Atec 212 Solo | Atec ATEC 212 SOLO ROTAX 912 UL instruction

Sole Manufacturer and Distributor in the Czech Republic:

ATEC v.o.s.

Location of factory: ATEC v.o.s., Opolanská 350, 289 07 Libice nad Cidlinou

Czech Republic

ATEC 212 SOLO

ROTAX 912 UL

Flight and Operations Manual

Libice nad Cidlinou January 2007

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Atec ATEC 212 SOLO ROTAX 912 UL manual Atec 212 Solo

Contents

Atec 212 Solo Type of aeroplane Atec 212 SoloPage Page Personal data of the owner Introduction Rescue System installed / not installed……… Specification DimensionsWeights Description of the Aeroplane Oil Temperature PowerTemperature of Engine Cylinders Operational Temperature Three-View Sketch Page Air Speeds Never exceed the maximum take-off weight of the aeroplaneDo not exceed this speed in any case Do not exceed this speed by flaps deflected Centre of Gravity CG Manoeuvre and Gust Envelope Type of operation Permitted ManoeuvresFuel Other limits WindPage Rescue system deployment Power-off flight Aborted landing Emergency landingVibrations Page Pre-Flight Inspection Procedures Before Entering the Cockpit Taxiing Warming up the EnginePre Take-Off Take Off and Climb Away Descent and landing Cruising flightPage Take off Distance at 15 m / 50 feet height Stalling Speeds CASRate of Climb Cruising SpeedsPage Dismantling the Horizontal and Vertical Rudder AssemblyDismantling the wings Page Fuselage WingTail Surfaces Landing Gear Instrument Equipment Fuel SystemSense of Motion of the Control Elements Page Page Flap Control Safety BeltsCanopy Open / Close Flight Control Instruments Aeroplane Repairs Cleaning and CareMajor Overhaul Anchorage of the AeroplanePage Maximum take-off weight Empty WeightOperation over this range is prohibited Centre of gravity determination Useful weight, weight table