PART II. PROCEDURES FOR CERTIFICATION AND CONTINUING AIRWORTHINESS
CHAPTER 1. TYPE CERTIFICATION
1.2 Design aspects of the appropriate airworthiness requirements
1.3 Proof of compliance with the appropriate airworthiness requirements
1.4 Issuance of Type Certificate
1.5 Suspension of Type Certificate
1.6 Revocation of Type Certificate
1.7 Transfer of Type Certificate
2.2 Aircraft, engine and propeller production
2.3 Aircraft parts production
CHAPTER 3. CERTIFICATE OF AIRWORTHINESS
3.2 Eligibility, issuance and continued validity of a Certificate of Airworthiness
3.5 Temporary loss of airworthiness
3.4 Aircraft limitations and information
3.3 Standard form of Certificate of Airworthiness
4.2 Responsibilities of Contracting States in respect of continuing airworthiness
CHAPTER 4. CONTINUING AIRWORTHINESS
CHAPTER 5. SAFETY MANAGEMENT
6.2 Maintenance organization approval
CHAPTER 6. MAINTENANCE ORGANIZATION APPROVAL
6.3 Maintenance organization’s procedures manual
6.4 Maintenance procedures and quality assurance system
PART III. LARGE AEROPLANES
PART IIIA. AEROPLANES OVER 5 700 KG FOR WHICH APPLICATION FOR CERTIFICATION WAS SUBMITTED ON OR AFTER 13 JUNE 1960 BUT BEFORE 2 MARCH 2004
1.4 Unsafe features and characteristics
1.3 Operating limitations
3.4 Ground and water loads
3.6 Flutter, divergence and vibration
CHAPTER 4. DESIGN AND CONSTRUCTION
5.3 Declared ratings, conditions and limitations
5.2 Design, construction and functioning
6.2 Design, construction and functioning
6.3 Declared ratings, conditions and limitations
CHAPTER 7. POWERPLANT INSTALLATION
7.2 Arrangement and functioning
8.1 Required instruments and equipment
8.3 Safety and survival equipment
8.4 Navigation lights and anti-collision lights
CHAPTER 8. INSTRUMENTS AND EQUIPMENT
9.2 Operating limitations
CHAPTER 9. OPERATING LIMITATIONS AND INFORMATION
9.3 Operating information and procedures
9.4 Performance information
9.6 Markings and placards
9.5 Aeroplane flight manual
10.2 Maintenance information
10.3 Maintenance programme information
10.4 Maintenance information resulting from the type design approval
CHAPTER 10. CONTINUING AIRWORTHINESS —MAINTENANCE INFORMATION
11.1 Aeroplanes used for domestic commercial operations
11.2 Least-risk bomb location
11.3 Protection of the flight crew compartment
PART IIIB. AEROPLANES OVER 5 700 KG FOR WHICH APPLICATIONFOR CERTIFICATION WAS SUBMITTED ON OR AFTER 2 MARCH 2004
1.3 Operating limitations
1.4 Unsafe features and characteristics
2.4 Stability and control
3.4 Strength and deformation
3.2 Mass and mass distribution
3.8 Structural durability
CHAPTER 4. DESIGN AND CONSTRUCTION
4.2 Systems design features
4.4 Occupants accommodation features
4.5 Electrical bonding and protection against lightning and static electricity
4.6 Emergency landing provisions
5.3 Powerplant installation
CHAPTER 6. SYSTEMS AND EQUIPMENT
6.5 Electromagnetic interference protection
6.3 Safety and survival equipment
6.4 Navigation lights and anti-collision lights
CHAPTER 7. OPERATING LIMITATIONS AND INFORMATION
7.2 Operating limitations
7.3 Operating information and procedures
7.6 Markings and placards
7.7 Continuing airworthiness — maintenance information
7.4 Performance information
8.2 Design emergency landing loads
8.3 Cabin fire protection
CHAPTER 8. CRASHWORTHINESS AND CABIN SAFETY
CHAPTER 9. OPERATING ENVIRONMENT AND HUMAN FACTORS
9.4 Operating environmental factors
10.1 Aeroplanes used for domestic commercial operations
10.2 Least-risk bomb location
10.3 Protection of the flight crew compartment
PART IVA. HELICOPTERS FOR WHICH APPLICATION FOR CERTIFICATIONWAS SUBMITTED ON OR AFTER 22 MARCH 1991BUT BEFORE 13 DECEMBER 2007
1.3 Unsafe features and characteristics
3.3 Main rotor(s) rotational speed limits
3.5 Ground and water loads
3.7 Flutter, divergence and vibration
CHAPTER 4. DESIGN AND CONSTRUCTION
5.2 Design, construction and functioning
5.3 Declared ratings, conditions and limitations
CHAPTER 6. ROTOR AND POWER TRANSMISSION SYSTEMSAND POWERPLANT INSTALLATION
6.2 Design, construction and functioning
6.3 Declared ratings, conditions and limitations
6.8 Arrangement and functioning
6.6 Control of engine rotation
6.5 Compliance with engine and rotor and powertransmission systems limitations
CHAPTER 7. INSTRUMENTS AND EQUIPMENT
7.4 Navigation lights and anti-collision lights
7.3 Safety and survival equipment
7.1 Required instruments and equipment
CHAPTER 8. ELECTRICAL SYSTEMS
9.2 Operating limitations
CHAPTER 9. OPERATING LIMITATIONS AND INFORMATION
9.3 Operating information and procedures
9.5 Helicopter flight manual
9.4 Performance information
9.6 Markings and placards
PART IVB. HELICOPTERS FOR WHICH APPLICATION FOR CERTIFICATION WAS SUBMITTED ON OR AFTER 13 DECEMBER 2007
1.2 Operating limitations
1.3 Unsafe features and characteristics
2.4 Stability and control
3.4 Strength and deformation
3.2 Mass and mass distribution
3.8 Ground and water loads
3.6 Main rotor(s) rotational speed limits
CHAPTER 4. DESIGN AND CONSTRUCTION
4.2 Systems design features
4.4 Occupant accommodation features
4.5 Electrical bonding and protection against lightning and static electricity
4.6 Emergency landing provisions
CHAPTER 5. ROTORS AND POWERPLANT
5.2 Rotors and powerplant installation
CHAPTER 6. SYSTEMS AND EQUIPMENT
6.3 Safety and survival equipment
6.4 Navigation lights and anti-collision lights
6.5 Electromagnetic interference protection
CHAPTER 7. OPERATING LIMITATIONS AND INFORMATION
7.2 Operating limitations
7.3 Operating information and procedures
7.7 Continuing airworthiness — maintenance information
7.6 Markings and placards
7.4 Performance information
8.3 Cabin fire protection
8.2 Design emergency landing loads
CHAPTER 8. CRASHWORTHINESS AND CABIN SAFETY
CHAPTER 9. OPERATING ENVIRONMENT AND HUMAN FACTORS
9.4 Operating environmental factors
1.2 Operating limitations
PART VA. AEROPLANES OVER 750 KG BUT NOT EXCEEDING 5 700 KG FOR WHICH APPLICATION FOR CERTIFICATION WAS SUBMITTED ON OR AFTER 13 DECEMBER 2007 BUT BEFORE 7 MARCH 2021
1.3 Unsafe features and characteristics
2.4 Stability and control
3.2 Mass and mass distribution
3.4 Strength and deformation
3.8 Structural durability
CHAPTER 4. DESIGN AND CONSTRUCTION
4.2 Systems design features
4.5 Electrical bonding and protection against lightning and static electricity
4.6 Emergency landing provisions
4.4 Occupant accommodation features
5.3 Powerplant installation
CHAPTER 6. SYSTEMS AND EQUIPMENT
6.5 Electromagnetic interference protection
6.3 Safety and survival equipment
6.4 Navigation lights and anti-collision lights
CHAPTER 7. OPERATING LIMITATIONS AND INFORMATION
7.2 Operating limitations
7.3 Operating information and procedures
7.4 Performance information
7.6 Markings and placards
7.7 Continuing airworthiness — maintenance information
8.2 Design emergency landing loads
CHAPTER 8. CRASHWORTHINESS AND CABIN SAFETY
8.3 Cabin fire protection
CHAPTER 9. OPERATING ENVIRONMENT AND HUMAN FACTORS
9.4 Operating environmental factors
1.2 Operating limitations
PART VB. AEROPLANES NOT EXCEEDING 5 700 KG FOR WHICH APPLICATION FOR CERTIFICATION IS SUBMITTED ON OR AFTER 7 MARCH 2021
1.3 Unsafe features and characteristics
2.4 Stability and control
3.2 Mass and mass distribution
3.4 Strength and deformation
3.8 Structural durability
CHAPTER 4. DESIGN AND CONSTRUCTION
4.2 Systems design features
4.4 Occupant accommodation features
4.5 Electrical bonding and protection against lightning and static electricity
4.6 Emergency landing provisions
5.3 Powerplant installation
CHAPTER 6. SYSTEMS AND EQUIPMENT
6.5 Electromagnetic interference protection
6.3 Safety and survival equipment
6.4 Navigation lights and anti-collision lights
CHAPTER 7. OPERATING LIMITATIONS AND INFORMATION
7.2 Operating limitations
7.3 Operating information and procedures
7.4 Performance information
7.6 Markings and placards
7.7 Continuing airworthiness — maintenance information
8.3 Cabin fire protection
8.2 Design emergency landing loads
CHAPTER 8. CRASHWORTHINESS AND CABIN SAFETY
CHAPTER 9. OPERATING ENVIRONMENT AND HUMAN FACTORS
9.4 Operating environmental factors
1.4 Continuing airworthiness – maintenance information
1.3 Declared ratings, conditions and limitations
1.2 Engine installation and interfaces
CHAPTER 2. DESIGN AND CONSTRUCTION
2.3 Materials and manufacturing methods
1.2 Declared ratings, conditions and limitations
1.3 Continuing airworthiness — maintenance information
2.4 Pitch control and indication
CHAPTER 2. DESIGN AND CONSTRUCTION
2.3 Materials and manufacturing methods
CHAPTER 3. TESTS AND INSPECTIONS
3.2 Operational and endurance tests
1.2 Operating limitations
PART VIII. REMOTELY PILOTED AEROPLANES
1.3 Unsafe features and characteristics
2.4 Stability and control
3.2 Mass and mass distribution
3.4 Strength and deformation
3.7 Structural durability
CHAPTER 4. DESIGN AND CONSTRUCTION
4.2 Systems design features
4.4 Electrical bonding and protection against lightning and static electricity
5.3 Powerplant installation
CHAPTER 6. SYSTEMS AND EQUIPMENT
6.3 Navigation lights and anti-collision lights
6.4 Electromagnetic interference protection
7.2 Operating limitations
CHAPTER 7. OPERATING LIMITATIONS AND INFORMATION
7.4 Performance information
7.3 Operating information and procedures
7.7 Continuing airworthiness — maintenance information
7.5 Remotely piloted aeroplane flight manual
7.6 Markings and placards
CHAPTER 9. OPERATING ENVIRONMENT AND HUMAN FACTORS
10.3 Controls and information
CHAPTER 10. REMOTE PILOT STATION INTEGRATION
CHAPTER 11. REMOTELY PILOTED AEROPLANE UNIQUE CONSIDERATIONS
11.2 Transportation, storage and assembly
11.6 Automatic taxi, take-off and landing
11.8 Detect and avoid, and other equipment
1.2 Operating limitations
PART IX. REMOTELY PILOTED HELICOPTERS (RPH)
1.3 Unsafe features and characteristics
2.4 Stability and control
3.2 Mass and mass distribution
3.4 Strength and deformation
3.6 Main rotor(s) rotational speed limits
3.8 Ground and water loads
CHAPTER 4. DESIGN AND CONSTRUCTION
4.2 Systems design features
4.4 Electrical bonding and protection against lightning and static electricity
CHAPTER 5. ROTORS AND POWERPLANT
5.2 Rotors and powerplant installation
CHAPTER 6. SYSTEMS AND EQUIPMENT
6.3 Navigation lights and anti-collision lights
6.4 Electromagnetic interference protection
7.2 Operating limitations
CHAPTER 7. OPERATING LIMITATIONS AND INFORMATION
7.4 Performance information
7.3 Operating information and procedures
7.7 Continuing airworthiness — maintenance information
7.5 Remotely piloted helicopter flight manual
7.6 Markings and placards
CHAPTER 9. OPERATING ENVIRONMENT AND HUMAN FACTORS
CHAPTER 10. REMOTE PILOT STATION INTEGRATION
10.3 Controls and information
CHAPTER 11. REMOTELY PILOTED HELICOPTER UNIQUE CONSIDERATIONS
11.2 Transportation, storage and assembly
11.6 Automatic taxi, take-off and landing
11.8 Detect and avoid, and other equipment
1.3 Continuing airworthiness — maintenance information
1.2 RPS interfaces and integration
PART X. REMOTE PILOT STATION (RPS)
2.5 Electrical bonding and protection against lightning and static electricity
CHAPTER 2. DESIGN AND CONSTRUCTION
2.1 Fire, smoke and toxic gas protection
2.4 Materials and manufacturing methods
2.6 Handling of the remote pilot station
3.3 Electromagnetic interference protection
CHAPTER 3. SYSTEM AND EQUIPMENT
3.2 Electrical power supply
3.4 Development assurance of complex electronic hardware and system software
CHAPTER 4. REMOTE FLIGHT CREW COMPARTMENT SAFETY
CHAPTER 5. OPERATING ENVIRONMENT AND HUMAN FACTORS
5.4 Operating environmental factors
6.2 Operating information and procedures
CHAPTER 6. OPERATING LIMITATIONS AND INFORMATION
7.1 Remote pilot station access control
APPENDIX. APPROVED MAINTENANCE ORGANIZATION (AMO) CERTIFICATE