- Development and design
- Specifications
- See also
- References Notes Bibliography
| name=PZL-112 Junior | image= | caption= }}{{Infobox aircraft type | type=Trainer | national origin=Poland | manufacturer=EADS PZL Warszawa-Okecie | designer= | first flight=17 Jun 2000 | introduced= | retired= | status= | primary user= | number built=1 | developed from= | variants with their own articles=
}} |
The EADS PZL PZL-112 Junior is a Polish single engine, two-seat trainer built by PZL Warszawa-Okecie. Development and designThe PZL-112 Junior was designed by PZL Warszawa-Okecie in collaboration with the Warsaw University of Technology as a low-cost trainer for Polish flying clubs. It was originally known as the Koliber Junior as it used some components from the PZL-110 Koliber. Specifications{{Aircraft specs
|ref=Jane's All the World's Aircraft 2003-04
|prime units?=met
|genhide=
|crew=two
|capacity=
|length m=6.651
|length ft=
|length in=
|length note=
|span m=8.803
|span ft=
|span in=
|span note=
|height m=2.625
|height ft=
|height in=
|height note=
|wing area sqm=11.44
|wing area sqft=
|wing area note=
|airfoil=
|empty weight kg=520
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=750
|max takeoff weight lb=
|max takeoff weight note=
|more general=
|eng1 number=1
|eng1 name=Lycoming O-235-L2C
|eng1 type=Flat-four piston engine
|eng1 kw=
|eng1 hp=116
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=
|prop blade number=2
|prop name=Hoffmann HO-14HM-175-131
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=
|perfhide=
|max speed kmh=210
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=
|cruise speed kmh=97
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=80
|stall speed mph=
|stall speed kts=
|stall speed note=Flaps down
|never exceed speed kmh=262
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=750
|range miles=
|range nmi=
|range note=
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=4000
|ceiling ft=
|ceiling note=
|g limits=+4.4/-1.8
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=689
|climb rate note=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=65.56
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2
|disk loading lb/sqft=
|disk loading note=
|power/mass met=
|power/mass imp=
|power/mass note=
|thrust/weight=
|thrust/weight note=
|more performance
|avionics=
}}
See also{{aircontent
|related=*PZL-110 Koliber
|see also=
|similar aircraft=
}}References{{commons category|PZL aircraft}}NotesBibliography{{refbegin}}- {{cite book |editor-last= Jackson|editor-first= Paul |authorlink= |title= Jane's All the World's Aircraft 2003-04|year= 2003|publisher= Jane's Information Group|location=Coulsdon, Surrey, United Kingdom|isbn=0-7106-2537-5}}
{{refend}}{{PZL aircraft}} 4 : PZL aircraft|Polish civil trainer aircraft 2000–2009|Single-engined tractor aircraft|Low-wing aircraft |