Browse all sections of Small Category VCA (Revision 0) SC-VTOL (Oct 2024)

• VTOL.2410 (reserved)
• EASA eRules
• MOC VTOL.2610 Instrument markings, control markings and placards
• VTOL.2620 Aircraft Flight Manual
• MOC VTOL.2310(b) Emergency Flotation
• MOC VTOL.2210 Structural Design Loads
• VTOL.2240 Structural Durability
• MOC VTOL.2325(a)(4) Fire Protection - Energy storage crash resistance
• MOC VTOL.2430(a)(6) Energy retention capability in an emergency landing
• VTOL.2550 (reserved)
• VTOL.2010 Accepted means of compliance
• VTOL.2515 Electrical and electronic system lightning protection
• MOC VTOL.2620 Electronic Aircraft Flight Manual
• VTOL.2315 Means of egress and emergency exits
• STRUCTURAL PERFORMANCE
• MOC VTOL.2435(f) Prevention of likely foreign object damage to the lift/thrust unit
• MOC VTOL.2425(b) Shutdown and Restart of a Lift/Thrust Unit in Flight
• VTOL.2005 Certification of small-category VTOL-capable aircraft
• MOC 2 VTOL.2500(b) Electromagnetic compatibility
• VTOL.2120 Climb requirements
• VTOL.2210 Structural design loads
• SUBPART F — SYSTEMS AND EQUIPMENT
• MOC VTOL.2520 High-intensity radiated fields (HIRF) protection
• MOC VTOL.2115 Take-off performance
• MOC VTOL.2250(c) No catastrophic effect from structural single failures in the Category Enhanced
• MOC VTOL.2440 Propulsion Batteries Thermal Runaway for VTOL category enhanced
• MOC VTOL.2600 Flight crew compartment
• VTOL.2140 Control forces
• VTOL.2340 Design and construction information
• MOC VTOL.2135 Minimum Acceptable Handling Qualities Rating
• MOC 3 VTOL.2500(b) Airworthiness Security in the Category Enhanced
• VTOL.2245 Aeroelasticity
• VTOL.2525 System power generation, energy storage, and distribution
• MOC VTOL.2430(a)(3) and (a)(4) Accessible energy in electrical energy storage systems
• VTOL.2320 Occupant physical environment
• MOC VTOL.2250(f) Aircraft capability after bird impact
• MOC VTOL.2555 Installation of recorders
• VTOL.2440 Lift/thrust system installation fire protection
• VTOL.2225 Component loading conditions
• MOC VTOL.2515 Electrical and electronic system lightning protection
• MOC VTOL.2400(b) Accepted Specifications for Electric/Hybrid Lift/Thrust Units
• MOC VTOL.2325(b)(1) and (b)(2) Fire Protection: fire extinguishers and design of interiors
• SUBPART G — FLIGHT CREW INTERFACE AND OTHER INFORMATION
• MOC VTOL.2240 (e) In-Service Monitoring
• MOC VTOL.2320(a)(2) Occupant physical environment
• MOC VTOL.2245 Aeroelasticity
• MOC VTOL.2205 Interaction of systems and structures
• MOC VTOL.2310(c) Ditching
• MOC VTOL.2430(a)(2) Protection of the fuel system against lightning
• SUBPART D — DESIGN AND CONSTRUCTION
• VTOL.2115 Take-off performance
• VTOL.2165 Flight in icing conditions
• Documents Incorporated in Revision 0
• SUBPART B — FLIGHT
• VTOL.2135 Controllability
• MOC VTOL.2005 Certification of small-category VTOL aircraft
• SUBPART C — STRUCTURES
• VTOL.2230 Limit and ultimate loads
• MOC 1 VTOL.2500(b) Intended function of systems and equipment
• VTOL.2425 Lift/thrust system operational characteristics
• VTOL.2420 (reserved)
• MOC VTOL.2270(e) Cargo and baggage compartments
• MOC VTOL.2320(a)(1) Clear communication between flight crew and passengers
• MOC VTOL.2605 Installation and operation information
• MOC VTOL.2510(a) Aircraft Parachute Rescue System
• VTOL.2150 Stall characteristics and stall warning
• VTOL.2260 Materials and processes
• VTOL.2160 Vibration
• SUBPART A — GENERAL
• VTOL.2510 Equipment, systems, and installations
• VTOL.2170 Operating Limitations
• VTOL.2000
• VTOL.2255 Protection of structure
• MOC 4 VTOL.2300 Common Mode Failures and Errors in Fly-by Wire Flight Control Functions
• STRUCTURAL OCCUPANT PROTECTION
• MOC VTOL.2300(a)(3) Control margin awareness
• MOC VTOL.2240(d) High Energy Fragments - Particular Risk Analysis
• VTOL.2400 Lift/thrust system installation
• Note from the editor
• VTOL.2215 Flight load conditions
• MOC VTOL.2300(a)(2) Protection against likely Hazards for Fly-by-Wire flight control systems
• MOC VTOL.2330 Fire Protection in designated fire zones
• VTOL.2300 Flight control systems
• VTOL.2335 Lightning Protection
• List of Revisions
• VTOL.2270 Emergency conditions
• MOC VTOL.2010 Accepted Means of compliance
• VTOL.2330 Fire Protection in designated fire zones
• MOC VTOL.2435(g) Flight crew awareness of the lift/thrust unit configuration
• MOC VTOL.2625 Instructions for Continued Airworthiness
• MOC VTOL.2105 Performance Data
• VTOL.2505 General requirements on equipment installation
• STRUCTURAL LOADS
• MOC 3 VTOL.2300 Validation of Electronic Flight Control Laws (FCL) in Fly-by-Wire flight control systems
• VTOL.2615 Flight, navigation, and lift/thrust system instruments
• MOC VTOL.2000 Applicability and definitions
• VTOL.2500 General requirements on systems and equipment function
• MOC VTOL.2240 (a) and (b) Structural durability
• MOC VTOL.2265 Special factors of safety
• VTOL.2610 Instrument markings, control markings and placards
• VTOL.2555 Installation of flight recorders
• VTOL.2265 Special factors of safety
• MOC 1 VTOL.2300 Fly-by-Wire control systems: Definition and Scope
• MOC VTOL.2270(a) and (c) Emergency landing conditions: General considerations
• VTOL.2205 Interaction of systems and structures
• VTOL.2250 Design and construction principles
• Preamble
• VTOL.2200 Structural design envelope
• VTOL.2530 External and cockpit lighting
• VTOL.2540 (reserved)
• VTOL.2435 Lift/thrust installation support systems
• MOC VTOL.2250(e) Doors, canopies and exits
• MOC VTOL.2335 Lightning Protection
• SUBPART E — LIFT/THRUST SYSTEM INSTALLATION
• VTOL.2535 Safety equipment
• MOC VTOL.2215 Flight load conditions
• FIRE AND HIGH ENERGY PROTECTION
• Disclaimer
• MOC 4 VTOL.2500(b) Certification credit for simulation and rig tests
• MOC VTOL.2510 Equipment, systems, and installations
• MOC VTOL.2255 Protection of structure
• VTOL.2325 Fire Protection
• Revised Paragraphs
• MOC VTOL.2320(a)(3) Occupant protection from breakage of windshields, windows, and canopies
• VTOL.2110 Flight Envelopes
• VTOL.2100 Mass and centre of gravity
• MOC VTOL.2305 Landing Gear Systems
• MOC VTOL.2270(c) Emergency Landing Conditions
• FLIGHT INFORMATION
• VTOL.2445 Lift/thrust system installation information
• VTOL.2520 High-intensity radiated fields (HIRF) protection
• VTOL.2625 Instructions for Continued Airworthiness
• VTOL.2600 Flight crew compartment
• MOC VTOL.2120 Climb requirements
• MOC VTOL.2270(b)(1) Emergency landing dynamic conditions
• VTOL.2220 Ground and water load conditions
• VTOL.2430 Lift/thrust system installation, energy storage and distribution systems
• VTOL.2125 Climb information
• MOC VTOL.2535 Safety Equipment
• MOC 5 VTOL.2300 Hidden Failures in Fly-by-Wire flight control systems
• VTOL.2305 Landing gear systems
• VTOL.2517 Electrical wiring interconnection system (EWIS)
• MOC 2 VTOL.2300 Acceptability of ASTM standard F3232/F3232M-20 for Fly-by-Wire flight control systems
• VTOL.2545 Pressurised systems elements
• MOC VTOL.2230 Limit and ultimate loads
• VTOL.2105 Performance data
• VTOL.2155 (reserved)
• OCCUPANT SYSTEM DESIGN PROTECTION
• MOC VTOL.2235 Structural strength
• MOC VTOL.2300(a)(1) Function and operation of Fly-by-Wire flight control system
• MOC VTOL.2220 Ground and water load conditions
• MOC VTOL.2225 Component Loading Conditions
• MOC VTOL.2315(a) Means of egress and emergency exits
• MOC VTOL.2200 Structural design envelope
• VTOL.2415 Lift/thrust system installation ice protection
• VTOL.2145 Flying qualities
• MOC VTOL.2260 Materials and processes
• MOC VTOL.2530 External and Cockpit Lighting
• VTOL.2130 Landing
• MOC VTOL.2130 Landing
• VTOL.2405 (reserved)
• VTOL.2235 Structural strength
• VTOL.2310 Flotation
• VTOL.2605 Installation and operation information
• MOC VTOL.2400(c)(3) Lift/thrust system installation - likely hazards in operation