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ATEC 212 SOLO ROTAX 912 UL manual Centre of Gravity CG
Models:
ATEC 212 SOLO ROTAX 912 UL
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Specifications
Assembly
Cleaning and Care
Oil Temperature
Weight
Safety
Power-off flight
Page 11
Image 11
2.4. Centre of Gravity ( CG )
CG of the empty aeroplane …………………
% MAC
Flight range of CG …………………………
28 – 36% MAC
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Page 11
Image 11
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Contents
Atec 212 Solo
Type of aeroplane
Atec 212 Solo
Page
Page
Personal data of the owner
Introduction
Description of the Aeroplane
Specification Dimensions
Rescue System installed / not installed………
Weights
Operational Temperature
Power
Oil Temperature
Temperature of Engine Cylinders
Three-View Sketch
Page
Do not exceed this speed by flaps deflected
Never exceed the maximum take-off weight of the aeroplane
Air Speeds
Do not exceed this speed in any case
Centre of Gravity CG
Manoeuvre and Gust Envelope
Fuel
Permitted Manoeuvres
Type of operation
Other limits
Wind
Page
Rescue system deployment
Power-off flight
Vibrations
Emergency landing
Aborted landing
Page
Pre-Flight Inspection
Procedures Before Entering the Cockpit
Take Off and Climb Away
Warming up the Engine
Taxiing
Pre Take-Off
Descent and landing
Cruising flight
Page
Cruising Speeds
Stalling Speeds CAS
Take off Distance at 15 m / 50 feet height
Rate of Climb
Page
Dismantling the wings
Assembly
Dismantling the Horizontal and Vertical Rudder
Page
Landing Gear
Wing
Fuselage
Tail Surfaces
Sense of Motion of the Control Elements
Fuel System
Instrument Equipment
Page
Page
Flight Control Instruments
Safety Belts
Flap Control
Canopy Open / Close
Anchorage of the Aeroplane
Cleaning and Care
Aeroplane Repairs
Major Overhaul
Page
Operation over this range is prohibited
Empty Weight
Maximum take-off weight
Centre of gravity determination
Useful weight, weight table