- Specifications
- References
{{short description|1920s French training aircraft}}name = S.42 | image = File:Bleriot SPAD S.42 L'Aéronautique December,1922.jpg | caption = }}{{Infobox aircraft type | type = biplane trainer | national origin =France | manufacturer = SPAD | designer = Louis Béchéreau | first flight = 6 August 1921 | primary user = Aéronautique Militaire | more users= | number built = 10 }} |
The SPAD S.42 was a French biplane trainer aircraft of the early 1920s, developed by Société Pour L'Aviation et ses Dérivés (SPAD) from prolific SPAD S.XIII fighter. Specifications{{Aircraft specs |ref=[1] |prime units?=met |genhide= |crew=1 |capacity= |length m=6.77 |length ft= |length in= |length note= |span m=8.65 |span ft= |span in= |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |swept m= |swept ft= |swept in= |swept note= |dia m= |dia ft= |dia in= |dia note= |width m= |width ft= |width in= |width note= |height m=2.65 |height ft= |height in= |height note= |wing area sqm=22.12 |wing area sqft= |wing area note= |swept area sqm= |swept area sqft= |swept area note= |volume m3= |volume ft3= |volume note= |aspect ratio= |airfoil= |empty weight kg=685 |empty weight lb= |empty weight note= |gross weight kg=1056 |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift kg= |lift lb= |lift note= |more general=
|eng1 number=1 |eng1 name=Hispano-Suiza 8Ab |eng1 type=V-8 water-cooled piston engine |eng1 kw= |eng1 hp=180 |eng1 shp= |eng1 kn= |eng1 lbf= |eng1 note= |power original= |thrust original= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 name= |eng2 type= |eng2 kw= |eng2 hp= |eng2 shp= |eng2 kn= |eng2 lbf= |eng2 note= |eng2 kn-ab= |eng2 lbf-ab= |eng3 number= |eng3 name= |eng3 type= |eng3 kw= |eng3 hp= |eng3 shp= |eng3 kn= |eng3 lbf= |eng3 note= |eng3 kn-ab= |eng3 lbf-ab= |more power= |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note= |rot number= |rot dia m= |rot dia ft= |rot dia in= |rot area sqm= |rot area sqft= |rot area note=
|perfhide= |max speed kmh=175 |max speed mph= |max speed kts= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh= |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=450 |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=5500 |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |disk loading kg/m2= |disk loading lb/sqft= |disk loading note= |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass= |thrust/weight= |more performance= }}
References{{commons category|Blériot-SPAD S.42}}1. ^{{cite web|url=https://www.aviafrance.com/spad-s-42-aviation-france-116.htm |title=SPAD S-42 - avion d'entrainement - Un siècle d'aviation française |publisher=Aviafrance.com |date=2004-01-19 |accessdate=2019-02-03}}
{{SPAD aircraft}} 4 : SPAD aircraft|Aircraft first flown in 1921|Biplanes|Single-engined tractor aircraft |