40:
469:
302:; the aircraft had been designed so that various powerplants could be selected; virtually any radial air-cooled engine of comparable weight and power could be installed. These engines were mounted on duralumin bearers that were attached to the nose of the fuselage or to the lower-wing spar by four screw-type bolts that facilitated rapid removal. Each of these engine bearer formed a block that comprised the engine, its immediate accessories,
243:, and the ailerons themselves. An elastic mounting was used for these ailerons and shared their pinion-and-ratchet actuation method with that of the Bréguet 270; whole span ailerons were fitted to both the upper and lower wings. Structurally, it is centred around a single box spar and was directly attached to the base of the fuselage by a pair of wide triangular-shaped vertical
445:
318:
contained a 300-liter (79.25-gal.) fuel tank; in addition, two other fuel tanks with a combined capacity of 300 liters (79.25 gal.), that were typically located at the base of the fuselage, exclusively supplied the central engine under standard operating conditions. However, all of the tanks could be
337:
brakes that could be applied either simultaneously or differentially at the pilot's discretion. Each wheel, which were equipped with straight-side tyres, was mounted in an axleless configuration upon a steel fork that, via steel tubing, directly attached to the spar of the lower wing. This tube slid
263:
were attached via tubular steel rivets to small stamped duralumin gussets that were also riveted to the spar webs. Each part of the rib was stamped as a single piece of sheet dura1umin; this same material was used for the covering of the wing. The wing tips were detachable. The wings are braced by
193:; however, the girder-based fuselage of the Bréguet 270 was substituted for a more conventional rectangular fuselage that provided sufficient internal volume to accommodation the carriage of up to ten passengers along with their baggage. The interior of the fuselage was divided by a series of
227:
configuration. The standard external door was already specifically designed from the onset to readily permit the passage of casualties on stretchers. Two separate baggage compartments were provided, a larger one at the front of the aircraft and another at the rear.
254:
The upper wing, while had a uniform profile across the whole span, consisted of two symmetrical sections that joined on top of the fuselage. It was supported by two identical spars composed of steel that were connected via rigid X-shaped
205:
In the cockpit, the pilot was seated on the left side, at which position relatively good external visibility was available. Close by, a second seat was present that could be used for various purposes, such as by a second pilot, mechanic,
218:
that was effectively concealed by the door from the cabin during the boarding and de-boarding of passengers. The door between the cabin and lavatory could be removed; reasons for this included the accommodation of bulky packages or
210:, or radio operator, or some combination thereof; dual flight controls were provided. Above their position was a movable panel, which was intended for emergency egress, for which the pilot was typically provided with a
275:
structure that comprised steel spars and duralumin ribs. The tail surfaces, which had symmetrical biconvex profiles, used steel hinges and a duralumin covering. The horizontal empennage had a single-piece
201:
covering was directly riveted to. One such bulkhead formed the partition between the passenger cabin and the cockpit, although a door was provided to permit internal passage between the two compartments.
323:; furthermore, all fuel tanks could be rapidly emptied mid-flight if required. The aircraft was reportedly designed to be capable of maintaining level flight if any one of its engines stopped.
353:
acquired a total of six 393Ts along with the sole 392T prototype from
Breguet. The latter was exclusively used as a cargo plane. The aircraft were originally deployed on the
689:
785:
814:
1497:
1446:
288:. The movable tail surfaces were actuated by the pilot via steel wires that ran along the top of the fuselage and were guided using
166:
routes, as well as various short haul routes between Paris and nearby
European destinations in the latter portion of their careers.
1477:
807:
280:
that could be controlled via a compact flap mounted on the middle of its trailing edge. The vertical empennage consists of a
468:
39:
362:
159:
1482:
1415:
1400:
1395:
1325:
1124:
1119:
1114:
800:
311:
182:
247:. Various core elements of the aircraft are directly supported by this spar, including the sliding forks of the
1441:
843:
1360:
1270:
1265:
1260:
1244:
1234:
1174:
1390:
1385:
1355:
1335:
1300:
1199:
1194:
1189:
1139:
1134:
1129:
959:
954:
949:
1405:
1380:
1370:
1365:
1320:
1280:
1184:
1179:
1169:
1164:
1159:
1154:
1149:
1144:
1059:
1054:
1049:
919:
277:
1487:
838:
338:
within a steel sleeve with bronze rings traversed by two solid pins with four lugs riveted to the spar.
259:; each spar had two flanges of drawn steel connected by a web of corrugated sheet steel. The three-part
256:
190:
1425:
1420:
1340:
1330:
1305:
1214:
1044:
1034:
1029:
1024:
1410:
1229:
1224:
1219:
194:
143:
First flown in
February 1931, the Bréguet 390T family attracted the attention of the recently-formed
326:
The undercarriage was equipped with various internally developed elements, including Bréguet-type
1492:
232:
150:, which acquired a total of six 393Ts along with the sole 392T prototype. These were used on the
1310:
747:
548:
429:
388:
303:
296:
215:
883:
878:
873:
868:
858:
823:
137:
85:
74:
63:
742:
863:
853:
1239:
1069:
999:
1350:
1345:
1275:
1209:
1204:
1109:
1104:
1099:
1094:
1089:
1084:
1079:
1074:
1064:
1039:
1019:
994:
989:
984:
979:
974:
969:
848:
330:
231:
The lower wing of the Bréguet 390T could be divided into several elements, such as the
186:
373:
and used on various short haul routes between Paris and nearby
European destinations.
1471:
1456:
1451:
964:
944:
939:
934:
929:
391:
299:
224:
782:"Breguet 390 T commercial airplane (French) : a ten-seat all-steel sesquiplane"
415:
366:
347:
248:
244:
236:
163:
144:
1375:
1315:
1295:
1290:
1285:
924:
914:
909:
904:
394:. One aircraft built, destroyed in a crash early on in the flight test programme.
178:
130:
888:
781:
457:
369:
route. Towards the end of their careers, all remaining 393Ts were recalled to
358:
350:
327:
272:
155:
147:
95:
334:
220:
211:
207:
198:
17:
223:-bound personnel. As such, the aircraft could be readily converted into an
572:
235 km/h (146 mph, 127 kn) at 1,000 m (3,280 ft)
354:
320:
307:
175:
151:
133:
50:
185:. Its general structure comprises the same principles as to the earlier
315:
240:
450:
289:
285:
126:
319:
interconnected to one another, which was controlled via a series of
792:
467:
370:
265:
777:. London, UK: Bright Star Publishing. pp. File 890 Sheet 81.
197:
that were joined by sturdy angle members to which the aircraft's
796:
281:
260:
295:
The Bréguet 390T was powered by three engines, such as the
472:
Breguet 393T 3-view drawing from L'Aerophile
February 1934
136:
designed and produced by the French aircraft manufacturer
722:
566:
249 km/h (155 mph, 134 kn) at sea level
251:
and the duralumin bearers of the two lateral engines.
1434:
1253:
897:
831:
578:
945–975 km (587–606 mi, 510–526 nmi)
743:"Le Trimoteur Commercial Breguet 393 T (France)"
808:
8:
346:During the mid 1930s, the newly constituted
786:National Advisory Committee for Aeronautics
769:. London, UK: Studio Editions. p. 199.
751:(in French). February 1934. pp. 53–54.
484:National Advisory Committee for Aeronautics
815:
801:
793:
590:11 minutes to 2,000 m (6,560 ft)
651:
649:
535:3,529–3,996 kg (7,780–8,810 lb)
680:
678:
676:
674:
672:
670:
639:
637:
635:
633:
631:
629:
627:
617:
615:
613:
611:
609:
789:, 1 August 1931. NACA-AC-149, 93R19744.
688:was invoked but never defined (see the
605:
181:of all-metal construction with a fixed
758:European Transport Aircraft since 1910
701:
480:European Transport Aircraft since 1910
29:
7:
529:66.46 m (715.4 sq ft)
271:The tail unit of the aircraft had a
239:, the area between the spar and the
683:
523:14.76 m (48 ft 5 in)
517:21.71 m (71 ft 3 in)
511:14.76 m (48 ft 5 in)
428:Definitive production version with
174:The Bréguet 390T family were large
404:Second prototype, similar to 390T.
25:
551:, 260 kW (350 hp) each
775:World Aircraft Information Files
684:Cite error: The named reference
443:
38:
767:Jane's Encyclopedia of Aviation
214:. To the rear of the cabin, an
27:1931 airliner family by Bréguet
765:Taylor, Michael J. H. (1989).
541:6,000 kg (13,228 lb)
1:
584:5,850 m (19,190 ft)
414:Freighter version powered by
1498:Aircraft first flown in 1931
387:First prototype, powered by
1514:
432:radial engines, six built.
418:radial engines, one built.
1421:Vultur (carrier aircraft)
37:
32:
490:General characteristics
361:route and later on the
191:reconnaissance aircraft
183:tailwheel undercarriage
1478:1930s French airliners
473:
314:. Each lateral engine
1447:Gyroplane Laboratoire
760:. London, UK: Putnam.
756:Stroud, John (1966).
471:
464:Specifications (393T)
264:two pairs of V-shape
713:NACA 1931, pp. 4-5.
664:NACA 1931, pp. 1-2.
655:NACA 1931, pp. 2-3.
342:Operational history
474:
333:and Bréguet-built
92:Primary user
1465:
1464:
704:, pp. 72–73.
588:Time to altitude:
416:Hispano-Suiza 9Qc
304:fire extinguisher
216:aircraft lavatory
129:propeller-driven
125:were a family of
111:
110:
16:(Redirected from
1505:
1483:Breguet aircraft
817:
810:
803:
794:
778:
770:
761:
752:
729:
720:
714:
711:
705:
699:
693:
687:
682:
665:
662:
656:
653:
644:
643:NACA 1931, p. 2.
641:
622:
621:NACA 1931, p. 1.
619:
582:Service ceiling:
559:
492:
449:
447:
446:
104:
54:Type of aircraft
42:
30:
21:
1513:
1512:
1508:
1507:
1506:
1504:
1503:
1502:
1468:
1467:
1466:
1461:
1430:
1426:Vultur (bomber)
1249:
893:
827:
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647:
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625:
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597:
555:
549:Gnome-Rhône 7Kd
521:Lower wingspan:
515:Upper wingspan:
488:
466:
444:
442:
439:
430:Gnome-Rhône 7Kd
389:Gnome-Rhône 5Kd
379:
344:
331:shock absorbers
297:Gnome-Rhône 7Kd
172:
102:
55:
28:
23:
22:
15:
12:
11:
5:
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645:
623:
604:
603:
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592:
591:
585:
579:
573:
567:
564:Maximum speed:
553:
552:
542:
536:
530:
524:
518:
512:
506:
505:ten passengers
500:
465:
462:
461:
460:
454:
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438:
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434:
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425:
424:
420:
419:
411:
410:
406:
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396:
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392:radial engines
384:
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171:
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109:
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105:
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986:
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928:
926:
923:
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918:
916:
913:
911:
908:
906:
903:
902:
900:
898:Model numbers
896:
890:
887:
885:
882:
880:
877:
875:
872:
870:
867:
865:
862:
860:
857:
855:
852:
850:
847:
845:
842:
840:
839:Aerhydroplane
837:
836:
834:
830:
825:
818:
813:
811:
806:
804:
799:
798:
795:
788:
787:
783:
780:
776:
772:
768:
763:
759:
754:
750:
749:
744:
740:
739:
735:
728:, p. 53.
727:
726:February 1934
725:
719:
716:
710:
707:
703:
698:
695:
691:
681:
679:
677:
675:
673:
671:
667:
661:
658:
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636:
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632:
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616:
614:
612:
610:
606:
599:
594:
589:
586:
583:
580:
577:
574:
571:
570:Cruise speed:
568:
565:
562:
561:
560:
558:
550:
546:
543:
540:
539:Gross weight:
537:
534:
533:Empty weight:
531:
528:
525:
522:
519:
516:
513:
510:
507:
504:
501:
498:
495:
494:
493:
491:
486:
485:
481:
478:
470:
463:
459:
456:
455:
452:
441:
440:
436:
431:
427:
426:
422:
421:
417:
413:
412:
408:
407:
403:
402:
398:
397:
393:
390:
386:
385:
381:
380:
376:
374:
372:
368:
364:
360:
356:
352:
349:
341:
339:
336:
332:
329:
328:oleopneumatic
324:
322:
317:
313:
309:
305:
301:
300:radial engine
298:
293:
291:
287:
283:
279:
274:
269:
267:
262:
258:
252:
250:
249:undercarriage
246:
242:
238:
234:
229:
226:
225:air ambulance
222:
217:
213:
209:
203:
200:
196:
192:
188:
184:
180:
177:
169:
167:
165:
161:
157:
153:
149:
146:
141:
139:
135:
132:
128:
124:
120:
116:
106:
101:
100:
97:
94:
91:
90:
87:
83:
81:Introduction
80:
79:
76:
72:
70:First flight
69:
68:
65:
62:
60:Manufacturer
59:
58:
52:
49:
46:
45:
41:
36:
33:Bréguet 393T
31:
19:
1488:Sesquiplanes
1271:Atlantique 2
1014:
1009:
1004:
784:
774:
766:
757:
746:
736:Bibliography
723:
718:
709:
697:
660:
587:
581:
575:
569:
563:
556:
554:
544:
538:
532:
526:
520:
514:
508:
502:
496:
489:
487:
483:
479:
476:
475:
367:Buenos Aires
348:flag carrier
345:
325:
312:oil radiator
294:
270:
253:
237:leading edge
230:
204:
179:sesquiplanes
176:three-engine
173:
164:Buenos Aires
145:flag carrier
142:
122:
118:
115:Bréguet 390T
114:
112:
103:Number built
18:Breguet 393T
1435:Helicopters
832:Early types
748:L'Aérophile
724:L'Aérophile
702:Stroud 1966
557:Performance
545:Powerplant:
187:Bréguet 270
131:sesquiplane
1472:Categories
1416:Universale
1326:Deux-Ponts
595:References
527:Wing area:
499:two pilots
458:Air France
359:Casablanca
351:Air France
273:cantilever
156:Casablanca
148:Air France
96:Air France
1493:Trimotors
1442:Gyroplane
1361:Louisette
1356:Leviathan
1316:de Chasse
1276:Bellatrix
844:Gyroplane
690:help page
600:Citations
503:Capacity:
477:Data from
437:Operators
335:hydraulic
321:stopcocks
221:stretcher
212:parachute
208:navigator
199:duralumin
195:bulkheads
189:military
134:airliners
73:February
1396:Provence
1391:Nymphale
1386:Nautilus
1376:Michelin
1346:Integral
1336:Fauvette
1331:Épaulard
1266:Atlantic
859:Type III
826:aircraft
377:Variants
355:Toulouse
308:oil tank
278:elevator
241:ailerons
158:and the
152:Toulouse
51:Airliner
1381:Mouette
1371:Mercure
1321:Cinzano
1311:Colibri
1301:Choucas
1281:Bizerte
1254:By name
864:Type IV
854:Type II
824:Breguet
509:Length:
316:nacelle
290:pulleys
257:bracing
245:gussets
138:Bréguet
64:Bréguet
1406:Saigon
1401:Sahara
1351:Jaguar
1341:Fulgur
1306:Colmar
884:Type U
879:Type G
874:Type A
869:Type V
849:Type I
686:naca 3
576:Range:
451:France
448:
286:rudder
284:and a
266:struts
170:Design
127:French
1457:G.111
1452:G.11E
1261:Alizé
497:Crew:
371:Paris
363:Natal
233:spars
160:Natal
84:July
47:Role
1411:Taon
1366:Mars
1245:1150
1240:1100
1235:1050
1230:1004
1225:1002
1220:1001
1015:393T
1010:392T
1005:390T
1000:280T
547:3 ×
423:393T
409:392T
399:391T
382:390T
310:and
261:ribs
123:393T
121:and
119:392T
113:The
86:1934
75:1931
1296:BUM
1291:BUC
1286:BLC
1215:960
1210:941
1205:940
1200:906
1195:905
1190:904
1185:902
1180:901
1175:900
1170:895
1165:894
1160:893
1155:892
1150:891
1145:890
1140:792
1135:791
1130:790
1125:765
1120:763
1115:761
1110:731
1105:730
1100:696
1095:695
1090:694
1085:693
1080:691
1075:690
1070:670
1065:610
1060:530
1055:522
1050:521
1045:500
1040:482
1035:470
1030:462
1025:460
1020:410
995:274
990:273
985:271
980:270
970:26T
282:fin
1474::
975:27
965:25
960:22
955:21
950:20
945:19
940:17
935:16
930:14
925:12
920:11
889:LE
745:.
692:).
669:^
648:^
626:^
608:^
482:,
306:,
292:.
268:.
235:,
140:.
117:,
107:9
915:6
910:5
905:4
816:e
809:t
802:v
365:-
357:-
162:-
154:-
20:)
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