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AM-69 Georges Payre

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light aircraft. The AM machine was to be a two-seat training aircraft and the design work occupied the students for some 3,000 hours. Its construction, undertaken by another group of ten students took 4,000 hours, with the AM-69 flying on 6 May 1973. It was named after one of their lecturers.
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The ENAM students began the design of an all-metal version, with larger tail surfaces and revised canopy and engine cowling, intending it to be homebuilt from plans but nothing seems to have come of this.
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with individual, starboard-hinged sections for access. Solo control was from the forward seat, over the wing. The conventional cantilever tail had swept, straight-edged vertical surfaces, with a
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for two years, after which the CoA lapsed and the aircraft was eventually removed from the Civil Register. The airframe was still in storage there in 1995.
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Design of the AM-69 began in 1969 as the name suggests, when a group of twelve students of the school started from the incomplete design of the
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that extended to the keel and horizontal surfaces mounted at mid-fuselage height forward of the rudder hinge. The control surfaces were
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ratio of 13.2%, notable for the large area of both upper and lower surfaces which were flat. There was
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borrowed heavily from other designs. The main legs and wheels, mounted onto the front wing
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Centre Recherche Application des Techniques d'Education Populaire et Sport
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engine in the nose of its rectangular section, round decked
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The Georges Payre was powered by a 67 kW (90 hp)
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over the whole wing and a full-span combination of inboard
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600 km (370 mi, 320 nmi) with maximum fuel
114:students in the early 1970s. It was intended as a 445:(2009 ed.). Brive: Ver Luisant. p. 151. 374:75 km/h (47 mph, 40 kn) flaps down 524: 443:Fox Papa - Registre des avions Français amateur 257: 242:After its first flight the AM-69 gained its 401:3.0 m/s (590 ft/min) at sea level 485:. London: Jane's Yearbooks. p. 460. 383:250 km/h (160 mph, 130 kn) 362:195 km/h (121 mph, 105 kn) 125: 476: 474: 472: 470: 468: 466: 464: 462: 246:(CoA) in July 1973 and was owned by the 160:234 section with a maximum thickness-to- 483:Jane's All the World's Aircraft 1976-77 368:160 km/h (99 mph, 86 kn) 265:Jane's All the World's Aircraft 1976/77 525: 480: 237: 499: 459: 436: 434: 432: 395:3,500 m (11,500 ft) service 142:The prototype AM-69 was an all-wood, 411:Landing distance from 15 m (50 ft): 297:11.20 m (120.6 sq ft) 149:monoplane. Its wings, skinned with 533:1970s French civil trainer aircraft 440: 344:2-bladed Ratier, ground adjustable 285:7.90 m (25 ft 11 in) 13: 429: 405:Take-off distance to 15 m (50 ft): 291:8.94 m (29 ft 4 in) 14: 559: 226:and the tailwheel was a modified 324:84 L (18.5 Imp gal; 22.2 US gal) 106:, was a conventionally laid out 538:Single-engined tractor aircraft 1: 515:. 1 August 1974. p. 117. 422: 548:Aircraft first flown in 1973 244:certificate of airworthiness 7: 318:728 kg (1,605 lb) 312:524 kg (1,155 lb) 10: 564: 258:Specifications (prototype) 216:conventional undercarriage 481:Taylor, John W R (1976). 338:, 67 kW (90 hp) 47:Arts et MĂ©tiers ParisTech 18: 100:Arts & MĂ©tiers AM-69 270:General characteristics 203:and there was a large 126:Design and development 110:designed and built by 306:Mureaux 234 modified 98:, also known as the 19:AM-69 Georges Payre 316:Max takeoff weight: 238:Operational history 214:The AM-69's fixed, 96:AM-69 Georges Payre 441:Chillon, Jacques. 379:Never exceed speed 252:Montceau-les-Mines 108:low wing monoplane 543:Low-wing aircraft 507:"Travail en bois" 452:978-2-355-51066-3 118:, seating two in 92: 91: 555: 517: 516: 503: 497: 496: 478: 457: 456: 438: 413:380 m (1,250 ft) 407:500 m (1,640 ft) 393:Service ceiling: 355: 334:-14F air-cooled 272: 88:Gaucher TRG-662 85: 75: 36:Type of aircraft 16: 15: 563: 562: 558: 557: 556: 554: 553: 552: 523: 522: 521: 520: 505: 504: 500: 493: 479: 460: 453: 439: 430: 425: 419: 351: 332:Continental C90 268: 260: 240: 181:Continental C90 156:had a modified 132:Gaucher TRG-662 128: 83: 73: 37: 27:Two seat light 12: 11: 5: 561: 551: 550: 545: 540: 535: 519: 518: 498: 491: 458: 451: 427: 426: 424: 421: 415: 414: 408: 402: 399:Rate of climb: 396: 390: 384: 375: 369: 363: 360:Maximum speed: 349: 348: 339: 325: 322:Fuel capacity: 319: 313: 307: 298: 292: 286: 280: 259: 256: 239: 236: 222:, were from a 127: 124: 90: 89: 86: 84:Developed from 80: 79: 76: 70: 69: 66: 62: 61: 58: 54: 53: 43: 39: 38: 35: 25: 21: 20: 9: 6: 4: 3: 2: 560: 549: 546: 544: 541: 539: 536: 534: 531: 530: 528: 514: 513: 508: 502: 494: 492:0-354-00538-3 488: 484: 477: 475: 473: 471: 469: 467: 465: 463: 454: 448: 444: 437: 435: 433: 428: 420: 417: 412: 409: 406: 403: 400: 397: 394: 391: 388: 385: 382: 380: 376: 373: 370: 367: 366:Cruise speed: 364: 361: 358: 357: 356: 354: 347: 343: 340: 337: 333: 329: 326: 323: 320: 317: 314: 311: 310:Empty weight: 308: 305: 303: 299: 296: 293: 290: 287: 284: 281: 278: 275: 274: 273: 271: 266: 264: 255: 253: 250:(CRATEPS) at 249: 245: 235: 231: 229: 225: 221: 217: 212: 210: 206: 202: 201:horn balanced 198: 194: 190: 186: 182: 177: 175: 171: 167: 163: 159: 155: 152: 148: 145: 140: 137: 133: 123: 121: 117: 113: 109: 105: 101: 97: 87: 82: 81: 77: 72: 71: 67: 64: 63: 59: 57:First flight 56: 55: 52: 48: 44: 42:Manufacturer 41: 40: 33: 30: 26: 23: 22: 17: 510: 501: 482: 442: 418: 416: 410: 404: 398: 392: 386: 377: 372:Stall speed: 371: 365: 359: 352: 350: 341: 327: 321: 315: 309: 300: 294: 288: 282: 276: 269: 267: 262: 261: 247: 241: 232: 224:Robin DR.220 213: 207:on the port 178: 141: 131: 129: 103: 99: 95: 93: 74:Number built 353:Performance 342:Propellers: 328:Powerplant: 230:component. 228:Stampe SV.4 183:air-cooled 136:tandem seat 60:6 May 1973 527:Categories 423:References 295:Wing area: 147:cantilever 104:ENAM-69/70 336:flat four 289:Wingspan: 263:Data from 185:flat four 29:homebuilt 209:elevator 205:trim tab 189:fuselage 174:ailerons 166:dihedral 144:low wing 102:and the 65:Retired 34:aircraft 302:Airfoil 283:Length: 154:plywood 116:trainer 32:trainer 512:Flight 489:  449:  387:Range: 197:rudder 193:canopy 158:Mureau 120:tandem 112:French 346:pitch 277:Crew: 170:flaps 162:chord 151:birch 68:1975 51:Cluny 24:Role 487:ISBN 447:ISBN 330:1 Ă— 220:spar 172:and 134:, a 94:The 45:AM ( 279:two 49:), 529:: 509:. 461:^ 431:^ 211:. 176:. 122:. 78:1 495:. 455:. 381:: 304::

Index

homebuilt
trainer
Arts et MĂ©tiers ParisTech
Cluny
low wing monoplane
French
trainer
tandem
tandem seat
low wing
cantilever
birch
plywood
Mureau
chord
dihedral
flaps
ailerons
Continental C90
flat four
fuselage
canopy
rudder
horn balanced
trim tab
elevator
conventional undercarriage
spar
Robin DR.220
Stampe SV.4

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