Table of contents
Browse all sections of CS-29 Amdt 12 - Large Rotorcraft (Mar 2026)
- CS 29.610 Lightning and static electricity protection
- AMC 29.1460 Data link recorders
- CS 29.303 Factor of safety
- CS 29.927 Additional tests
- AMC2 29.1555 Control markings
- CS 29.955 Fuel flow
- CS 29.675 Stops
- CS 29.1041 General
- MG5 Agricultural dispensing equipment installation
- CS 29.973 Fuel tank filler connection
- CS 29.1321 Arrangement and visibility
- CS 29.1045 Climb cooling test procedures
- CS 29.1439 Protective breathing equipment
- CS 29.1027 Transmissions and gearboxes: General
- CS 29.1191 Firewalls
- Appendix 2 -- Test specification rationale
- CS 29.563 Structural ditching and emergency flotation provisions
- CS 29.399 Dual control system
- CS 29.64 Climb: General
- AMC1 29.1555 Control markings
- CS 29.908 Cooling fans
- CS 29.1549 Powerplant instruments
- CS 29.143 Controllability and manoeuvrability
- CS 29.1157 Carburettor air temperature controls
- CS 29.1541 General
- GM1 29.1337(e) Power plant instruments
- MAIN COMPONENT REQUIREMENTS
- CS 29.691 Autorotation control mechanism
- GENERAL
- FLIGHT LOADS
- CS 29.957 Flow between inter-connected tanks
- AMC2 29.1337(e) Power plant instruments
- Subpart F -- Equipment
- CS 29.1543 Instrument markings: general
- AMC 29.1197 Fire extinguishing agents
- CS 29.723 Shock absorption tests
- AMC1 29.251 Vibration
- Disclaimer
- CS 29.773 Pilot compartment view
- CS 29.307 Proof of structure
- CS 29.151 Flight controls
- CS 29.959 Unusable fuel supply
- CS 29.1317 High-Intensity Radiated Fields (HIRF) protection
- CS 29.551 Auxiliary lifting surfaces
- CS 29.1555 Control markings
- AMC1 29.1413(a) Safety belts: passenger warning device
- Subpart E -- Powerplant
- CS 29.1589 Loading information
- CS 29.1189 Shutoff means
- CS 29.395 Control system
- CS 29.351 Yawing conditions
- AMC 29.563 Structural ditching and emergency flotation provisions
- CS 29.855 Cargo and baggage compartments
- CS 29.1201 Fire extinguishing system materials
- AMC3 29.917 Rotor drive system design
- Incorporated amendments
- AMC 29.547 Main rotor and tail rotor structure
- CS 29.1415 Ditching equipment
- OPERATING LIMITATIONS
- CS 29.1141 Powerplant controls: general
- CS 29.672 Stability augmentation, automatic, and power-operated systems
- CS 29.29 Empty weight and corresponding centre of gravity
- CS 29.81 Landing distance (ground level sites): Category A
- CS 29.813 Emergency exit access
- CS 29.777 Cockpit controls
- CS 29.735 Brakes
- CS 29.173 Static longitudinal stability
- CS 29.1325 Static pressure and pressure altimeter systems
- CONTROL SYSTEMS
- CS 29.1391 Minimum intensities in the horizontal plane of forward and rear position lights
- AMC 29.813 Emergency exit access
- CS 29.953 Fuel system independence
- MG 16 Certification guidance for rotorcraft Night Vision Imaging System (NVIS) aircraft lighting systems
- CS 29.427 Unsymmetrical loads
- CS 29.695 Power boost and power-operated control system
- Subpart G -- Operating Limitations and Information
- CS 29.1527 Maximum operating altitude
- CS 29.661 Rotor blade clearance
- CS 29.1109 Carburettor air cooling
- AMC1 29.571 Fatigue tolerance evaluation of metallic structure
- CS 29.1 Applicability
- CS 29.853 Compartment interiors
- CS 29.1337 Power plant instruments
- CS 29.1185 Flammable fluids
- CS 29.921 Rotor brake
- CS 29.1465 Vibration Health Monitoring
- CS 29.1419 lce protection
- AMC1 29.307 Proof of structure
- CS 29.783 Doors
- CS 29.1103 Induction systems ducts and air duct systems
- CS 29.785 Seats, berths, safety belts, and harnesses
- CS 29.1393 Minimum intensities in any vertical plane of forward and rear position lights
- CS 29.1187 Drainage and ventilation of fire zones
- CS 29.1459 Flight data recorders
- AMC 29.1470 Emergency locator transmitters (ELTs)
- AMC1 29.427 Unsymmetrical loads
- CS 29.901 Installation
- Appendix E - HIRF Environments and Equipment HIRF Test Levels
- MISCELLANEOUS FLIGHT REQUIREMENTS
- CS 29.977 Fuel tank outlet
- CS 29.1163 Powerplant accessories
- AMC2 29.853(c) Compartment interiors
- CS 29.65 Climb: All engines operating
- CS 29.1049 Hovering cooling test procedures
- CS 29.231 General
- AMC 29.803(c) Emergency evacuation
- AMC2 29.801(e) and 29.802(c) Model test method for flotation stability
- CS 29.809 Emergency exit arrangement
- CS 29.1193 Cowling and engine compartment covering
- CS 29.475 Tyres and shock absorbers
- CS 29.175 Demonstration of static longitudinal stability
- CS 29.729 Retracting mechanism
- AMC1 29.610 Lightning and static electricity protection
- CS 29.861 Fire protection of structure, controls, and other parts
- CS 29.1323 Airspeed indicating system
- CS 29.1019 Oil strainer or filter
- AMC1 29.917 Rotor drive system design
- COOLING
- AMC No 2 to CS 29.865 External loads operations using simple personnel-carrying device systems
- CS 29.1397 Colour specifications
- CS 29.341 Gust loads
- Subpart B -- Flight
- MARKINGS AND PLACARDS
- CS 29.961 Fuel system hot weather operation
- Appendix D - Criteria for demonstration of emergency evacuation procedures under CS 29.803
- CS 29.1521 Powerplant limitations
- CS 29.753 Main float design
- CS 29.611 Inspection provisions
- CS 29.1505 Never-exceed speed
- CS 29.1355 Distribution system
- CS 29.31 Removable ballast
- CS 29.1547 Magnetic direction indicator
- CS 29.1363 Electrical system tests
- CS 29.59 Take-off Path: Category A
- GROUND LOADS
- CS 29.547 Main and tail rotor structure
- CONTROL SURFACE AND SYSTEM LOADS
- CS 29.497 Ground loading conditions: landing gear with tail wheels
- CS 29.851 Fire extinguishers
- CS 29.1316 Electrical and electronic system lightning protection
- CS 29.673 Primary flight controls
- CS 29.1017 Oil lines and fittings
- CS 29.999 Fuel system drains
- CS 29.55 Take-off Decision Point: Category A
- CS 29.1151 Rotor brake controls
- AMC 29.1415 Ditching equipment
- CS 29.411 Ground clearance: tail rotor guard
- CS 29.87 Height-velocity envelope
- CS 29.631 Bird strike
- FLOATS AND HULLS
- CS 29.685 Control system details
- CS 29.1105 Induction system screens
- CS 29.549 Fuselage and rotor pylon structures
- CS 29.687 Spring devices
- CS 29.1013 Oil tanks
- CS 29.1322 Warning, caution, and advisory lights
- INSTRUMENTS: INSTALLATION
- CS 29.1559 Limitations placard
- CS 29.1470 Emergency locator transmitter (ELT)
- CS 29.1183 Lines, fittings, and components
- AMC1 29.1305(a)(4) Powerplant instruments
- CS 29.485 Lateral drift landing conditions
- CS 29.33 Main rotor speed and pitch limits
- CS 29.473 Ground loading conditions and assumptions
- AMC1 29.1505 Never-exceed speed
- CS 29.907 Engine vibration
- CS 29.62 Rejected take-off: Category A
- CS 29.1517 Limiting height-speed envelope
- CS 29.45 General
- GROUND AND WATER HANDLING CHARACTERISTICS
- CS 29.1551 Oil quantity indicator
- CS 29.865 External loads
- MG 1 Certification procedure for rotorcraft avionics equipment
- CS 29.605 Fabrication methods
- AMC 29.1587(c) Performance Information
- AMC 29.809 Emergency exit arrangement
- AMC1 29.1521 Powerplant limitations
- Appendix C - Icing Certification
- AMC No 2 to CS 29.351 Yaw manoeuvre conditions
- CS 29.659 Mass balance
- AMC1 29.1529 Instructions for Continued Airworthiness
- CS 29.1001 Fuel jettisoning
- CS 29.997 Fuel strainer or filter
- AMC1 29.807(d) Underwater emergency exits for passengers
- CS 29.1025 Oil valves
- CS 29.511 Ground load: unsymmetrical loads on multiple-wheel units
- CS 29.1147 Mixture controls
- AMC 29 General
- CS 29.61 Take-off distance: Category A
- CS 29.519 Hull type rotorcraft: Water-based and amphibian
- CS 29.321 General
- MISCELLANEOUS
- AMC2 29.307 Proof of structure
- CS 29.935 Shafting joints
- CS 29.1121 General
- MG 21 Guidance on creating a system level Functional Hazard Assessment (FHA)
- CS 29.1581 General
- AMC1 29.1310 Power source capacity and distribution
- CS 29.235 Taxying condition
- CS 29.471 General
- AMC 29.1561 Safety Equipment
- EASA eRules
- CS 29.1387 Position light system dihedral angles
- CS 29.815 Main aisle width
- CS 29.1413 Safety belts: passenger warning device
- CS 29.1583 Operating limitations
- CS 29.337 Limit manoeuvring load factor
- CS 29.1023 Oil radiators
- CS 29.1519 Weight and centre of gravity
- CS 29.521 Float landing conditions
- AMC 29.865 External Loads
- CS 29.1021 Oil system drains
- SAFETY EQUIPMENT
- AMC1 29.927 Additional tests
- CS 29.771 Pilot compartment
- CS 29.609 Protection of structure
- CS 29.674 Interconnected controls
- AMC 29.802 Emergency Flotation
- CS 29.1353 Electrical equipment and installations
- CS 29.683 Operation tests
- CS 29.807 Passenger emergency exits
- CS 29.607 Fasteners
- AMC1 29.607 Fasteners
- CS 29.251 Vibration
- PERFORMANCE
- CS 29.1461 Equipment containing high energy rotors
- ROTOR DRIVE SYSTEM
- AMC1 29.1319 Equipment, systems and network information security protection
- AMC1 29.1309 Equipment, systems, and installations
- MG 6 Emergency Medical Service (EMS) systems installations, including interior arrangements, equipment, Helicopter Terrain Awareness and Warning System (HTAWS), radio altimeter, and Flight Data Monitoring System (FDMS)
- CS 29.1399 Riding light
- CS 29.903 Engines
- CS 29.1523 Minimum flight crew
- AMC No 1 to CS 29.351 Yawing conditions
- CS 29.1307 Miscellaneous equipment
- CS 29.1101 Carburettor air preheater design
- CS 29.1333 Instrument systems
- CS 29.505 Ski landing conditions
- CS 29.479 Level landing conditions
- CS 29.779 Motion and effect of cockpit controls
- GM1 29.1465 Vibration health monitoring
- CS 29.1565 Tail rotor
- CS 29.481 Tail-down landing conditions
- CS 29.339 Resultant limit manoeuvring loads
- CS 29.1123 Exhaust piping
- CS 29.625 Fitting factors
- CS 29.1107 Inter-coolers and after-coolers
- POWERPLANT FIRE PROTECTION
- CS 29.493 Braked roll conditions
- LANDING GEAR
- Preamble
- AMC1 29.787 Cargo and baggage compartments
- AMC1 29.927(c) Additional tests
- FUEL SYSTEMS
- AMC3 29.307 Proof of structure
- CS 29.60 Elevated heliport take-off path: Category A
- CS 29.141 General
- CS 29.1309 Equipment, systems, and installations
- CS 29.671 General
- AMC2 29.917 Rotor drive system design
- CS 29.483 One-wheel landing conditions
- AMC 29.1585 Operating Procedures
- AMC1 29.853 Compartment interiors
- CS 29.1047 Take-off cooling test procedures
- CS 29.954 Fuel system lightning protection
- CS 29.181 Dynamic stability: Category A rotorcraft
- AMC1 29.1093(b)(1)(i) Induction system icing protection
- AMC2 29.903(e) Engines
- CS 29.305 Strength and deformation
- CS 29.653 Pressure venting and drainage of rotor blades
- CS 29.1199 Extinguishing agent containers
- CS 29.75 Landing: General
- CS 29.1301 Function and installation
- CS 29.1593 Exposure to volcanic cloud hazards
- AMC 29.1593 Exposure to volcanic cloud hazards
- CS 29.863 Flammable fluid fire protection
- FLIGHT CHARACTERISTICS
- CS 29.965 Fuel tank tests
- CS 29.737 Skis
- GENERAL
- CS 29.562 Emergency landing dynamic conditions
- CS 29.573 Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures
- AMC2 29.811(h) Underwater emergency exit markings
- AMC1 29.965 Fuel tank tests
- EXHAUST SYSTEM
- CS 29.177 Static directional stability
- CS 29.161 Trim control
- CS 29.952 Fuel system crash resistance
- CS 29.871 Levelling marks
- CS 29.787 Cargo and baggage compartments
- CS 29.1159 Supercharger controls
- CS 29.603 Materials
- AMC No 1 to CS 29.865 External loads
- AMC 29.851 Fire extinguishers
- LIGHTS
- CS 29.1043 Cooling tests
- CS 29.1435 Hydraulic systems
- CS 29.812 Emergency lighting
- CS 29.561 General
- CS 29.79 Landing: Category A
- CS 29.53 Take-off: Category A
- CS 29.939 Turbine engine operating characteristics
- CS 29.391 General
- AMC 29.1411 Safety equipment -- General
- AMC1 29.923 Rotor drive system and control mechanism tests
- CS 29.1585 Operating procedures
- CS 29.801 Ditching
- CS 29.991 Fuel pumps
- MG 17 Guidance on analysing an Advanced Flight Controls (AdFC) System
- CS 29.1357 Circuit protective devices
- CS 29.1093 Induction system icing protection
- CS 29.1145 Ignition switches
- CS 29.969 Fuel tank expansion space
- CS 29.963 Fuel tanks: general
- CS 29.1015 Oil tank tests
- PERSONNEL AND CARGO ACCOMMODATIONS
- CS 29.1203 Fire detector systems
- Subpart D -- Design and Construction
- AMC 29.1457 Cockpit Voice Recorders
- AMC1 29.811(d) Emergency exit marking
- ROTORS
- CS 29.623 Bearing factors
- AMC1 29.395 Control system
- CS 29.1142 Auxiliary power unit controls
- CS 29.967 Fuel tank installation
- INDUCTION SYSTEM
- CS 29.1319 Equipment, systems and network information security protection
- CS 29.477 Landing gear arrangement
- AMC1 29.801 Ditching
- AMC1 29.1145(a) Ignition switches
- CS 29.1460 Data link recorders
- CS 29.755 Hull buoyancy
- CS 29.1303 Flight and navigation instruments
- CS 29.241 Ground resonance
- CS 29.725 Limit drop test
- CS 29.51 Take-off data: General
- EXTERNAL LOADS
- CS 29.971 Fuel tank sump
- CS 29.1194 Other surfaces
- CS 29.833 Heaters
- CS 29.361 Engine torque
- CS 29.83 Landing: Category B
- Note from the editor
- CS 29.21 Proof of compliance
- CS 29.1457 Cockpit voice recorders
- CS 29.1503 Airspeed limitations: general
- CS 29.1545 Airspeed indicator
- CS 29.501 Ground loading conditions: landing gear with skids
- CS 29.1351 General
- CS 29.619 Special factors
- CS 29.1091 Air induction
- CS 29.873 Ballast provisions
- CS 29.1011 Engines: General
- FUEL SYSTEM COMPONENTS
- CS 29.571 Fatigue Tolerance Evaluation of Metallic Structure
- CS 29.1310 Power source capacity and distribution
- CS 29.859 Combustion heater fire protection
- CS 29.775 Windshields and windows
- CS 29.602 Critical parts
- CS 29.63 Take-off: Category B
- CS 29.1329 Automatic pilot system
- GENERAL
- CS 29.731 Wheels
- AMC1 29.903(d)(1) Turbine engine installation
- Appendix B - Airworthiness Criteria for Helicopter Instrument Flight
- CS 29.25 Weight limits
- FIRE PROTECTION
- AMC1 29.631 Bird strike
- CS 29.239 Spray characteristics
- CS 29.679 Control system locks
- CS 29.1165 Engine ignition systems
- GM1 29.1302 Explanatory material
- CS 29.733 Tyres
- CS 29.931 Shafting critical speed
- CS 29.1302 Installed systems and equipment for use by the crew members
- CS 29.67 Climb: One Engine Inoperative (OEI)
- CS 29.1401 Anti-collision light system
- CS 29.1431 Electronic equipment
- AMC1 29.1465 Vibration health monitoring
- CS 29.621 Casting factors
- GM2 29.1302 Examples of compliance matrices
- CS 29.811 Emergency exit marking
- CS 29.629 Flutter and divergence
- CS 29.85 Balked landing: Category A
- AMC 29.1302 Installed systems and equipment for use by the crew members
- CS 29.1385 Position light system installation
- AMC1 29.959 Unusable fuel supply
- CS 29.1381 Instrument lights
- Appendix A - Instructions for Continued Airworthiness
- CS 29.1561 Safety equipment
- GENERAL
- CS 29.1395 Maximum intensities in overlapping beams of forward and rear position lights
- Appendix 1 -- Worked example
- CS 29.1125 Exhaust heat exchangers
- CS 29.831 Ventilation
- CS 29.917 Design
- CS 29.1411 General
- CS 29.71 Helicopter angle of glide: Category B
- CS 29.1331 Instruments using a power supply
- CS 29.1143 Engine controls
- CS 29.1359 Electrical system fire and smoke protection
- AMC 29.805(c) Flight crew emergency exits
- Subpart C -- Strength requirements
- CS 29.802 Emergency Flotation
- CS 29.993 Fuel system lines and fittings
- WATER LOADS
- CS 29.1335 Flight director systems
- GENERAL
- CS 29.613 Material strength properties and design values
- CS 29.1522 Auxiliary power unit limitations
- OIL SYSTEM
- CS 29.751 Main float buoyancy
- AMC 29.1303 Flight and navigation instruments
- CS 29.601 Design
- CS 29.27 Centre of gravity limits
- CS 29.951 General
- AMC 29.1302 APPENDIX 1: Related regulatory material and documents
- CS 29.171 Stability: general
- CS 29.1181 Designated fire zones: regions included
- CS 29.1195 Fire extinguishing systems
- CS 29.1327 Magnetic direction indicator
- CS 29.975 Fuel tank vents and carburetor vapour vents
- CS 29.1433 Vacuum systems
- CS 29.803 Emergency evacuation
- AMC1 29.1301 Function and installation
- CS 29.681 Limit load static tests
- CS 29.979 Pressure refuelling and fuelling provisions below fuel level
- MISCELLANEOUS EQUIPMENT
- CS 29.49 Performance at minimum operating speed
- CS 29.1553 Fuel quantity indicator
- MG4 Full Authority Digital Electronic Controls (FADEC)
- CS 29.1383 Landing lights
- EMERGENCY LANDING CONDITIONS
- CS 29.1557 Miscellaneous markings and placards
- CS 29.77 Landing Decision Point: Category A
- CS 29.1501 General
- CS 29.663 Ground resonance prevention means
- GENERAL
- MG 23 Automatic Flight Guidance and Control Systems (AFGCS) installation in CS-29 Rotorcraft
- CS 29.757 Hull and auxiliary float strength
- POWERPLANT CONTROLS AND ACCESSORIES
- AMC 29.1583 Operating limitations
- CS 29.995 Fuel valves
- CS 29.1529 Instructions for Continued Airworthiness
- AMC1 29.337 Limit manoeuvring load factor
- Miscellaneous guidance
- CS 29.727 Reserve energy absorption drop test
- AMC 29.1459 Flight Data Recorders
- ROTORCRAFT FLIGHT MANUAL
- CS 29.301 Loads
- CS 29.397 Limit pilot forces and torques
- CS 29.805 Flight crew emergency exits
- FATIGUE EVALUATION
- CS 29.1197 Fire extinguishing agents
- CS 29.1525 Kinds of operation
- CS 29.1389 Position light distribution and intensities
- CS 29.309 Design limitations
- CS 29.1305 Powerplant instruments
- CS 29.923 Rotor drive system and control mechanism tests
- CS 29.1587 Performance information
- Subpart A -- General
- AMC1 29.613 Material strength properties and design values
- CS 29.1509 Rotor speed
- ELECTRICAL SYSTEMS AND EQUIPMENT