Atec ATEC 212 SOLO ROTAX 912 UL manual

Page 24

Chapter 6

6.Assembly and Dismantling

6.1.Introduction

6.2.Dismantling the Horizontal Tail Surface and the Rudder

6.3.Dismantling the Wings

6.4.Assembly

Image 24

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 Permitted Manoeuvres Type of operationFuel Wind Other limitsPage Power-off flight Rescue system deploymentEmergency landing Aborted landingVibrations 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 Assembly Dismantling the Horizontal and Vertical RudderDismantling the wings Page Wing FuselageTail Surfaces Landing GearFuel System Instrument EquipmentSense of Motion of the Control Elements Page Page Safety Belts Flap ControlCanopy Open / Close Flight Control InstrumentsCleaning and Care Aeroplane RepairsMajor Overhaul Anchorage of the AeroplanePage Empty Weight Maximum take-off weightOperation over this range is prohibited Useful weight, weight table Centre of gravity determination