aircraft specifications
OrderedDict([('plane or copter?', 'copter'), ('jet or prop?', 'prop'), ('ref', 'Boeing CH-47D/F,<ref>{{cite web |url=http://www.boeing.com/defense/ch-47-chinook/#/technical-specifications |title=CH-47 Technical Specifications |publisher=Boeing |accessdate=19 March 2016 |archive-url=https://web.archive.org/web/20160313152930/http://www.boeing.com/defense/ch-47-chinook/#/technical-specifications |archive-date=13 March 2016 |dead-url=no }}</ref> Army Chinook file,<ref>{{cite web |url=http://www.army.mil/article/137584/ |title=CH-47 CHINOOK HELICOPTER |date=4 November 2014 |work=army.mil |accessdate=19 March 2016 |archive-url=https://web.archive.org/web/20160329054721/http://www.army.mil/article/137584 |archive-date=29 March 2016 |dead-url=no }}</ref> International Directory<ref name="Frawley Military">Frawley, Gerard: \'\'The International Directory of Military Aircraft\'\', p. 49. Aerospace Publications Pty Ltd, 2002. {{ISBN|1-875671-55-2}}.</ref>'), ('crew', 'three (pilot, copilot, flight engineer or loadmaster)'), ('capacity', "<br />\n** 33–55 troops ''or''\n** 24 [[Litter (rescue basket)|litters]] and 3 attendants ''or''"), ('payload main', '24,000 lb'), ('payload alt', '10,886 kg'), ('length main', '98 ft 10 in<ref name=Boeing_CH-47F>{{cite web|url=http://www.boeing.com/defense/ch-47-chinook/#/technical-specifications|title=Boeing: H-47 Chinook|website=www.boeing.com|access-date=19 March 2016|archive-url=https://web.archive.org/web/20160313152930/http://www.boeing.com/defense/ch-47-chinook/#/technical-specifications|archive-date=13 March 2016|dead-url=no}}</ref>'), ('length alt', "30.1 m)\n* '''Fuselage length:''' 52 ft (15.85 m)\n* '''Fuselage width:''' 12 ft 5 in<ref name=Boeing_CH-47F/> (3.78 m"), ('span main', '60 ft '), ('span alt', '18.3 m'), ('height main', '18 ft 11 in'), ('height alt', '5.7 m'), ('area main', '5,600 ft<sup>2</sup>'), ('area alt', '520 m<sup>2</sup>'), ('empty weight main', '24,578 lb'), ('empty weight alt', '11,148 kg'), ('loaded weight main', ''), ('loaded weight alt', ''), ('max takeoff weight main', '50,000 lb'), ('max takeoff weight alt', '22,680 kg'), ('more general', ''), ('engine (prop)', '[[Lycoming T55|Lycoming T55-GA-714A]]'), ('type of prop', '[[turboshaft]]'), ('number of props', '2'), ('power main', '4,733 [[horsepower|shp]]'), ('power alt', '3,529 kW'), ('max speed main', '170 [[knot (unit)|knots]]'), ('max speed alt', '196 mph, 315 km/h'), ('cruise speed main', '160 kt'), ('cruise speed alt', '184 mph, 296 km/h'), ('stall speed main', ''), ('stall speed alt', ''), ('never exceed speed main', ''), ('never exceed speed alt', ''), ('range main', '400 [[nautical mile|nmi]]'), ('range alt', '450 mi, 741 km'), ('combat radius main', '200 nmi'), ('combat radius alt', '230 mi, 370 km'), ('combat radius more', ''), ('ferry range main', '1,216 nmi'), ('ferry range alt', "1,400 mi, 2,252 km<ref>United States of America. Naval Training Equipment Center. Department of the Navy. ''Recognition Study Cards – US and Foreign Aircraft''. Device 5E14H. LSN 6910-LL-C006462. Orlando, Florida. 1982. 55 Cards. '''Annotation''': 2252 kilometers.</ref>"), ('ferry range more', ''), ('ceiling main', '20,000 ft'), ('ceiling alt', '6100 m'), ('climb rate main', '1,522 ft/min'), ('climb rate alt', '7.73 m/s'), ('loading main', '9.5 lb/ft<sup>2</sup>'), ('loading alt', '47 kg/m<sup>2</sup>'), ('power/mass main', '0.28 hp/lb'), ('power/mass alt', '460 W/kg'), ('armament', '* Up to 3 pintle-mounted medium machine guns (1 on loading ramp and 2 at shoulder windows), generally 7.62 mm (0.308 in) [[M240 machine gun|M240]]/[[FN MAG]] machine guns, and can be armed with the 7.62 mm [[Minigun|M134]] rotary machine gun'), ('avionics', '* Rockwell Collins Common Avionics Architecture System (CAAS) (MH-47G/CH-47F)')])