- Specifications (acrobatic)
- References Notes
- External links
| name=Sbach 342 (XA42) | image=Sbach Xtremeair 342 Private D-EIXA, BBJ Bitburg (Bitburg Air Base), Germany PP1278607092.jpg | caption=On Bitburg Airport, Germany, 2010. }}{{Infobox Aircraft Type | type=Aerobatic monoplane | national origin=Germany | manufacturer=XtremeAir GmbH | designer= | first flight= | introduced= | retired= | status= | produced= | primary user= | number built=60+ | developed from= XtremeAir Sbach 300 | variants with their own articles= | developed into=
}} |
The XtremeAir Sbach 342 (XA42) is a German high performance two-seat aerobatic and touring monoplane designed by Philipp Steinbach with Albert Mylius and built by XtremeAir GmbH of Hecklingen. The Sbach 342 (a marketing name for the XA42) is a composite structure low-wing monoplane with a fixed conventional landing gear with a tailwheel and carbon fiber fuselage. Specifications (acrobatic){{Aircraft specs
|ref=
|prime units?=met
|genhide=
|crew=1
|capacity=2
|length m=6.67
|length ft=21
|length in=11
|length note=
|span m=7.5
|span ft=24
|span in=7
|span note=
|height m=2.54
|height ft=8
|height in=4
|height note=
|wing area sqm=11.25
|wing area sqft=121.1
|wing area note=
|airfoil=PS-1-16 (wing), PS-1-09 (wing tip), DU86-MOD1 (horizontal tail including elevator and vertical tail including rudder)
|empty weight kg=670
|empty weight lb=1477
|empty weight note=
|gross weight kg=850
|gross weight lb=1874
|gross weight note=for acrobatic flight, 999 kg (2,200 lb) for utility flight
|fuel capacity= 275 l (72.6 US gal) total, 273 l (72.1 US gal) usable, 64 l (16.9 US gal) usable for aerobatics
|more general=
|eng1 number=1
|eng1 name=Lycoming AEIO-580-B1A
|eng1 type=horizontally-opposed six-cylinder four stroke piston engine
|eng1 kw=235
|eng1 hp=315
|eng1 shp=
|eng1 note=at 2,700 rpm
|more power=
|prop blade number=3
|prop name=MT-Propeller MTV-9-B-C/C203-20d
|prop dia m=2.03
|prop dia ft=6
|prop dia in=8
|prop dia note=± 5 mm
|perfhide=
|max speed kmh=417
|max speed mph=259
|max speed kts=225
|max speed note=
|cruise speed kmh=343
|cruise speed mph=213
|cruise speed kts=185
|cruise speed note=
|stall speed kmh=100
|stall speed mph=62
|stall speed kts=54
|stall speed note=
|never exceed speed kmh=417
|never exceed speed mph=259
|never exceed speed kts=225
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=1296
|range miles=806
|range nmi=700
|range note=at 73% power and 4,000 ft with 60 min reserve
|ferry range km=1945
|ferry range miles=1208
|ferry range nmi=1050
|ferry range note=at 50% power at 10,000 ft with 60 min reserve
|ceiling m=4572
|ceiling ft=15000
|ceiling note=
|g limits=± 10
|roll rate=450 °/sec
|glide ratio=1:7
|climb rate ms=16.59
|climb rate ftmin=3266
|climb rate note= in acrobatic flight, 13.82 m/s (2,720 ft/min) in utility flight
|time to altitude=
|lift to drag=
|wing loading kg/m2=75.5
|wing loading lb/sqft=15.5
|wing loading note=in acrobatic flight, 84.4 kg/m2 (17.3 lb/sq ft)
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=2.01 kW/kg (1.22 hp/lb) in acrobatic configuration, 2.24 kW/kg (1.37 hp/lb) in utility configuration
|thrust/weight=
|more performance=
- Fuel flow: 57 L/h (15.1 US gal/h)
|avionics=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}ReferencesNotes1. ^1 {{cite web |author1=XtremeAir GmbH |title=Airplane Flight Manual XA42 |url=http://akvictoria.by/wp-content/uploads/2016/02/XA42.pdf |publisher=akvictoria.by |accessdate=30 June 2018 |language=en |date=27 January 2011}}
[1]
}}External links{{commons category|XtremeAir XA42}}- XtremeAir GmbH - company website
{{XtremeAir aircraft}}{{aero-2000s-stub}} 6 : German sport aircraft 2000–2009|Aerobatic aircraft|Single-engined tractor aircraft|Low-wing aircraft|Aircraft first flown in 2008|Conventional landing gear |