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PA-28R-180 Cherokee Arrow Four-place, retractable landing gear landplane, Lycoming IO-360-B1E engine of 180 hp (134 kW), gross weight 2,500 lb (1,134 kg). First certified on 8 June 1967. [19] Built in the following variants: PA-28R-180 Cherokee Arrow, initial version. [35] PA-28R-180B Cherokee Arrow B, as PA-28R-180 with minor changes ...
FM 100–5, Field Service Regulations, Operations (with included Change No. 1) 7 February 1964 [24] This manual supersedes FM 100–5, 27 September 1954, including C 1, 16 December 1954, C 2, 27 July 1956, and C 3, 24 January 1958. Earle G. Wheeler: INACTIVE: FM 100–5: FM 100–5, Field Service Regulations, Operations: 19 February 1962 [25]
The Continental IO-360 is a family of fuel-injected air-cooled, horizontally opposed six-cylinder aircraft engines manufactured by Continental Motors in the United States of America, now part of AVIC International since 2010.
PA-32R-300 (1976–1978) Marketed as the Piper Cherokee Lance.Initial version of the retractable PA-32 line, with a standard tail. [4]PA-32RT-300 (1978–1979) After the first half of 1978, Piper modified the tail to a "T" design with the stabilator (horizontal stabilizer/elevator) moved to the top of the vertical tail.
The Piper PA-34 Seneca is a twin-engined light aircraft, produced in the United States by Piper Aircraft.It has been in non-continuous production since 1971. [4] [5] [6] The Seneca is primarily used for personal and business flying [1] as well as multi-engine class rating flight training.
Chilton Cengage Archived 2017-12-28 at the Wayback Machine—the website of Chilton Cengage, current publisher of Chilton's automotive manuals. DIY Auto Repair Archived 2013-03-14 at the Wayback Machine by Chilton Online Car Manuals; Chilton Print Manuals (2018 archived link) by Chilton Manuals, part of Haynes North America, Inc.
However, these trainers had become exceedingly difficult to repair following passage of a US arms embargo in 1976. [3] The PA-28R-300 Pillán was developed by Piper Aircraft in the United States as a two-seat military trainer for assembly in Chile, based on a PA-32R fuselage with a new center-section and wing stressed for aerobatics. [4]
The PA-31-350T1020 (or T1020) was a PA-31-350 Chieftain optimized for and marketed for the commuter airline market, without the 40 US gal (151 L) auxiliary fuel tanks in each wing. [8] Up to eleven seats could be fitted, and baggage capacity was reduced from 700 to 600 lb (318 to 272 kg) maximum. [8] The first T1020 was delivered in December 1981.