Cessna 340#Specifications (340A)
{{Short description|Twin piston engine pressurized general aviation airplane}}
{{Use mdy dates|date=November 2021}}
{{Use American English|date=November 2021}}
{{Infobox aircraft
|name= Cessna 335/340
|image=File:Cessna 340A II, Private JP6927036.jpg
|caption= Cessna 340A
|type= Light twin aircraft
|manufacturer=Cessna
|designer=
|first_flight= 1970
|introduction=1972
|retired=
|status=
|primary_user =
|more_users =
|produced=1971 (prototype)
1972–1984 (production)
|number_built=1,351
|developed_from= Cessna 310
|variants=
}}
File:340Adoor.jpg door]]
The Cessna 340 is a twin piston engine pressurized business aircraft that was manufactured by Cessna.Plane and Pilot: 1978 Aircraft Directory, page 92. Werner & Werner Corp, Santa Monica CA, 1977. {{ISBN|0-918312-00-0}}Montgomery, MR & Gerald Foster: A Field Guide to Airplanes, Second Edition, page 106. Houghton Mifflin Company, 1992. {{ISBN|0-395-62888-1}}
The Cessna 335 is an unpressurized version, which appears the same externally as the 340. It sold in smaller numbers than the 340.{{cite web |last= |year=2008 |title=The Cessna 340 & 335 |url=http://www.airliners.net/aircraft-data/stats.main?id=151 |access-date=2008-08-09 |publisher=Demand Media, Inc}}
Design and development
The 340 was conceived as a cabin-class development of the successful Cessna 310.
The 340 is a six-seat aircraft, with four passenger seats, an aisle and an airstair door. The tail and landing gear were based on the Cessna 310's units, while its wings were from the Cessna 414. The 340's primary selling feature was its spacious, pressurized cabin, the first in a light twin.
Work on the 340 began in 1969, and the first aircraft was delivered in 1971, behind schedule due to a prototype crashing during flight testing in 1970.
The early models have two turbocharged Continental TSIO-520-K engines with 285 hp (214 kW) each. Starting in 1976, the engines were upgraded to the more powerful Continental TSIO-520-NB engines of 310 hp (233 kW). This variant is known as the 340A and it also features smaller {{convert|75.5|in|mm|adj=on}} diameter propellers to reduce noise and meet ICAO Annex 16 noise requirements.{{cite web |last= |date=October 19, 2018 |title=Type Certificate Data Sheet No. 3A25 |url=https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/dd3c5f3279413dce86258331005845f0/$FILE/3A25_Rev_27.pdf |access-date=2022-08-19 |publisher=Federal Aviation Administration}}
The Cessna 335 was marketed as a low-priced, non-pressurized, version powered by 300 hp (225 kW) Continental TSIO-520-EB engines. The prototype 335 made its maiden flight on December 5, 1978, with the first production aircraft flying in 1979.Taylor 1980, pp. 318–319. It was not a market success, with only 64 built by the time production ended in 1980. The 340 was more successful and remained in production until 1984 with 1287 built.
Variants
;340
:Pressurized six-seat twin powered by two Continental TSIO-520-K engines of {{cvt|285|hp}} each. Certified 15 October 1971. 350 built.Simpson 1991, p.108
;340A
:Pressurized six-seat twin powered by two Continental TSIO-520-NB engines of {{cvt|310|hp}} each. Certified 19 November 1975 948 built.
;335
:Unpressurized six-seat twin powered by Continental TSIO-520-EB engines of {{cvt|300|hp}} each. Certified 2 October 1979 65 built.Simpson 1991, p. 107
;Riley Rocket 340
:Conversion of Cessna 340 aircraft by fitting two {{cvt|340|hp}}) Lycoming TIO-540-R engines. Also designated R340L.Taylor 1982, p. 454.
;Riley Super 340
:Conversion of 1972–1975 Cessna 340 aircraft by fitting two {{cvt|310|hp}} Continental TSIO-520-J/-N engines. Also known as R340 Super.Taylor 1988, pp. 461–462.
Specifications (340A)
{{Aircraft specs
|ref=Jane's All The World's Aircraft 1980–81
|prime units?=kts
|genhide=
|crew= one pilot
|capacity= five passengers
|length m=
|length ft=34
|length in=4
|span m=
|span ft=38
|span in=1
|height m=
|height ft=12
|height in=7
|wing area sqm=
|wing area sqft=184
|airfoil=NACA 23018 (root) NACA 23009 (tip)
|aspect ratio=7.2:1
|empty weight kg=
|empty weight lb=3911
|gross weight kg=
|max takeoff weight lb=5990
|fuel capacity={{convert|203|USgal|impgal L|abbr=on}} (usable capacity)
|eng1 number=2
|eng1 name=Continental TSIO-520-NB
|eng1 type=air-cooled flat-six engines
|eng1 kw=
|eng1 hp=310
|prop blade number=3
|prop name=McCauley constant-speed propeller
|prop dia m=
|prop dia ft=6
|prop dia in=4+1/2
|prop dia sigfig=3
|perfhide=
|max speed kmh=
|max speed mph=
|max speed kts=244
|max speed note=at {{convert|20000|ft|m|abbr=on}}
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=172
|cruise speed note=at {{convert|25000|ft|m|abbr=on}} (econ. cruise)
|stall speed kts=71
|stall speed note= (flaps down, power off) CAS
|range km=
|range miles=
|range nmi=1405
|range note=at {{convert|10000|ft|m|abbr=on}} (econ. cruise)
|ceiling m=
|ceiling ft=29800
|climb rate ms=
|climb rate ftmin=1650
|climb rate note=at sea level
|more performance=*Takeoff run to 50 ft (15 m): {{convert|2175|ft|m|abbr=on}}
- Landing run from 50 ft (15 m): {{convert|1850|ft|m|abbr=on}}
|avionics=
}}
See also
{{aircontent|
|related=
|similar aircraft=
|sequence=
|lists=
|see also=
}}
References
{{Reflist|30em}}
- R.W.Simpson, Airlife's General Aviation, Airlife Publishing, England, 1991, {{ISBN|978-1-85310-194-6}}
- Taylor, John W. R. Jane's All The World's Aircraft 1980–81. London: Jane's Publishing Company, 1980. {{ISBN|0-7106-0705-9}}.
- Taylor, John W. R. Jane's All The World's Aircraft 1982–83. London: Jane's Yearbooks, 1982. {{ISBN|0-7106-0748-2}}.
- Taylor, John W. R. Jane's All The World's Aircraft 1988–89. Coulsdon, UK: Jane's Defence Data, 1988. {{ISBN|0-7106-0867-5}}.
External links
{{commons category|Cessna 340}}
- [https://web.archive.org/web/20130508225810/http://www.cessna.com/why-cessna/our-history Official website Cessna history]
{{Cessna 310 family}}
{{Cessna}}
Category:1970s United States civil utility aircraft