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SAB DB-80

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40: 300: 127:(SAB) who continued to work on its predecessor's designs, distinguished by their DB numbering as well as on their own, which had AB numbers. The DB-80 originated with Dyle and Bacalan but was not flown until 1930, built by SAB. It was Dyle and Bacalan's last design and a small aircraft by their standards but maintained their all-metal tradition. 248:
In late March 1930 the DB-80's test flights were awaiting better weather; a month later tests were underway but the first flight did not take place until 27 June 1930. The Lorraine powered DB-81 flew in August, after which testing of the pair continued successfully though interrupted by SAB test
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leg, with its upper side hinged from the fuselage longerons. The strengthened forward edge of the structure extended above the hinge and connected to an elastic block housed in a reinforced transverse beam which passed under the cockpit, incorporating
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aircraft giving easy access by two port-side doors to a well-lit cabin with two passenger seats and to a separate mail compartment behind them. The pilot sat ahead of the passengers under the wing
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with track of 1.90 m (75 in). The mainwheels were independently mounted and fitted with brakes. Each axle was mounted at the lower vertex of a triangular box acting as a
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light transports aimed at the air mail market whilst carrying two passengers. Identical apart from their engines, they flew in mid-1930.
76: 299: 228:, rather than the traditional one or two, and the detail of their caps or flanges, rather than the shape of the longitudinal braces or 896: 688: 871: 886: 173:. Its underside was smoothly bellied, its upper side flat. In plan its taper was delayed until aft of the cabin. Its 774: 358: 159: 216:
of 9. In plan it was straight tapered on both edges but with semi-elliptical tips curved particularly on the
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for official trials of the DB-20. In October the DB-80 was re-engined with a Lorraine and renamed DB-81.
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at mid-fuselage height. Like the fuselage, all the tail surfaces were covered with ribbed duralumin.
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was built around four longerons, with rectangular frames and covered in longitudinally ribbed
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There is no record of any further examples being built nor of measured performance figures.
711: 273: 182: 143: 138:. Two differently engined versions were built: the DB-80 had a 100 hp (75 kW) 206: 491: 860: 667: 646: 628: 588: 570: 552: 392: 287: 217: 155: 530: 512: 213: 197: 135: 810: 805: 388: 283: 212:
The DB-80's high, cantilever wing was unusual both in its construction and high
151: 276:. Re-engined with Lorraine in October 1930, becoming second DB-81. One built. 201: 51: 830: 825: 820: 815: 190: 174: 170: 131: 680: 185:, the latter cut away at its base to allow for movement of the one-piece 166: 17: 303:
Dyle et Bacalan DB-80 3-view drawing from NACA Aircraft Circular No.123
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profile. A similar but not identical wing structure was used on the
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NACA Aircraft Circular no.123 (1930) Performance figures calculated
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The DB-80 was aimed at the airmail market and was a single-engine,
298: 475:"NACA Aircraft Circulars no.123: The Dyle and Bacalan "D.B. 80"" 763: 684: 178: 395:, 89 kW (120 hp) maximum continuous, at 1,350 rpm 224:
were full span and broad. The wing was built around three
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was conventional, with a straight-tapered, blunt-topped
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180 L (40 imp gal; 48 US gal)
290:and 750 mm (29.5 in) shorter. One built. 647:"Aérodrome en aérodrome – à Bordeaux-Merignac" 629:"Aérodrome en aérodrome – à Bordeaux-Merignac" 589:"Aérodrome en aérodrome – à Bordeaux-Merignac" 571:"Aérodrome en aérodrome – à Bordeaux-Merignac" 553:"Aérodrome en aérodrome – à Bordeaux-Merignac" 775: 696: 8: 782: 768: 760: 703: 689: 681: 662: 660: 123:In 1929 Dyle and Bacalan were reformed as 507: 505: 416:200 km/h (120 mph, 110 kn) 422:170 km/h (110 mph, 92 kn) 455: 434:4,500 m (14,800 ft) practical 428:950 km (590 mi, 510 nmi) 531:"Le monoplan Dyle et Bacalan, D.B. 20" 469: 467: 465: 463: 461: 459: 29: 440:5 min to 1,000 m (3,300 ft) 7: 249:pilot Charles Deschamps' absence at 867:1930s French civil utility aircraft 606:Bruno Parmentier (30 August 1998). 272:upright six cylinder, water-cooled 142:six-cylinder, upright water-cooled 668:"Figure caption – Lorraine fitted" 25: 348:2.90 m (9 ft 6 in) 342:12 m (39 ft 4 in) 38: 882:Single-engined tractor aircraft 513:"L'avion postal léger D. B. 80" 492:"L'avion postal de jour D.B.80" 354:16 m (170 sq ft) 336:8 m (26 ft 3 in) 27:1930s French transport aircraft 111:were single-engine, all-metal 1: 375:1,100 kg (2,425 lb) 892:Aircraft first flown in 1930 635:(481): 12. 4 September 1930. 877:Société Aérienne Bordelaise 793:Société Aérienne Bordelaise 674:(488): 13. 23 October 1930. 369:678 kg (1,495 lb) 162:on the fuselage underside. 150:a 120 hp (89 kW) 125:Société Aérienne Bordelaise 77:Société Aérienne Bordelaise 913: 653:(486): 12. 9 October 1930. 446:80 km/h (50 mph) 801: 719: 577:(462): 13. 24 April 1930. 559:(458): 13. 27 March 1930. 282:120 hp (89 kW) 268:100 hp (75 kW) 50:Postal and two passenger 37: 32: 897:Dyle et Bacalan aircraft 519:(457): 3. 23 March 1930. 189:mounted on a triangular 872:1930s French mailplanes 595:(472): 13. 3 July 1930. 498:(132): 163–6. May 1930. 315:General characteristics 198:tailwheel undercarriage 196:The DB-80 had a fixed, 304: 295:Specifications (DB-81) 790:Aircraft produced by 302: 238:Dyle et Bacalan DB-20 541:: 3. 4 October 1928. 480:. NACA. August 1930. 887:High-wing aircraft 305: 52:transport aircraft 854: 853: 757: 756: 438:Time to altitude: 232:, determined the 183:unbalanced rudder 101: 100: 16:(Redirected from 904: 784: 777: 770: 761: 705: 698: 691: 682: 676: 675: 664: 655: 654: 643: 637: 636: 625: 619: 618: 616: 614: 603: 597: 596: 585: 579: 578: 567: 561: 560: 549: 543: 542: 527: 521: 520: 509: 500: 499: 488: 482: 481: 479: 471: 432:Service ceiling: 409: 317: 270:Hispano-Suiza 6P 140:Hispano-Suiza 6P 94: 63: 55:Type of aircraft 42: 30: 21: 912: 911: 907: 906: 905: 903: 902: 901: 857: 856: 855: 850: 797: 788: 758: 753: 715: 712:Dyle et Bacalan 709: 679: 666: 665: 658: 645: 644: 640: 627: 626: 622: 612: 610: 605: 604: 600: 587: 586: 582: 569: 568: 564: 551: 550: 546: 529: 528: 524: 511: 510: 503: 490: 489: 485: 477: 473: 472: 457: 453: 444:Take-off speed: 405: 313: 297: 262: 246: 207:shock absorbers 121: 92: 62:National origin 61: 56: 28: 23: 22: 15: 12: 11: 5: 910: 908: 900: 899: 894: 889: 884: 879: 874: 869: 859: 858: 852: 851: 849: 848: 843: 838: 833: 828: 823: 818: 813: 808: 802: 799: 798: 789: 787: 786: 779: 772: 764: 755: 754: 752: 751: 746: 741: 736: 731: 726: 720: 717: 716: 710: 708: 707: 700: 693: 685: 678: 677: 656: 638: 620: 598: 580: 562: 544: 522: 501: 496:L'Aéronautique 483: 454: 452: 449: 448: 447: 441: 435: 429: 423: 417: 414:Maximum speed: 403: 402: 396: 382: 379:Fuel capacity: 376: 370: 364: 355: 349: 343: 337: 331: 330:Two passengers 325: 296: 293: 292: 291: 286:five cylinder 280: 277: 266: 261: 258: 245: 242: 218:trailing edges 154:five-cylinder 120: 117: 99: 98: 95: 89: 88: 85: 81: 80: 74: 70: 69: 64: 58: 57: 54: 48: 44: 43: 35: 34: 26: 24: 14: 13: 10: 9: 6: 4: 3: 2: 909: 898: 895: 893: 890: 888: 885: 883: 880: 878: 875: 873: 870: 868: 865: 864: 862: 847: 844: 842: 839: 837: 834: 832: 829: 827: 824: 822: 819: 817: 814: 812: 809: 807: 804: 803: 800: 796: 794: 785: 780: 778: 773: 771: 766: 765: 762: 750: 747: 745: 742: 740: 737: 735: 732: 730: 727: 725: 722: 721: 718: 713: 706: 701: 699: 694: 692: 687: 686: 683: 673: 669: 663: 661: 657: 652: 648: 642: 639: 634: 630: 624: 621: 609: 608:"S.A.B DB-81" 602: 599: 594: 590: 584: 581: 576: 572: 566: 563: 558: 554: 548: 545: 540: 536: 532: 526: 523: 518: 514: 508: 506: 502: 497: 493: 487: 484: 476: 470: 468: 466: 464: 462: 460: 456: 450: 445: 442: 439: 436: 433: 430: 427: 424: 421: 420:Cruise speed: 418: 415: 412: 411: 410: 408: 400: 397: 394: 390: 386: 383: 380: 377: 374: 373:Gross weight: 371: 368: 367:Empty weight: 365: 362: 360: 356: 353: 350: 347: 344: 341: 338: 335: 332: 329: 326: 323: 320: 319: 318: 316: 311: 309: 301: 294: 289: 288:radial engine 285: 281: 278: 275: 274:inline engine 271: 267: 264: 263: 259: 257: 254: 252: 243: 241: 239: 235: 231: 227: 223: 219: 215: 210: 208: 203: 199: 194: 192: 188: 184: 180: 176: 172: 168: 163: 161: 157: 156:radial engine 153: 149: 145: 141: 137: 133: 128: 126: 118: 116: 114: 110: 106: 96: 91: 90: 87:27 June 1930 86: 84:First flight 83: 82: 78: 75: 73:Manufacturer 72: 71: 68: 65: 60: 59: 53: 49: 46: 45: 41: 36: 31: 19: 840: 835: 791: 748: 743: 671: 650: 641: 632: 623: 611:. Retrieved 601: 592: 583: 574: 565: 556: 547: 538: 534: 525: 516: 495: 486: 443: 437: 431: 425: 419: 413: 406: 404: 398: 389:Lorraine 5Pc 384: 378: 372: 366: 359:Aspect ratio 357: 351: 345: 339: 333: 327: 321: 314: 312: 307: 306: 284:Lorraine 5Pc 255: 251:Villacoublay 247: 220:, where its 214:aspect ratio 211: 195: 164: 152:Lorraine 5Pc 147: 136:leading edge 129: 122: 108: 104: 102: 93:Number built 811:SAB-SEMA 12 806:SAB-SEMA 10 407:Performance 399:Propellers: 391:5-cylinder 385:Powerplant: 244:Development 861:Categories 613:1 December 451:References 352:Wing area: 202:cantilever 33:SAB DB-80 672:Les Ailes 651:Les Ailes 633:Les Ailes 593:Les Ailes 575:Les Ailes 557:Les Ailes 535:Les Ailes 517:Les Ailes 340:Wingspan: 328:Capacity: 324:One pilot 308:Data from 191:tailplane 175:empennage 171:duralumin 132:high-wing 109:SAB DB-81 105:SAB DB-80 18:SAB DB-81 714:aircraft 401:2-bladed 260:Variants 222:ailerons 187:elevator 167:fuselage 160:radiator 146:and the 346:Height: 334:Length: 234:airfoil 426:Range: 393:radial 144:inline 119:Design 113:French 79:(SAB) 67:France 846:LH-70 841:DB-81 836:DB-80 831:AB-80 826:AB-22 821:AB-21 795:(SAB) 749:DB-81 744:DB-80 739:DB-70 734:DB-30 729:DB-20 724:DB-10 478:(PDF) 322:Crew: 279:DB-81 265:DB-80 226:spars 148:DB-81 47:Role 816:AB-2 615:2015 387:1 × 230:ribs 181:and 165:The 107:and 103:The 539:381 363:9.0 179:fin 863:: 670:. 659:^ 649:. 631:. 591:. 573:. 555:. 537:. 533:. 515:. 504:^ 494:. 458:^ 240:. 209:. 97:2 783:e 776:t 769:v 704:e 697:t 690:v 617:. 361:: 20:)

Index

SAB DB-81

transport aircraft
France
Société Aérienne Bordelaise
French
Société Aérienne Bordelaise
high-wing
leading edge
Hispano-Suiza 6P
inline
Lorraine 5Pc
radial engine
radiator
fuselage
duralumin
empennage
fin
unbalanced rudder
elevator
tailplane
tailwheel undercarriage
cantilever
shock absorbers
aspect ratio
trailing edges
ailerons
spars
ribs
airfoil

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