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aircraft, the Anjou's fabric-over-tube construction was something of an anachronism, and all development was soon ceased. Plans to develop a stretched version with three extra seats and
238:
450 L (118.9 US gal; 99.0 imp gal) in two wing tanks + 2x 100 L (26.4 US gal; 22.0 imp gal) optional wing-tip tanks
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42:
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engines, but found that they could not sell it either. At a time when the twin-engine light plane market was already dominated by
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98:. Intended by Boisavia as a touring aircraft, it did not find a market and only the single
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4-cylinder air-cooled inverted in-line piston engines, 130 kW (170 hp) each
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107:
622:
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378:. London: Jane's All the World's Aircraft Publishing Co. Ltd. p. 143.
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0.833 m/s (3 ft/s) on one engine at 1,500 m (4,900 ft)
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405:. London: Bright Star Publishing. pp. File 890 Sheet 73.
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was constructed. At this point, the firm sold the design to
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of conventional configuration with retractable tricycle
414:. Shrewsbury: Airlife Publishing. pp. 370, 408–09.
299:
240 km/h (150 mph, 130 kn) (economical)
106:, which modified the design and re-engined it with
620:
536:Société Industrielle Pour l’Aéronautique (SIPA)
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311:1,500 km (930 mi, 810 nmi)
293:300 km/h (190 mph, 160 kn)
157:
373:
367:
153:- Planned seven-seat version (not built)
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397:. London: Studio Editions. p. 192.
376:Jane's All the World's Aircraft 1958-59
166:Jane's All the World's Aircraft 1958-59
621:
392:
305:90 km/h (56 mph, 49 kn)
508:
465:
439:
659:Twin piston-engined tractor aircraft
639:1950s French civil utility aircraft
13:
386:
14:
670:
634:Abandoned civil aircraft projects
419:
211:21.5 m (231 sq ft)
193:7.2 m (23 ft 7 in)
403:World Aircraft Information Files
199:13 m (42 ft 8 in)
87:in the 1950s. It was a low-wing
75:(later developed by SIPA as the
395:Jane's Encyclopedia of Aviation
374:Bridgman, Leonard, ed. (1957).
323:6 m/s (1,200 ft/min)
278:2-bladed fixed-pitch propellers
205:3 m (9 ft 10 in)
393:Taylor, Michael J. H. (1989).
1:
360:
317:6,800 m (22,300 ft)
232:2,000 kg (4,409 lb)
226:1,300 kg (2,866 lb)
121:engines were also abandoned.
654:Aircraft first flown in 1956
83:light aircraft developed in
7:
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10:
675:
412:Airlife's General Aviation
133:- Boisavia prototype with
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18:
356:150 m (490 ft)
350:160 m (520 ft)
410:Simpson, R. W. (1995).
172:General characteristics
143:- SIPA conversion with
79:) was a four-seat twin-
158:Specifications (B.260)
27:Civil utility aircraft
147:engines (1 converted)
246:SNECMA Régnier 4L-02
73:Boisavia B.260 Anjou
431:luftfahrt-archiv.de
649:Low-wing aircraft
629:Boisavia aircraft
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137:engines (1 built)
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315:Service ceiling:
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29:Type of aircraft
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387:Further reading
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264:licence-built )
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420:External links
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321:Rate of climb:
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291:Maximum speed:
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145:Lycoming O-360
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108:Lycoming O-360
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644:SIPA aircraft
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583:S.200 Minijet
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484:B.60 Mercurey
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479:B.50 Muscadet
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348:Take-off run:
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297:Cruise speed:
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96:undercarriage
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77:Sipavia Anjou
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49:First flight
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35:Manufacturer
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489:B.80 Chablis
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354:Landing run:
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216:Aspect ratio
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61:Number built
19:B.260 Anjou
593:S.261 Anjou
494:B.260 Anjou
284:Performance
276:Propellers:
242:Powerplant:
623:Categories
361:References
209:Wing area:
135:Regnier 4L
89:cantilever
197:Wingspan:
185:Capacity:
163:Data from
112:all-metal
100:prototype
92:monoplane
538:aircraft
469:aircraft
467:Boisavia
125:Variants
119:Potez 4D
115:American
39:Boisavia
203:Height:
191:Length:
52:2 June
608:S.1100
603:S.1000
309:Range:
262:SNECMA
85:France
81:engine
598:S.300
187:3 pax
179:Crew:
151:S.262
141:S.261
131:B.260
24:Role
578:S.90
573:S.70
568:S.50
563:S.20
558:S.12
553:S.11
548:S.10
244:2 ×
104:SIPA
71:The
54:1956
43:SIPA
220:7.6
625::
65:1
41:,
528:e
521:t
514:v
459:e
452:t
445:v
260:(
218::
181:1
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