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The aircraft was to have a typical empty weight of 1,250 lb (570 kg) and a gross weight of 2,250 lb (1,020 kg), giving a useful load of 1,000 lb (450 kg). With full fuel of 60 U.S. gallons (230 L; 50 imp gal) the payload for the pilot, passengers and
172:
and feature a wing area of 135 sq ft (12.5 m). The cabin width was to be 43 in (110 cm), accessed via swing-up doors 53 in (135 cm) in width. The acceptable power range was to be 160 to 210 hp (119 to 157 kW) and the standard engines used are the
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The standard day, sea level, no wind, take off with a 210 hp (157 kW) engine was to be 425 ft (130 m) and the landing roll is 300 ft (91 m).
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133:, introduced in the mid-1990s. The aircraft was planned to be supplied as a kit for amateur construction.
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The manufacturer estimated the construction time from the supplied kit would be 1400 hours.
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sheet. Its 31.0 ft (9.4 m) span wing was to mount almost full span
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powerplant. Kit options included a heater, upholstery, cargo tie-downs and
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The
Freedom 210 STOL was to be a follow-on design to the single-seat
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that was designed by Neal H. Brutsche and intended to be produced by
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AeroCrafter - Homebuilt
Aircraft Sourcebook, Fifth Edition
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By 1998 the company reported that kits were available.
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311:60 U.S. gallons (230 L; 50 imp gal)
359:49 mph (79 km/h, 43 kn) flaps down
233:engine and a length of 24.08 ft (7.3 m)
243:engine and a length of 24.5 ft (7.5 m)
421:, page 346. BAI Communications, 15 July 1998.
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365:1,290 mi (2,080 km, 1,120 nmi)
192:baggage was to be 640 lb (290 kg).
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217:and it is likely that none were completed.
576:1990s United States civil utility aircraft
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353:195 mph (314 km/h, 169 kn)
347:207 mph (333 km/h, 180 kn)
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239:Version with 210 hp (157 kW)
229:Version with 180 hp (134 kW)
209:Since April 2015 no examples have been
383:16.7 lb/sq ft (82 kg/m)
26:
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149:, a four-seat enclosed cabin, fixed
287:31 ft 0 in (9.45 m)
281:24 ft 6 in (7.47 m)
25:
293:135 sq ft (12.5 m)
248:Specifications (Freedom 210 STOL)
177:or the 210 hp (157 kW)
164:The aircraft was to be made from
377:1,630 ft/min (8.3 m/s)
35:
581:Single-engined tractor aircraft
471:Federal Aviation Administration
215:Federal Aviation Administration
475:"Make / Model Inquiry Results"
213:in the United States with the
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446:"American airplanes: Bo - Bu"
371:22,000 ft (6,700 m)
305:2,250 lb (1,021 kg)
127:Brutsche Aircraft Corporation
321:four cylinder, air-cooled,
299:1,250 lb (567 kg)
145:. It features a cantilever
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332:, 108 hp (81 kW)
173:180 hp (134 kW)
151:conventional landing gear
113:Brutsche Freedom 210 STOL
95:Kit production completed
43:
34:
29:
18:Brutsche Freedom 180 STOL
260:General characteristics
157:and a single engine in
137:Design and development
159:tractor configuration
131:Salt Lake City, Utah
532:Fixed wing aircraft
202:Operational history
143:Brutsche Freedom 40
44:Three-view drawing
591:Homebuilt aircraft
586:High-wing aircraft
123:homebuilt aircraft
53:Homebuilt aircraft
571:Brutsche aircraft
558:
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473:(18 April 2015).
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87:Neal H. Brutsche
78:Brutsche Aircraft
30:Freedom 210 STOL
16:(Redirected from
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550:Freedom 210 STOL
545:Freedom 180 STOL
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369:Service ceiling:
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275:three passengers
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236:Freedom 210 STOL
226:Freedom 180 STOL
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56:Type of aircraft
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351:Cruise speed:
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478:. Retrieved
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453:. Retrieved
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417:Purdy, Don:
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357:Stall speed:
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170:Fowler flaps
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101:Number built
338:Performance
327:four stroke
315:Powerplant:
255:AeroCrafter
155:wheel pants
565:Categories
540:Freedom 40
388:References
291:Wing area:
211:registered
285:Wingspan:
273:Capacity:
253:Data from
147:high-wing
84:Designer
525:aircraft
523:Brutsche
480:18 April
455:16 April
221:Variants
166:aluminum
117:American
279:Length:
92:Status
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363:Range:
186:floats
267:Crew:
153:with
105:None
49:Role
482:2015
457:2015
423:ISBN
317:1 ×
120:STOL
111:The
269:one
129:of
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433:^
396:^
325:,
188:.
161:.
515:e
508:t
501:v
484:.
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20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
