673:
639:
243:, and formers were typically composed of light alloys instead. Light alloys had been intentionally avoided for primary structures due to its mechanical properties. One key advantage of this structural approach was to permit the size of the fuselage to be minimised considerably which, amongst other benefits, impinged less upon the range of both vision and fire of the observer, although visibility for the pilot remained broadly similar to that of conventional aircraft. Despite its unorthodox nature, evaluation of the design proved that the Bréguet 270's aerodynamic efficiency was equal to that of most conventional aircraft of the era.
721:
336:
cockpits formed an independent unit that was superimposed upon the central box to form, together with the engine cowling, the bodywork of the aircraft. Various different types of bodies, furnished with appropriate equipment for the mission to which the aircraft was to be tasked, with were available. The demountable body housing the pilot and observer's cockpits was of light duralumin construction; access to both cockpits was acquired via doors that were mounted so that they could be rapidly dropped mid-flight by merely knocking a lever so that emergency egress via
696:
349:
The design of the tail boom was particularly convenient in respect to the flight controls, all connections with the tail's movable surfaces were concealed inside of the spar while a conventional rudder bar was dispensed with in favour of a pair of pivoting pedals, one on each side of the spar. All connections with the tail surfaces and ailerons were rigid; dual control were fitted as standard although the observer's stick was removable. The use of tubes was intentionally avoided wherever possible.
615:
389:
332:. These ailerons were divided into two portions, one of which was elastically mounted in such a manner that the effort required by the pilot was relatively uniform. Actuation of the ailerons was achieved via a series of toothed rods. As a result of the unusual strut arrangement used, the upper wing's incidence could be adjusted relatively easily via the use of a special spanner.
592:
37:
352:
The Bréguet 270 was designed to be powered by virtually any engine in the 500 to 650 hp range; it uses a relatively simple steel engine mounting that gave good accessibility to all parts that required attention. It could be replaced in mere minutes, being secured to the forward portion of the central
344:
protected the occupant from external weather conditions. The observer's cockpit, which was also provided with a windshield, had a camera mounting installed in front of it, which, in combination with sliding apertures in the bodywork, facilitated convenient photography from both vertical and oblique
327:
attached to the tips of the lower wings in addition to the central cabane. The bracing members comprised two channel steel profiles that were riveted together back to back and disposed at right angles. It was strengthened using ribs, the majority of which were composed of duralumin while a minority
348:
The forward end of the tail boom was attached to the rear of the central box by means of a heavy triangular stamped steel frame and a U-shaped steel frame. The rear end of the tail boom supported the stabilizing surfaces of the tail unit along with a compact swivelling wheel for the undercarriage.
335:
The aircraft's backbone is composed of two distinct parts, a central box and the tail boom; the former consisted of a steel beam of a small cross-section, attached at its forward end to the central box and resting directly on the lower wing, to which is bolted to the detachable engine unit. The
270:
Being a sesquiplane, the lower wing of the Bréguet 270 was considerably smaller than the upper wing, accounting for only 17.6 per cent of the total area. Despite this, the lower wing was the centre point of the aircraft's structure, and thus had immense strength. Being a single-piece unit, it
214:
exhibited mediocre performance during flight trials. Nonetheless, the French military opted to place orders for 85 aircraft in 1930 and a further 45 in 1932, this latter batch having a more powerful engine fitted. Two high-altitude reconnaissance versions were also built as the
262:
in order that riveted stiffeners could be dispensed with. Seeking to ease the tasks of maintenance, repairs, and replacement, the assembly of the aircraft was deliberately shaped so to maximise interchangeability and standardise elements such pins and bolts. Permanent
271:
comprised a single spar of box construction composed of steel. It featured flanges made from large drawn plates with reinforcing corrugations joined by sheet webs stiffened in a similar manner. Internal frames of stamped steel provided considerable strength while the
322:
The structure of the upper wing comprised two identical I-shaped steel spars with corrugated sheet steel webs and butterfly drawn profiles as flanges. It was free of compression tubes, except where struts joined with the spars. The upper wing was supported via
279:
sheeting that ran lengthwise between two adjacent ribs and riveted along the edges of the latter through an interposed inverted U-shaped strips of duralumin. Attachments for steel fittings at each end of the spar were provided for the wing
250:, which studies has determined to be the preferential method; exceptions were occasionally made in order to make disassembly of the overall aircraft practical, thus in such circumstances bolts were used instead. Neither studs or
287:
In addition to its primary aerodynamic purpose, the lower wing served various secondary purposes. Its internal space accommodated, amongst other things, a total of four fuel tanks; for greater fuel capacity, the
365:; cooling was regulated using shutters fitted in the cowling. All three air intakes were mounted along the same horizontal line; short exhaust stacks were typically provided, although some aircraft had
206:
for all stressed elements of the structure, a choice that represented a considerable departure from accepted practice of the era; the Bréguet 27 would be the first aircraft to employ such construction.
254:
were used in the construction process. All parts were designed to facilitate automatic riveting by machine while the number of rivets was reduced to a minimum via the use of processes such as the
2029:
1254:
Cony, Christophe; Cortet, Pierre; Moulin, Jacques (October 2002). "Premier des "tout acier", le Bréguet 270 et sa descendance: 4 / De la "drôle du guerre" à la campagne de France".
292:
on either side could be replaced by a tank that had an identical external shape. The lower wing also bared a 'backbone' that substitutes for a conventional fuselage as well as the
319:. The relatively large track of the undercarriage made contract between the ground and a wing tip reasonably implausible while air resistance was also reduced to a minimum.
340:
was as easy as possible for both crew. The pilot's cockpit was relatively roomy and comfortable; all instrumentation was conveniently placed while a curved
275:, composed of sheet steel, featured rolled-edge lightening holes, slid on the spar and secured by riveted steel fittings. The wing covering was composed of
1328:
296:. This undercarriage, which was directly mounted onto the lower wing's single spar, comprised two completely independent wheels without any kind of leg or
239:
wires or rods and thus excluding rigging. All stressed structural members were composed of high-tensile steel, while secondary members, such as coverings,
1366:
2034:
396:
The two
Breguet 33 high-altitude reconnaissance prototypes were used to make significant long-distance flights. The first aircraft was flown from
385:
at the time of the initial German offensive. After they began suffering combat losses, the Army withdrew all remaining examples from service.
2054:
1998:
1290:
Cortet, Pierre; Moulin, Jacques (September 2002). "Premier des "tout acier", le Bréguet 270 et sa descendance: 3 / L'entre-deux-guerres".
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s, with a more powerful 484 kW (650 hp) engine, and larger useful load were ordered. Older 270s were modified for VIP
2044:
1359:
720:
627:
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before returning to Paris via Saigon, eventually covering around 35,000 km (22,000 mi). Hilsz also won the 1936
412:
in 7 days, 9 hours and 50 minutes, and back again in just 3 days 4 hours and 17 minutes. The second aircraft (christened
235:
aircraft that featured a somewhat unorthodox design. Its structure was entirely rigid, lacking any internal or external
198:. Bréguet decided to produce a new aircraft to submit for this requirement. This design, which was of a large all-metal
168:
on 23 February 1929. In addition to its adoption by the Armée de l'Ai, it was also sold on the export market to both
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of master ribs were composed of steel instead. A third false spar, composed of duralumin, was used to anchor the
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Cortet, Pierre; Moulin, Jacques (August 2002). "Premier des "tout acier", le Bréguet 270 et sa descendance".
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Cortet, Pierre; Moulin, Jacques (June 2002). "Premier des "tout acier", le Bréguet 270 et sa descendance".
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152:(French Air Force) for a new twin-seat observation aircraft. This clean-sheet aircraft featured unusual
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304:, that received the upper end of the fork supporting the wheel was used. The bracket incorporated a
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1325:"The Breguet 270 General-Purpose Military Airplane (French) : A Two-Seat All-Steel Sesquiplane"
879:
604:
1263:
Cony, Christophe; Cortet, Pierre; Moulin, Jacques (November 2002). "Les Bréguet 27 à l'étranger".
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Cortet, Pierre; Moulin, Jacques (December 2002). "Breguet 330 : Les derniers "tout acier"".
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engine, 13 built and one converted from a Bre 270. Ten more were built for China powered by
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140:
63:
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1405:
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radial engine. One built and first flown in
January 1934. Raced by Maryse Hilsz in 1935.
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Prototypes (ten built) and initial production version (143 built) powered by a single
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A single Bre.27S was constructed, modified from the Bre.330 No.2, powered by a single
2023:
2008:
2003:
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engines, with three also being modified from
Hispano-Suiza 12Ybrs powered versions.
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17:
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flying a
Breguet 27 at an average speed of 277 km/h (172 mph).
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36:
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aircraft designed and produced by the French aircraft manufacturer
798:
490 L (130 US gal; 110 imp gal) (maximum)
719:
688:
got ahold of remaining Bréguet 270's when France collapse in 1940.
433:
429:
401:
397:
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377:
Breguet 27s continued in military service through the outbreak of
324:
300:. Instead, a relatively sturdy bracket, akin to the head lug of a
297:
281:
247:
203:
173:
246:
The various parts of the aircraft were typically assembled using
935:
1348:
194:
that sought a new two-seat observation aircraft to replace the
44:
Breguet 274 with Gnome-Rhône 14K (Mistral Major) 900 HP engine
272:
1320:. London: Bright Star Publishing. pp. File 890 Sheet 81.
818:
2-bladed Bréguet, 3.05 m (10 ft 0 in) diameter
724:
Breguet 270 3-view drawing from NACA Aircraft
Circular No.127
146:
It was designed in response to a requirement released by the
579:
Second Bre.330 prototype optimised for long-duration flight.
164:
was mounted on a boom behind the fuselage. It performed its
854:
Six minutes and 10 seconds to 2,000 m (6,600 ft)
711:
operated three Bre.270 aircraft and nine Bre.273 aircraft.
515:) Version optimised for harsh colonial conditions with
443:
The French army ordered 85 270s in 1930. In 1932, 45
357:
was provided with horizontal hinges, akin to a car's
1986:
1805:
1449:
1383:
184:The Bréguet 27 was designed in response to a 1928
884:1 × trainable, rearward-firing 7.7 mm (.303 in)
845:7,750 m (25,430 ft) (absolute ceiling)
219:, but these did not lead to further production.
547:Version powered by a 825 hp (615 kW)
2030:1920s French military reconnaissance aircraft
1360:
8:
1329:National Advisory Committee for Aeronautics
878:1 × fixed, forward-firing 7.7 mm (.303 in)
857:29 minutes to 6,000 m (20,000 ft)
1367:
1353:
1345:
1332:, 1 September 1930. NACA-AC-127, 93R19708.
1303:(in French). No. 117. pp. 47–51.
1294:(in French). No. 114. pp. 34–47.
1285:(in French). No. 113. pp. 18–27.
1267:(in French). No. 116. pp. 41–51.
1258:(in French). No. 115. pp. 20–33.
1108:
1106:
1060:
1058:
1276:(in French). No. 111. pp. 7–14.
1120:
1118:
1016:
1014:
839:1,000 km (620 mi, 540 nmi)
833:236 km/h (147 mph, 127 kn)
607:received small batch of Bre.270 aircraft.
559:High-altitude version of Breguet 27 with
156:that ended abruptly, aft of the two open
1030:
1028:
1026:
995:
993:
991:
963:
961:
959:
957:
311:, the design of which Bréguet secured a
1312:. London: Studio Editions. p. 199.
928:
315:on, as well as a special type of wheel
630:received ten Bre.273 aircraft in 1934.
26:
202:, made extensive use of high-tensile
7:
774:49.67 m (534.6 sq ft)
756:17.01 m (55 ft 10 in)
762:7.58 m (24 ft 10 in)
513:Théatres des Operations Extérieures
1163:The Encyclopedia of World Aircraft
912:List of Interwar military aircraft
896:12 × 10 kg (22 lb) bombs
768:3.58 m (11 ft 9 in)
750:9.76 m (32 ft 0 in)
25:
531:variant for export, powered by a
267:were used for all subassemblies.
1318:World Aircraft Information Files
694:
671:
637:
613:
590:
227:The Bréguet 270 was a twin-seat
35:
2035:Single-engined tractor aircraft
1310:Jane's Encyclopedia of Aviation
1165:. Prospero Books. p. 118.
657:received 85 Bre.270 designated
563:engine, one later redesignated
111:Venezuelan Air Force and China
73:Marcel Vuillierme, Rene Dorand
1308:Taylor, Michael J. H. (1989).
369:fitted for night operations.
1:
792:2,900 kg (6,393 lb)
786:2,550 kg (5,622 lb)
780:1,676 kg (3,695 lb)
628:Chinese Nationalist Air Force
2055:Aircraft first flown in 1929
420:on a tour of Asia, visiting
1161:Donald, David, ed. (1997).
812:, 370 kW (500 hp)
716:Specifications (Bre.270A.2)
353:box by only four pins. The
2071:
1218:Cony, Cortet & Moulin
1202:Cony, Cortet & Moulin
1186:Cony, Cortet & Moulin
661:and 45 Bre.271 designated
256:corrugating of sheet metal
1973:Vultur (carrier aircraft)
43:
34:
29:
744:two (pilot and observer)
381:, still equipping three
735:General characteristics
519:radial engine, 1 built.
499:Version powered by the
487:Version powered by the
52:Reconnaissance aircraft
2045:French patrol aircraft
1082:NACA 1930, pp. 2-3, 5.
725:
686:Vichy French Air Force
393:
392:Codos and Robida, 1932
180:Design and development
1999:Gyroplane Laboratoire
1142:NACA 1930, pp. 10-11.
723:
391:
186:request for proposals
1234:Cortet & Moulin
1073:NACA 1930, pp. 3, 5.
1052:NACA 1930, pp. 9-10.
936:Cortet & Moulin
709:Venezuelan Air Force
537:Hispano-Suiza 12Ydrs
533:Hispano-Suiza 12Ybrs
438:Coupe Héléne Boucher
1133:NACA 1930, pp. 8-9.
1100:NACA 1930, pp. 3-7.
1091:NACA 1930, pp. 6-7.
1043:NACA 1930, pp. 2-5.
1020:NACA 1930, pp. 3-4.
985:NACA 1930, pp. 1-4.
976:NACA 1930, pp. 1-2.
951:NACA 1930, pp. 1-3.
880:Vickers machine gun
790:Max takeoff weight:
605:Brazilian Air Force
404:in January 1932 by
373:Operational history
102:Primary users
1224:, pp. 41, 43.
806:Hispano-Suiza 12Hb
726:
561:Hispano-Suiza 12Nb
549:Gnome-Rhône 14Kdrs
503:engine, two built.
477:Hispano-Suiza 12Hb
465:Hispano-Suiza 12Nb
394:
2017:
2016:
1151:NACA 1930, p. 11.
1112:NACA 1930, p. 12.
1064:NACA 1930, p. 10.
849:Time to altitude:
501:Gnome-Rhône 9Kdrs
491:engine, 45 built.
489:Hispano-Suiza 12Y
125:
124:
81:23 February 1929
16:(Redirected from
2062:
2050:Breguet aircraft
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999:NACA 1930, p. 4.
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54:Type of aircraft
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1337:External links
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309:shock absorber
306:oleo-pneumatic
233:reconnaissance
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191:Armée de l'Air
188:issued by the
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149:Armée de l'Air
137:reconnaissance
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119:
113:
112:
107:Armée de l'Air
103:
99:
98:
95:
91:
90:
87:
83:
82:
79:
75:
74:
71:
67:
66:
61:
57:
56:
53:
50:
46:
45:
41:
40:
32:
31:
24:
14:
13:
10:
9:
6:
4:
3:
2:
2067:
2056:
2053:
2051:
2048:
2046:
2043:
2041:
2038:
2036:
2033:
2031:
2028:
2027:
2025:
2010:
2007:
2005:
2002:
2000:
1997:
1995:
1992:
1991:
1989:
1985:
1979:
1976:
1974:
1971:
1969:
1966:
1964:
1961:
1959:
1956:
1954:
1951:
1949:
1946:
1944:
1941:
1939:
1936:
1934:
1931:
1929:
1926:
1924:
1921:
1919:
1916:
1914:
1911:
1909:
1906:
1904:
1901:
1899:
1896:
1894:
1891:
1889:
1886:
1884:
1881:
1879:
1876:
1874:
1871:
1869:
1866:
1864:
1861:
1859:
1856:
1854:
1851:
1849:
1846:
1844:
1841:
1839:
1836:
1834:
1831:
1829:
1826:
1824:
1821:
1819:
1816:
1814:
1811:
1810:
1808:
1804:
1798:
1795:
1793:
1790:
1788:
1785:
1783:
1780:
1778:
1775:
1773:
1770:
1768:
1765:
1763:
1760:
1758:
1755:
1753:
1750:
1748:
1745:
1743:
1740:
1738:
1735:
1733:
1730:
1728:
1725:
1723:
1720:
1718:
1715:
1713:
1710:
1708:
1705:
1703:
1700:
1698:
1695:
1693:
1690:
1688:
1685:
1683:
1680:
1678:
1675:
1673:
1670:
1668:
1665:
1663:
1660:
1658:
1655:
1653:
1650:
1648:
1645:
1643:
1640:
1638:
1635:
1633:
1630:
1628:
1625:
1623:
1620:
1618:
1615:
1613:
1610:
1608:
1605:
1603:
1600:
1598:
1595:
1593:
1590:
1588:
1585:
1583:
1580:
1578:
1575:
1573:
1570:
1568:
1565:
1563:
1560:
1558:
1555:
1553:
1550:
1548:
1545:
1543:
1540:
1538:
1535:
1533:
1530:
1528:
1525:
1523:
1520:
1518:
1515:
1513:
1510:
1508:
1505:
1503:
1500:
1498:
1495:
1493:
1490:
1488:
1485:
1483:
1480:
1478:
1475:
1473:
1470:
1468:
1465:
1463:
1460:
1458:
1455:
1454:
1452:
1450:Model numbers
1448:
1442:
1439:
1437:
1434:
1432:
1429:
1427:
1424:
1422:
1419:
1417:
1414:
1412:
1409:
1407:
1404:
1402:
1399:
1397:
1394:
1392:
1391:Aerhydroplane
1389:
1388:
1386:
1382:
1377:
1370:
1365:
1363:
1358:
1356:
1351:
1350:
1347:
1341:
1340:
1336:
1331:
1330:
1326:
1323:
1319:
1315:
1311:
1306:
1302:
1297:
1293:
1288:
1284:
1279:
1275:
1270:
1266:
1261:
1257:
1252:
1251:
1247:
1239:
1237:
1230:
1227:
1223:
1222:November 2002
1221:
1214:
1211:
1208:, p. 45.
1207:
1206:November 2002
1205:
1198:
1195:
1192:, p. 47.
1191:
1190:November 2002
1189:
1182:
1179:
1174:
1172:1-85605-375-X
1168:
1164:
1157:
1154:
1148:
1145:
1139:
1136:
1130:
1127:
1121:
1119:
1115:
1109:
1107:
1103:
1097:
1094:
1088:
1085:
1079:
1076:
1070:
1067:
1061:
1059:
1055:
1049:
1046:
1040:
1037:
1031:
1029:
1027:
1023:
1017:
1015:
1011:
1005:
1002:
996:
994:
992:
988:
982:
979:
973:
970:
964:
962:
960:
958:
954:
948:
945:
941:
939:
932:
929:
922:
917:
913:
910:
909:
908:
907:
906:Related lists
900:
895:
892:
887:
883:
881:
877:
876:
874:
871:
870:
869:
866:
856:
853:
852:
850:
847:
844:
841:
838:
835:
832:
829:
828:
827:
825:
817:
814:
811:
808:water-cooled
807:
803:
800:
797:
794:
791:
788:
785:
784:Gross weight:
782:
779:
778:Empty weight:
776:
773:
770:
767:
764:
761:
758:
755:
752:
749:
746:
743:
740:
739:
738:
736:
731:
730:
722:
715:
710:
707:
706:
703:
692:
691:
687:
684:
683:
680:
669:
668:
664:
660:
656:
655:
651:
650:
646:
634:
633:
629:
626:
625:
622:
611:
610:
606:
603:
602:
599:
588:
587:
583:
578:
573:
572:
571:
570:
566:
562:
558:
555:
554:
550:
546:
543:
542:
538:
534:
530:
526:
523:
522:
518:
514:
510:
507:
506:
502:
498:
495:
494:
490:
486:
483:
482:
478:
474:
471:
470:
466:
462:
459:
458:
454:
452:
450:
446:
441:
439:
435:
431:
427:
423:
419:
415:
411:
407:
403:
399:
390:
386:
384:
380:
372:
370:
368:
364:
360:
356:
350:
346:
343:
339:
333:
331:
326:
320:
318:
314:
310:
307:
303:
299:
295:
294:undercarriage
291:
285:
283:
278:
274:
268:
266:
261:
257:
253:
249:
244:
242:
238:
234:
230:
222:
220:
218:
213:
208:
205:
201:
197:
193:
192:
187:
179:
177:
175:
171:
167:
166:maiden flight
163:
159:
155:
151:
150:
144:
142:
138:
134:
130:
120:
115:
114:
109:
108:
104:
101:
100:
96:
93:
92:
88:
86:Introduction
85:
84:
80:
78:First flight
77:
76:
72:
69:
68:
65:
62:
60:Manufacturer
59:
58:
51:
48:
47:
42:
38:
33:
28:
19:
2040:Sesquiplanes
1823:Atlantique 2
1546:
1541:
1536:
1531:
1526:
1327:
1317:
1309:
1300:
1291:
1282:
1273:
1264:
1255:
1248:Bibliography
1235:
1229:
1219:
1213:
1203:
1197:
1187:
1181:
1162:
1156:
1147:
1138:
1129:
1096:
1087:
1078:
1069:
1048:
1039:
1004:
981:
972:
947:
937:
931:
905:
904:
893:
888:for observer
872:
864:
862:
848:
842:
836:
830:
823:
821:
815:
801:
795:
789:
783:
777:
771:
765:
759:
753:
747:
741:
734:
732:
728:
727:
679:Vichy France
662:
658:
652:
567:, two built.
564:
517:Renault 9Fas
512:
444:
442:
418:Maryse Hilsz
413:
410:Henri Robida
395:
382:
379:World War II
376:
351:
347:
334:
321:
290:leading edge
286:
269:
245:
226:
216:
209:
189:
183:
160:, while the
147:
145:
128:
126:
117:Number built
105:
1987:Helicopters
1384:Early types
942:, p. 7
824:Performance
816:Propellers:
802:Powerplant:
460:Breguet 27S
445:Breguet 271
229:sesquiplane
200:sesquiplane
133:sesquiplane
129:Bréguet 270
18:Breguet 270
2024:Categories
1968:Universale
1878:Deux-Ponts
918:References
886:Lewis Guns
810:V12 engine
772:Wing area:
663:Bre.271A.2
659:Bre.270A.2
574:Bre.330.01
508:Bre.272TOE
406:Paul Codos
342:windshield
302:motorcycle
217:Breguet 33
196:Bréguet 19
1994:Gyroplane
1913:Louisette
1908:Leviathan
1868:de Chasse
1828:Bellatrix
1396:Gyroplane
940:June 2002
923:Citations
729:Data from
702:Venezuela
584:Operators
367:silencers
338:parachute
277:duralumin
231:military
212:prototype
170:Venezuela
162:empennage
135:military
121:over 227
70:Designer
1948:Provence
1943:Nymphale
1938:Nautilus
1928:Michelin
1898:Integral
1888:Fauvette
1883:Épaulard
1818:Atlantic
1411:Type III
1378:aircraft
901:See also
865:Armament
455:Variants
451:duties.
422:Calcutta
363:radiator
330:ailerons
258:and the
248:riveting
241:cowlings
158:cockpits
154:fuselage
94:Retired
1933:Mouette
1923:Mercure
1873:Cinzano
1863:Colibri
1853:Choucas
1833:Bizerte
1806:By name
1416:Type IV
1406:Type II
1376:Breguet
766:Height:
748:Length:
565:Bre.27S
556:Bre.330
544:Bre.274
524:Bre.273
496:Bre.272
484:Bre.271
479:engine.
472:Bre.270
467:engine.
449:liaison
414:Joé III
383:Groupes
355:cowling
317:bearing
252:welding
237:bracing
141:Breguet
64:Breguet
1958:Saigon
1953:Sahara
1903:Jaguar
1893:Fulgur
1858:Colmar
1436:Type U
1431:Type G
1426:Type A
1421:Type V
1401:Type I
1301:Avions
1292:Avions
1283:Avions
1274:Avions
1265:Avions
1256:Avions
1236:Avions
1220:Avions
1204:Avions
1188:Avions
1169:
938:Avions
894:Bombs:
837:Range:
699:
676:
645:France
642:
618:
598:Brazil
595:
529:bomber
432:, and
426:Saigon
359:bonnet
325:struts
313:patent
282:struts
223:Design
131:was a
2009:G.111
2004:G.11E
1813:Alizé
873:Guns:
742:Crew:
621:China
434:Tokyo
430:Hanoi
402:Hanoi
398:Paris
298:strut
204:steel
174:China
97:1939
89:1930
49:Role
1963:Taon
1918:Mars
1797:1150
1792:1100
1787:1050
1782:1004
1777:1002
1772:1001
1567:393T
1562:392T
1557:390T
1552:280T
1167:ISBN
804:1 ×
408:and
273:ribs
265:jigs
210:The
172:and
127:The
30:270
1848:BUM
1843:BUC
1838:BLC
1767:960
1762:941
1757:940
1752:906
1747:905
1742:904
1737:902
1732:901
1727:900
1722:895
1717:894
1712:893
1707:892
1702:891
1697:890
1692:792
1687:791
1682:790
1677:765
1672:763
1667:761
1662:731
1657:730
1652:696
1647:695
1642:694
1637:693
1632:691
1627:690
1622:670
1617:610
1612:530
1607:522
1602:521
1597:500
1592:482
1587:470
1582:462
1577:460
1572:410
1547:274
1542:273
1537:271
1532:270
1522:26T
400:to
2026::
1527:27
1517:25
1512:22
1507:21
1502:20
1497:19
1492:17
1487:16
1482:14
1477:12
1472:11
1441:LE
1117:^
1105:^
1057:^
1025:^
1013:^
990:^
956:^
428:,
424:,
284:.
176:.
143:.
1467:6
1462:5
1457:4
1368:e
1361:t
1354:v
1175:.
665:.
511:(
20:)
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