Table of contents
Browse all sections of CS-27 Amdt 10 - Small Rotorcraft (Feb 2023)
- CS 27.955 Fuel flow
- CS 27.1549 Powerplant instruments
- CS 27.1399 Riding light
- CS 27.671 General
- CS 27.1021 Oil system drains
- CS 27.663 Ground resonance prevention means
- CS 27.931 Shafting critical speed
- AMC 27 General
- CS 27.1458 Lightweight flight recorder
- AMC1 27.251 Vibration
- SUBPART F — EQUIPMENT
- FLIGHT LOADS
- SUBPART E – POWERPLANT
- AMC1 27.853(c) Compartment interiors
- CS 27.927 Additional tests
- CS 27.561 General
- CS 27.681 Limit load static tests
- CS 27.45 General
- CS 27.321 General
- CS 27.1093 Induction system icing protection
- CS 27.923 Rotor drive system and control mechanism tests
- CS 27.855 Cargo and baggage compartments
- CS 27.1353 Storage battery design and installation
- CS 27.601 Design
- AMC1 27.307 Proof of structure
- CS 27.397 Limit pilot forces and torques
- CS 27.691 Autorotation control mechanism
- CS 27.753 Main float design
- CS 27.1470 Emergency locator transmitter (ELT)
- CS 27.1365 Electric cables
- ROTORS
- CS 27.562 Emergency landing dynamic conditions
- CS 27.1415 Ditching equipment
- Disclaimer
- AMC No 2 to CS 27.865 External loads
- CS 27.1337 Powerplant instruments
- AMC 27.807(d) Underwater emergency exits for passengers
- CS 27.609 Protection of structure
- AMC No 1 to CS 27.865 Class D (Human External Cargo) for Operations within Europe
- CS 27.755 Hulls
- GM1 27.1337(e) Powerplant instruments
- CS 27.1435 Hydraulic systems
- CS 27.1316 Electrical and electronic system lightning protection
- SUBPART D — DESIGN AND CONSTRUCTION
- CS 27.771 Pilot compartment
- CS 27.1583 Operating limitations
- Appendix C -- Criteria for Category A
- CS 27.1383 Landing lights
- AMC1 27.1521 Powerplant limitations
- CS 27.629 Flutter
- CS 27.787 Cargo and baggage compartments
- GENERAL
- AMC1 27.395 Control system
- FIRE PROTECTION
- CS 27.339 Resultant limit manoeuvring loads
- CS 27.685 Control system details
- CS 27.33 Main rotor speed and pitch limits
- CS 27.303 Factor of safety
- CS 27.351 Yawing conditions
- CONTROL SYSTEMS
- CS 27.672 Stability augmentation, automatic, and power-operated systems
- AMC1 27.965 Fuel tank tests
- CS 27.954 Fuel system lightning protection
- CS 27.475 Tyres and shock absorbers
- CS 27.1043 Cooling tests
- EMERGENCY LANDING CONDITIONS
- GM1 27.1302 Explanatory material
- CS 27.1397 Colour specifications
- MARKINGS AND PLACARDS
- CS 27.1461 Equipment containing high energy rotors
- GENERAL
- AMC2 27.1555 Control markings
- CS 27.805 Flight crew emergency exits
- CS 27.999 Fuel system drains
- LIGHTS
- LANDING GEAR
- AMC1 27.1045 Cooling test procedures
- FLIGHT CHARACTERISTICS
- AMC1 27.903(d) Engines
- CS 27.71 Glide performance
- CS 27.1189 Shut-off means
- CS 27.1143 Engine controls
- MG 1 Certification procedure for rotorcraft avionics equipment
- CS 27.143 Controllability and manoeuvrability
- CS 27.723 Shock absorption tests
- AMC1 27.1301 Function and installation
- CS 27.729 Retracting mechanism
- CS 27.1541 General
- CS 27.951 General
- CS 27.239 Spray characteristics
- SUBPART C – STRENGTH REQUIREMENTS
- AMC1 27.427 Unsymmetrical loads
- GENERAL
- AMC 27.1319 Equipment, systems and network information security protection
- AMC1 27.923 Rotor drive system and control mechanism tests
- AMC1 27.1505 Never-exceed speed
- CS 27.251 Vibration
- CS 27.973 Fuel tank filler connection
- CS 27.27 Centre of gravity limits
- CS 27.997 Fuel strainer or filter
- CS 27.1305 Powerplant instruments
- AMC 27.1411 Safety equipment - General
- CS 27.1509 Rotor speed
- CS 27.1501 General
- CS 27.659 Mass balance
- POWERPLANT CONTROLS AND ACCESSORIES
- CS 27.1525 Kinds of operations
- CS 27.1 Applicability
- AMC1 27.787 Cargo and baggage compartments
- AMC1 27.1305(l)(2) Powerplant instruments
- SUBPART A — GENERAL
- CS 27.479 Level landing conditions
- AMC 27.1415 Ditching equipment
- CS 27.235 Taxying condition
- CS 27.1367 Switches
- CS 27.621 Casting factors
- CS 27.549 Fuselage, landing gear, and rotor pylon structures
- GENERAL
- CS 27.1381 Instrument lights
- CS 27.1551 Oil quantity indicator
- AMC1 27.571 Fatigue evaluation of flight structure
- CS 27.1519 Weight and centre of gravity
- CS 27.1351 General
- CS 27.865 External loads
- CS 27.1557 Miscellaneous markings and placards
- CS 27.963 Fuel tanks: general
- CS 27.427 Unsymmetrical loads
- CS 27.141 General
- CS 27.1183 Lines, fittings, and components
- CS 27.563 Structural ditching and emergency flotation provisions
- AMC 27.1470 Emergency locator transmitters (ELTs)
- SUBPART G – OPERATING LIMITATIONS AND INFORMATION
- CS 27.631 Bird strike
- CS 27.1553 Fuel quantity indicator
- CS 27.737 Skis
- PERFORMANCE
- CS 27.965 Fuel tank tests
- CS 27.1327 Magnetic direction indicator
- CS 27.1385 Position light system installation
- CS 27.773 Pilot compartment view
- AMC1 27.607 Fasteners
- CS 27.395 Control system
- CS 27.301 Loads
- Incorporated amendments
- MG4 Full Authority Digital Electronic Controls (FADEC)
- CS 27.481 Tail-down landing conditions
- CS 27.1123 Exhaust piping
- CS 27.695 Power boost and power-operated control system
- CS 27.1323 Airspeed indicating system
- CS 27.779 Motion and effect of cockpit controls
- CS 27.871 Levelling marks
- AMC1 27.613 Material strength properties and design values
- CS 27.727 Reserve energy absorption drop test
- CS 27.505 Ski landing conditions
- CS 27.1019 Oil strainer or filter
- ROTOR DRIVE SYSTEM
- CS 27.777 Cockpit controls
- CS 27.1041 General
- CS 27.1555 Control markings
- Note from the editor
- CS 27.935 Shafting joints
- CS 27.785 Seats, berths, safety belts, and harnesses
- MG 16 Certification guidance for rotorcraft Night Vision Imaging System (NVIS) aircraft lighting systems
- CS 27.307 Proof of structure
- CS 27.1503 Airspeed limitations: general
- CS 27.861 Fire protection of structure, controls, and other parts
- CS 27.953 Fuel system independence
- CS 27.921 Rotor brake
- CS 27.611 Inspection provisions
- CS 27.602 Critical parts
- CS 27.605 Fabrication methods
- CS 27.975 Fuel tank vents
- CS 27.231 General
- CS 27.917 Design
- CS 27.959 Unusable fuel supply
- CS 27.1547 Magnetic direction indicator
- CS 27.1389 Position light distribution and intensities
- CS 27.29 Empty weight and corresponding centre of gravity
- CS 27.1013 Oil tanks
- CS 27.1302 Installed systems and equipment for use by the crew members
- CS 27.1543 Instrument markings: general
- CS 27.1457 Cockpit voice recorders
- CS 27.241 Ground resonance
- CS 27.1017 Oil lines and fittings
- AMC1 27.1529 Instructions for continued airworthiness
- CS 27.31 Removable ballast
- CS 27.1322 Warning, caution, and advisory lights
- CS 27.173 Static longitudinal stability
- CS 27.1045 Cooling test procedures
- CS 27.687 Spring devices
- CS 27.673 Primary flight control
- MISCELLANEOUS FLIGHT REQUIREMENTS
- CS 27.337 Limit manoeuvring load factor
- MG 21 Guidance on creating a system level Functional Hazard Assessment (FHA)
- GROUND LOADS
- CS 27.961 Fuel system hot weather operation
- CS 27.853 Compartment interiors
- CS 27.51 Take-off
- AMC 27.805(c) Flight crew emergency exits
- CS 27.1593 Exposure to volcanic cloud hazards
- CS 27.1585 Operating procedures
- CS 27.1301 Function and installation
- CS 27.977 Fuel tank outlet
- CS 27.177 Static directional stability
- CS 27.521 Float landing conditions
- CS 27.801 Ditching
- FUEL SYSTEM COMPONENTS
- AMC1 27.631 Bird strike
- CS 27.305 Strength and deformation
- AMC No 1 to CS 27.351 Yawing conditions
- CS 27.391 General
- CS 27.653 Pressure venting and drainage of rotor blades
- Appendix A - Instructions for Continued Airworthiness
- EXTERNAL LOADS
- Appendix 2 -- Test specification rationale
- CS 27.1321 Arrangement and visibility
- CS 27.833 Heaters
- AMC1 27.959 Unusable fuel supply
- CS 27.1505 Never-exceed speed
- GENERAL
- CS 27.1523 Minimum flight crew
- OIL SYSTEM
- AMC1 27.1337(b) Powerplant instruments
- FLOATS AND HULLS
- CS 27.731 Wheels
- CS 27.1141 Powerplant controls: general
- CS 27.1413 Safety belts
- GM2 27.1302 Examples of compliance matrices
- MG5 Agricultural dispensing equipment installation
- AMC 27.1593 Exposure to volcanic cloud hazards
- 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)
- MAIN COMPONENT REQUIREMENTS
- AMC2 27.801(e) and 27.802(c) Model test method for flotation stability
- COOLING
- AMC1 27.1093(b)(1)(i) Induction system icing protection
- CS 27.733 Tyres
- CS 27.497 Ground loading conditions: landing gear with tail wheels
- CS 27.1121 General
- CS 27.573 Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures
- CS 27.969 Fuel tank expansion space
- AMC1 27.610 Lightning and static electricity protection
- CS 27.775 Windshields and windows
- CS 27.501 Ground loading conditions: landing gear with skids
- CS 27.1393 Minimum intensities in any vertical plane of forward and rear position lights
- CS 27.1195 Fire detector systems
- CS 27.1587 Performance information
- CS 27.995 Fuel valves
- CS 27.1317 High-Intensity Radiated Fields (HIRF) protection
- CS 27.613 Material strength properties and design values
- CONTROL SURFACE AND SYSTEM LOADS
- CS 27.1559 Limitations placard
- CS 27.21 Proof of compliance
- CS 27.1163 Powerplant accessories
- GROUND AND WATER HANDLING CHARACTERISTICS
- CS 27.623 Bearing factors
- FATIGUE EVALUATION
- CS 27.341 Gust loads
- CS 27.25 Weight limits
- FUEL SYSTEM
- CS 27.901 Installation
- CS 27.1545 Airspeed indicator
- CS 27.661 Rotor blade clearance
- POWERPLANT FIRE PROTECTION
- SAFETY EQUIPMENT
- CS 27.735 Brakes
- CS 27.967 Fuel tank installation
- ELECTRICAL SYSTEMS AND EQUIPMENT
- CS 27.751 Main float buoyancy
- AMC 27.1302 Installed systems and equipment for use by the crew members
- CS 27.483 One-wheel landing conditions
- CS 27.863 Flammable fluid fire protection
- AMC No 3 27.865 External loads operations using simple personnel-carrying device systems
- CS 27.1565 Tail rotor
- GENERAL
- WATER LOADS
- CS 27.1521 Powerplant limitations
- AMC 27.783 Doors
- CS 27.802 Emergency Flotation
- CS 27.473 Ground loading conditions and assumptions
- CS 27.471 General
- AMC1 27.801 Ditching
- CS 27.1335 Flight director systems
- PERSONNEL AND CARGO ACCOMMODATIONS
- CS 27.939 Turbine engine operating characteristics
- CS 27.1091 Air induction
- CS 27.477 Landing gear arrangement
- CS 27.907 Engine vibration
- CS 27.1581 General
- Appendix D - HIRF Environments and Equipment HIRF Test Levels
- CS 27.1307 Miscellaneous equipment
- AMC No 2 to 27.351 Yaw manoeuvre conditions
- ROTORCRAFT FLIGHT MANUAL AND APPROVED MANUAL MATERIAL
- CS 27.1419 Ice protection
- AMC 27.1561 Safety equipment
- MISCELLANEOUS
- CS 27.1395 Maximum intensities in overlapping beams of forward and rear position lights
- AMC1 27.1555 Control markings
- CS 27.399 Dual control system
- CS 27.1319 Equipment, systems and network information security protection
- AMC2 27.1337(e) Powerplant instruments
- CS 27.675 Stops
- CS 27.1561 Safety equipment
- CS 27.547 Main rotor structure
- CS 27.361 Engine torque
- CS 27.49 Performance at minimum operating speed
- CS 27.1411 General
- CS 27.993 Fuel system lines and fittings
- CS 27.831 Ventilation
- CS 27.1194 Other surfaces
- AMC 27.45 Performance General
- CS 27.1529 Instructions for Continued Airworthiness
- CS 27.873 Ballast provisions
- CS 27.1145 Ignition switches
- CS 27.1151 Rotor brake controls
- CS 27.67 Climb: one-engine-inoperative
- CS 27.1361 Master switch
- CS 27.674 Interconnected controls
- CS 27.75 Landing
- CS 27.1011 Engines: general
- CS 27.1303 Flight and navigation instruments
- CS 27.783 Doors
- SUBPART B – FLIGHT
- Appendix 1 -- Worked example
- CS 27.1325 Static pressure systems
- CS 27.65 Climb: all-engines-operating
- CS 27.1589 Loading information
- CS 27.679 Control system locks
- CS 27.603 Materials
- CS 27.1027 Transmissions and gearboxes: general
- CS 27.1527 Maximum operating altitude
- CS 27.952 Fuel system crash resistance
- CS 27.991 Fuel pumps
- Preamble
- CS 27.1357 Circuit protective devices
- CS 27.1015 Oil tank tests
- Appendix B - Airworthiness Criteria for Helicopter Instrument Flight
- CS 27.625 Fitting factors
- AMC1 27.1458 Lightweight flight recorder
- CS 27.151 Flight controls
- EXHAUST SYSTEM
- CS 27.607 Fasteners
- OPERATING LIMITATIONS
- CS 27.2 Special Retroactive Requirements
- CS 27.1391 Minimum intensities in the horizontal plane of forward and rear position lights
- CS 27.1387 Position light system dihedral angles
- CS 27.859 Heating systems
- INDUCTION SYSTEM
- CS 27.903 Engines
- CS 27.175 Demonstration of static longitudinal stability
- CS 27.1309 Equipment, systems, and installations
- CS 27.1187 Ventilation and drainage
- CS 27.493 Braked roll conditions
- AMC1 27.337 Limit manoeuvring load factor
- CS 27.1329 Automatic pilot system
- CS 27.725 Limit drop test
- CS 27.1193 Cowling and engine compartment covering
- CS 27.161 Trim control
- AMC 27.865 External Loads
- AMC 27.802 Emergency Flotation
- CS 27.411 Ground clearance: tail rotor guard
- CS 27.485 Lateral drift landing conditions
- Miscellaneous guidance
- CS 27.1459 Flight recorders
- CS 27.171 Stability: general
- AMC 27.1302 APPENDIX 1: Related regulatory material and documents
- MG 17 Guidance on analysing an Advanced Flight Controls (AdFC) System
- CS 27.971 Fuel tank sump
- AMC 27.563 Structural ditching and emergency flotation provisions
- AMC2 27.307 Proof of structure
- CS 27.79 Limiting height-speed envelope
- CS 27.610 Lightning and static electricity protection
- AMC1 27.927 Additional tests
- AMC1 27.1309 Equipment, systems, and installations
- CS 27.309 Design limitations
- AMC 27.1587(b)(3) Performance Information
- INSTRUMENTS: INSTALLATION
- CS 27.683 Operation tests
- CS 27.807 Passenger emergency exits
- MG 23 Automatic Flight Guidance and Control Systems (AFGCS) installation in CS-27 Rotorcraft
- CS 27.619 Special factors
- CS 27.571 Fatigue evaluation of flight structure
- CS 27.1185 Flammable fluids
- AMC3 27.307 Proof of structure
- CS 27.1401 Anti-collision light system
- CS 27.1191 Firewalls
- CS 27.1147 Mixture controls