Knowledge (XXG)

Latécoère 340

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mail. The sponsons, symmetric in cross section and with a thickness/chord ratio of 12.5%, were entirely metal. The fuselage was aluminium covered, tapering towards the tail with decreasing skin thickness. Like the wings, the rear surfaces were metal structures with fabric covering. The tailplane was mounted a little way up the fin, the latter carrying a generous and rounded rudder, its lower edge blending elegantly into the lines of the lower fuselage. The rudder had a trim tab, but neither it nor the elevators had aerodynamic balances.
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each motor. The primary attachment of the wings was not to the fuselage but to the sponson tips, by two pairs of parallel steel struts to mid-wing. On each side, another pair of struts went almost vertically from the sponson to the wing below the outer engine. The outer engines were further supported by struts to the upper fuselage longerons, from which also a pair of inverted V struts supported the central engine.
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The hull of the Latécoère 340 had a planing bottom with two steps. It was built around a keel and four longerons and provided a mooring position in the nose, an enclosed cabin for pilot and radio operator and a passenger cabin with four windows on each side. Aft of the cabin there was a space for
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engines were mounted close together on top of the wing and out of the spray in well-streamlined cowlings; those of the forward-facing outer engines slimmed finely to the trailing edge. Each engine drove a two-bladed propeller. Flat radiators were placed on the underside of the upper wing, beneath
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official. It broke up in the air, killing both Prévot and his mechanic Hoff. The accident was ascribed to pilot error, with the suggestion that in his enthusiasm to demonstrate the aircraft's potential, Prévot exceed the safe speed range. It was the end of the programme, and
149:, piloted by Prévot. During that month and the next, the aircraft's trials went promisingly. It seemed to have the calculated performance and could maintain height under full load on the power of two engines. However, on 2 April 1930 it was demonstrated to a 120:
The Latécoère 340 (sometimes written 34-0) was a three-engined flying boat designed to serve medium-range routes, such as those across the Mediterranean from France to her African colonies. In general appearance it was similar to the
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The quite thick (13.5%) wings were fabric covered over a metal frame. They were of constant chord out to gently curved tips, each carrying two ailerons. The three 400 hp (298 kW) V-12 water-cooled
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both for stability on the water and extra lift in the air. It was smaller than the Latécoère 21, carrying only five passengers.
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for middle-distance, overseas routes. The sole prototype was destroyed early in the testing programme, and no more were built.
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The Latécoère 340 flew for the first time in February 1930 at
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144 km/h (232 mph, 202 kn) at sea level
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Paris: Editions Larivière. 222:3,485 kg (7,683 lb) 1161:Aircraft first flown in 1930 147:Saint-Laurent-de-la-Salanque 1141:1930s French civil aircraft 1177: 29: 158:was the only one built. 177:General characteristics 38:Medium-range passenger 116:Design and development 1156:Parasol-wing aircraft 101:was a three-engined, 108:designed in 1929 in 322:Cuny, Jean (1992). 236:Hispano-Suiza 12 Jb 135:Hispano Suiza 12 Jb 1146:Latécoère aircraft 307:, pp. 108–111 88:Primary user 1123: 1122: 95: 94: 16:(Redirected from 1168: 366: 359: 352: 343: 337: 308: 302: 257:Service ceiling: 246: 179: 51: 43:Type of aircraft 27: 21: 1176: 1175: 1171: 1170: 1169: 1167: 1166: 1165: 1126: 1125: 1124: 1119: 1078: 632: 376: 370: 340: 334: 321: 312: 311: 303: 278: 268: 242: 175: 164: 118: 50:National origin 49: 44: 23: 22: 15: 12: 11: 5: 1174: 1172: 1164: 1163: 1158: 1153: 1148: 1143: 1138: 1128: 1127: 1121: 1120: 1118: 1117: 1112: 1107: 1102: 1097: 1092: 1086: 1084: 1080: 1079: 1077: 1076: 1071: 1066: 1061: 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83:February 1930 81: 77: 76: 73: 69: 68: 62: 58: 57: 52: 46: 45: 42: 36: 32: 31: 30:Latécoère 340 24: 14: 13: 10: 9: 6: 4: 3: 2: 1173: 1162: 1159: 1157: 1154: 1152: 1149: 1147: 1144: 1142: 1139: 1137: 1134: 1133: 1131: 1116: 1113: 1111: 1108: 1106: 1103: 1101: 1098: 1096: 1093: 1091: 1088: 1087: 1085: 1081: 1075: 1072: 1070: 1067: 1065: 1062: 1060: 1057: 1055: 1052: 1050: 1047: 1045: 1042: 1040: 1037: 1035: 1032: 1030: 1027: 1025: 1022: 1020: 1017: 1015: 1012: 1010: 1007: 1005: 1002: 1000: 997: 995: 992: 990: 987: 985: 982: 980: 977: 975: 972: 970: 967: 965: 962: 960: 957: 955: 952: 950: 947: 945: 942: 940: 937: 935: 932: 930: 927: 925: 922: 920: 917: 915: 912: 910: 907: 905: 902: 900: 897: 895: 892: 890: 887: 885: 882: 880: 877: 875: 872: 870: 867: 865: 862: 860: 857: 855: 852: 850: 847: 845: 842: 840: 837: 835: 832: 830: 827: 825: 822: 820: 817: 815: 812: 810: 807: 805: 802: 800: 797: 795: 792: 790: 787: 785: 782: 780: 777: 775: 772: 770: 767: 765: 762: 760: 757: 755: 752: 750: 747: 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weight: 224: 221: 220:Empty weight: 218: 215: 212: 209: 206: 203: 200: 197: 194: 191: 188: 185: 182: 181: 180: 178: 173: 171: 168: 161: 159: 157: 152: 148: 143: 139: 136: 130: 128: 124: 115: 113: 111: 107: 104: 100: 99:Latécoère 340 90: 87: 86: 82: 80:First flight 79: 78: 75:Marcel Moine 74: 71: 70: 66: 63: 61:Manufacturer 60: 59: 56: 53: 48: 47: 41: 37: 34: 33: 28: 19: 1136:Flying boats 542: 492: 323: 262: 256: 250: 243: 241: 231: 225: 219: 213: 207: 201: 195: 192:5 passengers 189: 183: 176: 174: 166: 165: 155: 144: 140: 131: 123:Latécoère 21 119: 98: 96: 18:Latécoère 34 244:Performance 232:Powerplant: 151:French Navy 106:flying boat 40:flying boat 1130:Categories 266:References 214:Wing area: 373:Latécoère 305:Cuny 1992 271:Citations 202:Wingspan: 190:Capacity: 170:Cuny 1992 167:Data from 72:Designer 65:Latécoère 1083:Missiles 637:Projects 381:Aircraft 375:aircraft 127:sponsons 208:Height: 196:Length: 330:  156:F-AKDI 110:France 55:France 184:Crew: 35:Role 498:35-0 493:34-0 328:ISBN 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Index

Latécoère 34
flying boat
France
Latécoère
parasol winged
flying boat
France
Latécoère 21
sponsons
Hispano Suiza 12 Jb
Saint-Laurent-de-la-Salanque
French Navy
Cuny 1992
Hispano-Suiza 12 Jb











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

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