Atec ATEC 212 SOLO ROTAX 912 UL Aeroplane Repairs, Major Overhaul, Anchorage of the Aeroplane

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8.2.Aeroplane Repairs

The owner of aeroplane is obliged to report to the manufacturer each damage which may has an influence on an airframe strength or flight qualities. The manufacturer determines a way of repair.

Minor repairs are the repairs of those parts, which do not participate substantially in the aeroplane function and stiffness.

Among the permitted repairs are:

-the lacquer repair

-replacing the worn-out parts

-repairing the tyres of the landing wheels

These repairs can be carried out by the owner itself. Repairs of the torsion box, spars, wing or tail surfaces, landing gears and carrying load parts of airframe must be carried out in an special workshop. In case of surface finish repairs and changes the upper parts of aeroplane must always be kept in white.

8.3.Major Overhaul

The major overhaul is carried out after 1200 flight hours but not later than 10 years after putting the aeroplane into operation, unless decided otherwise during regular technical inspections or by the company bulletin. The overhaul will be carried out in a special workshop. The overhaul and maintenance are carried out according to the instructions of the engine producer.

8.4.Anchorage of the Aeroplane

The anchorage of the aeroplane is necessary in order to protect the aeroplane against eventual damage caused by the wind or wind blasts during parking outside the hangar. For the purpose, the aeroplane is equipped with threaded holes at the bottom side of the wing and at the tail skid. Threaded eye bars can be fastened into this points.

8.5.Cleaning and Care

The aeroplane surface should always be treated by using suitable cleaning agents. The oil and grease rests can be removed from the aeroplane surface by suitable surface active substances or eventually by petrol. The cockpit enclosure should be cleaned only by washing using a sufficient water flow with an addition of suitable surface active substances. Never use petrol or chemical solvents.

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Contents Atec 212 Solo Atec 212 Solo Type of aeroplanePage Page Introduction Personal data of the ownerSpecification Dimensions Rescue System installed / not installed………Weights Description of the AeroplanePower Oil TemperatureTemperature of Engine Cylinders Operational TemperatureThree-View Sketch Page Never exceed the maximum take-off weight of the aeroplane Air SpeedsDo not exceed this speed in any case Do not exceed this speed by flaps deflectedCentre of Gravity CG Manoeuvre and Gust Envelope Fuel Permitted ManoeuvresType of operation Wind Other limitsPage Power-off flight Rescue system deploymentVibrations Emergency landingAborted landing Page Procedures Before Entering the Cockpit Pre-Flight InspectionWarming up the Engine TaxiingPre Take-Off Take Off and Climb AwayCruising flight Descent and landingPage Stalling Speeds CAS Take off Distance at 15 m / 50 feet heightRate of Climb Cruising SpeedsPage Dismantling the wings AssemblyDismantling the Horizontal and Vertical Rudder Page Wing FuselageTail Surfaces Landing GearSense of Motion of the Control Elements Fuel SystemInstrument Equipment Page Page Safety Belts Flap ControlCanopy Open / Close Flight Control InstrumentsCleaning and Care Aeroplane RepairsMajor Overhaul Anchorage of the AeroplanePage Operation over this range is prohibited Empty WeightMaximum take-off weight Useful weight, weight table Centre of gravity determination