- Design and development
- Specifications (Horn Lil' Trouble)
- References
| name=Horn Lil' Trouble | image= | caption= }}{{Infobox Aircraft Type | type=Homebuilt aircraft | national origin=United States of America | manufacturer= | designer=Mark Horn | first flight=1953 | introduced= | retired= | status= | primary user= | more users= | produced= | number built=1 | program cost= | unit cost=$1500 in 1953 | developed from= | variants with their own articles=
}} |
The Horn Lil' Trouble is a single-seat low-wing, homebuilt aircraft designed by Mark Horn.[1] Design and developmentThe wings and reversed struts were sourced from a Monocoupe. The fuselage is a modified Aeronca Defender. Landing gear and tail section is from a Piper Cub. The aircraft features dual controls with a jump seat in the baggage compartment that can accommodate a {{convert|90|lb|kg|0|abbr=on}} or lighter co-pilot.[2] Specifications (Horn Lil' Trouble) {{Aircraft specs
|ref=Sport Aviation
|prime units?=kts
|genhide=
|crew=
|capacity=
|length m=
|length ft=17
|length in=
|length note=
|span m=
|span ft=
|span in=
|span note=
|height m=
|height ft=5
|height in=4
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=910
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|fuel capacity={{convert|10|u.s.gal}}
|more general=
|eng1 number=1
|eng1 name=Continental C-90
|eng1 type=
|eng1 kw=
|eng1 hp=90
|prop blade number=2
|prop name=71-51 McCauley propeller
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=
|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=165
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=80
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=
|ceiling ft=12,500
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=1700
|climb rate note=
|time to altitude=
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}
References1. ^{{cite book|title=Jane's all the world's aircraft|author=Frederick Thomas Jane}}
2. ^{{cite journal|magazine=Sport Aviation|date=March 1959}}
1 : Homebuilt aircraft |