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Latécoère 23

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wood apart from four duralumin longerons. They were set at an appropriate angle of incidence to provide extra lift. There was a mooring position in the nose, an open cockpit for pilot and mechanic. Two internal cabins, one ahead of the cockpit and one aft could each accommodate four passengers. The tail unit of the Latécoère 23 was much cleaner than that of its predecessor, with control surfaces merging smoothly into the lines of tailplane and fin. The former was unbraced and mounted about halfway up the fin, with a large cut-out for rudder movement.
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thickness. The Latécoère 23 carried full span ailerons in three sections per wing, fitted with trim tabs. The wings were not attached directly to the fuselage, but to the sponsons: on each side a parallel pair of streamlined struts leaned outwards from near the tip of the sponson to mid-wing, and a second pair ran inwards to the wing centreline below the engines. On the Latécoère 21 the engines were mounted on the chord line, but the two 500 hp (373 kW)
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The fuselage of the Latécoère 23 was 1.30 m (2 ft) shorter than that of its predecessor and the major hydrodynamic alteration was the inclusion of two steps rather than one. It was built of wood. The broad sponsons of airfoil section and almost rectangular plan were also mostly made of
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for stability on the water. Its wing, like that of the earlier aircraft was very rectangular and of mixed wood and metal construction. The span was increased by 27% and the wing area by about the same. The sharply cropped wingtips of the Latécoère 21 were replaced by bevelled ends of decreasing
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Achille Enderlin, Latécoère's test pilot was in charge of trials during the autumn of 1927. These passed without incident, but on 31 December 1927, with Enderlin and four others on board spun in during landing approach, killing everyone. No more Latécoère 23s were built, but by the time of the
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The Latécoère 23 was a development of the Latécoère 21, the latter Latécoère's first flying boat to leave the water. It kept the same general arrangement, a parasol winged machine with a centrally mounted push-pull pair of engines and
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of the later aircraft were mounted on the upper surface of the wing. Propellers were four bladed and wooden.
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aircraft. Only one was built, flying and crashing in late 1927. The similar
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water-cooled W-12 piston engine , 373 kW (500 hp) each
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crash the first examples of its rather similar successor, the
1093: 647: 391: 65:(La societe industrielle d'aviation Latécoère) 368: 8: 375: 361: 353: 266:187 km/h (116 mph, 101 kn) 295: 313: 311: 309: 307: 305: 303: 301: 299: 15: 7: 317: 217:28.00 m (91 ft 10 in) 211:16.60 m (54 ft 6 in) 336:Latécoère Les avions et hydravions 229:123 m (1,324 sq ft) 223:4.80 m (15 ft 9 in) 14: 184:Performance figures are estimates 24: 1162:Twin-engined push-pull aircraft 278:1.35 m/s (266 ft/min) 241:7,503 kg (16,541 lb) 235:5,006 kg (11,036 lb) 1: 338:. Paris: Editions Larivière. 272:3,500 m (11,500 ft) 141:was its immediate successor. 1172:Aircraft first flown in 1927 1147:1920s French civil aircraft 1188: 126:was a development of the 23: 18: 190:General characteristics 145:Design and development 1167:Parasol-wing aircraft 334:Cuny, Jean (1992). 1157:Latécoère aircraft 171:were in service. 1134: 1133: 133:, a twin-engined 120: 119: 73:Marcel Moine and 1179: 377: 370: 363: 354: 349: 321: 320:, pp. 101–2 315: 270:Service ceiling: 259: 192: 182:Cuny 1992 p.101 101: 91: 49: 41:Type of aircraft 28: 16: 1187: 1186: 1182: 1181: 1180: 1178: 1177: 1176: 1137: 1136: 1135: 1130: 1089: 643: 387: 381: 346: 333: 325: 324: 316: 297: 287: 255: 188: 177: 147: 99: 89: 48:National origin 47: 42: 12: 11: 5: 1185: 1183: 1175: 1174: 1169: 1164: 1159: 1154: 1149: 1139: 1138: 1132: 1131: 1129: 1128: 1123: 1118: 1113: 1108: 1103: 1097: 1095: 1091: 1090: 1088: 1087: 1082: 1077: 1072: 1067: 1062: 1057: 1052: 1047: 1042: 1037: 1032: 1027: 1022: 1017: 1012: 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195: 194: 193: 191: 186: 185: 181: 175:Specification 174: 172: 170: 164: 160: 158: 157:Farman 12 Wes 153: 144: 142: 140: 136: 132: 129: 125: 116: 113: 110: 109: 106: 103: 98: 97: 93: 88: 87: 83: 81:First flight 80: 79: 76: 75:P.G.Latécoère 72: 69: 68: 64: 61: 59:Manufacturer 58: 57: 54: 51: 46: 45: 38: 35: 32: 31: 27: 22: 19:Latécoère 23 17: 1152:Flying boats 473: 335: 328:Bibliography 281: 275: 269: 263: 256: 254: 244: 238: 232: 226: 220: 214: 208: 205:8 passengers 202: 196: 189: 187: 183: 179: 178: 169:Latécoère 32 165: 161: 148: 139:Latécoère 32 128:Latécoère 21 124:Latécoère 23 123: 121: 115:Latécoère 32 105:Latécoère 21 90:Number built 257:Performance 249:Farman 12We 245:Powerplant: 131:flying boat 37:Flying boat 1141:Categories 285:References 227:Wing area: 84:late 1927 384:Latécoère 318:Cuny 1992 290:Citations 215:Wingspan: 203:Capacity: 180:Data from 111:Variants 70:Designer 63:Latécoère 39:transport 1094:Missiles 648:Projects 392:Aircraft 386:aircraft 152:sponsons 221:Height: 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Index


Flying boat
France
Latécoère
P.G.Latécoère
Latécoère 21
Latécoère 32
Latécoère 21
flying boat
parasol winged
Latécoère 32
sponsons
Farman 12 Wes
Latécoère 32
Farman 12We








Cuny 1992
ISBN
2-84890-067-9
v
t
e
Latécoère

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