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Summary of Contents for RotorSport MC-338
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Copyright of RotorSport UK Ltd Document number RSUK0370 Addendum 1 to Cavalon Pro Gyroplane Pilot Operating Handbook. For the purpose of Gimbal mounted camera operation Document number RSUK0370 This document must be read in conjunction with the current issue of...
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U.S. and foreign patents of AutoGyro AG are used in the Calidus and Cavalon gyroplanes - (US.Pat.No. 8,690,100; US.Pat.No. D699,153) Every effort has been made to ensure that the information in this manual is accurate. Neither RotorSport UK Ltd or AutoGyro GmbH is not responsible for printing or clerical errors.
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This flight manual Addendum 1 should be carried on board of the aircraft and must be kept in current, up-to-date status. The latest revisions and version status is available at www.rotorsport.org. Extent and revision status of the manual is recorded in the revision log and the table of content.
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Document number RSUK0370 Applicability This manual addendum is applicable for Cavalon ‘Pro’ models only and when fitted the moving camera system specified under modification MC-338 and AAN29428 Addendum 2 Addendum 1_POH_Cavalon Pro Revision 1.0 – Issue Date 27 04 2016...
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Copyright of RotorSport UK Ltd Document number RSUK0370 REVISION LOG Issue Rev. Change summary Date Signature First formal release 27.04.2016 Pilots Flight and Operation Manual Document approval Signature Signature Signature Position: Head of Position: Chief Test Pilot Position: Engineering Airworthiness...
This manual addendum is designed as an operating guide for pilots, instructors, and owners/operators, providing information for the safe and efficient operation of this gyroplane when fitted with the moving camera mount specified under modification MC-338. It includes material required to be furnished to the pilot by the competent certification authority. This handbook addendum is not designed as a substitute for adequate and competent flight instruction.
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Copyright of RotorSport UK Ltd Document number RSUK0370 mount defined by modification MC-338 may be fitted under the authority of AAN29428 Addendum 2. Performance Data and Operating Procedures The legal basis for operating a gyroplane is provided by national law and its respective regulations.
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Copyright of RotorSport UK Ltd Document number RSUK0370 Definition of Terms This manual uses WARNINGs, CAUTIONs and NOTEs in bold capital letters to indicate especially critical and important instructions. Additionally, the colour of the panel (red, yellow, and grey shading) highlights the significance of the instruction. Definitions for each term are given below.
The cameraman must be briefed by the pilot and must agree responsibility for operation of the system controls. 2.1. A nose-mounted moving camera system specified under modification MC-338 is available for fitment to Cavalon Pro gyroplanes, and has been approved by UK CAA under AAN29428 Addendum 2.
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Copyright of RotorSport UK Ltd Document number RSUK0370 A schematic of the sliding mount is shown below: The mount is normally moved up/down by the pilot using a rotary valve mounted on the instrument panel to the left of the aircraft’s centre console. In the event of pneumatic system failure the air pressure can be released by means of a toggle-operated valve and the mount will then rise under power from the gas-struts alone.
Copyright of RotorSport UK Ltd Document number RSUK0370 SECTION 3 – PRE-FLIGHT CHECKS WARNING These additional pre-flight checks must be carried-out in addition to the aircraft’s Daily/Pre-flight inspection as defined in the body of POH RSUK0334 3.1. Visually inspect the vertical slide system structure for cracks, broken welds or other damage.
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Copyright of RotorSport UK Ltd Document number RSUK0370 3.11. Turn on the aircraft master switch and listen for the compressor running to establish system pressure. Ensure that the toggle-operated valve is set to “Closed”. Select the rotary valve to “Down” - the slide system should move slowly (about 18secs) to the down position.
Copyright of RotorSport UK Ltd Document number RSUK0370 SECTION 4 - FLIGHT CONTROLS AND LIMITATIONS 4.1. Pitch control is affected only by the additional nose weight and intuitive compensation by greater aft stick movement. 4.2. Roll control is not noticeably affected by the installation.
Copyright of RotorSport UK Ltd Document number RSUK0370 4.9 Day VFR limitation. The pitot fitted to the gimbal mounting is unheated, meaning the aircraft does not carry the required equipment for night flight. So with the camera gimbal mounting fitted the aircraft is only approved for day VFR operation.
Copyright of RotorSport UK Ltd Document number RSUK0370 SECTION 6 - WEIGHT AND BALANCE 6.1. Installation of the system (total system weight 38kg) has a significant impact on the aircraft empty weight and its centre-of-gravity. As part of approval under AAN29428 Addendum 2 the maximum take-off weight is unchanged (560kg).
It is the operators responsibility to ensure the system is properly functioning and without defects prior to use, and neither AutoGyro GmbH or RotorSport UK Ltd take any responsibility for any gimbal or camera damage in use whilst fitted to the Cavalon Pro.
Copyright of RotorSport UK Ltd Document number RSUK0370 SECTION 8 - MALFUNCTIONS AND EMERGENCIES 8.1. If the slide system cannot be raised by the normal or back-up controls try flying at Vmin (to reduce aerodynamic load on the gimbal) and cycling the pneumatic controls. If unsuccessful prepare for a very slow, nose-high approach to land on soft ground with minimised landing roll.
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Do you have a question about the MC-338 and is the answer not in the manual?
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