Content Inside:
This document published by Light Aircraft Manufacturers Association of Canada, by reading this document you’ll find information about design standards for advanced ultra-light aeroplanes. Its divided into 7 chapters as follow: Chapter A - General 1, 1. Applicability 1, 2. Advanced Ultra-Light Aeroplane Category 1, 3. Minimum Useful Load 1, 4. Maximum Empty Mass (Weight) 1. Chapter B - Flight 2, 5. Proof of Compliance 2 6. Load Distribution Limits 2,,7. Propeller Speed and Pitch Limits 2, 8. Performance, General 2, 9. Stalling Speeds 2, 10. Take-off 2, 11. Climb: All engines Operating 3, 12. Landing 3, 13. Balked Landing 3, 14. Controllability and Manoeuvrability 3, 15. Longitudinal Control 4 16. Directional and Lateral Control 4, 17. Static Longitudinal Stability 4, 18. Static Directional and Lateral Stability 4, 19. Dynamic Stability 4, 20. Wings Level Stall 4, 21. Turning Flight and Accelerated Stalls 4, 22. Directional Stability and Control 5. Chapter C - Structure 6 - Loads, Factor of Safety, Strength and Deformation, Proof of Structure, Control System and Supporting Structure, Ground Load Conditions, Braked Roll Conditions, Supplementary Conditions for Tail Wheel. Supplementary Conditions for Nose Wheel, Water Load Conditions, Emergency Landing Conditions. Chapter D - Design and Construction: Materials and Workmanship, Fabrication Methods, Self-Locking Nuts, Protection of Structure, Proof of Strength - Wings, Control System - Operation Test. Chapter E - Powerplant: Installation, Engines, Fuel Tank Tests, Fuel Tank Vents, Fuel Strainer or Filter, Induction System Icing Protection. Chapter F - Equipment: Flight and Navigation Instruments, Powerplant Instruments, Miscellaneous Equipment, Safety Belts and Harnesses. Chapter G - Operating Limitations and Information: Weight and Centre of Gravity, Powerplant Limitations, Instructions for Continued Airworthiness, Aeroplane Manual, Operating Limitations, Operating Procedures.
Tags : self locking nuts, powerplant installation, propeller speed, powerplant instruments, light aeroplanes, tank tests, induction system, tank vents, nose wheel, centre of gravity, longitudinal control, safety belts, empty mass, water load, supplementary conditions
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