- Design and development
- Operational history
- Operators
- Specifications
- References
- External links
name=Piaggio P.16 | image=Piaggio P.16.jpg | size=300px | caption= }}{{Infobox Aircraft Type | type=Heavy bomber | national origin=Italy | manufacturer=Piaggio | designer= | first flight=1934 | introduced= | retired= | status=Canceled | primary user=Regia Aeronautica | more users= | produced= | number built=1 | variants with their own articles= }} |
The Piaggio P.16 was an Italian heavy bomber designed and built by Piaggio for the Regia Aeronautica (Italian Royal Air Force). Design and developmentThe P.16 was a three-engine shoulder-wing monoplane of mostly metal construction, with inverted gull wings.[1] Its wing was thick and semi-elliptical, and its tail was mounted high on the fuselage. It had retractable main landing gear and a spatted, non-retractable tailwheel.[1] In addition to bombs, its armament consisted of four 7.62-millimeter (0.3-inch) machine guns, of which two were mounted in the leading edge of the wing, one in a retractable dorsal turret, and one in the rear of the fuselage beneath the tail.[1] The bombardier (bomb-aimer) manned a compartment set behind the nose engine on the underside of the fuselage. Operational historyThe P.16 first flew in November 1934,[1] and an order for 12 aircraft was placed and then cancelled,[1] with preference given to the Piaggio P.32, which was produced from 1936 to 1939.[1] Operators- {{flag|Kingdom of Italy}}
Specifications{{Aircraft specs |ref=Italian Civil and Military aircraft 1930–1945[2] |prime units?=met |genhide= |crew=4 |capacity= |length m= |length ft=43 |length in=9.5 |length note= |span m= |span ft=72 |span in=2 |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= |height ft=11 |height in=5.75 |height note= |wing area sqm= |wing area sqft=753.2 |wing area note= |swept area sqm= |swept area sqft= |swept area note= |volume m3= |volume ft3= |volume note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb=18,590 |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=3 |eng1 name=Piaggio Stella P.IX R.C.40 |eng1 type=9-cyl. air-cooled radial piston engine |eng1 kw= |eng1 hp=700 |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= |max speed mph=248 |max speed kts= |max speed note=at {{convert|3,170|m|ft|abbr=on|0}} |max speed mach= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph=65 |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= |range miles=1,242 |range nmi= |range note= with {{convert|1,000|kg|lb|abbr=on|0}} of bombs , or {{convert|1,500|km|mi|abbr=on|0}} with {{convert|500|kg|lb|abbr=on|0}} of bombs |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= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude={{convert|6,000|m|ft|abbr=on|0}} in 17 minutes |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=
|guns=
- 2 x fixed {{convert|7.62|mm|in|abbr=on|3}} Breda-SAFAT machine guns in wing leading edge
- 1 x flexible{{convert|7.62|mm|in|abbr=on|3}} machine gun in dorsal turret
- 1 x flexible {{convert|7.62|mm|in|abbr=on|3}} machine gun in rear underside of fuselage
|bombs= {{convert|1,000|kg|lb|abbr=on|0}} |rockets= |missiles= |hardpoints= |hardpoint capacity= |hardpoint rockets= |hardpoint missiles= |hardpoint bombs= |hardpoint other= |avionics= }}{{aircontent |see also= |related= |similar aircraft= |sequence= |lists= }}References1. ^1 2 3 4 5 {{cite web|last1=Pearce|first1=William|title=Piaggio P.16 Bomber|url=https://oldmachinepress.com/2015/11/29/piaggio-p-16-bomber/|website=oldmachinepress.com|accessdate=9 May 2016}} 2. ^{{cite book|last=Thompson|first=Jonathan W.|title=Italian Civil and Military aircraft 1930–1945|publisher=Aero Publishers Inc.|location=New York|edition=1st|pages=219–220|isbn=0-8168-6500-0}}
External links{{commons category|Piaggio P.16}}- http://www.flightglobal.com/pdfarchive/view/1936/1936%20-%200073.html
{{Piaggio aircraft}} 6 : Italian bomber aircraft 1930–1939|Piaggio aircraft|Trimotors|Shoulder-wing aircraft|Aircraft first flown in 1934|Inverted gull-wing aircraft |