SPCA 20

SPCA

Industry	Aerospace
Products	Aircraft

The SPCA 20 was a French-designed seaplane intended for use as a torpedo bomber. It featured a low-wing monoplane layout and was constructed entirely from metal.

Specifications

{{Aircraft specs |ref=Aviafrance:SPCA 20 |prime units?=met |genhide=

|crew=4 |length m=18.62 |length note= |span m=26.22 |span note= |height m=6.40 |height note= |wing area sqm=123 |wing area note= |aspect ratio= |airfoil= |empty weight kg=4300 |empty weight note= |gross weight kg=7300 |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= | eng1 number=2 | eng1 name=Gnome-Rhône 9Ae Jupiter | eng1 type=9-cylinder air-cooled radial piston engines, direct-drive | eng1 hp=480

| prop blade number=2 | prop name=fixed pitch propellers | prop dia m= | prop dia ft= | prop dia in= | prop dia note= | max speed kmh=180 | max speed note= | 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=1200 | 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=5000 | ceiling note= | climb rate ms= | climb rate ftmin= | climb rate note= | time to altitude= | wing loading kg/m2= | fuel consumption kg/km= | fuel consumption lb/mi= | power/mass= | thrust/weight=

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