Jump to content

FFA AS 202 Bravo: Difference between revisions

From Wikipedia, the free encyclopedia
Browse history interactively
← Previous edit
Content deleted Content added
VisualWikitext
m v2.02 - Repaired 1 link to disambiguation page - (You can help) - McCauley
m Reverted edit by 77.117.207.98 (talk) to last version by Nimbus227
 
(12 intermediate revisions by 9 users not shown)
Line 1: Line 1:
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
{|{{Infobox Aircraft Begin
{|{{Infobox aircraft begin
|name = AS/SA 202 ''Bravo''
|name = AS/SA 202 ''Bravo''
|image = FFA AS-202 Bravo N7746B-090117-01-8.jpg
|image = FFA AS-202 Bravo N7746B-090117-01-8.jpg
|caption =
|caption =
}}{{Infobox Aircraft Type
}}{{Infobox aircraft type
|type = Civil light aircraft
|type = Civil light aircraft
|national origin=[[Switzerland]]/[[Italy]]
|national origin=[[Switzerland]]/[[Italy]]<br>[[Germany]] NG models
|manufacturer = [[Flug- und Fahrzeugwerke Altenrhein|FFA]]/[[SIAI-Marchetti]]
|manufacturer = [[Flug- und Fahrzeugwerke Altenrhein|FFA]]/[[SIAI-Marchetti]]<br>GOMOLZIG Flugzeug und Maschinenbau
|designer =
|designer =
|first flight = 9 March 1969
|first flight = 9 March 1969
Line 15: Line 15:
|primary user = [[Indonesian Air Force]]
|primary user = [[Indonesian Air Force]]
|more users = [[Ugandan Air Force]]
|more users = [[Ugandan Air Force]]
|produced = 1969–1991
|produced = 1969–1991<br>2020-today
|number built = 214
|number built = 214
|unit cost =
|unit cost =
Line 41: Line 41:
: With 180 hp [[Lycoming AEIO-360]]-B1F engine, constant speed propeller, third aft seat, fully aerobatic.
: With 180 hp [[Lycoming AEIO-360]]-B1F engine, constant speed propeller, third aft seat, fully aerobatic.
;AS/SA 202/26A
;AS/SA 202/26A
:With 195 kW (260hp) [[Lycoming O-540|Lycoming AEIO-540]] engine. Only one aircraft manufactured so far.
:With 195 kW (260hp) [[Lycoming O-540|Lycoming AEIO-540]] engine. Only one aircraft was manufactured so far.
;AS 32T Turbo Trainer
;AS 32T Turbo Trainer
:Two-seat tandem trainer aircraft, powered by a 268 kW (360-hp) [[Allison Model 250|Allison 250-B17C]] turboprop engine. Only one aircraft manufactured.
:Two-seat tandem trainer aircraft, powered by a 268 kW (360-hp) [[Allison Model 250|Allison 250-B17C]] turboprop engine. Only one aircraft was manufactured.
;[[FFT Eurotrainer 2000|FFA 2000 / FFT 2000 / Eurotrainer 2000]]
;[[FFT Eurotrainer 2000|FFA 2000 / FFT 2000 / Eurotrainer 2000]]
:Composite derivative
:Composite derivative
;Gomolzig AS-202 BRAVO NG

modern version of the FFA AS 202 Bravo, since 2020
==Operators==
==Operators==


Line 78: Line 79:


==Specifications (202/15)==
==Specifications (202/15)==

{{Aircraft specs
{{Aircraft specs
|ref=Jane's All the World's Aircraft 1976-77<ref name=JAWA1976-77>{{cite book |title=Jane's All the World's Aircraft 1976-77 |editor1-last=Taylor |editor1-first=John W.R. |edition=67th |year=1976 |publisher=Jane's Yearbooks |location=London |isbn=0-3540-0538-3 |pages=164-165}}</ref>
|ref=''Jane's All the World's Aircraft 1976-77'' <ref name=JAWA1976-77>{{cite book |title=Jane's All the World's Aircraft 1976-77 |editor1-last=Taylor |editor1-first=John W.R. |edition=67th |year=1976 |publisher=Jane's Yearbooks |location=London |isbn=0-3540-0538-3 |pages=164–165}}</ref>
|prime units?=met
|prime units?=met
<!--
<!--
Line 95: Line 95:
|wing area note=
|wing area note=
|aspect ratio=<!-- sailplanes -->
|aspect ratio=<!-- sailplanes -->
|airfoil='''root:''' [[NACA airfoil| NACA 63<sub>2</sub>618 modified 17.63%]]; '''tip:''' [[NACA airfoil|NACA 63<sub>2</sub>415 modified 15%]]
|airfoil='''root:''' [[NACA airfoil|NACA 63<sub>2</sub>618 modified 17.63%]]; '''tip:''' [[NACA airfoil|NACA 63<sub>2</sub>415 modified 15%]]
|empty weight kg=630
|empty weight kg=630
|empty weight note=
|empty weight note=
Line 103: Line 103:
|max takeoff weight note=(and MLW) aerobatic
|max takeoff weight note=(and MLW) aerobatic
::::{{cvt|999|kg|0}} (and MLW) utility
::::{{cvt|999|kg|0}} (and MLW) utility
|fuel capacity={{cvt|140|l|USgal impgal|1}} in two wing leading-edge tanks
|fuel capacity={{cvt|140|L|USgal impgal|1}} in two wing leading-edge tanks
|more general=
|more general=
<!--
<!--
Line 124: Line 124:
|max speed note=(utility at MTOW) at sea level
|max speed note=(utility at MTOW) at sea level
|cruise speed kmh=211
|cruise speed kmh=211
|cruise speed note=(utility at MTOW) maximum ; 75% power at {{cvt|2440|m|0}}
|cruise speed note=(utility at MTOW) maximum; 75% power at {{cvt|2440|m|-3}}
::::{{cvt|203|km/h|mph kn}} (utility at MTOW) economical ; 66% power at {{cvt|3050|m|0}}
::::{{cvt|203|km/h|mph kn}} (utility at MTOW) economical; 66% power at {{cvt|3050|m|-3}}
|stall speed kmh=110
|stall speed kmh=110
|stall speed note=flaps up
|stall speed note=flaps up
Line 139: Line 139:
|endurance=<!-- if range unknown -->
|endurance=<!-- if range unknown -->
|ceiling m=4265
|ceiling m=4265
|ceiling sigfig=2
|ceiling note=
|ceiling note=
|g limits=<!-- aerobatic -->
|g limits=<!-- aerobatic -->
Line 149: Line 150:
|fuel consumption kg/km=
|fuel consumption kg/km=
|power/mass={{cvt|0.068|hp/lb|order=flip}}
|power/mass={{cvt|0.068|hp/lb|order=flip}}
|more performance=<!--</br>
|more performance=
*'''Take-off run:''' {{cvt|235|m|0}}
*'''Take-off distance to {{cvt|15|m|0}}:''' {{cvt|475|m|0}}
*'''Landing run:''' {{cvt|130|m|0}}
*'''Landing distance from {{cvt|15|m|0}}:''' {{cvt|415|m|0}}-->

|avionics=
|avionics=
}}
}}


==See also==
==See also==
⚫
{{commons category|FFA AS-202 Bravo}}
{{aircontent
{{aircontent
|related=
|related=
|similar aircraft=
|similar aircraft=
|sequence=
|lists=
|lists=
* [[List of civil aircraft]]
* [[List of civil aircraft]]
Line 171: Line 165:


==References==
==References==
⚫
{{commons category|FFA AS-202 Bravo}}
{{reflist}}
{{reflist}}

<!-- ==External links== -->


{{Flug- und Fahrzeugwerke Altenrhein aircraft}}
{{Flug- und Fahrzeugwerke Altenrhein aircraft}}
{{Savoia-Marchetti aircraft}}
{{Savoia-Marchetti aircraft}}
{{Portal bar|Italy|Companies|Aviation}}


⚫
[[Category:FFA aircraft|Bravo]]
⚫
[[Category:Savoia-Marchetti aircraft]]
[[Category:1960s international civil utility aircraft]]
[[Category:1960s international civil utility aircraft]]
[[Category:Single-engined tractor aircraft]]
[[Category:Single-engined tractor aircraft]]
⚫
[[Category:FFA aircraft|Bravo]]
[[Category:Low-wing aircraft]]
[[Category:Low-wing aircraft]]
⚫
[[Category:Savoia-Marchetti aircraft]]
[[Category:Aircraft first flown in 1969]]
[[Category:Aircraft first flown in 1969]]

Latest revision as of 01:59, 24 November 2024

AS/SA 202 Bravo
Role Civil light aircraft
National origin Switzerland/Italy
Germany NG models
Manufacturer FFA/SIAI-Marchetti
GOMOLZIG Flugzeug und Maschinenbau
First flight 9 March 1969
Retired Patria Pilot Training 2011
Status Active
Primary users Indonesian Air Force
Ugandan Air Force
Produced 1969–1991
2020-today
Number built 214
Variants FFT Eurotrainer 2000

The AS/SA 202 Bravo is a two to three-seat civil light aircraft jointly designed and manufactured by the Swiss company Flug- und Fahrzeugwerke Altenrhein (FFA) and the Italian company Savoia-Marchetti. The aircraft was designated the AS 202 in Switzerland, and the SA 202 in Italy.

Savoia-Marchetti manufactured the wings, undercarriage and engine installation, while FFA manufactured the fuselage, tail and controls, while both companies had assembly plants manufacturing the complete aircraft.

The first Swiss model flew on 9 March 1969, the first Italian aircraft following on 8 May.

Bravo is a rugged all-metal low-wing monoplane with a full vision canopy. Its tricycle landing gear is fixed.

34 15s and 180 18s were built, with most in service with military customers. The biggest civil operator was Patria Pilot Training at Helsinki-Malmi Airport, Finland during 2000–2011.

Variants

[edit]
AS/SA 202/10
With 115 hp Lycoming O-235-C2A engine
AS/SA 202/15
With 150 hp Lycoming O-320-E2A engine, fixed pitch propeller, optional third aft seat
AS/SA 202/18A
With 180 hp Lycoming AEIO-360-B1F engine, constant speed propeller, third aft seat, fully aerobatic.
AS/SA 202/26A
With 195 kW (260hp) Lycoming AEIO-540 engine. Only one aircraft was manufactured so far.
AS 32T Turbo Trainer
Two-seat tandem trainer aircraft, powered by a 268 kW (360-hp) Allison 250-B17C turboprop engine. Only one aircraft was manufactured.
FFA 2000 / FFT 2000 / Eurotrainer 2000
Composite derivative
Gomolzig AS-202 BRAVO NG

modern version of the FFA AS 202 Bravo, since 2020

Operators

[edit]

Civil operators

[edit]
  •  Finland
    • Patria Pilot Training – 7 aircraft in 2000–2011. Patria's Bravos are ex-British Aerospace Flying College aircraft. BAE Flying College owned 11 aircraft, but 1 was lost in Scotland claiming 2 lives. Remaining 10 aircraft were sold to private Finnish flying school Pilot Factory, which merged with Patria in 2004–2005.

7 aircraft out of original 10 remain in service. During merger with Patria, one aircraft was sold to private owner. Night-time accident at Helsinki-Malmi airport in 2002 claimed no lives but hull was damaged beyond repair. In August 2010 one aircraft veered off the runway at Helsinki-Malmi and was written off.

Patria's Bravos were replaced with Tecnam P2002JF.

  •  Uganda
    • Uganda Central Flying School – 8 aircraft.

Military operators

[edit]

Former military operators

[edit]

Specifications (202/15)

[edit]

Data from Jane's All the World's Aircraft 1976-77 [1]

General characteristics

  • Crew: 1 or 2
  • Length: 7.5 m (24 ft 7 in)
  • Wingspan: 9.75 m (32 ft 0 in)
  • Height: 2.81 m (9 ft 3 in)
  • Wing area: 13.86 m2 (149.2 sq ft)
  • Airfoil: root: NACA 632618 modified 17.63%; tip: NACA 632415 modified 15%
  • Empty weight: 630 kg (1,389 lb)
  • Max takeoff weight: 885 kg (1,951 lb) (and MLW) aerobatic
999 kg (2,202 lb) (and MLW) utility
  • Fuel capacity: 140 L (37.0 US gal; 30.8 imp gal) in two wing leading-edge tanks
  • Powerplant: 1 × Lycoming O-320-E2A 4-cylinder air-cooled horizontally-opposed piston engine, 112 kW (150 hp)
  • Propellers: 2-bladed McCauley 1C172 MGM, 1.88 m (6 ft 2 in) diameter fixed-pitch propeller

Performance

  • Maximum speed: 211 km/h (131 mph, 114 kn) (utility at MTOW) at sea level
  • Cruise speed: 211 km/h (131 mph, 114 kn) (utility at MTOW) maximum; 75% power at 2,440 m (8,000 ft)
203 km/h (126 mph; 110 kn) (utility at MTOW) economical; 66% power at 3,050 m (10,000 ft)
  • Stall speed: 110 km/h (68 mph, 59 kn) flaps up
89 km/h (55 mph; 48 kn) flaps down
  • Never exceed speed: 322 km/h (200 mph, 174 kn) (utility at MTOW)
  • Range: 890 km (550 mi, 480 nmi) max fuel no reserve
  • Service ceiling: 4,265 m (14,000 ft)
  • Rate of climb: 3.22 m/s (633 ft/min)
  • Wing loading: 72.2 kg/m2 (14.8 lb/sq ft)
  • Power/mass: 0.112 kW/kg (0.068 hp/lb)

See also

[edit]

Related lists

References

[edit]
Wikimedia Commons has media related to FFA AS-202 Bravo.
  1. ^ Taylor, John W.R., ed. (1976). Jane's All the World's Aircraft 1976-77 (67th ed.). London: Jane's Yearbooks. pp. 164–165. ISBN 0-3540-0538-3.
Retrieved from "https://en.wikipedia.org/enwiki/w/index.php?title=FFA_AS_202_Bravo&oldid=1259229143"