Atec ATEC 212 SOLO ROTAX 912 UL manual

Page 30

8.1.

Maintenance Schedule

 

 

 

 

 

 

 

 

 

 

 

 

 

Inspection, Mandatory Work

Inspection Period

 

 

 

 

 

 

 

 

 

10

25

50

100

200

Engine

 

 

 

 

 

As per ROTAX Manual attached.

 

 

 

 

 

 

 

 

 

 

 

Engine Compartment

 

 

 

 

 

Engine Attachment

 

 

 

x

 

Check integrity of construction with special care for welds, fixing points,

 

 

 

 

silent blocks, bushings. Surface finish quality.

 

 

 

 

 

Bolted Connections

 

 

 

 

 

Check

surface quality of bolted connections and bearing surfaces.

 

 

x

 

 

Securing, tightening. Tighten and re-secure if necessary, Replace self

 

 

 

 

 

 

 

 

 

locking nuts, split pins and securing wires.

 

 

 

 

 

Silent Blocks

 

 

 

 

 

Check elasticity of engine bearing, integrity of rubber blocks, degree of

 

 

 

x

 

permanent deformation. Replace silent blocks if necessary, tighten,

 

 

 

 

 

 

 

 

 

secure.

 

 

 

 

 

 

Oil, Water and Fuel Hoses

 

x

 

 

 

Check surface integrity, liquid leakage, quality of connections, protection

 

 

 

 

against oscillating parts and exhausts. Replace if necessary.

 

 

 

 

 

Working Liquids

x

 

 

 

 

Check level, refill keeping instruction of engine manufacturer.

 

 

 

 

 

 

 

 

 

Coolers

 

 

 

x

 

Check integrity, sealing, purity.

 

 

 

 

 

 

 

 

 

Controls

 

 

x

 

 

Check control forces, free play, hinges, end stops adjustment, self-

 

 

 

 

locking. Adjust, secure.

 

 

 

 

 

Exhausts

 

 

 

x

 

Check integrity, sealing, corrosion degree, springs quality and prestress.

 

 

 

 

Grease ball connections.

 

 

 

 

 

Carburetors

 

 

 

 

 

Check surface quality, controls adjustment, quality of elastic connection

 

x

 

 

 

flange – integrity, sealing. Replace flange if material degradations or

 

 

 

 

 

 

 

 

 

surface cracks appear.

 

 

 

 

 

Electric Installations

 

 

 

 

x

Check quality, integrity and purity if cables, contacts, welds, bunched

 

 

 

 

cable supports and bushings. Check gauges and senders connections.

 

 

 

 

 

Propeller Attachment

 

 

 

x

 

Check quality of bolts, tightening moments, securing.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Cockpit

 

 

 

 

 

Control Sticks

 

 

 

 

 

Check free movement in longitudinal and cross direction, clearance fits,

 

 

 

x

 

end stops adjustment, securing. Replace pins or bolts if worn-out, grease,

 

 

 

 

 

 

 

 

 

secure.

 

 

 

 

 

 

Rudder Control

 

 

 

x

 

Check integrity of pedals with special care for surface cracks near welds.

 

 

 

 

Full and free movement right and left (raise nose wheel off ground), end

 

 

 

 

 

30

Image 30
Contents Atec 212 Solo Atec 212 Solo Type of aeroplanePage Page Introduction Personal data of the ownerWeights Specification DimensionsRescue System installed / not installed……… Description of the AeroplaneTemperature of Engine Cylinders PowerOil Temperature Operational TemperatureThree-View Sketch Page Do not exceed this speed in any case Never exceed the maximum take-off weight of the aeroplaneAir Speeds 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 InspectionPre Take-Off Warming up the EngineTaxiing Take Off and Climb AwayCruising flight Descent and landingPage Rate of Climb Stalling Speeds CASTake off Distance at 15 m / 50 feet height Cruising SpeedsPage Assembly Dismantling the Horizontal and Vertical RudderDismantling the wings Page Tail Surfaces Wing Fuselage Landing GearFuel System Instrument EquipmentSense of Motion of the Control Elements Page Page Canopy Open / Close Safety BeltsFlap Control Flight Control InstrumentsMajor Overhaul Cleaning and CareAeroplane Repairs Anchorage of the AeroplanePage Empty Weight Maximum take-off weightOperation over this range is prohibited Useful weight, weight table Centre of gravity determination