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being l.lm (3.6 ft.) wide by 1.8 m (5.9 ft.) high, its base being very near to the ground, which eased access. It was often comfortably furnished, being occupied by eight seats in a standard configuration. The sides of the cabin were lined with large windows that permitted the passengers to have an unobstructed view of the landscape below. Passengers were able to regulate the climate of the cabin, somewhat, via the use of a series of trap doors, the opening and closing of which altering the rate of aeration; other passenger convenience features included a hot-water heating system. The
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125:. During the early 1920s, there was a strong preference amongst operators for single-engine airliners. Since even multi-engine aircraft could not keep flying in the (likely) event of a mid-flight engine failure, it was considered that a single engine offered just as much security while offering a greater ease of maintenance. At the time, Farman's engines were held in high regard, having demonstrated their endurance with multiple record-breaking flights (during 145, one aircraft equipped with a Farman engine was able to fly continuously for 45 hours.
155:. It possessed relatively favourable flight qualities, particularly in terms of its range of speed and manoeuvrability, while contributed to overall safety. The aircraft was also relatively durable for the era, in part due to its materials having been carefully selected; extensive measures were taken to protect against fire hazards, including the isolation of engine components, the positioning of the fuel tanks, the adoption of a metal engine bed, the provision of
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been operated at a moderate speed while the excess power capacity of the engine remained available to the pilot for occasional use, such as when the aircraft was flying close to the ground. While carrying 370 kg (816 lb.) of fuel and a payload of 850 kg, it was capable of flying non-stop for up to five hours, traversing roughly 900 km (560 miles) during this time.
193:
unit located at the read of the fuselage; this permitted a cleaner shaped engine hood. For ease of inspection and maintenance, the engine hood could be quickly removed in its entirety. To start the engine, an electric starter could be used by the pilot at any moment. Typically, the engine would have
128:
Farman's design team prioritised the achievement of a high level of flight efficiency, which would permit the aircraft to travel at relatively high speeds while carrying heavy payloads while requiring the minimal amount of engine power and fuel capacity. Furthermore, the F.170 was designed to be as
166:
The forward section of the fuselage's interior contains the engine bay and the cockpit; the pilot being fully insulated from both the engine and the passenger cabin, even being provided with a separate door for exiting and entering the aircraft. The main cabin was relatively spacious for the era,
205:
that were indirectly secured to the base of the fuselage. This wing, which was integrated into the top of the fuselage, had a perfectly rectangular shape and a uniform cross-section; this latter attribute eased construction as it permitted the use of uniform
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The F.170 could carry up to eight passengers and had a somewhat ungainly appearance. Since the aircraft was quite low on its wheels, it was often derisively called the
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136:, which was introduced in 1927, incorporated some metal construction and could carry up to nine passengers. The F.171bis was joined by the one and only
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was used. The main legs were located between the wing struts at the outer portions of the small plane secured to the base of the fuselage; both the
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that were actuated via a series of externally-ran wooden horns. The wing was primarily composed of wood which the covering was
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159:, and rapid draining facilities. To minimise noise within the aircraft, particularly the passenger cabin, two lengthy
296:(SGTA) from May 1926 and used on the Paris-Cologne-Berlin route. When the SGTA was incorporated in the newly created
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722:"Farman Monoplane F.170 : Commercial Airplane with One 500 HP. Farman Engine."
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A long-range derivative developed for a crossing of the North
Atlantic, one built.
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9-passenger airliner; an F.170 incorporating some metal construction, four built.
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was located directly behind the cabin; it was accessed via a separate door.
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709:. Collection Docavia. Vol. 21. Paris, France: Éditions Larivière.
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665:. London: Sampson Low, Marston & company, ltd. pp. 18d–19d.
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airline on 7 October 1933, some five F.170 were still being used.
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An 8-passenger sesquiplane powered by a 370 kW (500 hp)
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344:
Farman F.170 3 view drawing from NACA Aircraft
Circular No.12
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across its entire length. It was furnished with unbalanced
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The F.170 Jabiru was a single-engine evolution of the 1923
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W-12 water-cooled piston engine, 370 kW (500 hp)
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economic as possible from an operational perspective.
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197:The F.170 had a semi-thick wing, which was rigidly
90:designed and built by the French aircraft company
678:Histoire mondiale des avions de ligne depuis 1908
186:propeller. Unusually, cooling was achieved via a
290:The F.170 and F.170bis were used exclusively by
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8:
148:The Farman F.170 Jabiru was a single-engine
726:National Advisory Committee for Aeronautics
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471:2,000 m (6,600 ft) in 15 minutes
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453:180 km/h (110 mph, 97 kn)
222:was equipped with a two-part unbalanced
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459:500 km (310 mi, 270 nmi)
330:Société Générale des Transports Aériens
293:Société Générale des Transports Aériens
729:, 1 August 1926. NACA-AC-12, 93R18272.
680:. Boulogne-Billancourt, France: ETAI.
163:extended to the rear of the aircraft.
15:
486:0.1174 kW/kg (0.0714 hp/lb)
432:4-bladed wooden fixed-pitch propeller
356:Histoire Mondiale des Avions de Ligne
7:
663:Jane's all the World's Aircraft 1928
477:61 kg/m (12 lb/sq ft)
352:Jane's all the World's Aircraft 1928
392:16.1 m (52 ft 10 in)
386:11.75 m (38 ft 7 in)
14:
638:Parmentier, Bruno (30 May 1999).
615:Parmentier, Bruno (30 May 1999).
592:Parmentier, Bruno (30 May 1999).
404:52.5 m (565 sq ft)
398:3.2 m (10 ft 6 in)
174:The F.170 is powered by a single
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24:
1349:Single-engined tractor aircraft
1:
465:4,500 m (14,800 ft)
416:3,200 kg (7,055 lb)
410:1,800 kg (3,968 lb)
253:of the vertical stabiliser.
94:. It is a derivative of the
105:(belly to the ground). The
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741:"The Paris Aero Show 1926"
201:using a series of oblique
676:Pelletier, Alain (1908).
23:
18:
661:Grey, C.G., ed. (1928).
359:Aviafrance: Farman F-170
365:General characteristics
1339:1920s French airliners
749:: 779. 2 December 1926
345:
336:Specifications (F.170)
955:Farman Aviation Works
343:
92:Farman Aviation Works
705:Liron, Jean (1984).
109:took place in 1925.
83:was a single-engine
579:NACA 1926, pp. 2-3.
567:NACA 1926, pp. 1-2.
558:NACA 1926, pp. 3-4.
286:Operational history
169:baggage compartment
81:Farman F.170 Jabiru
1033:F.50 (Flying Boat)
642:(in French). Paris
619:(in French). Paris
596:(in French). Paris
346:
233:A relatively wide
157:fire extinguishers
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707:Les avions Farman
687:978-2-7268-9367-8
617:"Farman F-170bis"
469:Time to altitude:
269:engine, 13 built.
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1028:F.50 (Landplane)
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734:External links
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640:"Farman F-171"
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594:"Farman F-170"
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132:The improved
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52:First flight
51:
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44:Manufacturer
43:
42:
35:
32:
31:
27:
22:
19:F.170 Jabiru
17:
1344:Sesquiplanes
1163:F.200 (1923)
1147:
1098:F.121 Jabiru
1058:F.63 Goliath
1053:F.60 Goliath
802:Henri Farman
751:. Retrieved
744:
724:
706:
699:Bibliography
677:
671:
662:
656:
644:. Retrieved
633:
621:. Retrieved
610:
598:. Retrieved
563:
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480:
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424:Farman 12 We
419:
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267:Farman 12 We
251:leading edge
232:
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176:Farman 12 We
173:
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147:
137:
133:
131:
127:
116:
102:
100:
96:F.121 Jabiru
80:
78:
69:Number built
1063:FF.65 Sport
646:20 February
623:20 February
600:20 February
438:Performance
430:Propellers:
420:Powerplant:
247:streamlined
150:sesquiplane
113:Development
85:sesquiplane
1333:Categories
491:References
482:Power/mass
402:Wing area:
325:Air France
298:Air France
63:1925-1929
1068:Moustique
390:Wingspan:
378:Capacity:
349:Data from
304:Operators
220:empennage
188:honeycomb
60:Produced
795:aircraft
753:11 March
715:37146471
272:F.170bis
257:Variants
224:elevator
212:ailerons
191:radiator
153:airliner
134:F.170bis
88:airliner
36:airliner
396:Height:
384:Length:
184:tractor
47:Farman
1318:F.1020
1313:F.1010
1308:F.1000
900:HF.206
793:Farman
746:Flight
713:
684:
457:Range:
318:France
315:
228:rudder
218:. The
216:fabric
203:struts
199:braced
144:Design
1303:F.520
1298:F.510
1293:F.500
1288:F.480
1283:F.470
1278:F.460
1273:F.455
1268:F.450
1263:F.430
1258:F.420
1253:F.410
1248:F.400
1243:F.390
1238:F.380
1233:F.370
1228:F.360
1223:F.350
1218:F.310
1213:F.300
1208:F.290
1203:F.280
1198:F.270
1193:F.250
1188:F.230
1183:F.220
1178:F.211
1173:F.209
1168:F.200
1158:F.190
1153:F.180
1148:F.170
1143:F.169
1138:F.168
1133:F.167
1128:F.166
1123:F.162
1118:F.160
1113:F.150
1108:F.140
1103:F.130
1093:F.120
1088:F.110
943:MF.16
938:MF.11
895:HF.36
890:HF.35
885:HF.33
880:HF.31
875:HF.30
870:HF.27
865:HF.26
860:HF.24
855:HF.23
850:HF.22
845:HF.21
840:HF.20
835:HF.19
830:HF.16
825:HF.14
820:HF.10
372:Crew:
278:F.171
262:F.170
245:were
239:axles
138:F.171
123:F.121
55:1925
33:Role
1083:F.80
1078:F.73
1073:F.70
1048:F.60
1043:F.56
1038:F.51
1023:F.41
1018:F.40
1013:F.31
1008:F.30
1003:F.21
998:F.4X
993:F.3X
988:BN.4
933:MF.9
928:MF.8
923:MF.7
918:MF.6
815:HF.7
810:HF.6
755:2008
711:OCLC
682:ISBN
648:2018
625:2018
602:2018
422:1 ×
241:and
208:ribs
119:F.3X
79:The
983:B.2
978:A.2
973:III
73:18
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