Page 53 Copyright of RotorSport UK Ltd Document number RSUK0060 Rear stick A rear seat stick is available for training purposes. It may be fitted with either type of grip. The rear stick is easy to remove, for weight saving or simply if not required. Simply unplug the electrics, remove the two retaining bolts and pull out.
  • Page 54 Copyright of RotorSport UK Ltd Document number RSUK0060 Rudder The rear rudder pedals are connected to the nosegear via steel cable. The front pedals are connected via rods to the nosegear. The nosegear connects to the rudder via cables, retained inside an outer sheath through the keel. Pushing the right pedal will turn the aircraft right in the air and right when on the ground.
  • Page 55 Copyright of RotorSport UK Ltd Document number RSUK0060 Brake lever Brake locking pawl Choke lever Throttle Brake fluid container (with level marks, DOT4 fluid) Note: when topping up the brake fluid, take the cap off, then the rubber concertina between the cap and the reservoir. Top up, and refit the concertina (that keeps air/moisture from the fluid), flattening the concertina as required prior to fitment.
  • Page 56 Copyright of RotorSport UK Ltd Document number RSUK0060 Magneto switches Headset jack plugs and power supply Rear seat headset mounting with instructor kill switch option fitted. Throttle Brake Rear seat throttle and brake instructor pack When fitted, the rear instructor stick carries the same features as the pilots stick – PTT, pre rotate and trim functions.

  • Page 57: Instrument Panel

    Copyright of RotorSport UK Ltd Document number RSUK0060 6.3 INSTRUMENT PANEL The arrangement of the control elements and instrumentation in the cockpit is represented in the photos in fig. 2. Differences may occur depending on the equipment fitted – standard analogue, then with various GPS panel options. See table for warning lamp functions.
  • Page 58 Copyright of RotorSport UK Ltd Document number RSUK0060 Note re Rotor bearing temp indicator. The purpose of this is to advise the pilot of an unusual rise in temperature of the bearing. In general use it may be used to indicate the outside air temperature in the region of the rotor head.
  • Page 59 Copyright of RotorSport UK Ltd Document number RSUK0060 Standard GPSmap panel option. Flymap F7 installation (no antenna required) Page 59 of 101 Page issue 2, dated 12.09.11...
  • Page 60 Copyright of RotorSport UK Ltd Document number RSUK0060 Analogue panel – standard Page 60 of 101 Page issue 2, dated 12.09.11...
  • Page 61 Copyright of RotorSport UK Ltd Document number RSUK0060 Flymap L Instrument panel option. GPS antenna is located inside the nacelle, bonded to the upper surface, and the AHRS module (if fitted) is located on the keel in front of the nosegear..
  • Page 62 Copyright of RotorSport UK Ltd Document number RSUK0060 Airbox Foresight GPS installation with additional ‘on/off’ switch 39, GPS antenna View of AVmap panel Page 62 of 101 Page issue 3, dated 02.04.12...
  • Page 63 Copyright of RotorSport UK Ltd Document number RSUK0060 View of panel with GPS area in middle of panel for customer GPS mounting. It is the pilots responsibility to ensure that the stick does not foul the GPS, and that the GPS is secure before flight.
  • Page 64 Copyright of RotorSport UK Ltd Document number RSUK0060 Rear and front seat lockers. The push button locks the doors in place. The rear seat lockers are part covered by the seat cushion, and all are accessible in flight. They are locked closed by the single sprung push button.

  • Page 65: Wheels And Tyres

    Copyright of RotorSport UK Ltd Document number RSUK0060 6.4 Wheels/tyres Tyre pressures: 1.5 to 2.2 bar main wheels. 1.5 to 1.8 nosewheel The mainwheels use tyre size 400/100-2Ply (with inner tube), and the nosewheel 400-4 4ply (with inner tube). If flying in the winter with a frozen-over or snow covered runway, it is advisable to remove the wheel spats in order to avoid their damage and snow build up inside them.

  • Page 66: Engine

    Copyright of RotorSport UK Ltd Document number RSUK0060 Hinge attachment screws Front seat adjustment. The seat back is connected to the base of the aircraft via two hinges. Each hinge is bolted to the aircraft with two countersunk bolts. Removing these bolts allows the seat back to be moved fore and aft along the aircraft and then bolted back in place to match the required pilot seated position.
  • Page 67 Copyright of RotorSport UK Ltd Document number RSUK0060 Coolant system The principle of the coolant system is seen below. The numbers refer to the cylinder heads (the barrels are air cooled). Note that a thermostat is fitted to allow faster warm up and better temperature control.
  • Page 68 Copyright of RotorSport UK Ltd Document number RSUK0060 Side view Top view DESCRIPTION: 4-cylinder.-4 stroke double-piston engine with dry sump lubrication, hydraulic tappets, electronic double ignition, electric starter and slipper clutch transmission. For detail function, technical data etc. see engine manual. Always ensure oil level is correct before flight (oil reservoir is item 1)! The oil level is measured in aircraft level attitude and should reach between the marks on the dipstick.
  • Page 69 Copyright of RotorSport UK Ltd Document number RSUK0060 Oil tank access panel Access panel removed This picture shows the principle of the oil system, as shown in the Rotax handbook. For this aircraft a thermostat is included within the oil system for better control of the oil temperature, see the line diagram below.
  • Page 70 Copyright of RotorSport UK Ltd Document number RSUK0060 Undo these camlok fasteners all the way around the upper cowl View with cowl removed Heater box Page 70 of 101 Page issue 2, dated 12.09.11...

  • Page 71: Fuel System

    Copyright of RotorSport UK Ltd Document number RSUK0060 View with cowl removed. Coolant header tank Radiator electric fan Note that all fuel and oil hoses in the engine bay are covered in fireproof sleeve, and the engine face of the firewall and fuel tanks is covered in fireproof cladding. These must not be removed.
  • Page 72 Copyright of RotorSport UK Ltd Document number RSUK0060 Fuel filler cap (also available with lockable cap) To open, lift, then turn, the flap – and pull out. Reverse to replace. Cap is retained to the aircraft via a security cable. WARNING Fill tank up to max.
  • Page 73 Copyright of RotorSport UK Ltd Document number RSUK0060 Principle fuel system 914T Fuel regulator return feed to tank Regulator Filler Left Right Carb 1 Carb 2 KL145 KL145 (main) (optional) tank tank Metal gauze El. Pump El. Pump filter Inl. Filter Inl.

  • Page 74: Electrical System

    6.8 ELECTRICAL SYSTEM The diagram attached in the Maintenance handbook shows the electrical system of the autogyro. With the Ignition switch OFF the engine is isolated. However, be aware that unless the master switch is off other electrical items will work, and may draw current.
  • Page 75 Copyright of RotorSport UK Ltd Document number RSUK0060 Warning! Overloading the electrical system will drain the battery (rated at 7Ahr). On a 914UL aircraft, both fuel pumps are electrical, so draining the electrical system may stop the engine! Two warning lamps are fitted to warn the operator of electrical problems: 1) The ‘GEN’...
  • Page 76 Copyright of RotorSport UK Ltd Document number RSUK0060 Cockpit electrical gauges Automotive Inst. panel (rotor and engine rpm, oil pressure, water and oil temps, fuel gauge) and warning lamps Avionics Radio, Transponder and Automotive Inst. panel GPS units Landing lights Strobes, landing lights, Automotive Inst.

  • Page 77: Pitot And Static Pressure

    Copyright of RotorSport UK Ltd Document number RSUK0060 Fuse box, cover off. Each fuse is marked with the rating for that fuse 6.9 PITOT AND STATIC PRESSURE The measuring probe for dynamic pressure is in the nose of the enclosure. The hose connecting this to the ASI leads directly to the instruments in the cockpit.

  • Page 78: Options And Modifications

    Copyright of RotorSport UK Ltd Document number RSUK0060 Always read and understand the handbook before operation, and never rely only on the GPS. The software maps or data may be out of date, or it may simply fail. The safe way is to plan to use a chart and compass as primary navigation tools, and GPS as a backup.
  • Page 79 Copyright of RotorSport UK Ltd Document number RSUK0060 Fully enclosed canopy Semi-open canopy with sun-screen If an aircraft is purchased with two different canopies (e.g. fully enclosed for winter use, semi-open for summer use) it is permissible for the pilot to inter-change the canopies, although each such action must be recorded in the aircraft log-book together with the pilots name and CAA authorisation number.
  • Page 80 Copyright of RotorSport UK Ltd Document number RSUK0060 Standard canopy lever (inside/outside) Inside-only lever for semi-open canopy Canopy restraint arrangement Restraint strap fitting to enclosure Bungee fitting on canopy frame (nut cover removed) To remove/replace a canopy without damage it is necessary to use a helper, although there is no heavy lifting involved.
  • Page 81 Copyright of RotorSport UK Ltd Document number RSUK0060 3. Using small pliers and/or a small flat screwdriver remove the safety clip then unscrew the nyloc nut from each hinge pin. 4. With the helper steadying the load of the canopy remove the hinge pins taking note of the arrangement of the nylon and steel washers 5.
  • Page 82 Copyright of RotorSport UK Ltd Document number RSUK0060 Order of assembly in LH photo above: fwd/safety clip/nyloc nut/steel washer/nylon washer/pivot/nylon washer/……… ………/hinge plate/nylon washer/pivot/nylon washer/steel washer/bolt-head/aft Safety clip fitted at nut-end of hinge pins Inspection and adjustment of canopy lock: The interior canopy handle has a curved face that slides over a brass bush/bearing attached to the cockpit RH wall.
  • Page 83 Copyright of RotorSport UK Ltd Document number RSUK0060 Measured as above the release force should be 40-60N (equivalent to 3.8–5.7Nm or 4 to 6.1Kg) Detent locking force The tension loop should be placed again at about 95mm radius, and the load maintained at 90º...
  • Page 84 Copyright of RotorSport UK Ltd Document number RSUK0060 For detent release force – direct measurement at the handle end (effective radius 120mm). Max force here 32 – 48N (equivalent to 3.8 – 5.7Nm, or 3.3 – 4.9Kg) For detent locking force - use a small wire-loop placed at the handle’s bend-point (effective radius 75mm.) Max force here 38 –...
  • Page 85 Copyright of RotorSport UK Ltd Document number RSUK0060 The locking pin bush The hinge mounting Bushes are available with outside diameter nominally 12.0, 13.0, 13.5mm and mounting shims nominally 0.5, 1.0 and 2.0mm thickness. If changing the former ensure that the bush rotates freely on the inner steel bush (a light film of LM grease should be applied) and that the bush is not pinched when the nyloc nut is tightened.
  • Page 86 Copyright of RotorSport UK Ltd Document number RSUK0060 APPROVED MODIFICATIONS For confirmation of all modifications permissible in the UK, contact RotorSport UK Ltd, or reference the RotorSport website. Alternatively the aircraft TADS issued by the CAA lists all approved modifications for the type, and is available from the CAA website. Page 86 of 101 Page issue 2, dated 12.09.11...
  • Page 87 Copyright of RotorSport UK Ltd Document number RSUK0060 Intentionally blank Page 87 of 101 Page issue 2, dated 12.09.11...

  • Page 88: Introduction

    Openings to the engine, service points and airspeed indicator and static ports should be closed after the flight (beware of insects, birds etc.). Contamination of the autogyro can be removed with clean water, with low strength cleaning additives.

  • Page 89: Repairs

    Since the structure is designed for air use, this can induce a safety risk. Hard landings and rough ground (especially potholes) all induce high accelerations on the autogyro framework, as does being bounced around on the back of a road trailer. Therefore avoid unnecessary road transport, and use trailers with good suspension.
  • Page 90 Copyright of RotorSport UK Ltd Document number RSUK0060 Typical trailer for transport. This is car transporter trailer. The gap between the side walls is narrowed by bolting wooden runners either side of the metal walls, 100mm high. This prevents scuffing of the wheel spats when loading, protects the tyre side walls, and limits sideways movement of the aircraft during the journey.

  • Page 91: Cleaning And Care

    Copyright of RotorSport UK Ltd Document number RSUK0060 A strap is passed through the keel to prevent the aircraft moving forwards, and another across the keel to prevent vertical movement. A block is positioned under the keel to support it. 7.5 CLEANING AND CARE Contamination of the rotor system and propeller can be removed with clean water, with low strength cleaning additives.
  • Page 92 Copyright of RotorSport UK Ltd Document number RSUK0060 temperatures fall under this value, then drain the coolant, and if required for service, refill with pure antifreeze. Because anti freeze ages, renew the cooling agent every two years. Read the engine manual for the manufacturer’s recommendations.

  • Page 93: Equipment

    Copyright of RotorSport UK Ltd Document number RSUK0060 8. EQUIPMENT 8.1 MINIMUM EQUIPMENT The pilot must wear suitable personal clothing for the weather and flight planned – eg headset, footwear, sunglasses, heated clothing etc. Remember, sunshine through an enclosed canopy can cause discomfort to an exposed head. Suitable refreshments –eg water –...

  • Page 94: Ivo-Prop In-Flight Variable Pitch Propeller (Option)

    Copyright of RotorSport UK Ltd Document number RSUK0060 9. IVO-PROP IN-FLIGHT VARIABLE PITCH PROPELLER 9.1. INTRODUCTION A variable pitch propeller (VPP) manufactured by IVO Prop Corp of Long Beach California, is available as optional equipment to optimise propeller efficiency, fuel consumption and noise in all flight regimes and power settings.

  • Page 95: Manifold Absolute Pressure Indications

    Copyright of RotorSport UK Ltd Document number RSUK0060 The logic table for operation of the propeller controller is: Both LEDS off Propeller is not at an end position and no pitch change command active Upper LED blinking Propeller changing pitch to FINE Lower LED blinking Propeller changing pitch to COARSE Upper LED steady...

  • Page 96: Normal Procedures

    Copyright of RotorSport UK Ltd Document number RSUK0060 9.7. NORMAL PROCEDURES In order to set the propeller to FINE for start-up, take-off and approach use the following procedure:  Press rocker in direction FINE (forward or top position), status indicator FINE flashes, engine RPM increases ...

  • Page 97: Pre-Flight Inspection

    Copyright of RotorSport UK Ltd Document number RSUK0060 9.8. PRE-FLIGHT INSPECTION Visual: Check each of the propeller blades for damage, small nicks or delamination of the stainless-steel edge protector, and security of attachment to hub. Check the aluminium hub parts for cracks or damage and security of attachment to engine Check the security of the spinner and presence of 9-off attachment screws Check the fabricated bracket holding the brush carrier for security of attachment and absence of cracks...

  • Page 98: Coping With Malfunctions

    Copyright of RotorSport UK Ltd Document number RSUK0060 9.9 COPING WITH MALFUNCTIONS Coping with control malfunction Care must be taken to set an appropriate rpm for the flight conditions, and if at fine pitch, do not descend at more than 80mph to prevent engine overspeed. Coping with an propeller pitch fluctuation malfunction If a malfunction causes the propeller pitch to fluctuate, remove the 25A fuse from the instrument panel.
  • Page 99 Copyright of RotorSport UK Ltd Document number RSUK0060 3. Propeller will not make pitch change (determined by no audible effect from engine when at constant power setting). Probable cause: failed propeller mechanism, end-position controller or cable fault. Follow the appropriate actions in 1. or 2. above and consider the further scenarios in the table below: Before take-off Do not take-off...

  • Page 100: I Change Of Ownership Form

    Copyright of RotorSport UK Ltd Document number RSUK0060 Appendix 1 Change of ownership form This form is supplied to enable the new owner to register the change of ownership, so that he/she may receive any service or other information relating to the aircraft. The information is stored on a computer, and is only used within RotorSport UK for the above purpose.

  • Page 101: Incident Reporting Form

    Copyright of RotorSport UK Ltd Document number RSUK0060 Appendix 2 Incident reporting form This form is supplied to enable the owner/operator to inform (anonymously if needed) RotorSport UK Ltd of any incident, accident or other field or service failure that they feel appropriate. The owner must also, of course, inform the relevant authorities if that is appropriate –...

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