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{{Short description|Utility aircraft in the US}}
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->{{Infobox Aircraft
{{More citations needed|date=February 2009}}

<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{{Infobox aircraft
|name=Citabria
|name=Citabria
|image=Image:Citabria_7GCBC.jpg
|image=Citabria_7GCBC.jpg
|caption=<!--image caption; if it isn't descriptive it should be left blank-->
|caption=<!--image caption; if it isn't descriptive it should be left blank-->
|type=Light [[utility aircraft]] and [[sports plane]]
|type=Light [[utility aircraft]] and sports plane
|manufacturer=[[American Champion|American Champion Aircraft]]
|manufacturer=[[American Champion|American Champion Aircraft]]<br>[[AviaBellanca Aircraft|Bellanca]]<br>[[Champion Aircraft]]
|designer=[[Champion Aircraft (Wisconsin)|Champion Aircraft]]
|designer=[[Champion Aircraft (Wisconsin)|Champion Aircraft]]
|first flight=1964
|first_flight=1964
|introduced=1964
|introduction=1964
|retired=
|retired=
|status=In production<ref>{{cite web |url=http://www.amerchampionaircraft.com/NewSite2013/NewAircraft/NewAircraft.html |title=American Champion Aircraft |publisher=Amerchampionaircraft.com |access-date=2014-06-17 |url-status=dead |archive-url=https://web.archive.org/web/20140817113954/http://amerchampionaircraft.com/NewSite2013/NewAircraft/NewAircraft.html |archive-date=2014-08-17 }}</ref>
|status=
|primary_user=
|primary user=
|more users=
|more_users=
|produced= 1964-present
|produced=<!--years in production, e.g. 1970-1999, if still in active use but no longer built-->
|number_built=over 5,238
|number built=
|unit cost=
|unit cost=
|variants with their own articles=
|variants=
}}
}}
The '''Citabria''' is a two-seat fixed [[conventional gear]] [[general aviation]] [[airplane]] which entered production in the United States in 1964. Designed for [[flight training]] and personal use, it is capable of sustaining [[aerobatic]] stresses (+5/-2 [[acceleration due to gravity#Usage of the unit|g loads]]). Its name, "airbatic" spelled backward, reflects this.
The '''Citabria''' is a light single-engine, two-seat, fixed [[conventional gear]] [[airplane]] which entered production in the United States in 1964. Designed for [[flight training]], [[utility aircraft|utility]] and personal use, it is capable of sustaining [[aerobatic]] stresses from +5g to -2[[g-force|g]]. Its name, "airbatic" backwards, reflects this.


==Production history==
==Production history==
The Citabria was designed and initially produced by [[Champion Aircraft (Wisconsin)|Champion Aircraft Corporation]], and was a derivative of designs the company had been building since acquiring the 7-series [[Aeronca Champ|Champ]] from [[Aeronca Aircraft|Aeronca]] in 1954. The model 7ECA Citabria entered production at Champion in 1964. The 7GCAA and 7GCBC variants, added in 1965, were joined by the 7KCAB in 1968.
The Citabria was designed and initially produced by [[Champion Aircraft]] Corporation, and was a derivative of designs the company had been building since acquiring the 7-series [[Aeronca Champ|Champ]] from [[Aeronca Aircraft|Aeronca]] in 1954. The model 7ECA Citabria entered production at Champion in 1964. The 7GCAA and 7GCBC variants, added in 1965, were joined by the 7KCAB in 1968.


In 1970, Champion was acquired by [[AviaBellanca Aircraft Corporation|Bellanca]], which continued production of all of the Champion-designed variants. Bellanca introduced two designs with close connections to the Citabria: The [[Decathlon (aircraft)|8KCAB Decathlon]] and the [[American Champion Scout (aircraft)|8GCBC Scout]]. Production at Bellanca ended in 1980 and the company's assets were liquidated in 1982.
In 1970, Champion was acquired by [[AviaBellanca Aircraft|Bellanca Aircraft Corporation]], which continued production of all of the Champion-designed variants. Bellanca introduced two designs with close connections to the Citabria: The [[8KCAB Decathlon]] and the [[8GCBC Scout]]. Production at Bellanca ended in 1980 and the company's assets were liquidated in 1982.


The Citabria designs passed through the hands of a number of companies through the 1980s, including a [[Champion Aircraft (Texas)|Champion Aircraft Company]] which was no relation to the Champion Aircraft of the 1960s. In that period, only one Citabria was built—a 7GCBC which was built as a "Citabria 150S." [[American Champion|American Champion Aircraft Corporation]] acquired the Citabria, Decathlon, and Scout designs in 1990 and brought the 7ECA, 7GCAA, and 7GCBC models back into production over a period of years.
The Citabria designs passed through the hands of a number of companies through the 1980s, including a [[Champion Aircraft (Texas)|Champion Aircraft Company]] which was no relation to the Champion Aircraft of the 1960s. In that period, only one Citabria model was built—a 7GCBC marketed as "Citabria 150S." [[American Champion|American Champion Aircraft Corporation]] acquired the Citabria, Decathlon, and Scout designs in 1989 and returned the 7ECA, 7GCAA, and 7GCBC models to production over a period of years.


==Design==
==Design==
The Citabria traces its lineage back to the Champ. The most noticeable external changes to the design are the Citabria's squared-off [[rudder#Aircraft rudders|rudder]] surface, wing tips, and rear windows. Like the Champ, the Citabria features tandem seating. The [[fuselage]] and tail surfaces are constructed of welded metal tubing. The outer shape of the fuselage is created by a combination of wooden [[former|formers]] and [[longeron|longerons]], covered with fabric. The cross-section of the metal fuselage truss is triangular, a design feature which can be traced all the way back to the earliest [[Aeronca C-2]] design of the late 1920s.
The Citabria traces its lineage back to the Champ. The most noticeable external changes to the design are the Citabria's squared-off [[rudder#Aircraft rudders|rudder]] surface, wingtips, and rear windows. Like the Champ, the Citabria features tandem seating. The [[fuselage]] and tail surfaces are constructed of welded metal tubing. The outer shape of the fuselage is created by a combination of wooden [[former]]s and [[longeron]]s, covered with fabric. The cross-section of the metal fuselage truss is triangular, a design feature which can be traced all the way back to the earliest [[Aeronca C-2]] design of the late 1920s.


[[File:Bellanca.citabria.arp.jpg|thumb|1980-built Bellanca 7ECA Citabria]]
The strut-braced [[wing#Artificial wings|wings]] of the Citabria are, like the fuselage and tail surfaces, fabric covered, utilizing aluminum [[rib (aircraft)|ribs]]. Most Citabrias were built with wooden [[spar (aviation)|spars]]. American Champion has been using aluminum spars in the aircraft it has produced and has, as well, made the aluminum-spar wings available for retrofit installation on older aircraft.
The strut-braced [[wing#Artificial wings|wings]] of the Citabria are, like the fuselage and tail surfaces, fabric covered, utilizing aluminum [[rib (aircraft)|ribs]]. Most Citabrias were built with wooden [[spar (aviation)|spars]]. American Champion has been using aluminum spars in the aircraft it has produced and has, as well, made the aluminum-spar wings available for retrofit installation on older aircraft.


The landing gear of the Citabria is in a conventional arrangement. The main gear legs of most Citabrias are made of spring steel, though American Champion began to use aluminum gear legs in 2004. Early Citabrias were fitted with steel tube main gear which use an oleo strut for shock absorption. All of the variants are discussed in more detail below.
The landing gear of the Citabria is in a [[Conventional landing gear|conventional arrangement]]. The main gear legs of most Citabrias are made of spring steel, though American Champion began to use aluminum gear legs in 2004. Early Citabrias were fitted with a steel tube main gear which uses an oleo strut for shock absorption. All of the variants are discussed in more detail below.


==Operational history==
==Operational history==
[[File:SchweizerSGS1-34C-FDUZ31.JPG|thumb|right|A Champion 7GCAA Citabria towing a [[Schweizer SGS 1-34]] sailplane]]
When the Citabria was introduced, it was the only airplane being commercially produced in the United States which was certified for aerobatics. From the mid 1960s through the end of the 1970s, sport flying in the United States enjoyed great popularity. Pilots who flew for personal enjoyment were interested in the unusual and exciting, and aerobatics provided an avenue for this interest. Citabrias were popular as trainers—because of their conventional gear and their aerobatic capabilities—and as personal aircraft. They were also found in utility roles such as [[bush flying]]—thanks to their [[STOL|short take off and landing]] ability, [[aerial application|agriculture]], and pipeline patrol. Though variants of the design, and other better-suited designs, have largely taken over the Citabria's utility roles, Citabrias remain popular as trainers and for personal use.
When the Citabria was introduced, it was the only airplane being commercially produced in the United States which was certified for aerobatics. Citabrias were also popular as trainers—because of their conventional gear and their aerobatic capabilities—and as personal aircraft. They were also found in utility roles as [[bush planes]]—thanks to their [[STOL|short take off and landing (STOL)]] ability, [[aerial application|agriculture]], pipeline patrol, and as [[glider towplane]]s. Though variants of the design, and other better-suited designs have largely taken over the Citabria's utility roles, Citabrias remain popular as trainers, glider towplanes, and for personal use.

==Military operators==
The 7GCBC Citabria was used as an observation aircraft by the [[Turkish Army]]. An example of one of these aircraft is displayed at the [[Rahmi M Koç Museum]] in [[Istanbul]].


==Variants==
==Variants==
As noted above, various versions of the Citabria have been tested and produced since 1964. These are discussed in order below.


===7ECA, Citabria Standard, Citabria Aurora===
===7ECA, Citabria Standard, Citabria Aurora===
[[File:American Champion 7ECA Citabria Aurora Kyneton Vabre.jpg|thumb|7ECA at [[Kyneton, Victoria]]]]
Introduced in 1964, the 7ECA was the first version of the design and utilized the [[Continental O-200|Continental O-200-A]] engine of 100 horsepower. When introduced, it featured wood-spar wings and [[Oleo (shock absorber)|oleo-shock]] main gear. Within the first year of production, Champion began offering the [[Lycoming O-235|Lycoming O-235-C1]] engine of 115 horsepower as an alternative to the Continental. In 1967, Champion switched to [[spring steel]] main gear legs; by then, the Lycoming engine had become the standard. On acquiring the design, Bellanca gave this model the name Citabria "Standard" and at some point began using the 115-horsepower Lycoming O-235-K2C engine. When American Champion reintroduced the 7ECA in 1995 as the Citabria "Aurora, " the biggest change was the use of metal-spar wings; the most recent significant design change has been the switch to aluminum main gear legs in 2004.
Introduced in 1964, the 7ECA was the first version of the design and utilized the [[Continental O-200|Continental O-200-A]] engine of {{convert|100|hp}}. When introduced, it featured wood-spar wings and [[Oleo (shock absorber)|oleo-shock]] main gear. Within the first year of production, Champion began offering the [[Lycoming O-235|Lycoming O-235-C1]] engine of {{convert|115|hp}} as an alternative to the Continental. In 1967, Champion switched to [[spring steel]] main gear legs; by then, the Lycoming engine had become the standard. On acquiring the design, Bellanca gave this model the name Citabria "Standard" and began using the {{convert|115|hp}} Lycoming O-235-K2C engine. When American Champion reintroduced the 7ECA in 1995 as the Citabria "Aurora, " the biggest change was the use of metal-spar wings; the most recent significant design change has been the switch to aluminum main gear legs in 2004.


===7GCAA, Citabria "A" Package, Citabria Adventure===
===7GCAA, Citabria 150, Citabria "A" Package, Citabria Adventure===
[[File:Bellanca 7GCAA (N2745Z).jpg|thumb|Bellanca 7GCAA]]
Introduced in 1965, the Champion 7GCAA, like the 7ECA, featured wood-spar wings and oleo-shock main gear. The major difference was in the engine, which in the 7GCAA was a [[Lycoming O-320|Lycoming O-320-A2B]] of 150 horsepower. Champion switched to spring steel main gear legs in 1967. Bellanca continued production of the 7GCAA as the Citabria "A" Package (a designation apparently begun by Champion), but with no significant design changes. American Champion's 7GCAA, reintroduced in 1997 as the Citabria "Adventure," is similar to earlier versions, with the exception of the metal-spar wings and the use of the Lycoming O-320-B2B engine of 160 horsepower; the most recent significant design change has been the switch to aluminum main gear legs in 2004. An "Ultimate Adventure" version, with a [[Superior Air Parts|Superior]] [[Vantage O-360|Vantage O-360-A3A2]] engine of 180 horsepower and a [[composite material|composite]] [[propeller]], is also produced by American Champion.
Introduced in 1965, the Champion 7GCAA, like the 7ECA, featured wood-spar wings and oleo-shock main gear. The major difference was in the engine, which in the 7GCAA was a [[Lycoming O-320|Lycoming O-320-A2B]] of {{convert|150|hp}}. Champion switched to spring steel main gear legs in 1967. Bellanca continued production of the 7GCAA as the Citabria "A" Package (a designation apparently begun by Champion), but with no significant design changes. American Champion's 7GCAA, reintroduced in 1997 as the Citabria "Adventure," is similar to earlier versions, with the exception of the metal-spar wings and the use of the Lycoming O-320-B2B engine of {{convert|160|hp}}; the most recent significant design change has been the switch to aluminum main gear legs in 2004. An "Ultimate Adventure" version, with a [[Superior Air Parts|Superior]] [[Vantage O-360|Vantage O-360-A3A2]] engine of {{convert|180|hp}} and a [[composite material|composite]] [[propeller (aircraft)|propeller]], is also produced by American Champion.


===7GCBC, Citabria "C" Package, Citabria Explorer===
===7GCBC, Citabria 150s, Citabria "C" Package, Citabria Explorer===
[[File:Bellanca 7GCBC (N68576).jpg|thumb|Bellanca 7GCBC]]
Champion introduced the 7GCBC in 1965. It was substantially similar to the 7GCAA of the same year, with a Lycoming O-320-A2B engine of 150 horsepower, wood-spar wings, and spring steel main gear legs. The major differences between these two models are that the 7GCBC has a wingspan of 34.5 feet, 1 foot longer than the 7ECA and 7GCAA, and carries wing [[flap (aircraft)|flaps]]. Bellanca continued production of the 7GCBC, calling it the Citabria "C" Package (a designation apparently begun by Champion). American Champion's 7GCBC, reintroduced in 1994 as the Citabria "Explorer," is similar to earlier versions, with the exception of the metal-spar wings and the use of the Lycoming O-320-B2B of 160 horsepower; the most recent significant design change has been the switch to aluminum main gear legs in 2004. A "High Country Explorer" version, with a Superior Vantage O-360-A3A2 engine of 180 horsepower and larger wheels, is also produced by American Champion.
Champion introduced the 7GCBC in 1965. It was substantially similar to the 7GCAA of the same year, with a Lycoming O-320-A2B engine of {{convert|150|hp}}, wood-spar wings, and spring steel main gear legs. The major differences between these two models are that the 7GCBC has a wingspan of {{convert|34.5|ft|m}}, {{convert|1|ft|m|adj=on}} longer than the 7ECA and 7GCAA, and carries wing [[flap (aircraft)|flaps]]. Bellanca continued production of the 7GCBC, calling it the Citabria "C" Package (a designation apparently begun by Champion). American Champion's 7GCBC, reintroduced in 1994 as the Citabria "Explorer," is similar to earlier versions, with the exception of the metal-spar wings and the use of the Lycoming O-320-B2B of {{convert|160|hp}}; the most recent significant design change has been the switch to aluminum main gear legs in 2004. A "High Country Explorer" version, with a Superior Vantage O-360-A3A2 engine of {{convert|180|hp}} and larger wheels, is also produced by American Champion.


===7KCAB, Citabria "B" Package===
===7KCAB, Citabria "B" Package===
[[File:Bellanca 7KCAB (N333JS).jpg|thumb|Bellanca 7KCAB]]
Champion introduced the 7KCAB in 1968. It was substantially similar to the 7GCAA of the same year, with wood-spar wings and spring steel main gear legs. The major differences between the7GCAA and 7KCAB were in the fuel system and the engine oil system. The engine was replaced with a Lycoming IO-320-E2A of 150 horsepower, while a header tank of 1.5 gallons—located beneath the instrument panel—was added to the fuel system. In addition, the [[carburetor]] was replaced with a [[fuel_injection|fuel injection]] system, and a [[Christen Industries]] inverted oil system was fitted to the engine. All of these changes were made in order to allow for extended inverted flight, a mode not possible in the earlier models. Bellanca continued production of the 7KCAB as the Citabria "B" Package (a designation apparently begun by Champion).
Champion introduced the 7KCAB in 1968. It was substantially similar to the 7GCAA of the same year, with wood-spar wings and spring steel main gear legs. The major differences between the 7GCAA and 7KCAB were in the fuel system and the engine oil system. The engine was replaced with a Lycoming IO-320-E2A of {{convert|150|hp}}, while a header tank of 1.5 gallons—located beneath the instrument panel—was added to the fuel system. In addition, the [[carburetor]] was replaced with a [[fuel injection]] system, and a [[Christen Industries]] inverted oil system was fitted to the engine. All of these changes were made in order to allow for extended inverted flight, a mode not possible in the earlier models. Bellanca continued production of the 7KCAB as the Citabria "B" Package (a designation apparently begun by Champion).


===Citabria Pro===
===Citabria Pro===
The 8KCAB Citabria Pro was first flown by Champion on 2 August 1968, and was a dedicated aerobatic aircraft based on the standard Citabria.<ref name="jawa69p308"/> It was a [[parasol wing]]ed monoplane, with a revised wing section and a longer fuselage. The prototype had an open cockpit for a single pilot, but the design allowed for conversion to a two seat layout. The aircraft was powered by a {{convert|200|hp|kW|abbr=on}} [[Lycoming IO-360]] Special engine driving a two-bladed propeller.<ref name="jawa69p308"/> It was never put into production at Champion nor by Bellanca which acquired the company and designs only a short time later.
The Citabria Pro was tested by Champion in 1968, but was never put into production at Champion nor by Bellanca which acquired the company and designs only a short time later. The Citabria Pro was based on the 7KCAB, but with a vertically shortened fuselage, a wing of semi-symmetric [[airfoil]] mounted in a parasol configuration, and a unique engine, the Lycoming IO-360SPL. While it was flown as a single-seat, there was a second set of controls and room for a second seat. The design changes were intended to produce an aircraft capable of more complex maneuvers and better performance in inverted flight. Sources conflict over whether the Citabria Pro was assigned model number 8KCAB or 9KCAB. Since the 8KCAB designation ultimately belonged to the [[Decathlon_(aircraft)|Decathlon]] design, which was in development at Champion at the same time, it is unlikely that it was used for the Citabria Pro.


==Military operators==
==Specifications (1975 7GCAA Citabria "A" Package)==
The 7GCBC Citabria was used as an observation aircraft by the [[Turkish Army]]. One of these aircraft is displayed at the [[Rahmi M Koç Museum]] in [[Istanbul]].
[[Image:Catabria01.jpg|thumb|300px|Citabria above [[Palo Alto, California|Palo Alto]] airfield]]
;{{flag|Turkey}}
{{aircraft specification|
*[[Turkish Army]]
;{{flag|Tonga}}
*[[Tonga Defence Services aviation|Tongan Maritime Force Air Force]]


==Specifications (7GCAA Citabria)==
|plane or copter?=plane
[[File:Catabria01.jpg|thumb|Citabria in flight]]
|jet or prop?=prop
{{Aircraft specs
|ref=Jane's All the World's Aircraft 1969–70<ref name="jawa69p308">Taylor 1969, p. 308</ref>
|prime units?=imp<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification,
met(ric) first for all others. You MUST choose a format, or no specifications will show -->
<!--
General characteristics
-->
|genhide=


|crew=one pilot
|crew=one
|capacity=one passenger
|capacity=one passenger
|length main= 22 ft 9 in
|length m=
|length alt= 6.9 m
|length ft=22
|length in=8
|span main= 33 ft 5 in
|length note=
|span alt= 10.2 m
|span m=
|height main= 6 ft 9 in
|span ft=33
|height alt= 2.4 m
|span in=5
|area main= 165 ft²
|span note=
|area alt= 15.3 m²
|height m=
|airfoil= NACA 4412
|height ft=6
|empty weight main= 1,110 lb
|height in=7+3/4
|empty weight alt= 503.5 kg
|height sigfig=3
|loaded weight main= 1,650 lb
|height note=
|loaded weight alt= 748 kg
|wing area sqm=
|useful load main= 540 lb
|wing area sqft=165
|useful load alt= 244.5 kg
|wing area note=
|max takeoff weight main= 1,650 lb
|aspect ratio=6.72:1
|max takeoff weight alt= 748 kg
|airfoil=NACA 4412
|empty weight kg=
|empty weight lb=1037
|empty weight note=
|gross weight kg=
|gross weight lb=1650
|gross weight note=
|fuel capacity={{convert|39|USgal|impgal L|abbr=on}}
|more general=
|more general=
<!--
Powerplant
-->
|eng1 number=1
|eng1 name=[[Lycoming O-320-A2B]]
|eng1 type=four cylinder, [[horizontally opposed]] aircraft engine
|eng1 kw=<!-- prop engines -->
|eng1 hp=150<!-- prop engines -->
|eng1 shp=<!-- prop engines -->


|prop blade number=2<!-- propeller aircraft -->
|engine (jet)=
|prop name=McCauley 1C172AGM fixed-pitch metal propeller
|type of jet=
|prop dia m=<!-- propeller aircraft -->
|number of jets=
|prop dia ft=<!-- propeller aircraft -->
|thrust main= lbf
|prop dia in=<!-- propeller aircraft -->
|thrust alt= kN
|prop dia note=
|thrust original=
|thrust more=
|afterburning thrust main= lbf
|afterburning thrust alt= kN
|engine (prop)= [[Lycoming O-320]]-A2B
|type of prop=
|number of props= 1
|power main= 150 hp
|power alt= 111.9 kW
|power original=
|power more=
|max speed main=
|max speed alt=
|max speed more=
|cruise speed main= 126 mph
|cruise speed alt= 202.8 km/h
|cruise speed more=
|never exceed speed main= 162 mph
|never exceed speed alt= 260.7 km/h
|stall speed main= 51 mph
|stall speed alt= 82.1 km/h
|stall speed more=
|range main= 500 mi
|range alt= 804.7 km
|range more=
|ceiling main= ft
|ceiling alt= m
|climb rate main= 1,120 ft/min
|climb rate alt= 5.69 m/s
|loading main= 10 lb/ft²
|loading alt= 48.9 kg/m²
|thrust/weight=
|power/mass main= 11 lb/hp
|power/mass alt= 6.7 kg/kW
|more performance=


<!--
|armament=
Performance
-->
|perfhide=

|max speed kmh=
|max speed mph=130
|max speed kts=
|max speed note=at sea level
|cruise speed kmh=
|cruise speed mph=125
|cruise speed kts=
|cruise speed note=at {{convert|8000|ft|m|abbr=on}}
|stall speed kmh=
|stall speed mph=50
|stall speed kts=
|stall speed note=(without flaps)
|never exceed speed kmh=
|never exceed speed mph=162
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=537
|range nmi=
|range note=(at max cruise speed)
|endurance=<!-- if range unknown -->
|ceiling m=
|ceiling ft=17000
|ceiling note=
|g limits=
|roll rate=<!-- aerobatic -->
|glide ratio=<!-- sailplanes -->
|climb rate ms=
|climb rate ftmin=1120
|climb rate note=
|time to altitude=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=*'''Take-off run to 50 ft (15 m):''' {{convert|630|ft|m|0|abbr=on}}
* '''Landing run from 50 ft (15 m):''' {{convert|755|ft|m|0|abbr=on}}
|avionics=
}}
}}


==References==
==See also==
{{aircontent
*{{cite web | url=http://aerofiles.com/_aeron.html | title=American airplanes: Aeronca | work=Aerofiles: A Century of American Aviation | accessdate=2006-08-12 }}
*{{cite web | url=http://aerofiles.com/_al.html | title=American airplanes: Al - av | work=Aerofiles: A Century of American Aviation | accessdate=2006-08-12 }}
*{{cite web | url=http://aerofiles.com/_ca.html | title=American airplanes: Ca - ci | work=Aerofiles: A Century of American Aviation | accessdate=2006-08-12 }}
*{{cite web | url=http://aerofiles.com/_bella.html | title=Bellanca | work=Aerofiles: A Century of American Aviation | accessdate=2006-08-12 }}
*{{cite book|author=Bellanca Aircraft Corporation|title=Pilot's operating manual: Bellanca Citabria, 1975-1977 Series|publisher=Bellanca Aircraft Corporation|year=1978}}
*{{cite web | url=http://www.joeld.net/citabria/history.html | author=Dirnberger, Joel | title=Citabria Pro History | work=A Brief History of the Citabria Pro | accessdate=2006-09-10 }}
* Gilbert, James. (Feb. 1965). "Champion Citabria: pilot report." Flying, pp. 57-60.
* Gilbert, James. (Apr. 1966). "And in this corner, the champ: a pilot report on the Champion Citabria." Flying, pp. 36-41.
*Type Certificate Data Sheet A-759, Revision 67. (Jun. 3, 2005.) Department of Transportation. Federal Aviation Administration.

==External links==
* [http://www.amerchampionaircraft.com/ American Champion Aircraft Corporation]
* [http://www.bellanca-championclub.com/ Bellanca-Champion Club]
* [http://www.rmk-museum.org.tr/english/exhibit/aviation.html#2/ Aviation displays at the Rahmi M Koç Museum]
*[http://www.popularaviation.com/Citabria/ Gallery of enthusiasts' photographs]

==Related content==
{{aircontent|

|sequence=
[[Aeronca Champ|7GCB]] -
[[Aeronca Champ|7KC]] -
[[Aeronca Champ|7GCBA]] -
'''7ECA''' -
'''7GCAA''' -
'''7GCBC''' -
'''7KCAB''' -
[[Decathlon (aircraft)|8KCAB]] -
[[American Champion Scout (aircraft)|8GCBC]]

|related=
|related=
*[[8KCAB Decathlon|8KCAB Decathlon and Super Decathlon]]
*[[Decathlon (aircraft)|8KCAB]]
*[[American Champion Scout (aircraft)|8GCBC]]
*[[8GCBC Scout]]

|similar aircraft=
|similar aircraft=
*Clipped-wing [[Piper Cub]]
*Clipped-wing [[Piper Cub]]
*Swick Clipped-wing [[Taylorcraft B|Taylorcraft]]
*Swick Clipped-wing [[Taylorcraft B|Taylorcraft]]
*[[Aviat Husky]]
*[[Aviat Husky]]

|lists=
|lists=

|see also=
|see also=

}}
}}


==References==
[[Category:U.S. civil utility aircraft 1960-1969]]
{{Reflist}}
[[Category:U.S. civil trainer aircraft 1960-1969]]
*Aircraft specification no. A-759. Revision 67. (Jun. 3, 2005.) Department of Transportation. Federal Aviation Administration.
[[Category:U.S. sports planes 1960-1969]]
*{{cite web | url=http://aerofiles.com/_aeron.html | title=American airplanes: Aeronca | work=Aerofiles: A Century of American Aviation | access-date=2006-08-12 }}
*{{cite web | url=http://aerofiles.com/_al.html | title=American airplanes: Al - av | work=Aerofiles: A Century of American Aviation | access-date=2006-08-12 | archive-url= https://web.archive.org/web/20060815075607/http://aerofiles.com/_al.html| archive-date= 15 August 2006 | url-status= live}}
*{{cite web | url=http://aerofiles.com/_ca.html | title=American airplanes: Ca - ci | work=Aerofiles: A Century of American Aviation | access-date=2006-08-12 | archive-url= https://web.archive.org/web/20060823142142/http://aerofiles.com/_ca.html| archive-date= 23 August 2006 | url-status= live}}
*{{cite web | url=http://aerofiles.com/_bella.html | title=Bellanca | work=Aerofiles: A Century of American Aviation | access-date=2006-08-12 | archive-url= https://web.archive.org/web/20060720235706/http://www.aerofiles.com/_bella.html| archive-date= 20 July 2006 | url-status= live}}
*{{cite book|author=Bellanca Aircraft Corporation|title=Pilot's operating manual: Bellanca Citabria, 1975-1977 Series|publisher=Bellanca Aircraft Corporation|year=1978}}
*{{cite web | url=http://www.joeld.net/citabria/history.html | author=Dirnberger, Joel | title=Citabria Pro History | work=A Brief History of the Citabria Pro | access-date=2006-09-10 }}
* {{cite magazine |last=Gilbert |first=James |title=Champion Citabria: Pilot Report |magazine=[[Flying (magazine)|Flying]] |date=February 1965 |volume=76 |issue=2 |pages=58–60 |url=https://books.google.com/books?id=x6cP6D0WSjEC}}
* {{cite magazine |last=Gilbert |first=James |title=And In This Corner, The Champ: A Pilot Report on the Champion Citabria |magazine=[[Flying (magazine)|Flying]] |date=April 1966 |volume=78 |issue=4 |pages=36–41 |url=https://books.google.com/books?id=cmBx0b22S9MC}}
*{{cite book |editor-last=Taylor |editor-first= John W. R. |editor-link=John W. R. Taylor |title=Jane's All the World's Aircraft 1969–70 |year=1969 |location=London |publisher=Sampson Low, Marston & Co., Ltd. |isbn=0-354-000-519}}

==External links==
{{commons category|American Champion Citabria}}
* [https://www.americanchampionaircraft.com/ American Champion Aircraft Corporation]

{{Aeronca Chief family}}
{{Champion Aircraft}}
{{Bellanca}}
{{American Champion}}
{{Aeronca model numbers}}

[[Category:1960s United States civil utility aircraft]]
[[Category:1960s United States civil trainer aircraft]]
[[Category:1960s United States sport aircraft]]
[[Category:Champion aircraft|Citabria]]
[[Category:American Champion aircraft|Citabria]]
[[Category:Bellanca aircraft|Citabria]]
[[Category:Glider tugs]]
[[Category:Aerobatic aircraft]]
[[Category:Single-engined tractor aircraft]]
[[Category:High-wing aircraft]]
[[Category:Aircraft first flown in 1964]]
[[Category:Aircraft with fixed conventional landing gear]]
[[Category:Single-engined piston aircraft]]

Latest revision as of 10:13, 12 December 2024

Citabria
General information
TypeLight utility aircraft and sports plane
ManufacturerAmerican Champion Aircraft
Bellanca
Champion Aircraft
Designer
StatusIn production[1]
Number builtover 5,238
History
Manufactured1964-present
Introduction date1964
First flight1964

The Citabria is a light single-engine, two-seat, fixed conventional gear airplane which entered production in the United States in 1964. Designed for flight training, utility and personal use, it is capable of sustaining aerobatic stresses from +5g to -2g. Its name, "airbatic" backwards, reflects this.

Production history

[edit]

The Citabria was designed and initially produced by Champion Aircraft Corporation, and was a derivative of designs the company had been building since acquiring the 7-series Champ from Aeronca in 1954. The model 7ECA Citabria entered production at Champion in 1964. The 7GCAA and 7GCBC variants, added in 1965, were joined by the 7KCAB in 1968.

In 1970, Champion was acquired by Bellanca Aircraft Corporation, which continued production of all of the Champion-designed variants. Bellanca introduced two designs with close connections to the Citabria: The 8KCAB Decathlon and the 8GCBC Scout. Production at Bellanca ended in 1980 and the company's assets were liquidated in 1982.

The Citabria designs passed through the hands of a number of companies through the 1980s, including a Champion Aircraft Company which was no relation to the Champion Aircraft of the 1960s. In that period, only one Citabria model was built—a 7GCBC marketed as "Citabria 150S." American Champion Aircraft Corporation acquired the Citabria, Decathlon, and Scout designs in 1989 and returned the 7ECA, 7GCAA, and 7GCBC models to production over a period of years.

Design

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The Citabria traces its lineage back to the Champ. The most noticeable external changes to the design are the Citabria's squared-off rudder surface, wingtips, and rear windows. Like the Champ, the Citabria features tandem seating. The fuselage and tail surfaces are constructed of welded metal tubing. The outer shape of the fuselage is created by a combination of wooden formers and longerons, covered with fabric. The cross-section of the metal fuselage truss is triangular, a design feature which can be traced all the way back to the earliest Aeronca C-2 design of the late 1920s.

1980-built Bellanca 7ECA Citabria

The strut-braced wings of the Citabria are, like the fuselage and tail surfaces, fabric covered, utilizing aluminum ribs. Most Citabrias were built with wooden spars. American Champion has been using aluminum spars in the aircraft it has produced and has, as well, made the aluminum-spar wings available for retrofit installation on older aircraft.

The landing gear of the Citabria is in a conventional arrangement. The main gear legs of most Citabrias are made of spring steel, though American Champion began to use aluminum gear legs in 2004. Early Citabrias were fitted with a steel tube main gear which uses an oleo strut for shock absorption. All of the variants are discussed in more detail below.

Operational history

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A Champion 7GCAA Citabria towing a Schweizer SGS 1-34 sailplane

When the Citabria was introduced, it was the only airplane being commercially produced in the United States which was certified for aerobatics. Citabrias were also popular as trainers—because of their conventional gear and their aerobatic capabilities—and as personal aircraft. They were also found in utility roles as bush planes—thanks to their short take off and landing (STOL) ability, agriculture, pipeline patrol, and as glider towplanes. Though variants of the design, and other better-suited designs have largely taken over the Citabria's utility roles, Citabrias remain popular as trainers, glider towplanes, and for personal use.

Variants

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7ECA, Citabria Standard, Citabria Aurora

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7ECA at Kyneton, Victoria

Introduced in 1964, the 7ECA was the first version of the design and utilized the Continental O-200-A engine of 100 horsepower (75 kW). When introduced, it featured wood-spar wings and oleo-shock main gear. Within the first year of production, Champion began offering the Lycoming O-235-C1 engine of 115 horsepower (86 kW) as an alternative to the Continental. In 1967, Champion switched to spring steel main gear legs; by then, the Lycoming engine had become the standard. On acquiring the design, Bellanca gave this model the name Citabria "Standard" and began using the 115 horsepower (86 kW) Lycoming O-235-K2C engine. When American Champion reintroduced the 7ECA in 1995 as the Citabria "Aurora, " the biggest change was the use of metal-spar wings; the most recent significant design change has been the switch to aluminum main gear legs in 2004.

7GCAA, Citabria 150, Citabria "A" Package, Citabria Adventure

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Bellanca 7GCAA

Introduced in 1965, the Champion 7GCAA, like the 7ECA, featured wood-spar wings and oleo-shock main gear. The major difference was in the engine, which in the 7GCAA was a Lycoming O-320-A2B of 150 horsepower (110 kW). Champion switched to spring steel main gear legs in 1967. Bellanca continued production of the 7GCAA as the Citabria "A" Package (a designation apparently begun by Champion), but with no significant design changes. American Champion's 7GCAA, reintroduced in 1997 as the Citabria "Adventure," is similar to earlier versions, with the exception of the metal-spar wings and the use of the Lycoming O-320-B2B engine of 160 horsepower (120 kW); the most recent significant design change has been the switch to aluminum main gear legs in 2004. An "Ultimate Adventure" version, with a Superior Vantage O-360-A3A2 engine of 180 horsepower (130 kW) and a composite propeller, is also produced by American Champion.

7GCBC, Citabria 150s, Citabria "C" Package, Citabria Explorer

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Bellanca 7GCBC

Champion introduced the 7GCBC in 1965. It was substantially similar to the 7GCAA of the same year, with a Lycoming O-320-A2B engine of 150 horsepower (110 kW), wood-spar wings, and spring steel main gear legs. The major differences between these two models are that the 7GCBC has a wingspan of 34.5 feet (10.5 m), 1-foot (0.30 m) longer than the 7ECA and 7GCAA, and carries wing flaps. Bellanca continued production of the 7GCBC, calling it the Citabria "C" Package (a designation apparently begun by Champion). American Champion's 7GCBC, reintroduced in 1994 as the Citabria "Explorer," is similar to earlier versions, with the exception of the metal-spar wings and the use of the Lycoming O-320-B2B of 160 horsepower (120 kW); the most recent significant design change has been the switch to aluminum main gear legs in 2004. A "High Country Explorer" version, with a Superior Vantage O-360-A3A2 engine of 180 horsepower (130 kW) and larger wheels, is also produced by American Champion.

7KCAB, Citabria "B" Package

[edit]
Bellanca 7KCAB

Champion introduced the 7KCAB in 1968. It was substantially similar to the 7GCAA of the same year, with wood-spar wings and spring steel main gear legs. The major differences between the 7GCAA and 7KCAB were in the fuel system and the engine oil system. The engine was replaced with a Lycoming IO-320-E2A of 150 horsepower (110 kW), while a header tank of 1.5 gallons—located beneath the instrument panel—was added to the fuel system. In addition, the carburetor was replaced with a fuel injection system, and a Christen Industries inverted oil system was fitted to the engine. All of these changes were made in order to allow for extended inverted flight, a mode not possible in the earlier models. Bellanca continued production of the 7KCAB as the Citabria "B" Package (a designation apparently begun by Champion).

Citabria Pro

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The 8KCAB Citabria Pro was first flown by Champion on 2 August 1968, and was a dedicated aerobatic aircraft based on the standard Citabria.[2] It was a parasol winged monoplane, with a revised wing section and a longer fuselage. The prototype had an open cockpit for a single pilot, but the design allowed for conversion to a two seat layout. The aircraft was powered by a 200 hp (150 kW) Lycoming IO-360 Special engine driving a two-bladed propeller.[2] It was never put into production at Champion nor by Bellanca which acquired the company and designs only a short time later.

Military operators

[edit]

The 7GCBC Citabria was used as an observation aircraft by the Turkish Army. One of these aircraft is displayed at the Rahmi M Koç Museum in Istanbul.

 Turkey
 Tonga

Specifications (7GCAA Citabria)

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Citabria in flight

Data from Jane's All the World's Aircraft 1969–70[2]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 22 ft 8 in (6.91 m)
  • Wingspan: 33 ft 5 in (10.19 m)
  • Height: 6 ft 7+34 in (2.03 m)
  • Wing area: 165 sq ft (15.3 m2)
  • Aspect ratio: 6.72:1
  • Airfoil: NACA 4412
  • Empty weight: 1,037 lb (470 kg)
  • Gross weight: 1,650 lb (748 kg)
  • Fuel capacity: 39 US gal (32 imp gal; 150 L)
  • Powerplant: 1 × Lycoming O-320-A2B four cylinder, horizontally opposed aircraft engine, 150 hp (110 kW)
  • Propellers: 2-bladed McCauley 1C172AGM fixed-pitch metal propeller

Performance

  • Maximum speed: 130 mph (210 km/h, 110 kn) at sea level
  • Cruise speed: 125 mph (201 km/h, 109 kn) at 8,000 ft (2,400 m)
  • Stall speed: 50 mph (80 km/h, 43 kn) (without flaps)
  • Never exceed speed: 162 mph (261 km/h, 141 kn)
  • Range: 537 mi (864 km, 467 nmi) (at max cruise speed)
  • Service ceiling: 17,000 ft (5,200 m)
  • Rate of climb: 1,120 ft/min (5.7 m/s)
  • Take-off run to 50 ft (15 m): 630 ft (192 m)
  • Landing run from 50 ft (15 m): 755 ft (230 m)

See also

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Related development

Aircraft of comparable role, configuration, and era

References

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  1. ^ "American Champion Aircraft". Amerchampionaircraft.com. Archived from the original on 2014-08-17. Retrieved 2014-06-17.
  2. ^ a b c Taylor 1969, p. 308
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