EASA PART 66 MODULE 11 P1, AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS,11.1.1,11.1.2,11.2

EASA PART 66 MODULE 11 AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS PART 1
(11.1 Theory of Flight 11.1.1 Aeroplane Aerodynamics and Flight Controls 11.1.2 High Speed Flight 11.2 Airframe Structures — General Concepts a b)

11.1 Theory of Flight

11.1.1 Aeroplane Aerodynamics and Flight Controls 
Operation and effect of:
— roll control: ailerons and spoilers;
— pitch control: elevators, stabilators, variable incidence stabilisers and canards;
— yaw control, rudder limiters;




  • Control using elevons, ruddervators;
  • High lift devices, slots, slats, flaps, flaperons;
  • Drag inducing devices, spoilers, lift dumpers, speed brakes;
  • Effects of wing fences, saw tooth leading edges;
  • Boundary layer control using, vortex generators, stall wedges or leading edge devices;
  • Operation and effect of trim tabs, balance and antibalance (leading) tabs, servo tabs,
  • spring tabs, mass balance, control surface bias, aerodynamic balance panels;


11.1.2 High Speed Flight
Speed of sound, subsonic flight, transonic flight, supersonic flight,
Mach number, critical Mach number, compressibility buffet, shock wave, aerodynamic heating, area rule;
Factors affecting airflow in engine intakes of high speed aircraft;
Effects of sweepback on critical Mach number.

11.2 Airframe Structures — General Concepts
(a)


  • Airworthiness requirements for structural strength;
  • Structural classification, primary, secondary and tertiary;
  • Fail safe, safe life, damage tolerance concepts;
  • Zonal and station identification systems;
  • Stress, strain, bending, compression, shear, torsion, tension, hoop stress, fatigue;
  • Drains and ventilation provisions;
  • System installation provisions;
  • Lightning strike protection provision.
  • Aircraft bonding

(B)
  • Construction methods of: stressed skin fuselage, formers, stringers, longerons, bulkheads,
  • frames, doublers, struts, ties, beams, floor structures, reinforcement, methods of skinning, anti-corrosive protection, wing, empennage and engine attachments;
  • Structure assembly techniques: riveting, bolting, bonding Methods of surface protection, such as chromating, anodising, painting;
  • Surface cleaning.
  • Airframe symmetry: methods of alignment and symmetry checks.


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