Atec ATEC 212 SOLO ROTAX 912 UL guide

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 owner Specification Dimensions Rescue System installed / not installed………Weights Description of the Aeroplane Power Oil TemperatureTemperature of Engine Cylinders Operational Temperature Three-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 deflected Centre of Gravity CG Manoeuvre and Gust Envelope Permitted Manoeuvres Type of operationFuel Wind Other limitsPage Power-off flight Rescue system deployment Emergency landing Aborted landingVibrations Page Procedures Before Entering the Cockpit Pre-Flight Inspection Warming up the Engine TaxiingPre Take-Off Take Off and Climb Away Cruising 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 Gear Fuel System Instrument EquipmentSense of Motion of the Control Elements Page Page Safety Belts Flap ControlCanopy Open / Close Flight Control Instruments Cleaning 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

Atec ATEC 212 SOLO ROTAX 912 UL manual