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ATEC 212 SOLO ROTAX 912 UL manual Manoeuvre and Gust Envelope
Models:
ATEC 212 SOLO ROTAX 912 UL
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12
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Specification
Assembly
Cleaning and Care
Oil Temperature
Weight
Safety
Power-off flight
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2.5.
Manoeuvre and Gust Envelope
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Contents
Atec 212 Solo
Atec 212 Solo
Type of aeroplane
Page
Page
Introduction
Personal data of the owner
Specification Dimensions
Rescue System installed / not installed………
Weights
Description of the Aeroplane
Power
Oil Temperature
Temperature of Engine Cylinders
Operational Temperature
Three-View Sketch
Page
Never exceed the maximum take-off weight of the aeroplane
Air Speeds
Do 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 operation
Fuel
Wind
Other limits
Page
Power-off flight
Rescue system deployment
Emergency landing
Aborted landing
Vibrations
Page
Procedures Before Entering the Cockpit
Pre-Flight Inspection
Warming up the Engine
Taxiing
Pre Take-Off
Take Off and Climb Away
Cruising flight
Descent and landing
Page
Stalling Speeds CAS
Take off Distance at 15 m / 50 feet height
Rate of Climb
Cruising Speeds
Page
Assembly
Dismantling the Horizontal and Vertical Rudder
Dismantling the wings
Page
Wing
Fuselage
Tail Surfaces
Landing Gear
Fuel System
Instrument Equipment
Sense of Motion of the Control Elements
Page
Page
Safety Belts
Flap Control
Canopy Open / Close
Flight Control Instruments
Cleaning and Care
Aeroplane Repairs
Major Overhaul
Anchorage of the Aeroplane
Page
Empty Weight
Maximum take-off weight
Operation over this range is prohibited
Useful weight, weight table
Centre of gravity determination