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Module 12

Module 12: Helicopter Aerodynamics, Structures and Systems

A3 A4 B1.3 B1.4
Commission Implementing Regulation (EU) 2023/989 amending Regulation (EU) No 1321/2014, Annex III (Part-66), Appendix I 12 June 2024

Knowledge Level Overview

RefTopicA3/A4B1.3/B1.4
12.1Theory of flight – rotary wing aerodynamics12
12.2Flight control systems (ATA 67)23
12.3Blade tracking and vibration analysis (ATA 18)13
12.4Transmission13
12.5(a)Airframe structures (ATA 51) — General concept22
12.5(b)Airframe structures (ATA 51) — Construction methods of the principal elements12
12.6.1Air conditioning (ATA 21) — Air supply12
12.6.2Air conditioning (ATA 21) — Air conditioning13
12.7.1Instrument systems (ATA 31)12
12.7.2Avionics systems11
12.8Electrical power (ATA 24)13
12.9(a)Equipment and furnishings (ATA 25) — Emergency equipment; seats, harnesses & belts; lifting systems22
12.9(b)Equipment and furnishings (ATA 25) — Emergency flotation; cabin layout; cargo retention; equipment & furnishing installation11
12.10(a)Fire protection (ATA 26) — Fire & smoke detection and fire-extinguishing systems13
12.10(b)Fire protection (ATA 26) — Portable fire extinguishers11
12.11Fuel systems (ATA 28)13
12.12Hydraulic power (ATA 29)13
12.13Ice and rain protection (ATA 30)13
12.14(a)Landing gear (ATA 32) — System description and operation23
12.14(b)Landing gear (ATA 32) — Sensors23
12.15Lights (ATA 33)23
12.16(Reserved)
12.17(a)Integrated modular avionics (ATA 42) — Overall system description and theory12
12.17(b)Integrated modular avionics (ATA 42) — Typical system layouts12
12.18On-board maintenance systems (ATA 45)12
12.19Information systems (ATA 46)12

Knowledge levels: 1 = basic familiarisation, 2 = general knowledge, 3 = detailed knowledge. A dash (—) means the topic is not required for that category.

Note: In Appendix I the levels are listed under two combined columns — A3 and A4 share identical requirements, as do B1.3 and B1.4.

1 Basic familiarisation 2 General knowledge 3 Detailed knowledge

Examination

CategoryQuestionsDuration
A (A3/A4)100125 min
B1 (B1.3/B1.4)128160 min

Detailed Syllabus

12.1Theory of Flight — Rotary Wing Aerodynamics

  • Terminology (rotor disc, tip path plane, advancing/retreating blade, etc.)
  • Aerodynamic principles of rotary wing flight
  • Torque reaction and directional control (tail rotor, NOTAR, Fenestron)
  • Gyroscopic precession and phase lag
  • Dissymmetry of lift and blade flapping
  • Ground effect and translational lift
  • Autorotation principles
  • Vortex ring state, blade stall, compressibility effects
  • Coriolis effect on blade lead-lag
  • Hovering, forward flight, climbing, descending, turning flight

12.2Flight Control Systems (ATA 67)

  • Swashplate assembly: rotating and non-rotating stars
  • Collective pitch control system
  • Cyclic pitch control system
  • Tail rotor / yaw control system
  • Mixing unit and control rods
  • Servo and hydraulic boost units
  • Flight control rigging and adjustment
  • Stability augmentation systems (SAS)
  • Autopilot systems and AFCS (Automatic Flight Control Systems)
  • Trim systems
  • Active vibration control systems
  • FBW (fly-by-wire) helicopter applications

12.3Blade Tracking and Vibration Analysis (ATA 18)

  • Vibration theory: frequency, amplitude, sources
  • Rotor track and balance fundamentals
  • Blade tracking methods (flag, strobe, electronic)
  • Vibration analysis techniques
  • 1-per-rev, 2-per-rev, and higher-order vibration identification
  • Span-wise and chord-wise balance
  • Autobalance and automatic tracking systems
  • Vibration health monitoring (VHM) systems

12.4Transmissions

  • Main gearbox: types, construction, operation
  • Intermediate and tail rotor gearboxes
  • Freewheeling units (sprag clutches, roller clutches)
  • Rotor brakes
  • Transmission lubrication and cooling systems
  • Drive shafts, couplings, and hangers
  • Chip detectors and debris monitoring
  • Health and Usage Monitoring Systems (HUMS) for transmissions
  • Gearbox inspection and maintenance requirements
  • Over-torque and over-speed procedures

12.5Airframe Structures

12.5(a)Structural Requirements

  • Airworthiness requirements for helicopter structures (CS-27, CS-29)
  • Structural classification: primary, secondary, tertiary
  • Damage tolerance and safe-life concepts
  • Crashworthiness requirements
  • Fatigue life and component retirement
  • Zonal and structural inspections

12.5(b)Construction Methods

  • Fuselage construction: skin, frames, bulkheads, stringers, longerons
  • Tailboom and tail pylon construction
  • Composite materials in helicopter structures
  • Bonded and riveted construction
  • Structural repairs: temporary and permanent
  • Rotor blade construction (spars, skins, honeycomb, erosion strips)
  • Main rotor head components (hub, grips, dampers, bearings)
  • Elastomeric bearings (spherical, lamiflex)
  • Pylon mounting and vibration isolation
  • Engine mounting systems

12.6Air Conditioning (ATA 21)

12.6.1Air Supply (ATA 21)

  • Sources of bleed air (engine, APU)
  • APU bleed air
  • Ram air and fresh air ventilation
  • Combustion heaters

12.6.2Air Conditioning (ATA 21)

  • Heating and ventilation systems
  • Vapour cycle cooling systems
  • Air cycle machine cooling
  • Temperature control and distribution
  • Pressurisation systems (where applicable)
  • Cabin environmental monitoring

12.7Instruments / Avionic Systems

12.7.1Instruments

  • Pitot-static instruments (ASI, altimeter, VSI)
  • Gyroscopic instruments (attitude indicator, HSI, turn coordinator)
  • Engine instruments (torque, N1, N2, TOT/TGT, oil pressure/temp)
  • Rotor RPM indicators (Nr, Nf)
  • EFIS and glass cockpit displays
  • Caution and warning systems

12.7.2Avionic Systems

  • Communication systems (VHF, HF, SATCOM, intercom)
  • Navigation systems (VOR, ILS, GPS, RNAV, ADF)
  • TCAS and transponder systems
  • Radio altimeter
  • Weather radar
  • ELT (Emergency Locator Transmitter)
  • CVR and FDR (recorders)
  • TAWS/EGPWS (Terrain Awareness)

12.8Electrical Power (ATA 24)

  • DC generation (starter-generators, battery systems)
  • AC generation (alternators, inverters)
  • Power distribution and bus architecture
  • Circuit protection (breakers, fuses, current limiters)
  • External power connections
  • Battery types and maintenance (lead-acid, NiCd, Li-ion)
  • Emergency power systems
  • Electrical load management

12.9Equipment and Furnishings (ATA 25)

12.9(a)Emergency Equipment (ATA 25)

  • Emergency equipment (ELT, life rafts, flotation)
  • Emergency flotation systems
  • Life jackets and emergency breathing systems
  • First aid kits, portable fire extinguishers
  • Emergency exit marking and lighting

12.9(b)Cabin/Cargo Layout (ATA 25)

  • Cabin layout and configuration
  • Seats, harnesses, and restraint systems
  • Cargo handling and securing
  • Emergency exits and jettison systems
  • Soundproofing and insulation

12.10Fire Protection (ATA 26)

  • Fire detection systems (thermocouple, thermistor, continuous loop)
  • Fire extinguishing systems (engine, APU, baggage)
  • Fire extinguishing agents (Halon alternatives, dry powder)
  • Fire zones and firewall construction
  • Smoke detection systems
  • Portable fire extinguishers
  • Fire protection system testing and maintenance

12.11Fuel Systems (ATA 28)

  • Fuel system layout (gravity feed, pressure feed)
  • Fuel tanks (bladder, integral, crashworthy)
  • Fuel pumps (boost, transfer, engine-driven)
  • Fuel quantity indication systems
  • Fuel jettison and crossfeed systems
  • Fuel filtration and water separation
  • Refuelling and defuelling procedures
  • Crashworthy fuel system requirements

12.12Hydraulic Power (ATA 29)

  • Hydraulic system architecture (single, dual, utility/flight)
  • Hydraulic pumps (engine-driven, electric, hand)
  • Reservoirs, accumulators, filters
  • Hydraulic fluid types and maintenance
  • Servo actuators for flight controls
  • System monitoring and warnings
  • Hydraulic system maintenance and troubleshooting

12.13Ice and Rain Protection (ATA 30)

  • Ice formation and effects on helicopters
  • Anti-icing systems (electrical, bleed air)
  • De-icing systems (pneumatic boots, electro-thermal)
  • Rotor blade de-icing/anti-icing
  • Windshield wiper and rain repellent systems
  • Engine intake anti-icing
  • Ice detection systems

12.14Landing Gear (ATA 32)

  • Skid-type landing gear (cross tubes, skid shoes)
  • Wheeled landing gear (fixed, retractable)
  • Ground resonance and shimmy dampers
  • Float gear and emergency flotation systems
  • Helicopter Ground Handling Wheels (HGW)
  • Bear paw / snow shoes
  • Shock absorbers and energy absorption

12.15Lights (ATA 33)

  • External lighting (navigation, anti-collision, landing, search)
  • Internal lighting (cockpit, cabin, instrument)
  • Emergency lighting systems
  • NVG-compatible lighting

12.16Reserved

12.17Integrated Modular Avionics (ATA 42)

  • IMA concept and architecture
  • Common computing resources
  • Core processing and I/O modules
  • ARINC 653 partitioning
  • IMA advantages for helicopter systems
  • Configuration and line replaceable modules

12.18On Board Maintenance Systems (ATA 45)

  • Central maintenance computers
  • Built-in test equipment (BITE)
  • Data loading systems
  • Health and Usage Monitoring Systems (HUMS)
  • Vibration health monitoring integration
  • Fault reporting and diagnosis

12.19Information Systems (ATA 46)

  • Electronic Flight Bag (EFB)
  • Aircraft communications addressing and reporting (ACARS)
  • Cabin management systems
  • Data network systems
  • Software configuration management

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