CHAPTER 1. TYPE CERTIFICATION
PART II. PROCEDURES FOR CERTIFICATION ANDCONTINUING AIRWORTHINESS
1.2 Design aspects of the appropriateairworthiness requirements
1.3 Proof of compliance with theappropriate 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
2.3 Aircraft parts production
2.2 Aircraft, engine and propeller production
3.2 Eligibility, issuance and continued validityof a Certificate of Airworthiness
CHAPTER 3. CERTIFICATE OF AIRWORTHINESS
3.3 Standard form of Certificate of Airworthiness
3.4 Aircraft limitations and information
3.5 Temporary loss of airworthiness
4.2 Responsibilities of Contracting Statesin respect of continuing airworthiness
CHAPTER 4. CONTINUING AIRWORTHINESS
CHAPTER 5. SAFETY MANAGEMENT
6.2 Maintenance organization approval
CHAPTER 6. MAINTENANCE ORGANIZATION APPROVAL. Applicable as of 5 November 2020.
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
1.3 Operating limitations
1.4 Unsafe features and characteristics
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
7.2 Arrangement and functioning
CHAPTER 7. POWERPLANT INSTALLATION
8.1 Required instruments and equipment
CHAPTER 8. INSTRUMENTS AND EQUIPMENT
*8.4 Navigation lights and anti-collision lights
8.3 Safety and survival equipment
9.2 Operating limitations
CHAPTER 9. OPERATING LIMITATIONS AND INFORMATION
9.3 Operating information and procedures
9.4 Performance information
9.5 Aeroplane flight manual
9.6 Markings and placards
10.2 Maintenance information
10.3 Maintenance programme information
CHAPTER 10. CONTINUING AIRWORTHINESS —MAINTENANCE INFORMATION
10.4 Maintenance information resulting from the type design approval
11.1 Aeroplanes used for domestic commercial operations
11.3 Protection of the flight crew compartment
11.2 Least-risk bomb location
PART IIIB. AEROPLANES OVER 5 700 KG FOR WHICH APPLICATION FOR CERTIFICATION WAS SUBMITTED ON OR AFTER 2 MARCH 2004
1.3 Operating limitations
1.4 Unsafe features and characteristics
2.4 Stability and control
3.2 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 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
7.7 Continuing airworthiness — maintenance information
7.6 Markings and placards
7.4 Performance information
CHAPTER 8. CRASHWORTHINESS AND CABIN SAFETY
8.2 Design emergency landing loads
8.3 Cabin fire protection
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 CERTIFICATION WAS SUBMITTED ON OR AFTER 22 MARCH 1991 BUT 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
5.3 Declared ratings, conditions and limitations
5.2 Design, construction and functioning
6.3 Declared ratings, conditions and limitations
CHAPTER 6. ROTOR AND POWER TRANSMISSION SYSTEMS AND POWERPLANT INSTALLATION
6.2 Design, construction and functioning
6.8 Arrangement and functioning
6.5 Compliance with engine and rotor and power transmission systems limitations
6.6 Control of engine rotation
7.4 Navigation lights and anti-collision lights
CHAPTER 7. INSTRUMENTS AND EQUIPMENT
7.1 Required instruments and equipment
7.3 Safety and survival equipment
CHAPTER 8. ELECTRICAL SYSTEMS
9.2 Operating limitations
CHAPTER 9. OPERATING LIMITATIONS AND INFORMATION
9.3 Operating information and procedures
9.4 Performance information
9.5 Helicopter flight manual
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
3.2 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 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
7.4 Performance information
7.6 Markings and placards
7.7 Continuing airworthiness — maintenance information
CHAPTER 8. CRASHWORTHINESS AND CABIN SAFETY
8.2 Design emergency landing loads
8.3 Cabin fire protection
CHAPTER 9. OPERATING ENVIRONMENT AND HUMAN FACTORS
9.4 Operating environmental factors
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
1.2 Operating limitations
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
6.3 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
7.4 Performance information
7.6 Markings and placards
7.7 Continuing airworthiness — maintenance information
CHAPTER 8. CRASHWORTHINESS AND CABIN SAFETY
8.2 Design emergency landing loads
8.3 Cabin fire protection
CHAPTER 9. OPERATING ENVIRONMENT AND HUMAN FACTORS
9.4 Operating environmental factors
PART VB. AEROPLANES NOT EXCEEDING 5 700 KG FOR WHICH APPLICATION FOR CERTIFICATION IS SUBMITTED ON OR AFTER 7 MARCH 2021
1.2 Operating limitations
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
6.3 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
7.4 Performance information
CHAPTER 8. CRASHWORTHINESS AND CABIN SAFETY
8.2 Design emergency landing loads
8.3 Cabin fire protection
CHAPTER 9. OPERATING ENVIRONMENT AND HUMAN FACTORS
9.4 Operating environmental factors
1.2 Engine installation and interfaces
1.3 Declared ratings, conditions and limitations
1.4 Continuing airworthiness – maintenance information
CHAPTER 2. DESIGN AND CONSTRUCTION
2.3 Materials and manufacturing methods
1.2 Declared ratings, conditions and limitations
1.3 Continuing airworthiness — maintenance information
CHAPTER 2. DESIGN AND CONSTRUCTION
2.3 Materials and manufacturing methods
2.4 Pitch control and indication
CHAPTER 3. TESTS AND INSPECTIONS
3.2 Operational and endurance tests
APPENDIX. APPROVED MAINTENANCE ORGANIZATION (AMO) CERTIFICATE. Applicable as of 5 November 2020.