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Piper PA-34 Seneca

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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.<ref name="Plane and Pilot"/><ref name="Piper"/><ref name="A7SO1"/> The Seneca is primarily used for personal and business flying<ref name="Foster"/> as well as multi-engine class rating flight training.

DevelopmentEdit

The Seneca was developed as a twin-engined version of the Piper Cherokee Six. The prototype was a Cherokee Six that had wing-mounted engines installed, retaining its nose engine. The prototype was flown as a tri-motor aircraft in the initial stages of the test-flying program.<ref name="Foster"/>

PA-34-180 Twin SixEdit

With the decision to abandon the three-engined design tested on the PA-32-3M, the PA-34 was developed as a twin-engined aircraft. The prototype PA-34-180 Twin Six, registered as N3401K, first flew on 25 April 1967. The prototype had two Template:Convert Lycoming O-360 engines, a fixed nosewheel landing gear and a Cherokee Six vertical tail. The second prototype flew on 30 August 1968, still with the Template:Convert Lycomings but had retractable landing gear and a taller vertical tail. During development flying the wingspan was increased by two feet. The third prototype was closer to the production standard and flew on 20 October 1969; it was fitted with Template:Convert Lycoming IO-360-A1A engines.<ref name="Peperell" />

PA-34-200 SenecaEdit

Certified on 7 May 1971 and introduced in late 1971 as a 1972 model, the PA-34-200 Seneca is powered by a pair of Lycoming IO-360-C1E6 engines. The righthand engine is a Lycoming LIO-360-C1E6 engine variant, the "L" in its designation indicating that the crankshaft turns in the opposite direction, giving the Seneca counter-rotating engines. The counter-rotating engines eliminate the critical engine limitations of other light twins and make the aircraft more controllable in the event of a shut down or failure of either engine.<ref name="Plane and Pilot"/><ref name="A7SO1"/> A total of 934 Seneca models were built, including one prototype.<ref name="A7SO1"/><ref name="MM34I"/>

The early Seneca models have a maximum gross weight of Template:Convert, while later serial numbers allowed a takeoff weight of Template:Convert.<ref name="A7SO1"/>

PA-34-200T Seneca IIEdit

File:Piper.seneca.arp.750pix.jpg
A Piper Seneca II

Responding to complaints about the aircraft's handling qualities, Piper introduced the PA-34-200T Seneca II. The aircraft was certified on 18 July 1974 and introduced as a 1975 model.<ref name="A7SO1"/>

The new model incorporated changes in the aircraft's control surfaces, including enlarged and balanced ailerons, the addition of a rudder anti-servo tab, and a stabilator bobweight.<ref name="Plane and Pilot"/>

The "T" in the new model designation reflected a change to turbocharged, six-cylinder Continental TSIO-360E or EB engines for improved performance, particularly at higher altitudes. The Seneca II retained the counter-rotating engine arrangement of the earlier Seneca I.<ref name="A7SO1"/>

The Seneca II also introduced optional "club seating" whereby the two center-row seats face rearwards and the two back seats face forward allowing more legroom in the passenger cabin.<ref name="Plane and Pilot"/> A total of 2,588 Seneca IIs were built.<ref name="aerofiles"/>

Gross weights are Template:Convert for takeoff and Template:Convert for landing, with all weight in excess of Template:Convert required to be fuel.<ref name="A7SO1"/>

PA-34-220T Seneca IIIEdit

File:Piper PA-34-220T Seneca III, with one piece windshield.jpg
Piper Seneca III showing the one piece windshield

In 1981, the PA-34-220T Seneca III was introduced, having completed certification on 17 December 1980.<ref name="A7SO1"/>

The change in model designation reflected an engine upgrade. Continental TSIO-360-KB engines were used which produced 220 horsepower (165 kW), although only rated as such for five minutes and then dropping to Template:Convert.<ref name="A7SO1"/>

The horsepower increase, with the new engines limit of 2800 rpm (up from 2575 rpm), combined for much improved climb and cruise performance. The new aircraft also incorporated a one-piece windshield and a bare metal instrument panel instead of one covered with a removable plastic fascia. Because of the raised zero-fuel weight and the raised maximum take-off weight, the Seneca III has the highest useful load of all the PA-34 variants. Some later models have electrically-actuated flaps. More than 930 Seneca IIIs were built; the last 37 Seneca IIIs built had a 28-volt electrical system rather than the 14-volt system of previous aircraft.<ref name="A7SO1"/>

The aircraft's gross weight was increased to Template:Convert for takeoff and Template:Convert for landing.<ref name="A7SO1"/> A typical Seneca III with air conditioning and deicing equipment has a useful load of Template:Convert.<ref name="POH Seneca III"/>

PA-34-220T Seneca IVEdit

In 1994, the "New" Piper Aircraft company introduced the Seneca IV, having achieved certification on 17 November 1993. This model was similar to the Seneca III offering minor improvements, such as a streamlined engine cowl for increased cruise performance. It continued to use the counter-rotating Continental TSIO-360-KB engines and gross weights remained unchanged.<ref name="A7SO1"/> A total of 71 Seneca IVs were built.<ref name="A7SO1"/>

PA-34-220T Seneca VEdit

File:SenecaV.jpg
Two examples of Seneca V

Certified on 11 December 1996, the Seneca V was put into production as a 1997 model year. Again the cowls were redesigned for increased performance, several cockpit switches were relocated from the panel to the headliner, and an improved engine variant, the Continental TSIO-360-RB,<ref name="A7SO1"/> fitted with an intercooler, was used.

The Seneca V's gross weights remain the same as the Seneca III and IV at Template:Convert for takeoff and Template:Convert for landing,<ref name="A7SO1"/> therefore, with all of the added features, the useful load is reduced by about Template:Convert. The standard useful load for the 2014 model is Template:Convert but typically is Template:Convert when the aircraft is equipped with air conditioning, deicing equipment and co-pilot instruments.<ref name="POH"/>

Embraer EMB-810 SenecaEdit

From 1975 the Seneca was built under licence in Brazil by Embraer as the EMB-810.<ref name="Peperell" /> The PA-34-200T was produced as the EMB-810C Seneca (452 built) and the PA-34-220T as the EMB-810D (228 built).<ref name="Peperell" /> The EMB-810C is designated U-7 in Brazilian Air Force service.<ref>{{#invoke:citation/CS1|citation |CitationClass=web }}</ref>

OperatorsEdit

File:Piper Seneka At Centennial.jpg
A Piper Seneca II with the engine cowl removed

CivilEdit

The aircraft is popular with air charter companies and small feeder airlines, and is operated by private individuals and companies. One notable civil operator is Eid Air Aviation,<ref>{{#invoke:citation/CS1|citation |CitationClass=web }}</ref> a flight school located in Bromont, Canada

MilitaryEdit

Brazil
  • Brazilian Air Force (EMB 810C Seneca)<ref name="Flight WAF 88 p31">Flight International 3 December 1988, p.31.</ref>
Belize
Colombia

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Dominican Republic
Ecuador
Honduras

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Panama
Peru
Serbia

Notable accidents and incidentsEdit

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Specifications (PA-34-220T Seneca V)Edit

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See alsoEdit

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ReferencesEdit

Notes

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Bibliography

External linksEdit

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