26:
180:
and tail unit have a fabric covered steel tube structure, with the open cockpit positioned just behind the swept upper wing trailing edge which has a rounded cut-out for upward visibility. There is a long and prominent faired headrest behind the cockpit, on top of the curved upper fuselage surface.
224:
Starduster plans remain available more than 50 years after the first flight and homebuilding building continues. A Starduster register currently shows 27 SA-100 Stardusters and 3 SA-101 Super
Stardusters built and building. The FAA register shows 64 SA-100s and 1 SA-101, though not all are assigned
212:. The mainwheels are mounted on V-struts hinged from the lower fuselage longeron, with rubber shock absorbers on diagonal extension struts between wheel and a short, central, under fuselage V-form mounting bracket. The main legs are often partially or completely faired and the wheels enclosed in
204:
The
Starduster has a recommended power range of 125 to 160 hp (93 to 119 kW) and is usually powered by a four-cylinder, horizontally opposed, 125 hp (93 kW)
66:
165:
join the upper wing to the fuselage, basically two pairs in N-form but with the forward strut doubled. The lower wing is unswept and has 1.5° of
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730:
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740:
142:
126:
70:
154:
421:
639:
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The SA-100 Starduster was designed by Louis A. Stolp and George M. Adams as a light sports aircraft for
321:
237:
Original version, designed for non-aerobatic flight. Although many have proven stress to +6g -4G and a
209:
146:
720:
632:
169:; the upper wing has 6° of sweep on its leading edge, no dihedral and a greater span. There are
576:
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166:
208:, though more powerful engines of up to 200 hp (150 kW) have been fitted. It has a
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150:
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250:
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25:
8:
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34:
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129:. Though the first flight was in 1957, Stardusters continue to be built and flown.
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426:
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198:
360:
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engine to produce a maximum speed of over 170 mph (275 km/h).
182:
363:
4-cylinder horizontally opposed air cooled, 125 hp (93 kW)
177:
624:
330:
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170:
118:
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The
Starduster has a conventional tail unit, with a wire braced
190:
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Larger and more powerful — uses the longer wings of the
162:
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and no dihedral, together with a 180 hp (134 kW)
225:
and some further
Stardusters appear without a type number.
238:
186:
273:
Jane's All the World's
Aircraft 1966/7, p.331, Aerofiles
454:, page 121. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
416:
Aircraft of comparable role, configuration, and era
33:Stolp-Adams Starduster, amateur-built in 1966, at
193:, the latter extending to the keel between split
712:
153:wings, each pair braced by a single, wide chord
640:
477:. London: Sampson Low, Marston & Co. Ltd.
571:, page 128. Flying Pages Europe SARL, 2015.
452:World Directory of Leisure Aviation 2011–12
647:
633:
265:
569:World Directory of Light Aviation 2015–16
450:Bayerl, Robby; Martin Berkemeier; et al:
394:130 mph (210 km/h, 110 kn)
388:148 mph (238 km/h, 129 kn)
132:
468:
466:
464:
462:
460:
446:
444:
475:Jane's All the World's Aircraft 1966–67
406:400 mi (640 km, 350 nmi)
173:on the lower wings only, but no flaps.
713:
581:
521:
501:
481:
472:
400:55 mph (89 km/h, 48 kn)
219:
628:
561:
457:
441:
601:
317:110.0 sq ft (10.22 m)
210:conventional tailwheel undercarriage
567:Tacke, Willi; Marino Boric; et al:
185:and straight tapered, round topped
161:. A total of eight centre section
81:Louis A. Stolp and George M. Adams
13:
726:1950s United States sport aircraft
654:
541:
305:18 ft 0 in (5.49 m)
299:19 ft 0 in (5.79 m)
293:16 ft 6 in (5.03 m)
127:Aircraft Spruce & Specialty Co
71:Aircraft Spruce & Specialty Co
14:
752:
311:6 ft 0 in (1.83 m)
197:. Both rudder and elevators are
117:is an American single-seat sport
24:
731:Single-engined tractor aircraft
1:
434:
246:SA-101 Stolp Super Starduster
115:Stolp-Adams SA-100 Starduster
741:Aircraft first flown in 1957
353:20 Imp gal (24 US gal, 91 L)
253:, which have a symmetric M6
7:
410:
347:1,247 lb (566 kg)
228:
10:
757:
422:D'Apuzzo Senior Aero Sport
45:Single seat sport aircraft
660:
473:Taylor, John W R (1966).
341:700 lb (318 kg)
32:
23:
18:
589:"SA101 Super Starduster"
675:SA-101 Super Starduster
278:General characteristics
266:Specifications (SA-100)
97:Plans available (2012)
489:"Starduster One SA100"
133:Design and development
37:, California, in 1971
695:SA-750 Acroduster Too
680:SA-300 Starduster Too
529:"Starduster registry"
141:from plans. It is a
251:CA300 Starduster Too
106:Stolp Starduster Too
690:SA-700 Acroduster I
662:Fixed wing aircraft
509:"Kits – Starduster"
373:M74DM61 fixed pitch
345:Max takeoff weight:
259:Lycoming I0-360-A1A
220:Operational history
361:Lycoming O-290-D-1
206:Lycoming O-290-D-1
143:single bay biplane
35:Long Beach Airport
708:
707:
670:SA-100 Starduster
609:"Aerofiles-Stolp"
234:SA-100 Starduster
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427:Shober Willie II
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155:interplane strut
149:, wooden framed
123:built from plans
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47:Type of aircraft
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303:Lower wingspan:
297:Upper wingspan:
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121:designed to be
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54:National origin
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721:Stolp aircraft
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549:"FAA register"
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386:Maximum speed:
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351:Fuel capacity:
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147:fabric covered
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89:November 1957
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67:Stolp Aircraft
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58:United States
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700:SA-900 V-Star
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392:Cruise speed:
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339:Empty weight:
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159:bracing wires
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86:First flight
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63:Manufacturer
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612:. Retrieved
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592:. Retrieved
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552:. Retrieved
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532:. Retrieved
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512:. Retrieved
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492:. Retrieved
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398:Stall speed:
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322:Aspect ratio
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139:homebuilding
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125:supplied by
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379:Performance
367:Propellers:
357:Powerplant:
19:Starduster
715:Categories
614:2011-05-11
594:2011-05-12
554:2011-05-12
534:2011-05-12
514:2011-05-12
494:2011-05-12
435:References
315:Wing area:
577:1368-485X
371:Sensenich
369:2-bladed
335:NACA 4412
285:Capacity:
271:Data from
241:of 185 kn
195:elevators
183:tailplane
157:aided by
151:staggered
102:Variants
78:Designer
736:Biplanes
411:See also
229:Variants
178:fuselage
171:ailerons
167:dihedral
331:Airfoil
309:Height:
291:Length:
255:airfoil
119:biplane
94:Status
575:
404:Range:
191:rudder
163:struts
214:spats
145:with
42:Role
573:ISSN
359:1 ×
326:6.33
189:and
176:The
113:The
239:Vne
187:fin
717::
459:^
443:^
216:.
201:.
73:.
648:e
641:t
634:v
617:.
597:.
557:.
537:.
517:.
497:.
333::
324::
287:1
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