Knowledge

Transport category

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most transport category airplanes do not have duplicated nosewheel assemblies; and some do not have duplicated wheels on each main undercarriage. A transport category helicopter is permitted to have only one main rotor head, and may have only one engine. If a transport category helicopter has only one engine it is only eligible to be a Class B (or Performance Group 2) helicopter. An example of a transport category helicopter with only one engine is the
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duplicated elements wherever failure of one element is likely to cause an accident. For example, transport category airplanes must have at least two engines and be flown by at least two pilots. The loads on the wings and tailplanes are usually carried by multiple load paths. If one element of the primary structure fails due to
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principle is not required in airplanes and helicopters that are not certificated in the transport category. If an element in a transport category airplane or helicopter is not highly critical, or if its failure is relatively benign, it is possible for that element not to be duplicated. For example,
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A principle behind transport category design standards is that any element in an airplane or helicopter can fail, but the risk of such a failure causing an accident should be acceptable under certain airworthiness requirements. Consequently, transport category airplanes and helicopters have
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is a category of airworthiness applicable to large civil airplanes and large civil helicopters. Any aircraft's airworthiness category is shown on its airworthiness certificate. The name "transport category" is used in the US, Canada, Europe and many other countries.
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Design requirements for the transport category do not specify upper or lower limits on the maximum takeoff weight or number of passenger seats but examples of these helicopters typically have maximum takeoff weights greater than 7,000 lb (3 175 kg).
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the remaining sound elements of the structure must carry the loads until the failed structural element is discovered in scheduled maintenance.
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has similar certification requirements, also titled Parts 25 and 29, for application to transport category airplanes and helicopters.
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Modern propeller-driven airplanes with more than 19 passenger seats or a MTOW greater than 19,000 lb (8618 kg); or
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Jets with 10 or more passenger seats or maximum takeoff weights greater than 12,500 lb (5700 kg); or
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Design requirements for the transport category do not specify upper or lower limits on the
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Older propeller-driven airplanes with MTOW greater than 12,500 lb (e.g.
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of transport category airplanes and helicopters respectively. In Europe the
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Easily recognisable examples of transport category helicopters are
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Easily recognizable examples of transport category airplanes are
113: 109: 23: 192: 61:Parts 25 and 29 are applied to the design and 24:Concept of transport category airworthiness 172:FAA design approval Transport Airplanes 193: 13: 14: 212: 186:FAA site - Aircraft certification 179: 201:Federal Aviation Administration 67:European Aviation Safety Agency 165: 131: 1: 159: 77: 59:Federal Aviation Regulations 52: 7: 146:Eurocopter AS332 Super Puma 10: 217: 122:de Havilland Canada Dash 8 126:Embraer EMB 120 Brasilia 84:maximum takeoff weight 72: 57:In the United States, 154:AgustaWestland AW139 150:MBB/Kawasaki BK 117 102:CASA C-212 Aviocar 17:Transport category 208: 174: 169: 216: 215: 211: 210: 209: 207: 206: 205: 191: 190: 182: 177: 170: 166: 162: 134: 80: 75: 55: 26: 12: 11: 5: 214: 204: 203: 189: 188: 181: 180:External links 178: 176: 175: 163: 161: 158: 133: 130: 106: 105: 94: 91: 79: 76: 74: 71: 54: 51: 25: 22: 9: 6: 4: 3: 2: 213: 202: 199: 198: 196: 187: 184: 183: 173: 168: 164: 157: 155: 151: 147: 143: 138: 129: 127: 123: 119: 115: 111: 103: 99: 95: 92: 89: 88: 87: 85: 70: 68: 64: 63:certification 60: 50: 48: 43: 38: 36: 32: 31:metal fatigue 21: 18: 167: 139: 135: 107: 81: 56: 47:Bell 204/205 41: 39: 27: 16: 15: 132:Helicopters 100:13,650 lb, 160:References 118:Learjet 35 116:aircraft, 104:17,000 lb) 98:Boeing 247 78:Airplanes 53:Standards 42:fail-safe 35:corrosion 195:Category 142:Bell 412 114:Airbus 110:Boeing 40:This 112:and 73:FAA 33:or 197:: 156:. 152:, 148:, 144:, 128:. 124:, 120:, 49:.

Index

metal fatigue
corrosion
Bell 204/205
Federal Aviation Regulations
certification
European Aviation Safety Agency
maximum takeoff weight
Boeing 247
CASA C-212 Aviocar
Boeing
Airbus
Learjet 35
de Havilland Canada Dash 8
Embraer EMB 120 Brasilia
Bell 412
Eurocopter AS332 Super Puma
MBB/Kawasaki BK 117
AgustaWestland AW139
FAA design approval Transport Airplanes
FAA site - Aircraft certification
Category
Federal Aviation Administration

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