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Summary of Contents for Antares MA-33M R582
- Page 1 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 ANTARES MA-33M R582 AIRCRAFT OPERATING INSTRUCTION (AOI) Manufactured by Antares U.S. Corporation Antares_us@yahoo.com www.antares-us.com ____________________________________________________...
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Page 2: Amendment Record Sheet
AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 AMENDMENT RECORD SHEET Amendment Date Affected Section Affected page Date Inspected Signature... -
Page 3: Operator's Responsibility
The amendment should be logged and recorded in the table above by the owner. The data and information contained in this document is the property on Antares US Corporation. This document may not be reproduced or transmitted to a third party, in any form of by any means. - Page 4 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 WARNING THE OWNER AND OPERATOR MUST UNDERSTAND THAT DUE TO INHERENT RISK INVOLVED IN FLYING AN AIRCRAFT, NO WARRANTY IS MADE OR IMPLIED, OF ANY KIND, AGAINST ACCIDENTS, WHICH CANNOT BY LAW BE EXCLUDED.
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Page 5: Table Of Contents
AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 TABLE OF CONTENTS 1. INTRODUCTION ……………………………………………………………………………………………………... 6 2. GENERAL INFORMATION ………………………………………………..............6 3. LIMITATIONS ……………………………………………………………………………………………………….. 9 4. ULTRALIGHT AIRCRAFT & SYSTEMS DESCRIPTION ………………………………………………………... 12 5. PREPARE AIRCRAFT FOR FLIGHT ……………………………………..............19 6. ULTRALIGHT AIRCRAFT FLYING ……………………………………………………………………………….. 22 7. -
Page 6: Introduction
ANTARES MA-33M R582 1. INTRODUCTION. The Antares MA-33M R582 has been designed and manufactured in accordance with the design standard specified by the ASTM consensus standard body for weight shift control aircraft. The design requirements are detailed in ASTM document F 2317/F 2317M. This instruction follows the product information required under ASTM standard F 2457. - Page 7 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 2.3 General dimensions.
- Page 8 2.4 General description. The Antares MA-33M R582 trike is a two seat (tandem type) weight shift controlled Ultralight aircraft, includes the trike (buggy), and the wing. The trike (buggy) is the tricycle undercarriage, the landing gear, the cockpit (front fairing), the gas tank, the power plant (engine), and propeller.
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Page 9: Limitations
AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 or lowered. Vertical mast tube is attached to the base tube through the two 4 mm. thick titanium plates. There is 46 mm. OD front upright tube which connected in between the bottom base tube and the vertical mast tube. There is rectangular seat frame and engine mount assembly component in the trike base. -
Page 10: Engine Limitations
AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 3.3 Engine operating limitations. 3.3.1 Engine. Manufacturer: Rotax Bombardier Model: Rotax 582 UL 2 (2stroke) Gearbox ratio: 2.62: 1 ENGINE LIMITATIONS Metric Imperial Engine RPM Take off (Max 5 minutes) 6600 6600 Maximum (continuous) - Page 11 (hang bracket). Variations of cockpit and fuel loading cannot influence the aircraft’s balance. The Antares MA-33M R582 aircraft is therefore not critical in regards to centre of gravity. However, distribution of load in a trike has an affect on the in-flight attitude of the aircraft.
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Page 12: Ultralight Aircraft Systems Description
AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 3.7 Other limitations. Maximum Cross Wind - 6m/s Maximum Wind Strength - 12m/s Maximum Ambient Operating Temperature + 40 …-10 deg C No person who is untrained or unqualified in weight shift controlled flight or, who is unfamiliar with the wing and trike combination, should ever attempt to pilot the ultralight aircraft unless under professional instruction. -
Page 13: Specification
AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 4.3 In-flight electrical trim mechanism operation (optionally). Antares MA-33M R582 Ultralight aircraft could be equipped with the electrical trim mechanism for trimming the ultralight aircraft in pitch. SPECIFICATION: 9 – 14 V Voltage supply... - Page 14 ALWAYS CHECK THE POSITION OF THE AIRCRAFT HANG BLOCK BEFORE TAKE OFF. 4.4 Instrument panel. The Antares MA-33M R582 trike is equipped with standard flight and engine control instruments or with the optional all digital Fly-Star screen. The instruments arrangement is shown on the pictures below.
- Page 15 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 4.5 Occupants restrain harness. Both front and rear seats are fitted with a restraint harness system. WARNING ALWAYS FASTEN YOUR SEAT BEALTS BEFORE FLIGHT NOTE IT IS IMPORTANT TO ALWAYS BUCKLE UP THE REAR SEAT BELT WHILE FLYING SOLO, TO PREVENT CONTACT OF THE SEAT BELT WITH THE ENGINE HOT COMPONENTS.
- Page 16 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 Aero prop K1750-100 is a 3-blade composite propeller with an Aluminum hub and metric class 8.8 hardware. Propeller equipped with ground pitch adjustable tool. The acceptable pitch range is specified by markings of the pitch tool. For more information please refer to the propeller manual.
- Page 17 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 4.8 Dual steering control system. The dual steering control system is allowed to operate the trike from the rear seat. It is allowed to operate with acceleration and steer while taxing the aircraft. The dual control steering system is the...
- Page 18 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 4.9 Antares MA-33M R582 trike electrical system diagram.
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Page 19: Prepare Aircraft For Flight
AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 Electrical diagram description: 1 – Dual EGT gauge 2 – Water temperature gauge 3 – Tachometer 4 – Engine starter Key Switch 5 – Engine ignition Keys Switches 6 – 12V, 18A/H Battery 7 – Starter Solenoid 8 –... - Page 20 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 5.2.1 Wing preflight inspection. The design of the wing is such that junctions not open to view may be reached from zipped inspection panels or by spreading the sail open. Start at the A-frame or control frame of right wing and move around the wing making the following checks.
- Page 21 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 5.2.2 Trike Pre-flight Inspection. No leaks from fuel system and engine. No leaks from oil system and engine Fuel filter clean and operational. Sufficient fuel for flight. Coolant is level. Radiator mounts secure and operational.
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Page 22: Ultralight Aircraft Flying
IGNITING FUEL 5.5 Helmet recommendation. The open cockpit of the Antares trike exposes the occupants to the elements during flight and exposes them to objects outside of the ultralight in an emergency situation. Helmets and eye protection are recommended for occupants for protection from precipitation, strike by insects. Helmets are also recommended for risk reduction during an emergency landing of the ultralight aircraft. - Page 23 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 WARNING NEVER LEAVE YOUR ULTRALIGHT AIRCRAFT UNATTENDED WHILE THE ENGINE IS RUNNING. CAUTION BEWARE OF LOOSE STONES IN THE RUN UP AREA. LOOSE STONES CAN BE SUCKED UP BY THE PROPELLER AND CAUSE SEVERE PROPELLER DAMAGE IN A VERY SHORT TIME.
- Page 24 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 Always maintain climb angle within limits 30 degrees nose up. Very steep climb is dangerous and can result in an aircraft stall. CAUTION HIGH ANGLE CLIMBS NEAR THE GROUND SHOULD BE AVOIDED. WARNING NEVER STALL THE AIRCRAFT WITH THE NOSE PITCHED UP BEYOND 45 DEGREES.
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Page 25: Emergency Procedures
AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 WARNING The upward wing may need to be lowered at the start of the take off procedure in higher crosswinds but make sure the wings are level at the point of liftoff or a turn immediately following the liftoff will result. - Page 26 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 7.3 Engine failure on climb out. If your engine quits on climb out, maintain airspeed, reduce angle of attack and land straight a head if possible. Proceed as follows: Maintain control. Maintain airspeed and best glide speed or higher.
- Page 27 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 7.7 Engine Fire While In-Flight. For fire occurring while in-flight, the initial procedure would be to maintain control of the aircraft and evaluate the extent of the fire. This emergency is unlikely to occur but to avoid any further problems, use common sense and land the ultralight safely.
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Page 28: Performance
AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 For using emergency rescue system proceed as follows: Throttle OFF. Ignition OFF. Tighten seat belts. Check that emergency rescue system pin is removed. Deploy emergency parachute. Prepare for the forced landing. 7.12 Ignition Circuit Failure. - Page 29 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 There are following factors which will increase takeoff distance: 1). Reduced engine power. 2). Rough runway surfaces. 3). Tail or cross wind. 4). Uphill takeoff. 5). Air temperature above 15 deg C. 6). Runway elevation above sea level.
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Page 30: Handling Service And Maintenance
The Antares trike has a single fuel tank. When the tank is being filled there may be a slight pressure differential between the sides of the tank, causing the fuel cap side to fill slightly faster than the other side. Allow time for the breather valves to equalize the pressure to allow complete filling and, check that both sides are sufficiently full. -
Page 31: Transportation And Storage
AIRCRAFT OPERATING INSTRUCTION ANTARES MA-33M R582 9.8 Cooling System. Water-cooling system capacity is 2.5 L. The coolant should be replaced according to the Rotax maintenance manual, current issue. Please refer to the directive, which is available from the Rotax website: SB-912-043, September 04. - Page 32 AIRCRAFT OPERATING INSTRUCTION ANTARES MA-34 MR-912 BEAVER...
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