Extra EA-200: Difference between revisions
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{{Infobox aircraft |
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| name=Extra EA-200 |
| name=Extra EA-200 |
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| image= |
| image=SN-004 N960SS Extra200.jpg |
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| caption=Extra 200 |
| caption=Extra 200 |
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}}{{Infobox Aircraft Type |
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| type= Aerobatic Aircraft |
| type= Aerobatic Aircraft |
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| |
| national_origin=[[Germany]] |
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| manufacturer= [[Extra Flugzeugbau]] |
| manufacturer= [[Extra Flugzeugbau]] |
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| designer= [[Walter Extra]] |
| designer= [[Walter Extra]] |
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| first_flight=2 April 1996 |
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| first flight= |
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| introduction= |
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| introduced=1996 |
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| retired= |
| retired= |
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| status= |
| status= Active |
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| primary_user= |
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| |
| more_users= <!--Limited to three in total; separate using <br /> --> |
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| produced= |
| produced= 1996-present |
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| number_built= |
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| program cost= <!--Total program cost--> |
| program cost= <!--Total program cost--> |
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| unit cost= |
| unit cost=370,000 [[United States dollar|USD]] (2016)<!--Incremental or flyaway cost for military or retail price for commercial aircraft--> |
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| developed_from=[[Extra EA-300]] |
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| variants |
| variants= |
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}} |
}} |
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The ''' |
The '''Extra 200''' (Type EA-200) is a two-seat, tandem arrangement, low-wing aerobatic monoplane with conventional ([[taildragger]]) landing gear fully capable of Unlimited category [[Competition aerobatics|competition]], built by [[Extra Flugzeugbau]].<ref>{{cite web|url=http://www.extraaircraft.com/200.php/ |title=''EXTRA Aerobatic Airplanes'' |publisher=EXTRA Flugzeugproduktions - und Vertriebs - GmbH |accessdate=2015-03-09}}</ref> |
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Designed by [[Walter Extra]], it was introduced to the [[United States]] market in [[1996 in aviation|1996]].<ref>{{cite web|url=http://www.pilotfriend.com/aircraft%20performance/Extra/extra.htm |title=''Extra Aircraft history performance and specifications'' |publisher=Certified Aircraft Database |accessdate=2015-03-09}}</ref> The Extra 200 is slightly smaller than the [[Extra EA-300|Extra 300]], and is powered by a 200 hp (149 kW) rather than the Extra 300's 300 hp (224 kW) [[Lycoming engine]]. It offers the flying characteristics of the EA-300, is capable of all unlimited maneuvers, and makes a great all-round training/sports aerobatic aircraft. |
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==Design== |
==Design== |
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The Extra 200 is based on the design of the [[Extra 300]], and the two aircraft share many similarities. The Extra 200 has a [[welded]] [[steel]] (4130) tube fuselage covered in [[fiberglass]] and fabric with a carbon/glass hybrid composite [[empennage]] (i.e., the tail assembly, including the horizontal and vertical stabilizers, elevators, and rudder), and a bubble canopy. The [[monocoque]] wings have a [[carbon fiber]] composite spar with fiberglass skins and an integral fuel tank. A symmetrical [[airfoil]], mounted with a zero [[angle of incidence]], provides equal performance in both upright and inverted flight. The landing gear is fixed [[taildragger]] style with composite main legs and fiberglass wheel pants. The [[piston-engine]]d powerplant is a [[fuel-injected]] [[Lycoming AEIO-360]]-A1E that produces 200 horsepower (149 kW), and it is equipped with a 3-bladed constant-speed MTV-12-B-C/C 183-17e propeller made of laminated wood encased in glass-fiber reinforced plastic. The Extra 200 is stressed for ±10 G with one person on board and ±8 G with two, and has an [[FAA]] certified load factor in the [[United States|US]] to ±10 G. |
The Extra 200 is based on the design of the [[Extra EA-300|Extra 300]], and the two aircraft share many similarities. The Extra 200 has a [[welded]] [[steel]] (4130) tube fuselage covered in [[fiberglass]] and fabric with a carbon/glass hybrid composite [[empennage]] (i.e., the tail assembly, including the horizontal and vertical stabilizers, elevators, and rudder), and a bubble canopy. The [[monocoque]] wings have a [[carbon fiber]] composite spar with fiberglass skins and an integral fuel tank. A symmetrical [[airfoil]], mounted with a zero [[angle of incidence (aerodynamics)|angle of incidence]], provides equal performance in both upright and inverted flight. The landing gear is fixed [[taildragger]] style with composite main legs and fiberglass wheel pants. The [[piston-engine]]d powerplant is a [[fuel-injected]] [[Lycoming AEIO-360]]-A1E that produces 200 horsepower (149 kW), and it is equipped with a 3-bladed constant-speed MTV-12-B-C/C 183-17e propeller made of laminated wood encased in glass-fiber reinforced plastic. The Extra 200 is stressed for ±10 G with one person on board and ±8 G with two, and has an [[FAA]] certified load factor in the [[United States|US]] to ±10 G. |
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==Background== |
==Background== |
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In the late 1990s, the Extra 200 was considerably less expensive, at $170,000 (1996 new), versus the |
In the late 1990s, the Extra 200 was considerably less expensive, at $170,000 (1996 new), versus the Extra 300L's price of $235,000 (1996 new). The Extra 200 is now back in limited production (2007) after a hiatus in which [[Extra Flugzeugbau|Extra Aircraft]] focused on the development of the [[Extra EA-500]] whose costs of development forced the company into bankruptcy. With new ownership, the company is again producing a range of aerobatic aircraft including the EA-200. The base price is $225,000 as of 2007. |
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==Specifications (Extra 200 EA-200)== |
==Specifications (Extra 200 EA-200)== |
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Data from flugzeuginfo.net <ref>{{cite web|title=Extra Aircraft EA-200 (EA 300/200)|url=http://www.flugzeuginfo.net/acdata_php/acdata_extra_ea200_en.php|accessdate=Feb 27, 2017}}</ref> |
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===General characteristics=== |
===General characteristics=== |
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* '''Crew:''' one pilot or two in tandem |
* '''Crew:''' one pilot or two in tandem |
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* '''Length:''' 6.80 m (22 ft 4 in) |
* '''Length:''' 6.80 m (22 ft 4 in) |
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* '''Wingspan:''' 7.50 m (24 ft 7 in) |
* '''Wingspan:''' 7.50 m (24 ft 7 in) |
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* '''Airfoil: '''symmetrical''' |
* '''Airfoil:''' '''symmetrical''' |
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* '''Height:''' 2.56 m (8 ft 5 in) |
* '''Height:''' 2.56 m (8 ft 5 in) |
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* '''Wing area:''' 10.4 m |
* '''Wing area:''' 10.4 m<sup>2</sup> (112 ft<sup>2</sup>) |
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* '''Empty:''' 540 kg (1,190 lb) |
* '''Empty:''' 540 kg (1,190 lb) |
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* '''Loaded:''' 800 |
* '''Loaded:''' 800 kg (1770 lb) (two pilot aerobatic configuration) |
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* '''Maximum takeoff:''' 870 kg (1,914 lb) |
* '''Maximum takeoff:''' 870 kg (1,914 lb) |
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* '''Powerplant:''' [[Lycoming AEIO-360]]-A1E, 149 kW (200 hp) |
* '''Powerplant:''' [[Lycoming AEIO-360]]-A1E, 149 kW (200 hp) |
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===Performance=== |
===Performance=== |
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* '''Never Exceed Speed:''' 396 km/h |
* '''Never Exceed Speed:''' 396 km/h, 217 kn (248 mph) |
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* '''Maneuvering Speed:''' 154 |
* '''Maneuvering Speed:''' 154 kn |
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* '''Stall Speed:''' 53-59 kn<ref>{{cite web|title=Extra Aircraft|url=http://www.extraaircraft.com/aerobatic/ex200.php|accessdate=May 15, 2012|url-status=dead|archiveurl=https://web.archive.org/web/20120608094426/http://www.extraaircraft.com/aerobatic/ex200.php|archivedate=June 8, 2012|df=}}</ref> |
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* '''Stall Speed:''' 53-59 kts |
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* '''Range:''' 1,080 |
* '''Range:''' {{convert|1,080|km|mi|abbr=on}} |
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* '''Service ceiling:''' 4,573 m (15,000 ft) |
* '''Service ceiling:''' 4,573 m (15,000 ft) |
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* '''Rate of climb:''' 686 m/min (2,250 ft/min) |
* '''Rate of climb:''' 686 m/min (2,250 ft/min) |
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* '''Wing loading:''' 83,65 |
* '''Wing loading:''' 83,65 kg/m<sup>2</sup> ( 17,09 lb/ft<sup>2</sup>) |
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* '''Power/Mass:''' 0,1713 |
* '''Power/Mass:''' 0,1713 kW/kg ( 0,1045 hp/lb) |
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==See also== |
==See also== |
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*[[Pitts S-2]] |
*[[Pitts S-2]] |
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*[[Giles G-202]] |
*[[Giles G-202]] |
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==References== |
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<references /> |
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==External links== |
==External links== |
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{{commons category|Extra 200}} |
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*[http://www.extraaircraft.com/aerobatic/ex200.php Manufacturer's Website]—Specifications, addresses of the company dealers, pictures and movies. |
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*[http://www.extraaircraft.com/ |
*[https://web.archive.org/web/20120608094426/http://www.extraaircraft.com/aerobatic/ex200.php] Manufacturer's Website—Specifications, addresses of the company dealers, pictures and movies. |
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*[http://www.extraaircraft.com/docs/tech-manuals/MM300200/Temporary_Revision_N_07702-TR-01-20130708.pdf] Service Manual — Provides information necessary for servicing, maintaining, and repair of the EA-200. |
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*[https://www.extraaircraft.com/docs/service/POH%20EA200%20CUS%202008-07-14.pdf] '''Pilots Information Handbook:''' This document is a "generic" version of the EA-200 Pilot's Operating Handbook (POH) and it allows a pilot to study specific aircraft attributes and procedures without removing the regulatory document from the aircraft. |
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{{Extra aircraft}} |
{{Extra aircraft}} |
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{{Aviation lists}} |
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{{DEFAULTSORT:Extra Ea-200}} |
{{DEFAULTSORT:Extra Ea-200}} |
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[[Category:Extra aircraft|EA-200]] |
[[Category:Extra aircraft|EA-200]] |
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[[Category:German sport aircraft |
[[Category:1990s German sport aircraft]] |
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[[Category:Aerobatic aircraft]] |
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[[Category:Low-wing aircraft]] |
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[[fr:Extra 200]] |
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[[Category:Single-engined tractor aircraft]] |
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[[Category:Aircraft first flown in 1996]] |
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[[Category:Conventional landing gear]] |
Latest revision as of 18:51, 9 September 2024
This article needs additional citations for verification. (October 2010) |
Extra EA-200 | |
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General information | |
Type | Aerobatic Aircraft |
National origin | Germany |
Manufacturer | Extra Flugzeugbau |
Designer | |
Status | Active |
History | |
Manufactured | 1996-present |
First flight | 2 April 1996 |
Developed from | Extra EA-300 |
The Extra 200 (Type EA-200) is a two-seat, tandem arrangement, low-wing aerobatic monoplane with conventional (taildragger) landing gear fully capable of Unlimited category competition, built by Extra Flugzeugbau.[1]
Designed by Walter Extra, it was introduced to the United States market in 1996.[2] The Extra 200 is slightly smaller than the Extra 300, and is powered by a 200 hp (149 kW) rather than the Extra 300's 300 hp (224 kW) Lycoming engine. It offers the flying characteristics of the EA-300, is capable of all unlimited maneuvers, and makes a great all-round training/sports aerobatic aircraft.
Design
[edit]The Extra 200 is based on the design of the Extra 300, and the two aircraft share many similarities. The Extra 200 has a welded steel (4130) tube fuselage covered in fiberglass and fabric with a carbon/glass hybrid composite empennage (i.e., the tail assembly, including the horizontal and vertical stabilizers, elevators, and rudder), and a bubble canopy. The monocoque wings have a carbon fiber composite spar with fiberglass skins and an integral fuel tank. A symmetrical airfoil, mounted with a zero angle of incidence, provides equal performance in both upright and inverted flight. The landing gear is fixed taildragger style with composite main legs and fiberglass wheel pants. The piston-engined powerplant is a fuel-injected Lycoming AEIO-360-A1E that produces 200 horsepower (149 kW), and it is equipped with a 3-bladed constant-speed MTV-12-B-C/C 183-17e propeller made of laminated wood encased in glass-fiber reinforced plastic. The Extra 200 is stressed for ±10 G with one person on board and ±8 G with two, and has an FAA certified load factor in the US to ±10 G.
Background
[edit]In the late 1990s, the Extra 200 was considerably less expensive, at $170,000 (1996 new), versus the Extra 300L's price of $235,000 (1996 new). The Extra 200 is now back in limited production (2007) after a hiatus in which Extra Aircraft focused on the development of the Extra EA-500 whose costs of development forced the company into bankruptcy. With new ownership, the company is again producing a range of aerobatic aircraft including the EA-200. The base price is $225,000 as of 2007.
Specifications (Extra 200 EA-200)
[edit]Data from flugzeuginfo.net [3]
General characteristics
[edit]- Crew: one pilot or two in tandem
- Capacity: two pilots
- Length: 6.80 m (22 ft 4 in)
- Wingspan: 7.50 m (24 ft 7 in)
- Airfoil: symmetrical
- Height: 2.56 m (8 ft 5 in)
- Wing area: 10.4 m2 (112 ft2)
- Empty: 540 kg (1,190 lb)
- Loaded: 800 kg (1770 lb) (two pilot aerobatic configuration)
- Maximum takeoff: 870 kg (1,914 lb)
- Powerplant: Lycoming AEIO-360-A1E, 149 kW (200 hp)
- FAA/EASA Certified Load Factor: ±10 G with one person on board
Performance
[edit]- Never Exceed Speed: 396 km/h, 217 kn (248 mph)
- Maneuvering Speed: 154 kn
- Stall Speed: 53-59 kn[4]
- Range: 1,080 km (670 mi)
- Service ceiling: 4,573 m (15,000 ft)
- Rate of climb: 686 m/min (2,250 ft/min)
- Wing loading: 83,65 kg/m2 ( 17,09 lb/ft2)
- Power/Mass: 0,1713 kW/kg ( 0,1045 hp/lb)
See also
[edit]Related development:
Comparable aircraft:
References
[edit]- ^ "EXTRA Aerobatic Airplanes". EXTRA Flugzeugproduktions - und Vertriebs - GmbH. Retrieved 2015-03-09.
- ^ "Extra Aircraft history performance and specifications". Certified Aircraft Database. Retrieved 2015-03-09.
- ^ "Extra Aircraft EA-200 (EA 300/200)". Retrieved Feb 27, 2017.
- ^ "Extra Aircraft". Archived from the original on June 8, 2012. Retrieved May 15, 2012.
External links
[edit]- [1] Manufacturer's Website—Specifications, addresses of the company dealers, pictures and movies.
- [2] Service Manual — Provides information necessary for servicing, maintaining, and repair of the EA-200.
- [3] Pilots Information Handbook: This document is a "generic" version of the EA-200 Pilot's Operating Handbook (POH) and it allows a pilot to study specific aircraft attributes and procedures without removing the regulatory document from the aircraft.