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
  • Subchapter E - Powerplant
  • 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 and Flight Guidance 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
  • 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