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and dual controls were fitted. The windscreen was split. A large access door was provided on each side of the fuselage, and all fuel was carried in a 250 L (55 imp gal; 66 US gal) tank installed in the wing. After the prototype, no further examples of the type were completed.
176:, the prototype of which was first flown in that year. The S-5 was based on the design of the S-4, and was of all-wooden construction and had side-by-side seating for two persons. The
507:
152:
Société d'Etudes et de
Construction d'Avions de Tourisme (SECAT) had been established in the late 1930s, and in 1938 had built the two-seat, high-wing
133:
522:
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527:
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Roclincourt
Airport. The aircraft was still extant in 1967; however, it was struck off the French civil aircraft register during the 1970s.
438:
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25:
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high-set wing comprised a wooden box-spar, chordwise ribs and a stressed plywood skin. The trailing edge carried
144:. Only one example of the type was ever built, and it flew for a variety of private owners for several decades.
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220:, near Paris. By 1964, it was owned by M. Rene Dupuis, and it was hangared at
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Design work on light aircraft was resumed by SECAT in 1946, resulting in the
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The SECAT S-5 in 1965 showing the unusual design of the split windscreen
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156:, the development of which was interrupted by the hostilities.
416:. Merseyside Society of Aviation Enthusiasts. p. 120.
66:
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four cylinder air cooled piston, 56 kW (75 hp)
134:
291:
250 L (55 imp gal; 66 US gal)
350:
Aircraft of comparable role, configuration, and era
386:. Macdonald & Co (Publishers) Ltd. p. 66.
439:
8:
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316:196 km/h (122 mph, 106 kn)
128:was a light, high-wing, two-seat touring
401:. London: Sampson Low, Marston & Co.
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328:800 km (497 mi, 432 nmi)
322:150 km/h (93 mph, 81 kn)
15:
7:
399:Jane's all the World's Aircraft 1948
132:aircraft, designed and built by the
508:1940s French civil utility aircraft
209:The sole example of the SECAT S-5,
273:2.11 m (6 ft 11 in)
267:8.99 m (29 ft 6 in)
261:6.15 m (20 ft 2 in)
14:
24:
523:Single-engined tractor aircraft
414:French Civil Aircraft Register
340:3.0 m/s (590 ft/min)
216:, was initially operated from
1:
334:3,600 m (11,810 ft)
528:Aircraft first flown in 1946
255:1 passenger or student pilot
285:570 kg (1,257 lb)
544:
397:Bridgman, Leonard (1948).
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384:The Aircraft of the World
279:350 kg (772 lb)
235:The Aircraft of the World
140:shortly after the end of
32:
23:
18:
218:Toussus-le-Noble Airport
35:Toussus-le-Noble Airport
382:Green, William (1965).
240:General characteristics
169:
33:The sole SECAT S-5 at
412:Butler, P.H. (1964).
167:
45:Training and touring
205:Operational history
37:near Paris in 1967
518:High-wing aircraft
454:Aircraft built by
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118:SECAT S-4 Mouette
95:Primary user
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332:Service ceiling:
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47:Type of aircraft
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98:private pilots
54:National origin
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314:Maximum speed:
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228:Specifications
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198:semi-monocoque
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114:Developed from
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320:Cruise speed:
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283:Gross weight:
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277:Empty weight:
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196:was a wooden
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87:Introduction
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79:First flight
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74:Rémy Goucher
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63:Manufacturer
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299:Regnier 4D.2
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142:World War II
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104:Number built
307:Performance
295:Powerplant:
154:S-4 Mouette
148:Development
502:Categories
364:References
211:registered
182:elliptical
178:cantilever
19:SECAT S-5
356:Piper J-3
265:Wingspan:
253:Capacity:
233:Data from
174:SECAT S-5
130:monoplane
126:SECAT S-5
71:Designer
345:See also
194:fuselage
186:ailerons
271:Height:
259:Length:
58:France
326:Range:
214:F-PIIC
192:. The
160:Design
138:France
487:RG-75
482:RG-60
456:SECAT
247:Crew:
222:Arras
190:flaps
90:1946
82:1946
42:Role
297:1 ×
188:and
124:The
477:S-5
472:S-4
136:in
504::
467:VI
372:^
180:,
108:1
447:e
440:t
433:v
249:1
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