| Preface |
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xi | |
| Introduction |
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xiii | |
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Chapter 1 Aircraft Design |
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1 | (16) |
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Military Standard---(Mil-Std-1530C) Aircraft Structural Integrity Program |
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2 | (2) |
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Military Standard---(Mil-Std-882E) Standard Practice for System Safety |
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4 | (1) |
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Military Standard---(Mil-Std-8861B) Airplane Strength and Rigidity Flight Loads |
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4 | (2) |
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Military Standard---(MIL-A-8870C) Airplane Strength and Rigidity, Vibration, Flutter, and Divergence |
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6 | (8) |
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14 | (1) |
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15 | (2) |
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Chapter 2 Aircraft Material |
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17 | (12) |
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17 | (3) |
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Materials Used in Aircraft Construction |
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20 | (3) |
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Nonmetallic Aircraft Materials |
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23 | (2) |
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Materials of Aircraft Hardware |
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25 | (2) |
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Materials---Aircraft Lubricants |
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27 | (1) |
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27 | (1) |
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28 | (1) |
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Chapter 3 Loads on the Aircraft |
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29 | (22) |
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29 | (4) |
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33 | (2) |
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Moment, Moment Arm, and Torque |
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35 | (1) |
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The Vector and Vector Components |
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36 | (1) |
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Lift Pressure and Wing Loading |
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37 | (1) |
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Centripetal and Centrifugal Forces |
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38 | (1) |
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39 | (2) |
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41 | (2) |
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Fuel Tank Loads during Emergency Landing |
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43 | (1) |
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44 | (2) |
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46 | (2) |
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48 | (1) |
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49 | (2) |
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Chapter 4 Stress Analysis |
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51 | (16) |
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Strain and Stress-Strain Relations |
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51 | (3) |
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54 | (1) |
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55 | (3) |
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Fatigue-Stress Concentration |
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58 | (2) |
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Behavior of Materials under Stress |
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60 | (1) |
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Factors Affecting Elastic Properties |
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61 | (1) |
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62 | (1) |
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Elasticity; Proportionality of Stress and Strain |
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62 | (2) |
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64 | (1) |
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65 | (1) |
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66 | (1) |
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Chapter 5 Torsion, Compression, and Bending Loads |
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67 | (12) |
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67 | (1) |
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68 | (1) |
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69 | (1) |
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70 | (1) |
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Compressive Strength and Failures |
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71 | (2) |
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73 | (1) |
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Elastic Stability---General Condition |
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74 | (1) |
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75 | (2) |
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Nonuniform Loading of Circular Plates |
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77 | (1) |
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Flat-Plate Ultimate Strength |
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77 | (1) |
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77 | (1) |
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78 | (1) |
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Chapter 6 Aircraft Structure Riveted Joints and Pressure Vessels |
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79 | (14) |
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79 | (1) |
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80 | (1) |
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Modes of Failure in Riveted Joints |
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80 | (2) |
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82 | (1) |
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Eccentric Loading of Riveted Joints |
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83 | (1) |
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Stress Analysis of Riveted Joints |
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83 | (1) |
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Riveted Joints---Common Terms |
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84 | (1) |
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Pressure Vessels and Pressure Lines |
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84 | (1) |
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85 | (1) |
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86 | (3) |
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Difference between Pneumatic and Hydraulic Systems |
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89 | (2) |
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91 | (1) |
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91 | (2) |
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Chapter 7 Heat Treatment of Aircraft Metals |
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93 | (22) |
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93 | (1) |
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94 | (1) |
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95 | (4) |
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Time, Temperature, and Transformation |
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99 | (1) |
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Continuous Cooling Transformation |
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100 | (1) |
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Difference between TTT and CCT |
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101 | (1) |
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102 | (1) |
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Aluminum and Aluminum Alloys |
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102 | (1) |
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103 | (2) |
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Magnesium and Magnesium Alloys |
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105 | (1) |
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Titanium and Titanium Alloys |
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105 | (2) |
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107 | (1) |
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108 | (1) |
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Substitution of Aircraft Metals |
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108 | (1) |
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Cold-Working and Hardening |
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109 | (1) |
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110 | (1) |
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111 | (2) |
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113 | (1) |
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113 | (2) |
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Chapter 8 Aircraft Fatigue and Aircraft Material Fatigue |
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115 | (12) |
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115 | (1) |
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Fatigue Testing (S-N Curve) |
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116 | (1) |
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117 | (1) |
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Military Standard---(Mil-A-83444) Airplane Damage Tolerance Requirements |
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118 | (2) |
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Stress-Corrosion Cracking |
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120 | (1) |
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Control of Stress-Corrosion Cracking |
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121 | (1) |
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122 | (2) |
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124 | (1) |
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125 | (2) |
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Chapter 9 Aircraft Corrosion |
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127 | (20) |
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127 | (1) |
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128 | (2) |
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130 | (3) |
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133 | (1) |
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134 | (1) |
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134 | (2) |
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136 | (1) |
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Corrosion of Ferrous Metals |
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137 | (1) |
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Factors Affecting Corrosion |
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138 | (1) |
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Corrosion-Prone Areas in Aircraft |
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139 | (2) |
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Factors in Corrosion Control |
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141 | (1) |
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Corrosion Inspection and Detection |
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142 | (1) |
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Preventive Maintenance of Corrosion |
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143 | (1) |
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144 | (1) |
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145 | (2) |
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Chapter 10 Dynamic Stress, Temperature Stress, and Experimental Methods |
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147 | (8) |
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147 | (2) |
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Remarks on Stress due to Impact |
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149 | (1) |
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149 | (1) |
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150 | (2) |
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Stress Pattern Analysis by Thermal Emission |
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152 | (1) |
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153 | (1) |
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153 | (2) |
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155 | (18) |
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Applications of Composites on Aircraft |
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155 | (1) |
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Fiber-Reinforced Materials |
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156 | (2) |
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Laminar or Laminated Composites |
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158 | (1) |
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Particulate-Reinforced Composites |
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159 | (1) |
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Mechanics of Composite Material |
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160 | (1) |
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Stress and Strain in a Laminate |
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160 | (1) |
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Composite Fatigue and Damage Tolerance |
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161 | (1) |
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Aircraft Accident--Crashworthiness |
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162 | (3) |
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165 | (1) |
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Composite Manufacturing and In-Service Defects and Damages |
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165 | (3) |
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Composite Maintenance and Inspection |
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168 | (1) |
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169 | (1) |
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169 | (1) |
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170 | (3) |
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Chapter 12 Nondestructive Testing and Nondestructive Inspection |
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173 | (26) |
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175 | (1) |
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175 | (2) |
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Liquid Penetrant (Dye Penetrant) Inspection |
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177 | (2) |
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Magnetic Particle Inspection |
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179 | (5) |
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Radiographic Inspection (X-Rays and Gamma Rays) |
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184 | (4) |
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188 | (3) |
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191 | (6) |
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197 | (1) |
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198 | (1) |
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Chapter 13 Aviation Maintenance Management |
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199 | (22) |
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199 | (6) |
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Typical Airline Definition of Maintenance |
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205 | (1) |
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Goals of a Maintenance Program |
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205 | (1) |
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Functional and Potential Failure |
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205 | (1) |
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Documentation for Maintenance |
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206 | (2) |
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Requirements for a Maintenance Program |
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208 | (3) |
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Material Support---Stores and Logistics |
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211 | (2) |
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Material Department---Budgeting Efforts |
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213 | (1) |
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214 | (1) |
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214 | (1) |
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215 | (1) |
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215 | (3) |
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218 | (1) |
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219 | (1) |
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219 | (2) |
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Chapter 14 Case Studies and Human Factors |
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221 | (32) |
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Case Study 14-1 TWA Flight 843 |
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221 | (5) |
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Case Study 14-2 Atlantic Southeast Airlines Flight 2311 |
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226 | (6) |
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Case Study 14-3 United Airlines Flight 232 |
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232 | (9) |
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Case Study 14-4 American Airlines Flight 191 |
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241 | (5) |
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Case Study 14-5 USAir Flight 427 |
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246 | (2) |
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248 | (1) |
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Human Factors in Aircraft Maintenance |
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248 | (2) |
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Maintenance Error Decision Aid |
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250 | (1) |
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251 | (1) |
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252 | (1) |
Answers to
Chapter Questions |
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253 | (8) |
| Index |
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261 | |
