The flight controls (ATA group 27) is concerned with the system between the pilot and the control surfaces. The control surfaces themselves fall under the ATA code section of the major sub assembly to which they attach.
FAA-H-8083-30, 2008) AA-SB-001: Analysis And Design Of Composite And Metallic Flight Vehicle Structures
Third Edition
- Table of Contents
- Revision History and Copyright Notice
- 1. SCOPE
- 2. REFERENCES
- 3. INTRODUCTION
- 4. MATERIALS
- 4.1. Composite Materials
- 4.1.1 Introduction
- 4.1.2. Basic Composite Material Primer
- 4.1.3. Fundamental Behavior of Carbon Fiber Epoxy Resin Composite Laminates
- 4.1.4. Environmental Conditions Considered
- 4.1.5. Manufacturing Effects Considered
- 4.1.6. Strength of Laminates
- 4.1.7. General Composite Laminate Analysis Approach
- 4.1.8. General Laminate Design Guidelines
- 4.2. Metallic Materials
- 4.3. Other Common Aircraft Materials
- 4.4. Corrosion
- 5. LOADS
- 6. SECTION PROPERTIES
- 7. STIFFNESS
- 8. BEAM ANALYSIS
- 9. TORSION
- 10. PLATE STRENGTH ANALYSIS
- 11. PRESSURE VESSELS
- 12. JOINTS
- 12.1. Adhesive Joints
- 12.2. Mechanically Fastened Joints
- 12.2.1. Introduction
- 12.2.2. Mechanical Joint Strength
- 12.2.3. Mechanical Joints in Metal Panels
- 12.2.4. Mechanical Joints in Composite Panels
- 12.2.5. Mechanical Joints, Examination of the Fastener
- 12.2.6. Potted Inserts in Cored Laminates
- 12.2.7. Fastener Interaction of Shear Load and Tension Load Effects
- 12.2.8. Mechanical Joints – Tension Clip Installations
- 12.2.9. Mechanical Joints – Lugs
- 12.2.10. Mechanical Joints – Lugs – Additional checks
- 12.2.11. Other Mechanical Connections
- 12.3. General Treatment of Contact Stresses
- 12.4. Strength of Brazed Joints
- 12.5. Strength of Welded Joints
- 13. COMBINED STRESSES
- 14. ULTIMATE STRENGTH OF METALLIC ELEMENTS
- 15. LOCAL STABILITY – ISOTROPIC MATERIALS
- 15.1. Introduction
- 15.2. General Buckling Expression
- 15.2.1. Introduction
- 15.2.2. Buckle Wavelength
- 15.2.3. Web Shear Buckling (Rectangular)
- 15.2.4. Panel Compression Buckling (Rectangular)
- 15.2.5. Interaction of Shear and Compression Buckling (Rectangular)
- 15.2.6. Flange Compression Buckling
- 15.2.7. Bending Buckling
- 15.2.8. Buckling of Triangular Panels
- 15.2.9. Reduction Factors Due to Cladding
- 15.2.10. Panel and Flange Buckling Summary
- 15.2.11. Inter-Rivet Buckling
- 15.3. Column Buckling
- 15.4. Buckling – Specific Cases
- 15.5. Crippling
- 16. LOCAL STABILITY – COMPOSITE MATERIALS
- 17. RESERVED
- 18. RESERVED
- 19. FINITE ELEMENT MODELLING
- 20. NOMENCLATURE
- 21. NUMERICAL METHODS
- 22. AIRCRAFT SPECIFIC DESIGN FEATURES AND DESIGN METHODS
- 22.1. Introduction
- 22.2. 06 Dimensions and Areas
- 22.3. 07 Lifting and Shoring
- 22.4. 08 Levelling and Weighing
- 22.5. 09 Towing and Taxiing
- 22.6. 25 Equipment and Furnishings (Interiors)
- 22.7. 27 Flight Controls
- 22.8. 28 Fuel
- 22.9. 29 Hydraulic Power
- 22.10. 32 Landing Gear
- 22.11. 52 Doors
- 22.12. 53 Fuselage
- 22.13. 54 Nacelles & Pylons
- 22.14. 55 Empennage/Stabilizers
- 22.15. 56 Windows
- 22.16. 57 Wings
- 22.17. 71 Powerplant
- 23. FIXED WING AIRCRAFT PERFORMANCE
- 24. OTHER AIRCRAFT TYPES: DESIGN AND ANALYSIS
- 25. CERTIFICATION
- 26. MICROSOFT EXCEL AS A REPORT WRITING TOOL
- 27. COMMON AIRCRAFT HARDWARE
22.7. 27 Flight Controls
FAA-H-8083-30, 2008) 22.7. 27 Flight Controls
The flight controls (ATA group 27) is concerned with the system between the pilot and the control surfaces. The control surfaces themselves fall under the ATA code section of the major sub assembly to which they attach.
FAA-H-8083-30, 2008)