Aerostar R40S Festival: Difference between revisions
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| type=[[Ultralight aircraft]] and [[Light-sport aircraft]] |
| type=[[Ultralight aircraft]] and [[Light-sport aircraft]] |
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| national origin=[[Romania]] |
| national origin=[[Romania]] |
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| manufacturer=[[Aerostar]] |
| manufacturer=[[Aerostar (Romanian company)|Aerostar]] |
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| designer= |
| designer= |
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| first flight=3 May 2001<ref>{{cite web|url=https://aeropedia.com.au/content/aerostar-festival-r40s/|title=AEROSTAR FESTIVAL R-40S|author=David C. Eyre|work=aeropedia|date=8 May 2019}}</ref> |
| first flight=3 May 2001<ref>{{cite web|url=https://aeropedia.com.au/content/aerostar-festival-r40s/|title=AEROSTAR FESTIVAL R-40S|author=David C. Eyre|work=aeropedia|date=8 May 2019}}</ref> |
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The '''Aerostar R40S Festival''' is a [[Romania]]n made [[ultralight aircraft|ultralight]] and [[light-sport aircraft]], designed and produced by [[Aerostar]] of [[Bacău]]. The aircraft is supplied as a complete ready-to-fly-aircraft.<ref name="WDLA11">Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011–12'', page 22. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X</ref><ref name="WDLA15">Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015–16'', page 20. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}</ref> |
The '''Aerostar R40S Festival''' is a [[Romania]]n made [[ultralight aircraft|ultralight]] and [[light-sport aircraft]], designed and produced by [[Aerostar (Romanian company)|Aerostar]] of [[Bacău]]. The aircraft is supplied as a complete ready-to-fly-aircraft.<ref name="WDLA11">Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011–12'', page 22. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X</ref><ref name="WDLA15">Tacke, Willi; Marino Boric; et al: ''World Directory of Light Aviation 2015–16'', page 20. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}</ref> |
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==Design and development== |
==Design and development== |
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The aircraft was designed to comply with the [[Fédération Aéronautique Internationale]] microlight, and US [[light-sport aircraft]] rules. It features a cantilever [[low-wing]], a two-seats-in-[[side-by-side configuration]] enclosed cockpit, fixed [[tricycle landing gear]] and a single engine in [[tractor configuration]].<ref name="WDLA11" /><ref name="WDLA15"/><ref name="SLSA">{{cite web|url = http://www.sportpilot.org/learn/slsa/|title = EAA's Listing of Special Light-Sport Aircraft| |
The aircraft was designed to comply with the [[Fédération Aéronautique Internationale]] microlight, and US [[light-sport aircraft]] rules. It features a cantilever [[low-wing]], a two-seats-in-[[side-by-side configuration]] enclosed cockpit, fixed [[tricycle landing gear]] and a single engine in [[tractor configuration]].<ref name="WDLA11" /><ref name="WDLA15"/><ref name="SLSA">{{cite web|url = http://www.sportpilot.org/learn/slsa/|title = EAA's Listing of Special Light-Sport Aircraft|access-date = 17 April 2012|last = Experimental Aircraft Association|author-link = Experimental Aircraft Association|year = 2012|archive-url = https://web.archive.org/web/20140228070151/http://sportpilot.org/learn/slsa|archive-date = 2014-02-28}}</ref> |
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The aircraft is made from [[ |
The aircraft is made from [[aluminium]] sheet. Its {{convert|9.17|m|ft|1|abbr=on}} span wing employs manually operated [[Flap (aircraft)|flaps]]. The standard engine is the {{convert|100|hp|kW|0|abbr=on}} [[Rotax 912ULS]] [[four-stroke]] powerplant, driving a three-bladed [[Woodcomp]] propeller.<ref name="WDLA11" /><ref name="WDLA15"/><ref name="Specs">{{cite web |website=[[Aerostar (Romanian company)|Aerostar]] |date=n.d. |title=Festival R40S – Light Sport Aircraft |url=http://www.aerostar.ro/festival/doc/Commercial2011.pdf |access-date=24 April 2012}}{{dead link|date=June 2017|bot=InternetArchiveBot|fix-attempted=yes}}</ref> |
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<!-- ==Operational history== --> |
<!-- ==Operational history== --> |
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[[Category:Light-sport aircraft]] |
[[Category:Light-sport aircraft]] |
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[[Category:Single-engined tractor aircraft]] |
[[Category:Single-engined tractor aircraft]] |
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[[Category:Aerostar aircraft|R40S]] |
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[[Category:Single-engined piston aircraft]] |
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[[Category:Low-wing aircraft]] |
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[[Category:Aircraft with fixed tricycle landing gear]] |
Latest revision as of 19:31, 20 December 2024
R40S Festival | |
---|---|
Role | Ultralight aircraft and Light-sport aircraft |
National origin | Romania |
Manufacturer | Aerostar |
First flight | 3 May 2001[1] |
Status | In production |
The Aerostar R40S Festival is a Romanian made ultralight and light-sport aircraft, designed and produced by Aerostar of Bacău. The aircraft is supplied as a complete ready-to-fly-aircraft.[2][3]
Design and development
[edit]The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight, and US light-sport aircraft rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.[2][3][4]
The aircraft is made from aluminium sheet. Its 9.17 m (30.1 ft) span wing employs manually operated flaps. The standard engine is the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant, driving a three-bladed Woodcomp propeller.[2][3][5]
Variants
[edit]- R40F
- Initial ultralight model
- R40FS
- Improved model
- R40S
- Base model with dial instruments[5]
- R40S-GC
- Version for IFR flight, with a Dynon Skyview glass cockpit[5]
Operators
[edit]Specifications (R40F/FS Festival)
[edit]Data from Aerostar operating manual[7]
General characteristics
- Crew: one
- Capacity: one passenger
- Length: 6.74 m (22 ft 1 in)
- Wingspan: 9.17 m (30 ft 1 in)
- Height: 2.47 m (8 ft 1 in)
- Wing area: 13.97 m2 (150.4 sq ft)
- Empty weight: 354 kg (780 lb) with Rotax ULS912 engine
- Gross weight: 535 kg (1,179 lb)
- Fuel capacity: 80 litres (18 imp gal; 21 US gal)
- Powerplant: 1 × Rotax 912ULS four cylinder, liquid and air-cooled, four stroke, 75 kW (101 hp)
- Propellers: 3-bladed Klassic 170/3/R, 1.7 m (5 ft 7 in) diameter
Performance
- Maximum speed: 175 km/h (109 mph, 95 kn) V(A)
- Cruise speed: 150 km/h (94 mph, 82 kn)
- Stall speed: 67 km/h (42 mph, 36 kn) flaps at 30 degrees
- Never exceed speed: 215 km/h (134 mph, 116 kn)
- Range: 800 km (500 mi, 430 nmi) with no reserves
- Endurance: 5.8 hours
- Service ceiling: 4,000 m (13,000 ft)
- g limits: +4/-2
- Maximum glide ratio: 12:1
- Rate of climb: 4.35 m/s (856 ft/min)
References
[edit]- ^ David C. Eyre (8 May 2019). "AEROSTAR FESTIVAL R-40S". aeropedia.
- ^ a b c Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011–12, page 22. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ^ a b c Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015–16, page 20. Flying Pages Europe SARL, 2015. ISSN 1368-485X
- ^ Experimental Aircraft Association (2012). "EAA's Listing of Special Light-Sport Aircraft". Archived from the original on 28 February 2014. Retrieved 17 April 2012.
- ^ a b c "Festival R40S – Light Sport Aircraft" (PDF). Aerostar. n.d. Retrieved 24 April 2012.[permanent dead link ]
- ^ Isby, David C.; Willis, David (December 2013). "Mozambique Rebuilding its Air Force". Air International. Vol. 85, no. 6. p. 26. ISSN 0306-5634.
- ^ Manual de utilizare si intretinere XR00-00-0000-F(FS) Editia A Data 05.2004