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RotorSport MT-03 Pilot's Handbook Manual

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Copyright of RotorSport UK Ltd
Document number RSUK0011
Pilots Handbook
Gyroplane Type MT-03 (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 64
Page issue 11, dated 01.04.15

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Summary of Contents for RotorSport MT-03

  • Page 1 Copyright of RotorSport UK Ltd Document number RSUK0011 Pilots Handbook Gyroplane Type MT-03 (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...
  • Page 2 Copyright of RotorSport UK Ltd Document number RSUK0011 Applicability Aircraft Registration: Aircraft serial no. RSUK/MT-03/ Engine type: Rotax 912ULS or 914UL Engine serial No: Rotor blade type & diameter: Autogyro 8,4m (black end cap),, or Autogyro hub/Aircopter blade (supplied with aircraft serial 004 and 005), or...

  • Page 3: Table Of Contents

    Copyright of RotorSport UK Ltd Document number RSUK0011 Table of contents Page 1. GENERAL INFORMATION 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...
  • Page 4 Copyright of RotorSport UK Ltd Document number RSUK0011 6.10 Avionics 6.11 Navigation lights 6.12 Options and Modifications 7. HANDLING, SERVICE AND MAINTENANCE 7.1 Introduction 7.2 Regular Maintenance Requirements 7.3 Repairs 7.4 Ground handling & road transport 7.5 Cleaning and care 7.6 Winter operation...
  • Page 5 MENDMENTS ONTROL 1. Where & when necessary RotorSport UK Ltd (hereafter referred to as RSUK) will issue updates to this maintenance standard, 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 Page 31 21.06.16 Page 32 21.06.16 Page 33 01.04.15 Page 34 01.04.15 Page 35 01.04.15 RotorSport UK Ltd approval signatures for this Pilots Handbook Signature: Signature: Signature: Position: Position: Position: Test Pilot & Eng. Manager Flight Test Observer Head of Airworthiness &...

  • Page 7: General Information

    1.2 AUTHORITY FOR FLIGHT WITHIN THE UK The legal basis for the operation of this MT-03 autogyro is regulated in the Airworthiness Approval Notification (AAN29134), issued by the Civil Aviation Authority (CAA). It has been shown to comply with the requirements of BCAR Section T issue 3, and is considered as a factory built aircraft.

  • Page 8: Aircraft Description

    RotorSport UK Ltd takes no responsibility for your decision to fly. In common with other aircraft of this type the MT-03 utilises a non-certified engine. This means that there may be a higher risk of engine failure than in a certified aircraft, with the associated risks of damage or injury as the result of an unplanned landing.

  • Page 9: Pictorial Views

    Copyright of RotorSport UK Ltd Document number RSUK0011 1.5 PICTORIAL VIEWS OF THE MT-03 View from the left hand side Page 9 of 64 Page issue 8, dated 17.12.10...
  • Page 10 Copyright of RotorSport UK Ltd Document number RSUK0011 View from the rear Page 10 of 64 Page issue 8, dated 17.12.10...
  • Page 11 Copyright of RotorSport UK Ltd Document number RSUK0011 View from in front View from left side, second generation front seat Page 11 of 64 Page issue 8, dated 17.12.10...
  • Page 12 Copyright of RotorSport UK Ltd Document number RSUK0011 Intentionally blank Page 12 of 64 Page issue 8, dated 17.12.10...

  • Page 13: Operational Limits

    2. OPERATIONAL LIMITS 2.1 INTRODUCTION This section defines the limit values for safe operation of the MT-03 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 14: Engine

    Copyright of RotorSport UK Ltd Document number RSUK0011 2.4 ENGINE Manufacturer: Bombardier Rotax, Gunskirchen/A Type: Rotax 912 ULS or Rotax 914UL Take-off power: 100 HP/5800 rpm (5 minutes max operation) for 912ULS, 115HP/5800 rpm for 914UL (5 mins max operation)

  • Page 15: Weight And Balance

    Document number RSUK0011 2.6 WEIGHT & BALANCE The maximum take-off weight of the MT-03 is 450Kg (or 500kg if incorporating RotorSport Service Bulletin SB-013/AAN 29134 addendum 4). This represents the empty weight (with normal equipment), occupant weight(s), fuel and luggage.

  • Page 16: Fuel

    A small detachable bag is fitted inside the aircraft. Its purpose is to carry the rotor tie down strap and basic aircraft documents only. Note: MC-184 enables replacement of a damaged MT-03 enclosure with the MTOsport enclosure. The latter has a fwd luggage locker accessible through a hatch in the nose of the aircraft.

  • Page 17: General Placards

    Copyright of RotorSport UK Ltd Document number RSUK0011 2.8 GENERAL PLACARDS AND MARKINGS: In conformity with BCAR Section T the following placards and markings are installed: - All emergency controls are coloured red. - All cockpit controls are clearly marked as to their function and method of operation.
  • Page 18 Copyright of RotorSport UK Ltd Document number RSUK0011 Occupant warning OCCUPANT WARNING This aircraft has not been certificated to an International Requirement Primary control marking CHOKE BRAKE ↓ ↑ ↓ THROTTLE ENGAGE Limitations OPERATING LIMITATIONS Aerobatic Limitations Intentional spinning is prohibited.
  • Page 19 Copyright of RotorSport UK Ltd Document number RSUK0011 Rotor RPM gauge (only where the gauge is marked internally as ‘x100’, but actually reads x10) X 10 Coolant overflow bottle Engine oil tank Coolant Header Tank. Oil tank Filled with Evans NPG+, Capacity 3 ltrs.
  • Page 20 Note! Where a deviation exists between the front master and rear seat slave ASI’s, it is permissible at initial build for RotorSport UK Ltd only to placard the rear seat ASI accordingly to show the error (front is assumed as the correct ‘master’). E.g.
  • Page 21 Copyright of RotorSport UK Ltd Document number RSUK0011 - Other If the compass deviation is more than 5° on all headings, then a deviation placard must be present. (new placard format from serial /004 and /006) COMPASS DEVIATION For Set For Set For Set...
  • Page 22 Copyright of RotorSport UK Ltd Document number RSUK0011 Intentionally blank Page 22 of 64 Page issue 12, dated 21.06.16...

  • Page 23: Emergency Procedures

    Copyright of RotorSport UK Ltd Document number RSUK0011 3. EMERGENCY PROCEDURES 3.1 INTRODUCTION The MT-03 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. NOTE: Plan your flight route to allow for unplanned engine failures and subsequent forced landings.

  • Page 24: Abandoning The Aircraft

    Copyright of RotorSport UK Ltd Document number RSUK0011 3.4 ABANDONING THE AIRCRAFT In normal circumstances occupants should not leave the aircraft while either the propeller or the rotors are turning. If abandoning the aircraft in an emergency the pilot should turn the off the engine magneto switches and turn the Master switch to “OFF”...

  • Page 25: Precautionary Landings

    Section 4. contains check lists and procedures to be used for the normal operation. Procedures for additional equipment are in Section 8. REMARK! There are two rotor head assemblies released on the MT-03, as of the release of change MC-105. This latter change reduces the stick travel in pitch, giving a more positive stick force, and increased clearance to the instrument panel and back of the rear seat.

  • Page 26: Rotor Rigging

    Copyright of RotorSport UK Ltd Document number RSUK0011 4.2 ROTOR RIGGING Assembly rotor: The rotor blades, spacer extrusion and hub are provided with numbers to define the installation direction. By matching these numbers, put the blades into the hub. Fit the 9 bolts fitted with ‘thin’...
  • Page 27 7. Grease the bolt via the grease nipple where fitted. 8. Ensure the rotor teeters to the stops freely. NOTE! From serial no. 004 a new rotor hub is fitted. Refer to the RotorSport UK Ltd if this later design is wanted for 002 or 003.
  • Page 28 Copyright of RotorSport UK Ltd Document number RSUK0011 Page 28 of 64 Page issue 12, dated 21.06.16...
  • Page 29 Copyright of RotorSport UK Ltd Document number RSUK0011 Top view of rotor installed Match parts using dot marks on tower, spacer and hub (normally one dot or two dots) Additional views below show the differences between the original and RotorSystem II construction.
  • Page 30 Copyright of RotorSport UK Ltd Document number RSUK0011 Section view of rotor head with RotorSystem II parts shown. Old rotor head assy RotorSystem II head assy Page 30 of 64 Page issue 12, dated 21.06.16...
  • Page 31 Copyright of RotorSport UK Ltd Document number RSUK0011 View of RotorSystem II fitted (rotor blades not installed). 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.

  • Page 32: Daily Inspection

    The full pre-flight checklist is shown below. MT-03 GYROPLANE PRE FLIGHT CHECKLIST This list is a guideline of items to be checked prior to the flight. No checklist is "All Inclusive", nor is it to be construed as a substitute for proper training or pilot experience.
  • Page 33 Copyright of RotorSport UK Ltd Document number RSUK0011 Inspect - Engine mountings in place and secure and rubbers free of cracks or any deterioration Inspect - Plugs and plug caps secure Inspect – coolant and oil radiator for condition, security and leakage, Note: inspect all soldered joints for evidence of cracking.

  • Page 34: Flight Operation

    Copyright of RotorSport UK Ltd Document number RSUK0011 Other Op/C – brake lever operates normally and brakes function. Op/C - Ground run. Check both electric fuel pumps (where fitted) are operational before starting engine. Confirm full power obtainable (if practical), & that engine, propeller &...
  • Page 35 Copyright of RotorSport UK Ltd Document number RSUK0011 TO START ENGINE (WITH STANDARD IGNITION SYTEM) Main switch ON (generator warning light on) Choke Engage (until engine warm and will run without choke.) Throttle Closed Propeller Danger area – keep clear!
  • Page 36 Copyright of RotorSport UK Ltd Document number RSUK0011 supply voltage has exceeded the set levels, and is overcharging. In this case stop and resolve. Once started the ‘Gen’ light will go off, indicating the alternator is working. In low light conditions it may be seen to flicker gently.
  • Page 37 Copyright of RotorSport UK Ltd Document number RSUK0011 After reaching 260ft, throttle back to about level flight rpm, between 4 and 5,000rpm. Pay attention in hot weather to the cylinder head and oil temperatures. If these should rise with long climbs over the placarded values, then adjust your speed or attitude to compensate.
  • Page 38 Copyright of RotorSport UK Ltd Document number RSUK0011 WARNING! FUEL MANAGEMENT! The fuel tanks retain an increasing amount of unusable fuel depending on the nose down (descent) angle. At a 5 degree descent there is approximately 1.1ltr of unusable fuel per tank.
  • Page 39 Copyright of RotorSport UK Ltd Document number RSUK0011 Intentionally blank Page 39 of 64 Page issue 9, dated 12.9.11...

  • Page 40: Performance

    Single-seat 1,200fpm (912S) or over 1,500fpm (914T) Two seat 600fpm at MTOW (912S) or 900fpm (914T) At 500kg take-off weight (only if RotorSport service bulletin SB-013 incorporated) Single-seat 1,200fpm (912S) or over 1,500fpm (914T) Two seat 500 fpm at MTOW (912S) or 700 fpm (914T)

  • Page 41: Further Data

    Landing should always be made into wind where practical. The maximum landing crosswind 15kts. NOISE DATA The MT-03 meets the German BUT noise protection requirements for ultralight autogyro of 68dB(A) max. TYRE PRESSURE Main landing gear wheels 1.5 to 2.2 bar Nose gear wheel 1.5 to 1.8 bar...

  • Page 42: Height Speed Diagram

    Copyright of RotorSport UK Ltd Document number RSUK0011 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. Engine failures whilst flying at heights and speeds to the left of the graph line may prove fatal for the pilot and passenger.

  • Page 43: Description

    Copyright of RotorSport UK Ltd Document number RSUK0011 6. DESCRIPTION 6.1 GENERAL STRUCTURE The framework of the autogyro consists of an inert gas-welded high-grade stainless steel tubing framework. The tail unit structure is manufactured in GRP (or in certain cases Carbon fibre RP).
  • Page 44 Copyright of RotorSport UK Ltd Document number RSUK0011 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 45 Copyright of RotorSport UK Ltd Document number RSUK0011 Rear stick A rear seat stick is available for training purposes. It has a simple rubber grip with no push-buttons. There are two rear seat stick options. The standard stick is the same length as the front stick, and is general purpose.
  • Page 46 Copyright of RotorSport UK Ltd Document number RSUK0011 Rudder The rear rudder pedals are connected to the rudder via steel cable, and to the front pedals by linkages via the nosewheel for steering. Pushing the right pedal will turn the aircraft right in the air and right when on the ground.
  • Page 47 Copyright of RotorSport UK Ltd Document number RSUK0011 The rear seat is not fitted with a throttle as standard – this is an instructor option fit. The unit is retained with two screws from the top, and one screw and nut retaining the link to the front throttle.

  • Page 48: Instrument Panel

    Copyright of RotorSport UK Ltd Document number RSUK0011 Rear seat kill switches Trim switch Throttle Brake Fuel cut off Rear seat ASI A PTT button is mounted to the left of the seat, and a 12v aux socket fitted if required.
  • Page 49 Copyright of RotorSport UK Ltd Document number RSUK0011 Fig. 2: Control elements and instrumentation in the cockpit – first generation panel REMARK: Note the pushbutton on the fuel gauges shown above and below. If such a button is fitted in or adjacent to the gauge it must be pressed before reading the fuel level.
  • Page 50 Copyright of RotorSport UK Ltd Document number RSUK0011 Fig 3: Second generation panel Page 50 of 64 Page issue 9, dated 12.9.11...
  • Page 51 Copyright of RotorSport UK Ltd Document number RSUK0011 Under modification MC-218 a new design of rpm gauge was introduced (engine rpm and rotor rpm) and may be supplied as spares. They are visually and functionally similar to the earlier gauges but carry-out a full sweep of the gauge face as a self-test feature when powered-up by the aircraft master switch.

  • Page 52: Wheels And Tyres

    Copyright of RotorSport UK Ltd Document number RSUK0011 6.4 Wheels/tyres Both the mainwheels and nose wheel use tyre size 400/100-2Ply (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 53: Engine

    Copyright of RotorSport UK Ltd Document number RSUK0011 6.6 ENGINE The engine provided is either a 4 stroke Rotax 912 or 914. This engine is appropriate for the market, and is in use on many other similar aircraft – but possesses no certification.
  • Page 54 Copyright of RotorSport UK Ltd Document number RSUK0011 Top view DESCRIPTION: 4-cylinder.-4 stroke double-piston engine with dry sump lubrication, hydraulic tappets, electronic double ignition, electric starter and transmission. For detail function, technical data etc. see engine manual. REMARK: 912ULS engines after S/no. 6.775.360 have redesigned ignition modules which give improved starting but different slow-running characteristics (See RSUK SIL-003) REMARK: The aircraft may be retrofitted with SB-041 “Conair Sports SSM”.

  • Page 55: Fuel System

    Since the exhaust and its attachment are exposed to high loads by temperature and thermal expansion, these should be frequently checked. The MT-03 propeller is a 3-Blade-HTC with a diameter of 1,73 m. 6.7 FUEL SYSTEM The fuel system is under the rear seat and has a capacity of 35 ltr per tank. The tank is ventilated by a ventilation line above the tank to the rear of the mast.

  • Page 56: Electrical System

    75amps. Overuse may result in internal battery damage and early failure. Use of optional items such as heated clothing all draw a significant amount of current. The amount will depend on individual circumstances. Engine current availability and usage - MT-03 gyroplane Item Amperage Wattage...

  • Page 57: Pitot And Static Pressure

    Copyright of RotorSport UK Ltd Document number RSUK0011 Notes: normally only the mechanical or one electrical fuel pump is used in flight, saving 3 amps Warning! Overloading the electrical system will drain the battery (rated at 8Ahr). On a 914UL...
  • Page 58 Copyright of RotorSport UK Ltd Document number RSUK0011 The installation of further devices is possible, but the operator must be aware that this increases the unloaded weight and current draw on the engine. Note that the avionics are an approved package – modification or other installations require CAA/RSUK approval.
  • Page 59 See the aircraft certificate of conformity for modifications fitted at point of release to service. For confirmation of all modifications permissible in the UK, contact RotorSport UK Ltd or check the RotorSport website aircraft owner’s page where they are listed. Alternatively the aircraft TADS issued by the CAA lists all approved modifications for the type, and is available from the CAA website.
  • Page 60 Insect debris build up on the rotors and propeller reduce performance and increase vibration. In order to avoid bird droppings or soiling of the MT-03, one should cover the aircraft with a light plastic tarpaulin or a cloth. Openings to the engine, service points and airspeed indicator should be closed after the flight (beware of insects, birds etc.).
  • Page 61 CAA publications. Unless documented in the Maintenance manual, only original spare parts may be used, supplied with an Approved Certificate. Parts are available from RotorSport UK Ltd. See the maintenance manual for detail information 7.4 GROUND HANDLING & ROAD TRANSPORT Aircraft are generally exposed to larger loads on the ground than in air, especially in road transport.
  • Page 62 Take care when installing additional equipment in case it changes the magnetic field of the aircraft, and hence the compass accuracy. 8.2 ADDITIONAL EQUIPMENT. Various options are available from RotorSport UK Ltd. Do not fit unapproved accessories as these may invalidate your Permit to Fly! REMARK Further individual equipment is available on customer's request.
  • Page 63 The information is stored on a computer, and is only used within RotorSport UK for the above purpose. If the new owner does not register, then they will not be automatically updated, which may lead to unsafe flight or an un-airworthy aircraft.
  • Page 64 Depending on the incident information supplied, a corrective action is investigated and, if needed, supplied back to the customer(s) The information given is stored on a computer, and is only used within RotorSport UK for the above purpose. Return this form to:...

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