<!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Short description| British touring aircraft}} {{Use dmy dates|date=May 2017}} {{Use British English|date=May 2017}} {{Infobox aircraft | name = Pirate | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = Three-seat touring aircraft | aim = | outcome = | related = | national_origin = United Kingdom | manufacturer = Pobjoy Airmotors and Aircraft Ltd, Rochester airport, Kent | design_group = | designer = Harold Boultbee | builder = | issuer = | status = | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = 1 | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = 25 June 1935 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }} The '''Pobjoy Pirate''' was a three-seat, high-wing monoplane designed to compete with the de Havilland Leopard Moth using a low-power but light Pobjoy radial engine. Flight tests showed the Pirate to be uncompetitive and its development was rapidly abandoned.

==Design and development==

The success of the three-seat, high-wing de Havilland Leopard Moth, introduced in 1933, had proved that there was a market for this class of aircraft.<ref name="OHdH">{{harvnb|Ord-Hume|2000|pp=340–1}}</ref> Until 1935 Pobjoy Airmotors Ltd had not previously built an aircraft, but concentrated successfully on engines.<ref>{{harvnb|Ord-Hume|2000|pp=587–9}}</ref> In June 1935 the company name was changed to Pobjoy Airmotors and Aircraft Ltd and at the same moment they introduced their only original aircraft design, the Pobjoy Pirate, aimed at the Leopard Moth market. They naturally chose to power it with one of their own seven cylinder radial engines. At the time, the most powerful variant was the 90&nbsp;hp (67&nbsp;kW) Niagara III, much less powerful than the 145&nbsp;hp (108&nbsp;kW) Gipsy Major 10 of the Leopard Moth. The Pobjoy, though was less than half the weight of the de Havilland engine and Pobjoy believed that with the advantage of this weight saving (about 160&nbsp;lb or 73&nbsp;kg) they could build a lighter and smaller aircraft that would perform as well.<ref name="OH">{{harvnb|Ord-Hume|2000|pp=453–4}}</ref>

The designer of the Pirate was the experienced Harold Boultbee, who had recently produced the Civilian Coupé, and construction began early in 1935. The high wings were straight edged, but tapered, slightly swept on the leading edge and fully slotted. The trailing edge carried differential ailerons and interacting flaps. A pair of V-shaped lift struts ran from the two wing spars down to the lower fuselage side where there was a universal joint to facilitate wing folding. The folding mechanism was unusual: unlocked, the wings slid forward and tipped leading edge down, so that when the front spar was released from its fitting the wings could fold rearwards and downwards about the rear spar. Because of the initial forward movement, the folded length was less than it would have been with conventional geometries.<ref name="OH"/>

The fuselage was of wooden construction, plywood-covered and tapering strongly in elevation to the tail. The fin was triangular and carried a semicircular rudder moving above the tailplane and elevators. The main undercarriage oleo legs were attached close to the fuselage end of the lift struts. A glazed cabin placed the pilot ahead of the two side-by-side seated passengers. Ahead of them, the Niagara, under a characteristically neat Pobjoy cowling with "helmet" exhaust ports drove a two-bladed propeller.<ref name="OH"/>

In mid-1935 Pobjoy were collaborating with Shorts over the Pobjoy powered Short Scion, so Short's test pilot, John Lankester Parker was available to try the Pirate. It first flew on 25 June and by 10 July had been in the air for a total of 70 minutes. Parker reported that the machine was underpowered and uncompetitive and it was never flown again. It was registered as ''G-ADEY''<ref>[http://www.caa.co.uk/application.aspx?catid=60&pagetype=65&appid=1&mode=reg&fullregmark=ADEY Registration details for ''G-ADEY'']</ref> but never carried these letters; it was broken up the following summer.<ref name="OH"/>

The Pirate was lighter and smaller than the Leopard Moth: the span was 3&nbsp;ft 6 in (1.07 m) or 10% smaller and the all-up weight 624&nbsp;lb (283&nbsp;kg, 28%) lighter, but this did not make up for the 38% decease in power.<ref name="OHdH"/><ref name="OH"/> <!-- ==Operational history== --> <!-- ==Variants== --> <!-- ==Units using this aircraft/Operators (choose)== -->

==Specifications== {{Aircraft specs |ref={{harvnb|Ord-Hume|2000|pp=454}} |prime units?=imp<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> <!-- General characteristics --> |genhide=

|crew= |capacity= |length m= |length ft= |length in= |length note= |span m= |span ft=34 |span in=0 |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=<!-- swing-wings --> |swept ft=<!-- swing-wings --> |swept in=<!-- swing-wings --> |swept note= |dia m=<!-- airships etc --> |dia ft=<!-- airships etc --> |dia in=<!-- airships etc --> |dia note= |width m=<!-- if applicable --> |width ft=<!-- if applicable --> |width in=<!-- if applicable --> |width note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft=180 |wing area note=estimate |swept area sqm=<!-- swing-wings --> |swept area sqft=<!-- swing-wings --> |swept area note= |volume m3=<!-- lighter-than-air --> |volume ft3=<!-- lighter-than-air --> |volume note= |aspect ratio=<!-- sailplanes --> |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb=1600 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift kg=<!-- lighter-than-air --> |lift lb=<!-- lighter-than-air --> |lift note= |more general= <!-- Powerplant --> |eng1 number=1 |eng1 name=Pobjoy Niagara III |eng1 type=7-cylinder radial |eng1 kw=<!-- prop engines --> |eng1 hp=90<!-- prop engines --> |eng1 kn=<!-- jet/rocket engines --> |eng1 lbf=<!-- jet/rocket engines --> |eng1 note= |power original= |thrust original= |eng1 kn-ab=<!-- afterburners --> |eng1 lbf-ab=<!-- afterburners -->

|eng2 number= |eng2 name= |eng2 type= |eng2 kw=<!-- prop engines --> |eng2 hp=<!-- prop engines --> |eng2 kn=<!-- jet/rocket engines --> |eng2 lbf=<!-- jet/rocket engines --> |eng2 note= |eng2 kn-ab=<!-- afterburners --> |eng2 lbf-ab=<!-- afterburners -->

|eng3 number= |eng3 name= |eng3 type= |eng3 kw=<!-- prop engines --> |eng3 hp=<!-- prop engines --> |eng3 kn=<!-- jet/rocket engines --> |eng3 lbf=<!-- jet/rocket engines --> |eng3 note= |eng3 kn-ab=<!-- afterburners --> |eng3 lbf-ab=<!-- afterburners --> |more power=

|prop blade number=<!-- propeller aircraft --> |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop note=

|rot number=<!-- helicopters --> |rot dia m=<!-- helicopters --> |rot dia ft=<!-- helicopters --> |rot dia in=<!-- helicopters --> |rot area sqm=<!-- helicopters --> |rot area sqft=<!-- helicopters --> |rot area note= <!-- Performance --> |perfhide=

|max speed kmh= |max speed mph=125 |max speed kts= |max speed note= |max speed mach=<!-- supersonic aircraft --> |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh=<!-- aerobatic --> |stall speed mph=<!-- aerobatic --> |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= |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=<!-- if range unknown --> |ceiling m= |ceiling ft= |ceiling note= |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |glide ratio=<!-- sailplanes --> |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms=<!-- sailplanes --> |sink rate ftmin=<!-- sailplanes --> |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=

|power/mass= |thrust/weight=

|more performance= <!-- Armament --> |armament=<!-- add bulleted list here or if you want to use the following specific parameters, remove this parameter--> |guns= |bombs= |rockets= |missiles= |hardpoints= |hardpoint capacity= |hardpoint rockets= |hardpoint missiles= |hardpoint bombs= |hardpoint other=

|avionics= }} <!-- ==See also== --> {{aircontent <!-- include as many lines are appropriate. additional lines/entries with carriage return. --> |see also= |related=<!-- related developments --> |similar aircraft=<!-- similar or comparable aircraft --> |lists=<!-- related lists --> }}

==References==

===Citations=== {{reflist}}

===Cited sources=== {{refbegin}} *{{cite book |title= British Civil Aircraft 1919-59|last=Jackson|first=A.J.| year=1960|volume= 2|publisher=Putnam Publishing |location=London }} *{{cite book |last1=Ord-Hume |first1=Arthur W. J. G. |title=British Light Aeroplanes |date=2000 |publisher=GMS Enterprises |location=Peterborough, UK |isbn=1-870384-76-8 }} {{refend}}

<!-- ==External links== -->

Category:1930s British civil utility aircraft Category:High-wing aircraft Category:Aircraft first flown in 1935