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Historical PZL P.11c

The Historical PZL P.11c is an American homebuilt aircraft that was designed and produced by Historical Aircraft Corporation of Nucla, Colorado. The aircraft is a 66% scale replica of the Polish PZL P.11c fighter and when it was available was supplied as a kit for amateur construction.[1]

PZL P.11c
Role Homebuilt aircraft
National origin United States
Manufacturer Historical Aircraft Corporation
Status Production completed
Developed from PZL P.11c

Design and development

The aircraft features a strut-braced high-wing, a single-seat open cockpit with a windshield, fixed conventional landing gear and a single engine in tractor configuration.[1]

The aircraft is made from welded steel tubing and wood, with its flying surfaces covered in doped aircraft fabric. Its 30.00 ft (9.1 m) span wing employs a NACA 2412 airfoil and has a wing area of 84.00 sq ft (7.804 m2). The cockpit width is 21 in (53 cm). The standard engine used is the 100 hp (75 kW) CAM 100 four stroke powerplant.[1][2]

The aircraft has a typical empty weight of 800 lb (360 kg) and a gross weight of 1,100 lb (500 kg), giving a useful load of 300 lb (140 kg). With full fuel of 11 U.S. gallons (42 L; 9.2 imp gal) the payload for the pilot and baggage is 234 lb (106 kg).[1]

The kit included prefabricated assemblies, the engine and scale fixed pitch propeller, basic VFR instruments, fabric and even paint. Also included were replica 7.9 mm machine guns and a ring gun site. The manufacturer indicated that the design was intended for novice builders and estimated the construction time from the supplied kit as 1400 hours.[1]

Specifications (PZL P.11c)

Data from AeroCrafter and The Incomplete Guide to Airfoil Usage[1][2]

General characteristics

  • Crew: one
  • Length: 18.30 ft (5.58 m)
  • Wingspan: 30.00 ft (9.14 m)
  • Wing area: 84.00 sq ft (7.804 m2)
  • Airfoil: NACA 2412
  • Empty weight: 800 lb (363 kg)
  • Gross weight: 1,100 lb (499 kg)
  • Fuel capacity: 11 U.S. gallons (42 L; 9.2 imp gal)
  • Powerplant: 1 × CAM 100 four cylinder, air-cooled, four stroke aircraft engine, 100 hp (75 kW)
  • Propellers: 2-bladed composite

Performance

  • Maximum speed: 105 mph (169 km/h, 91 kn)
  • Cruise speed: 90 mph (140 km/h, 78 kn)
  • Stall speed: 55 mph (89 km/h, 48 kn)
  • Range: 300 mi (480 km, 260 nmi)
  • Service ceiling: 12,500 ft (3,800 m)
  • Rate of climb: 800 ft/min (4.1 m/s)
  • Wing loading: 13.1 lb/sq ft (64 kg/m2)

Armament

References

  1. ^ a b c d e f Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 177. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1
  2. ^ a b Lednicer, David (2010). . Archived from the original on April 20, 2010. Retrieved January 2, 2014.

historical, american, homebuilt, aircraft, that, designed, produced, historical, aircraft, corporation, nucla, colorado, aircraft, scale, replica, polish, fighter, when, available, supplied, amateur, construction, 11crole, homebuilt, aircraftnational, origin, . The Historical PZL P 11c is an American homebuilt aircraft that was designed and produced by Historical Aircraft Corporation of Nucla Colorado The aircraft is a 66 scale replica of the Polish PZL P 11c fighter and when it was available was supplied as a kit for amateur construction 1 PZL P 11cRole Homebuilt aircraftNational origin United StatesManufacturer Historical Aircraft CorporationStatus Production completedDeveloped from PZL P 11cDesign and development EditThe aircraft features a strut braced high wing a single seat open cockpit with a windshield fixed conventional landing gear and a single engine in tractor configuration 1 The aircraft is made from welded steel tubing and wood with its flying surfaces covered in doped aircraft fabric Its 30 00 ft 9 1 m span wing employs a NACA 2412 airfoil and has a wing area of 84 00 sq ft 7 804 m2 The cockpit width is 21 in 53 cm The standard engine used is the 100 hp 75 kW CAM 100 four stroke powerplant 1 2 The aircraft has a typical empty weight of 800 lb 360 kg and a gross weight of 1 100 lb 500 kg giving a useful load of 300 lb 140 kg With full fuel of 11 U S gallons 42 L 9 2 imp gal the payload for the pilot and baggage is 234 lb 106 kg 1 The kit included prefabricated assemblies the engine and scale fixed pitch propeller basic VFR instruments fabric and even paint Also included were replica 7 9 mm machine guns and a ring gun site The manufacturer indicated that the design was intended for novice builders and estimated the construction time from the supplied kit as 1400 hours 1 Specifications PZL P 11c EditData from AeroCrafter and The Incomplete Guide to Airfoil Usage 1 2 General characteristicsCrew one Length 18 30 ft 5 58 m Wingspan 30 00 ft 9 14 m Wing area 84 00 sq ft 7 804 m2 Airfoil NACA 2412 Empty weight 800 lb 363 kg Gross weight 1 100 lb 499 kg Fuel capacity 11 U S gallons 42 L 9 2 imp gal Powerplant 1 CAM 100 four cylinder air cooled four stroke aircraft engine 100 hp 75 kW Propellers 2 bladed compositePerformance Maximum speed 105 mph 169 km h 91 kn Cruise speed 90 mph 140 km h 78 kn Stall speed 55 mph 89 km h 48 kn Range 300 mi 480 km 260 nmi Service ceiling 12 500 ft 3 800 m Rate of climb 800 ft min 4 1 m s Wing loading 13 1 lb sq ft 64 kg m2 Armament Guns replica 7 9 mm machine gunsReferences Edit a b c d e f Purdy Don AeroCrafter Homebuilt Aircraft Sourcebook Fifth Edition page 177 BAI Communications 15 July 1998 ISBN 0 9636409 4 1 a b Lednicer David 2010 The Incomplete Guide to Airfoil Usage Archived from the original on April 20 2010 Retrieved January 2 2014 Retrieved from https en wikipedia org w index php title Historical PZL P 11c amp oldid 1066041934, wikipedia, wiki, book, books, library,

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