Airworthiness Manual Chapter 529 - Transport Category Rotorcraft - Canadian Aviation Regulations (CARs)

  • See also CAR 529

  • Preamble
  • Subchapter A - General
    • 529.1 - Applicability
    • 529.2 - Special Retroactive Requirements
  • Subchapter B - Flight - General
    • 529.21 - Proof of Compliance
    • 529.25 - Weight Limits
    • 529.27 - Centre of Gravity Limits
    • 529.29 - Empty Weight and Corresponding Centre of Gravity
    • 529.31 - Removable Ballast
    • 529.33 - Main Rotor Speed and Pitch Limits
  • Performance
    • 529.45 - General
    • 529.49 - Performance at Minimum Operating Speed
    • 529.51 - Take-off Data: General
    • 529.53 - Take-off: Category A
    • 529.55 - Take-off Decision Point (TDP): Category A
    • 529.59 - Take-off Path: Category A
    • 529.60 - Elevated Heliport Take-off Path: Category A
    • 529.61 - Take-off Distance: Category A
    • 529.62 - Rejected Take-off: Category A
    • 529.63 - Take-off: Category B
    • 529.64 - Climb: General
    • 529.65 - Climb: All Engines Operating
    • 529.67 - Climb: One Engine Inoperative (OEI)
    • 529.71 - Helicopter Angle of Glide: Category B
    • 529.75 - Landing: General
    • 529.77 - Landing Decision Point (LDP): Category A
    • 529.79 - Landing: Category A
    • 529.81 - Landing Distance: Category A
    • 529.83 - Landing: Category B
    • 529.85 - Balked Landing: Category A
    • 529.87 - Height-Velocity Envelope
  • Flight Characteristics
    • 529.141 - General
    • 529.143 - Controllability and Manoeuvrability
    • 529.151 - Flight Controls
    • 529.161 - Trim Control
    • 529.171 - Stability: General
    • 529.173 - Static Longitudinal Stability
    • 529.175 - Demonstration of Static Longitudinal Stability
    • 529.177 - Static Directional Stability
    • 529.181 - Dynamic Stability: Category A Rotorcraft
  • Ground and Water Handling Characteristics
  • Miscellaneous Flight Requirements
  • Subchapter C - Strength Requirements - General
  • Flight Loads
  • Control Surface and System Loads
  • Ground Loads
    • 529.471 - General
    • 529.473 - Ground Loading Conditions and Assumptions
    • 529.475 - Tires and Shock Absorbers
    • 529.477 - Landing Gear Arrangement
    • 529.479 - Level Landing Conditions
    • 529.481 - Tail-down Landing Conditions
    • 529.483 - One-wheel Landing Conditions
    • 529.485 - Lateral Drift Landing Conditions
    • 529.493 - Braked Roll Conditions
    • 529.497 - Ground Loading Conditions: Landing Gear with Tail Wheels
    • 529.501 - Ground Loading Conditions: Landing Gear with Skids
    • 529.505 - Ski Landing Conditions
    • 529.511 - Ground Load: Unsymmetrical Loads on Multiple-Wheel Units
  • Water Loads
    • 529.519 - Hull Type Rotorcraft: Water-based and Amphibian
    • 529.521 - Float Landing Conditions
  • Main Component Requirements
    • 529.547 - Main and Tail Rotor Structure
    • 529.549 - Fuselage and Rotor Pylon Structures
    • 529.551 - Auxiliary Lifting Surfaces
  • Emergency Landing Conditions
    • 529.561 - General
    • 529.562 - Emergency Landing Dynamic Conditions
    • 529.563 - Structural ditching provisions
  • Fatigue Evaluation
    • 529.571 - Fatigue Tolerance Evaluation of Metallic Structures
    • 529.573 - Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures
  • Subchapter D - Design And Construction - General
  • Rotors
    • 529.631 - Bird Strike
    • 529.653 - Pressure Venting and Drainage of Rotor Blades
    • 529.659 - Mass Balance
    • 529.661 - Rotor Blade Clearance
    • 529.663 - Ground Resonance Prevention Means
  • Control Systems
    • 529.671 - General
    • 529.672 - Stability Augmentation, Automatic, and Power operated Systems
    • 529.673 - Primary Flight Controls
    • 529.674 - Interconnected controls
    • 529.675 - Stops
    • 529.679 - Control System Locks
    • 529.681 - Limit Load Static Tests
    • 529.683 - Operation Tests
    • 529.685 - Control System Details
    • 529.687 - Spring Devices
    • 529.691 - Autorotation Control Mechanism
    • 529.695 - Power Boost and Power-operated Control System
  • Landing Gear
  • Floats and Hulls
  • Personnel and Cargo Accommodations
  • Fire Protection
    • 529.851 - Fire Extinguishers
    • 529.853 - Compartment Interiors
    • 529.855 - Cargo and Baggage Compartments
    • 529.859 - Combustion Heater Fire Protection
    • 529.861 - Fire Protection of Structure, Controls, and Other Parts
    • 529.863 - Flammable Fluid Fire Protection
  • External Loads
  • Miscellaneous
  • Subchapter E - Powerplant - General
  • Rotor Drive System
  • Fuel System
    • 529.951 - General
    • 529.952 - Fuel System Crash Resistance
    • 529.953 - Fuel System Independence
    • 529.954 - Fuel System Lightning Protection
    • 529.955 - Fuel Flow
    • 529.957 - Flow Between Interconnected Tanks
    • 529.959 - Unuseable Fuel Supply
    • 529.961 - Fuel System Hot Weather Operation
    • 529.963 - Fuel Tanks: General
    • 529.965 - Fuel Tank Tests
    • 529.967 - Fuel Tank Installation
    • 529.969 - Fuel Tank Expansion Space
    • 529.971 - Fuel Tank Sump
    • 529.973 - Fuel Tank Filler Connection
    • 529.975 - Fuel Tank Vents and Carburetor Vapour Vents
    • 529.977 - Fuel Tank Outlet
    • 529.979 - Pressure Refuelling and Fuelling Provisions Below Fuel Level
  • Fuel System Components
  • Oil System
  • Cooling
  • Induction System
    • 529.1091 - Air Induction
    • 529.1093 - Induction System Icing Protection
    • 529.1101 - Carburetor Air Preheater Design
    • 529.1103 - Induction Systems Ducts and Air Duct Systems
    • 529.1105 - Induction System Screens
    • 529.1107 - Inter-coolers and After-coolers
    • 529.1109 - Carburetor Air Cooling
  • Exhaust System
  • Powerplant Controls and Accessories
  • Powerplant Fire Protection
  • Subchapter F - Equipment General
    • 529.1301 - Function and Installation
    • 529.1301-1 - Rotorcraft Operations After Ground Cold Soak
    • 529.1303 - Flight and Navigation Instruments
    • 529.1305 - Powerplant Instruments
    • 529.1307 - Miscellaneous Equipment
    • 529.1309 - Equipment, Systems, and Installations
    • 529.1316 - Electrical and Electronic System Lightning Protection
    • 529.1317 - High-intensity Radiated Fields (HIRF) Protection
  • Instruments Installation
    • 529.1321 - Arrangement and Visibility
    • 529.1322 - Warning, Caution, and Advisory Lights
    • 529.1323 - Airspeed Indicating System
    • 529.1325 - Static Pressure and Pressure Altimeter Systems
    • 529.1327 - Magnetic Direction Indicator
    • 529.1329 - Automatic Pilot System
    • 529.1331 - Instruments Using a Power Supply
    • 529.1333 - Instrument Systems
    • 529.1335 - Flight Director Systems
    • 529.1337 - Powerplant Instruments
  • Electrical Systems and Equipment
  • Lights
    • 529.1381 - Instrument Lights
    • 529.1383 - Landing Lights
    • 529.1385 - Position Light System Installation
    • 529.1387 - Position Light System Dihedral Angles
    • 529.1389 - Position Light Distribution and Intensities
    • 529.1391 - Minimum Intensities in the Horizontal Plane of Forward and Rear Position Lights
    • 529.1393 - Minimum Intensities in Any Vertical Plane of Forward and Rear Position Lights
    • 529.1395 - Maximum Intensities in Overlapping Beams of Forward and Rear Position Lights
    • 529.1397 - Colour Specifications
    • 529.1399 - Riding Light
    • 529.1401 - Anticollision Light System
  • Safety Equipment
  • Miscellaneous Equipment
  • Subchapter G - Operating Limitations And Information
  • Operating Limitations
  • Markings and Placards
  • Rotorcraft Flight Manual
  • Appendix A - Instructions for Continued Airworthiness
  • Appendix B - Airworthiness Criteria For Helicopter Instrument Flight
  • Appendix C - Icing Certification
  • Appendix D - Criteria for Demonstration of Emergency Evacuation Procedures under 529.803
  • Appendix E - HIRF Environments and Equipment HIRF Test Levels