311:
358:
26:
126:
290:
and three-blade propellers. Though these engines had a smaller displacement than the earlier 9Ks and consequently a lower power output, they were more compact with a diameter of 0.950 m (37.4 in) compared with 1.306 m (51.4 in), reducing the engine frontal area by 47%. The
199:
covered. The observer could also access a long, rectangularly framed, largely transparent, ventral observation structure. The rear fuselage section was also spruce-framed but internally wire-braced and fabric-covered. A rear-facing glazed enclosure over the wing
204:
held the rear gunner/radio operator. A transverse metal structure within the fuselage connected it to the two pairs of wing struts. There was another metal frame aft for mounting the
302:, was further aerodynamically cleaned and speeded, chiefly by the removal of the ventral gondola. It first flew on 28 June 1939. Two were completed but no production order was won.
187:
The fuselage consisted of two sections, both rounded in cross-section. The forward part, including the enclosed cockpit where the pilot was seated forward of the wing
1366:
969:
133:
The Société Nationale de
Constructions Aéronautique du Centre (SNCAC) was formed via 1936 legislation in February 1937 as a nationalised merging of the
711:
1346:
1361:
689:
547:
1351:
962:
164:. Between the engines and fuselage the wing was rectangular in plan and externally braced; the outboard panels were tapered
704:
1356:
921:
900:
310:
237:
153:
110:
41:
955:
177:
282:. By December that year it was on display at the Paris Aero Salon with 14-cylinder 680 hp (507 kW)
1341:
1285:
1260:
1240:
697:
141:
companies, in whose design offices several SNCAC types began. Thus the NC.510 was often referred to as the
106:
1265:
1255:
993:
1003:
998:
931:
916:
890:
885:
745:
590:
487:
651:
672:
610:
595:
279:
117:, built in the late 1930s. Three were built and refined but production orders were not forthcoming.
1270:
1250:
1028:
221:
209:
1023:
1013:
176:
and skinning. Outboard their construction was mixed, with wooden ribs and a mixture of metal and
926:
825:
820:
815:
336:
283:
1209:
865:
543:
431:
348:
Modified fuselage without ventral pod; engines as NC.510M. First flew 28 June 1939. Two built.
323:
271:
157:
114:
45:
291:
cleaned-up version first flew with its new engines on 14 January 1939 and was designated the
260:
252:
208:, a braced wooden structure mounted on top of the fuselage. The tailplane had significant
229:
181:
169:
936:
810:
805:
800:
267:
in addition to a mixture of handheld and remotely operated cameras for reconnaissance.
244:
357:
1335:
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895:
860:
795:
765:
760:
750:
740:
735:
188:
1008:
855:
850:
845:
840:
835:
830:
509:
270:
The NC.510 first flew on 20 June 1938, powered by two 574 kW (770 hp)
256:
247:
legs attached to the forward wing spar just inside the engines, braced with a
241:
165:
205:
161:
263:
and the ventral positions. There were racks for flares and for phosphorus
233:
978:
196:
138:
225:
217:
192:
134:
103:
60:
947:
25:
721:
Société Nationale de
Constructions Aéronautiques du Centre (SNCAC)
720:
309:
248:
125:
124:
71:
264:
951:
693:
459:
350 km/h (220 mph, 190 kn) at 3,000 m (9,840 ft)
438:, 570 kW (770 hp) each , rated at 3,000 m (9,840 ft)
255:, and there was a sprung tail skid. The aircraft carried three
213:
191:
and an observer, provided with dual controls, behind him, was
173:
599:. Vol. XXXV, no. 1579. 30 March 1939. p. 1138.
259:, one fixed in the nose and one moveable in each of the rear
1219:
Lorraine-Hanriot 1930-33, Hanriot 1933-37 and SNCAC 1937-40
70:
251:
to the rear spar. Legs and wheels were enclosed in
1218:
1037:
986:
909:
728:
512:, one in each of nose, dorsal and ventral positions
228:were fabric-covered with mass and aerodynamically
172:and the centre section was all metal, with metal
220:. Its fixed surfaces were plywood-covered; the
542:. London: David & Charles. pp. 102c.
342:. NC.510 modified, first flew 14 January 1939.
314:Hanriot NC.530 photo from L'Aerophile May 1940
963:
705:
368:Jane's All the World's Aircraft 1938 p.113-4c
8:
129:NC.510M at the December 1938 Paris Aero Show
970:
956:
948:
712:
698:
690:
567:
565:
563:
561:
559:
465:1,350 km (840 mi, 730 nmi)
168:. The wings were built around two metal
646:
644:
642:
585:
583:
356:
530:
278:driving two-blade, wooden, fixed-pitch
987:Pre-1916, including some Ponnier types
335:14-cylinder 680 hp (507 kW)
322:9-cylinder, 770 hp (574 kW)
15:
483:118 kg/m (24 lb/sq ft)
471:7,000 m (23,000 ft) service
7:
1367:Twin piston-engined tractor aircraft
633:Jane's All the World's Aircraft 1938
574:Jane's All the World's Aircraft 1938
540:Jane's All the World's Aircraft 1938
394:15.00 m (49 ft 3 in)
388:10.12 m (33 ft 2 in)
14:
406:13.5 m (145 sq ft)
400:2.91 m (9 ft 7 in)
24:
1347:1930s French military aircraft
1:
418:3,720 kg (8,201 lb)
412:2,757 kg (6,078 lb)
1362:Aircraft first flown in 1938
444:2-bladed fixed pitch, wooden
361:3-views of the SNCAC NC.510.
152:The NC.510 was designed for
477:6 min to 3,000 m (9,840 ft)
424:480 kg (1,058 lb)
236:. The NC.510 had a fixed,
1383:
518:racks for bombs and flares
238:conventional undercarriage
591:"Army Co-operation Types"
32:
23:
18:
1038:Hanriot (Dupont) 1916-30
160:. It was a twin-engined
156:work and as an advanced
373:General characteristics
353:Specifications (NC.510)
1352:French patrol aircraft
492:300 W/kg (0.182 hp/lb)
362:
315:
212:and carried twin oval
130:
121:Design and development
360:
313:
298:A final version, the
128:
652:"S.N.C.A.C. NC-510M"
673:"S.N.C.A.C. NC-530"
611:"S.N.C.A.C. NC-510"
538:Grey, C.G. (1972).
232:. The rudders had
576:. pp. 113–4c.
436:air-cooled radials
363:
316:
276:air-cooled radials
162:mid-wing monoplane
131:
102:was a twin-engine
1357:Mid-wing aircraft
1329:
1328:
945:
944:
723:(Centre) aircraft
635:. pp. 43–4d.
475:Time to altitude:
158:training aircraft
154:army co-operation
115:training aircraft
111:army co-operation
96:
95:
46:training aircraft
42:army co-operation
1374:
972:
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707:
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601:
600:
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578:
577:
569:
554:
553:
535:
500:
469:Service ceiling:
452:
432:Gnome-Rhône 9Kfr
375:
324:Gnome-Rhône 9Kfr
272:Gnome-Rhône 9Kfr
89:
57:
49:Type of aircraft
28:
16:
1382:
1381:
1377:
1376:
1375:
1373:
1372:
1371:
1332:
1331:
1330:
1325:
1214:
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994:1909 monoplanes
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976:
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718:
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571:
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537:
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532:
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496:
448:
371:
355:
337:Gnome-Rhône 14M
308:
284:Gnome-Rhône 14M
240:with vertical,
178:fabric covering
123:
87:
56:National origin
55:
50:
12:
11:
5:
1380:
1378:
1370:
1369:
1364:
1359:
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1342:SNCAC aircraft
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519:
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466:
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457:Maximum speed:
446:
445:
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425:
422:Fuel capacity:
419:
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407:
401:
395:
389:
383:
354:
351:
350:
349:
346:
343:
340:radial engines
333:
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327:radial engines
320:
307:
304:
288:radial engines
245:shock absorber
147:Hanriot NC.510
122:
119:
107:reconnaissance
94:
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511:
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491:
489:
485:
482:
481:Wing loading:
479:
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461:
458:
455:
454:
453:
451:
443:
440:
437:
433:
429:
426:
423:
420:
417:
416:Gross weight:
414:
411:
410:Empty weight:
408:
405:
402:
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387:
384:
381:
378:
377:
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374:
369:
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231:
227:
223:
219:
215:
211:
207:
203:
202:trailing edge
198:
194:
190:
185:
184:were fitted.
183:
179:
175:
171:
167:
163:
159:
155:
150:
148:
144:
140:
136:
127:
120:
118:
116:
112:
108:
105:
101:
91:
86:
85:
82:20 June 1938
81:
79:First flight
78:
77:
73:
69:
67:Manufacturer
66:
65:
62:
59:
54:
53:
47:
43:
40:
37:
36:
31:
27:
22:
19:SNCAC NC.510
17:
1320:
927:Chardonneret
790:
785:
676:. Retrieved
667:
655:. Retrieved
632:
626:
614:. Retrieved
605:
594:
573:
549:0715-35734-4
539:
533:
521:
515:
510:machine guns
505:
497:
495:
486:
480:
474:
468:
462:
456:
449:
447:
441:
427:
421:
415:
409:
403:
397:
391:
385:
379:
372:
370:
365:
364:
299:
297:
292:
269:
257:machine guns
189:leading edge
186:
151:
146:
142:
132:
113:or advanced
100:SNCAC NC.510
99:
97:
88:Number built
44:or advanced
450:Performance
442:Propellers:
434:9-cylinder
428:Powerplant:
329:. One only.
286:double-row
274:9-cylinder
195:framed and
182:Split flaps
166:cantilevers
143:Hanriot 510
1336:Categories
1004:1911 types
999:1910 types
525:References
488:Power/mass
404:Wing area:
280:propellers
922:Belphégor
729:by number
392:Wingspan:
366:Data from
234:trim tabs
222:elevators
206:empennage
981:aircraft
937:Martinet
932:Cormoran
498:Armament
306:Variants
253:fairings
230:balances
210:dihedral
979:Hanriot
917:Abeille
910:by name
901:NC.3021
886:NC.2001
881:NC 1080
876:NC.1071
871:NC.1070
781:NC.47-2
776:NC.47-1
771:NC.47-0
756:NC.4-10
398:Height:
386:Length:
332:NC.510M
293:NC.510M
226:rudders
218:rudders
197:plywood
139:Hanriot
33:NC.510
1291:LH.161
1241:LH.21S
896:NC.271
891:NC 211
866:NC.900
861:NC.860
856:NC.856
851:NC.855
846:NC.854
841:NC.853
836:NC.851
831:NC.850
826:NC.841
821:NC.840
816:NC.832
811:NC.702
806:NC.701
801:NC.700
796:NC.600
791:NC.530
786:NC.510
766:NC.433
761:NC.420
751:NC.223
746:NC.211
741:NC.150
736:NC.130
678:26 May
657:26 May
631:Grey.
616:26 May
596:Flight
572:Grey.
546:
516:Bombs:
463:Range:
345:NC.530
319:NC.510
300:NC.530
261:dorsal
193:spruce
135:Farman
104:French
61:France
1321:H.510
1316:H.230
1311:H.220
1306:H.190
1301:H.180
1296:H.170
1286:H.130
1281:H.115
1276:H.110
1271:LH.80
1266:LH.70
1261:LH.60
1256:LH.41
1251:LH.40
1246:LH.30
1236:LH.16
1231:LH.12
1226:LH.10
1195:HD.40
1165:HD.32
1150:HD.28
1145:HD.27
1130:HD.24
1125:HD.22
1120:HD.20
1115:HD.19
1110:HD.18
1105:HD.17
1100:HD.15
1095:HD.14
1090:HD.12
1029:D.VII
1019:D.III
506:Guns:
382:Three
380:Crew:
265:bombs
249:strut
170:spars
72:SNCAC
38:Role
1210:H.46
1205:H.43
1200:H.41
1190:H.38
1185:H.36
1180:H.35
1175:H.34
1170:H.33
1160:H.31
1155:H.29
1140:H.26
1135:H.25
1085:HD.9
1080:HD.8
1075:HD.7
1070:HD.6
1065:HD.5
1060:HD.4
1055:HD.3
1050:HD.2
1045:HD.1
1024:D.IV
1014:D.II
680:2013
659:2013
618:2013
544:ISBN
430:2 ×
242:oleo
224:and
216:and
214:fins
174:ribs
137:and
98:The
1009:D.I
145:or
1338::
641:^
593:.
582:^
558:^
508:3
295:.
180:.
149:.
109:,
92:3
74:)
971:e
964:t
957:v
713:e
706:t
699:v
682:.
661:.
620:.
552:.
490::
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