|National origin||United States|
|Manufacturer||Parks Aircraft Division, Parks Air Lines, Parks Air College|
Design and development
Based in St.Louis, pilot, salesman and entrepreneur Oliver Parks founded an air school, airline and aircraft manufacturing business shortly after Lindbergh's 1927 transatlantic flight. Parks bought the rights to the Kreider-Reisner Challenger and modified it for production. The P-1 was built in a new facility in Cahokia, Illinois.
The P-1 was both sold as a commercial aircraft and placed into service as a trainer at Parks Air College. Although the OX-5 engine was out of production since 1917, there were still enough war surplus engines available at low enough cost to justify installing them on the 1929 design. This made the P-1 the last new aircraft produced using the outdated engine. Parks located his engines by sending out his associate, Joeseph Wecker, to buy OX-5 engines from flight schools in the region. Production ended at number 45, before the onset of the Great Depression and the temporary takeover of the company by the Detroit Aircraft Corporation.
While part of the Detroit Aircraft Corporation, one experimental P-1 (X289W) was modified with a faired in, tail mounted, all-plane parachute. It was filmed in a live deployment for Paramount Sound News. The 60 ft diameter Russell parachute was designed to hold 2600 to 3000 lbs. A secondary 24 ft diameter parachute was installed for the pilot.
- Parks P-1
- 45 units built, based on the Kreider-Reisner Challenger.
- Parks P-1H
- Powered by a 100hp Kinner K-5, received ATC on 23 November 1932. 7 aircraft modified as the Hammond 100 Sportster.
- Parks P-1T
- Powered by a 115hp Milwaukee Tank engine.
- Parks P-1X
- Three-seater with a 90hp Curtiss OX-5 engine.
Specifications (Parks P-1)
Data from Specifications of American Commercial Airplanes
- Crew: 1
- Capacity: 2 passengers
- Length: 24 ft 7 in (7.49 m)
- Wingspan: 29 ft 8 in (9.04 m)
- Height: 9 ft 4 in (2.84 m)
- Wing area: 290 sq ft (27 m2)
- Empty weight: 1,311 lb (595 kg)
- Gross weight: 2,078 lb (943 kg)
- Fuel capacity: 35 US gal (29 imp gal; 130 L)
- Powerplant: 1 × Curtiss OX-5 water-cooled V8 engine, 90 hp (67 kW)
- Maximum speed: 102 mph (164 km/h; 89 kn)
- Cruise speed: 90 mph (145 km/h; 78 kn)
- Range: 305 mi (265 nmi; 491 km)
- Service ceiling: 11,000 ft (3,400 m)
- Rate of climb: 500 ft/min (2.5 m/s)
- Aircraft of comparable role, configuration and era
- Aerospace Industries Association of America, Manufacturers Aircraft Association, Aeronautical Chamber of Commerce of America (1929). Aircraft year book.
- "Parks P-1, 1929". Advert. Flying. Vol. 72 no. 5. May 1963. p. 89.
- "The OX-5 Era". Retrieved 1 March 2012.
- Barnes Warnock McCormick, Conrad F. Newberry, Eric Jumper, American Institute of Aeronautics and Astronautics. Aerospace engineering education during the first century of flight. p. 822.
- "Parks P-1". Retrieved 1 March 2012.
- "Hammond 100". Retrieved 1 March 2012.
- Aviation March 22, 1930, pp. 606, 608, 610
- "Specifications of American Commercial Airplanes". Aviation. Vol. 28 no. 12. March 22, 1930. pp. 606–611. (registration required (. ))