ED Decision 2017/013/R
(a) The aeroplane is designed to minimise the risk of fire initiation due to:
(1) anticipated heat or energy dissipation or system failures or overheat that are expected to generate heat sufficient to ignite a fire;
(2) ignition of flammable fluids, gases or vapours; and
(3) fire-propagating or -initiating system characteristics (e.g. oxygen systems).
(b) The aeroplane is designed to minimise the risk of fire propagation by:
(1) providing adequate fire or smoke awareness and extinguishing means when practical;
(2) application of self-extinguishing, flame-resistant, or fireproof materials that are adequate to the application, location and certification level; or
(3) specifying and designing designated fire zones that meet the specifications of CS 23.2330.
ED Decision 2019/020/R
ASTM F44 F3264-18b Standard Specification for Normal Category Aeroplanes Certification
7.6 Fire Protection:
F3061/F3061M-17 Standard Specification for Systems and Equipment in Small Aircraft
F3231/F3231M-17 Standard Specification for Electrical Systems in Small Aircraft
F3234/F3234M-17 Standard Specification for Exterior Lighting in Small Aircraft
F3066/F3066M-18 Standard Specification for Aircraft Powerplant Installation Hazard Mitigation
F3083/F3083M-16 Standard Specification for Emergency Conditions, Occupant Safety and Accommodations
Remarks
F3066 revised from -15 to -18
ED Decision 2017/025/R
CS-23 Amdt 4
23.1453 Protection of oxygen equipment from rupture
23.851 Fire extinguishers
23.853 Passenger and crew compartment interiors (With Appendix F)
23.855 Cargo and baggage compartment fire protection (With Appendix F)
23.859(a) Combustion heater fire protection
23.863 Flammable Fluid Fire Protection
23.1337(a) Powerplant instruments installation
23.1351 Electrical system: General
23.1359(a), (c) Electrical System fire protection
23.1383(d) Taxi and landing lights (With Appendix F)
23.1385(d) Position light system installation
ED Decision 2017/025/R
CS VLA Amdt 1
VLA.853 Passenger and crew compartment interiors (With Appendix F)
VLA.857 Electrical bonding
VLA.863 Flammable Fluid Fire Protection
VLA.1337 Powerplant instruments installation
VLA.1351 Electrical system: General
VLA.1384 External lights
CS 23.2330 Fire protection in designated fire zones
ED Decision 2017/013/R
(a) Flight controls, engine mounts, and other flight structures within or adjacent to designated fire zones must be capable of withstanding the effects of a fire.
(b) A fire in a designated fire zone must not preclude continued safe flight and landing.
(c) Terminals, equipment, and electrical cables used during emergency procedures must be fire-resistant.
AMC1 23.2330 Fire protection in designated fire zones
ED Decision 2019/020/R
ASTM F44 F3264-18b Standard Specification for Normal Category Aeroplanes Certification
7.7 Fire Protection in Designated Fire Zones and Adjacent Areas:
F3061/F3061M-17 Standard Specification for Systems and Equipment in Small Aircraft
F3231/F3231M-17 Standard Specification for Electrical Systems in Small Aircraft
F3114-15 Standard Specification for Structures
F3066/F3066M-18 Standard Specification for Aircraft Powerplant Installation Hazard Mitigation
F3083/F3083M-16 Standard Specification for Emergency Conditions, Occupant Safety and Accommodations
Remarks
F3066 revised from -15 to -18
Different from ASTM F3264-18b paragraph 7.7, ASTM F3083-16 has been added as means of complying with CS 23.2325.
AMC2 23.2330 Fire protection in designated fire zones
ED Decision 2017/025/R
CS-23 Amdt 4
23.865 Fire protection of flight controls, engine mounts, and other flight structure
23.1359(a), (b) Electrical System fire protection (With Appendix F)
23.1365(b) Electrical Cables and equipment
AMC3 23.2330 Fire protection in designated fire zones
ED Decision 2017/025/R
CS VLA Amdt 1
VLA.865 Fire protection of flight controls and other flight structure
VLA.1365 Electrical Cables and equipment
CS 23.2335 Lightning protection
ED Decision 2017/013/R
For operations where the exposure to lightning is likely, the aeroplane must be protected against catastrophic effects of lightning.
AMC1 23.2335 Lightning protection
ED Decision 2019/020/R
ASTM F44 F3264-18b Standard Specification for Normal Category Aeroplanes Certification
7.8 Lightning Protection:
F3061/F3061M-17 Standard Specification for Systems and Equipment in Small Aircraft
AMC2 23.2335 Lightning protection
ED Decision 2017/025/R
CS-23 Amdt 4
23.867 Electrical bonding and protection against lightning and static electricity
23.1365 Electrical Cables and equipment
AMC3 23.2335 Lightning protection
ED Decision 2017/025/R
CS VLA Amdt 1
VLA.857 Electrical bonding
VLA.1365 Electrical Cables and equipment
CS 23.2340 Design and construction information
ED Decision 2017/013/R
The following design and construction information is established:
(a) operating limitations, procedures and instructions necessary for the safe operation of the aeroplane;
(b) the need for instrument markings or placards;
(c) any additional information necessary for the safe operation of the aeroplane; and
(d) inspections or maintenance to assure continued safe operation.
AMC1 23.2340 Design and construction information
ED Decision 2019/020/R
ASTM F44 F3264-18b Standard Specification for Normal Category Aeroplanes Certification
None
Remarks
No AMC expected
AMC2 23.2340 Design and construction information
ED Decision 2017/025/R
CS-23 Amdt 4
23.1523 Minimum Flight Crew
23.1524 Maximum passenger seating configuration
23.1529 Instructions for continued airworthiness (With Appendix G)
23.1541 Markings and placards: General
AMC3 23.2340 Design and construction information
ED Decision 2017/025/R
CS VLA Amdt 1
VLA.1529 Instructions for continued airworthiness
VLA.1541 Markings and placards: General