Atec ATEC 212 SOLO ROTAX 912 UL Flap Control, Canopy Open / Close, Flight Control Instruments

Page 31

stops adjustment, rudder cable tensioning, clearance fits, securing.

 

 

 

 

 

Adjust, replace worn-out parts, grease, secure.

 

 

 

 

 

Flap Control

 

 

x

 

 

Check free movement of flap control lever, stable bearing in every flap

 

 

 

 

position, interlock pin wear. Replace worn-out parts, grease, secure.

 

 

 

 

 

Canopy – Open / Close

 

 

 

 

x

Check quality and function of locks and hinges, canopy bearing. Adjust,

 

 

 

 

replace worn-out parts, grease, secure.

 

 

 

 

 

Flight Control Instruments

 

 

 

 

x

Check legibility, markings, attachment instruments in panel, installations,

 

 

 

 

wiring.

 

 

 

 

 

Electric Installations

 

 

 

 

x

Check quality, integrity and purity of cables, insulations, contacts and

 

 

 

 

welds. Battery attachment, working condition.

 

 

 

 

 

Safety Belts

 

 

 

x

 

Check fixing points rigidity, belt surface quality, adjustment.

 

 

 

 

 

 

 

 

 

Fuel System

 

x

 

 

 

Check leak-proof condition, fuel supply quality, fuel pumps and valve

 

 

 

 

function, tank de-aeration. Replace fuel filters.

 

 

 

 

 

Parachute Rescue System

 

 

 

 

x

Check general condition, attachment. Do mandatory work as per

 

 

 

 

instructions of rescue system manufacturer.

 

 

 

 

 

 

 

 

 

 

 

Landing Gears

 

 

 

 

 

Main Gear

 

 

x

 

 

Check attachment rigidity, surface quality, degree of permanent

 

 

 

 

deformation.

 

 

 

 

 

Wheels

 

x

 

 

 

Check attachment, brakes condition, brake pads, disc quality, leak-proof

 

 

 

 

condition. Attachment and purity of wheel spats.

 

 

 

 

 

Front Gear

 

 

 

 

 

Check general condition, integrity, rubber damper, clearance, springing

 

x

 

 

 

deflection, steering quality. Grease sliding bearings, replace rubber

 

 

 

 

 

 

 

 

 

springs if worn-out.

 

 

 

 

 

 

 

 

 

 

 

Fuselage

 

 

 

 

x

Check general condition, integrity. Antennas, lights and coverings

 

 

 

 

attachment.

 

 

 

 

 

 

 

 

 

 

 

Wing

 

 

 

 

 

Check general condition, surface quality, integrity, attachment, fittings,

 

 

x

 

 

clearance. Ailerons and flaps condition, surface quality, hinges,

 

 

 

 

clearance, securing. Controls condition, free movement, end positions,

 

 

 

 

 

clearance. Pitot tube condition and attachment.

 

 

 

 

 

 

 

 

 

 

 

Tail Surfaces

 

 

 

 

 

Rudder, Elevator

 

 

 

 

x

Check general condition, hinges, movement, clearance, securing.

 

 

 

 

 

 

 

 

 

HT Stabilizer

 

 

 

x

 

Check general condition, attachment, fittings, securing.

 

 

 

 

 

 

 

 

 

 

10

25

50

100

200

31

Image 31
Contents Atec 212 Solo Type of aeroplane Atec 212 SoloPage Page Personal data of the owner IntroductionDescription of the Aeroplane Specification DimensionsRescue System installed / not installed……… WeightsOperational Temperature PowerOil Temperature Temperature of Engine CylindersThree-View Sketch Page Do not exceed this speed by flaps deflected Never exceed the maximum take-off weight of the aeroplaneAir Speeds Do not exceed this speed in any caseCentre of Gravity CG Manoeuvre and Gust Envelope Type of operation Permitted ManoeuvresFuel Other limits WindPage Rescue system deployment Power-off flightAborted landing Emergency landingVibrations Page Pre-Flight Inspection Procedures Before Entering the CockpitTake Off and Climb Away Warming up the EngineTaxiing Pre Take-OffDescent and landing Cruising flightPage Cruising Speeds Stalling Speeds CASTake off Distance at 15 m / 50 feet height Rate of ClimbPage Dismantling the Horizontal and Vertical Rudder AssemblyDismantling the wings Page Landing Gear WingFuselage Tail SurfacesInstrument Equipment Fuel SystemSense of Motion of the Control Elements Page Page Flight Control Instruments Safety BeltsFlap Control Canopy Open / CloseAnchorage of the Aeroplane Cleaning and CareAeroplane Repairs Major OverhaulPage Maximum take-off weight Empty WeightOperation over this range is prohibited Centre of gravity determination Useful weight, weight table