197 ktas maximum cruise speed. !– Great for flight training, time building and family flying. Permalink. Two 25-gallon aluminum tanks in each wing are interconnected to eliminate problems of tank selection and to simplify fuel management. With a useful load of 1,500 pounds and 128 gallons of fuel it has a range of 700 to 800 nm in economy cruise. Already a member? "It's not so much that it's got a second engine — though that's a big factor for those who spend a lot of time crossing the Great Lakes — it's that the airplane can get in and out of Michigan and the other states up north in the winter.". Recent Annual inspection, Always hangered with 1,314 LBS. The Seneca IV added high-end instrument options, a deicing package, a leather interior, and optional air conditioning. Certification for flights into known icing conditions and the nice single engine behaviour made the Seneca a popula… Of all the light twins, the Seneca is among the most benign in the runway environment. 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 200 hp (149 kW). Aircraft Owners & Pilots Association Find it free on the store. The PA-32R also came with Piper’s automatic extension system for the landing gear. Chris Layson, president of Northern Air, a Grand Rapids, Michigan-based New Piper dealership, says that the typical Seneca V buyer has owned a New Piper Saratoga II for two to three years, although some "come right out of an Archer, just to build multiengine time." A7SO Revision 17", "Shoddy work cut short Central Park art exhibit: suit", Serbian air force receives multirole Seneca, "Pilot of Obenshain Plane Called 'Very Cautious, "Small plane with DILG Secretary Jesse Robredo crashes off Masbate | News | GMA News Online", The Piper PA-34 Seneca V - Aircraft images and seat map, https://en.wikipedia.org/w/index.php?title=Piper_PA-34_Seneca&oldid=994902596, 1960s United States civil utility aircraft, Articles with dead external links from March 2018, Articles with permanently dead external links, Short description is different from Wikidata, Articles with unsourced statements from July 2013, Official website different in Wikidata and Wikipedia, Creative Commons Attribution-ShareAlike License. In normal operation, each engine operates with an independent fuel system, drawing fuel from the tanks in the wing on the same side as the engine. It continued to use the counter-rotating Continental TSIO-360-KB engines and gross weights remained unchanged. Certified kits are available for a range of single- and twin-engine aircraft. Get the latest news on coronavirus impacts on general aviation, including what AOPA is doing to protect GA, event cancellations, advice for pilots to protect themselves, and more. In three years, Piper sold 933 Seneca Is, dramatically outdoing the Aztec and Comanche. You either buy the full, approved FIKI (flight into known icing) package or nothing at all. Electrical power is supplied by two 60 ampere alternators, one mounted on each engine. The airplane is approved for day and night VFR/IFR operations when equipped in accordance with F.A.R. Each engine produces a maximum power of 220 hp to drive the three-bladed McCauley Propeller propeller at constant speed. Performance Specifications Engine Manufacturer: Continental Model: TSI0-360-RB & L/TSIO-360-RB Horsepower: 220 hp Take off, 200 hp MCP Number of Cylinders: 6 Propeller Manufacturer: Hartzell Number of Blades: 2 Type: Constant Speed, Full Feathering Weights [7], The aircraft's gross weight was increased to 4,750 lb (2,155 kg) for takeoff and 4,513 lb (2,047 kg) for landing. Baron 58 v Piper Seneca V? Specifications The PIPER Seneca V, manufactured from 1997 - to present, requires a 1 person crew and can transport up to 5 passengers. On short final, the Seneca V can be flown as slow as 82 knots and yes, the airplane is easy to land. Both tanks in each wing are filled from a single opening in the outboard tank, and fuel from the outboard tank flows into the inboard tank as the fuel from the inboard tank is consumed. The Piper Seneca V Tour Coming to Texas in November 2012. Anyone have any good insights on the pros/cons of the Seneca vs the 310? The introduction of the Seneca V is just one just more example of Piper's ability to identify market potential for its designs and then implement a program of systematic improvements to attract new buyers. 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. The aircraft has a maximum operating altitude of 25,000', a normal cruise speed of 200 KTS/230 MPH, and a 412 NM/475 SM seats-full range. Realistically, Senecas spend most of their time at lower altitudes that don’t demand supplemental O2. You simply throttle up to the manifold pressure you want, and the wastegates hold that value as you climb to the critical altitude — the altitude where the wastegates are closed and power output begins to drop off, approximately 19,000 feet according to New Piper. The fuel system is similar to the Seneca’s. The Seneca II PA-34-200T produced by Piper. The PA-34 Seneca is a twin-engine development of the Piper PA-32 Cherokee Six. [10], In 1994, the "New" Piper Aircraft company introduced the Seneca IV, having achieved certification on 17 November 1993. Match My Mission; Advanced Mission Match ... 1983 PIPER PA-34-220T Seneca III ... Best Range… Each engine produces a maximum power of 220 hp to drive the three-bladed McCauley Propeller propeller at constant speed. The Piper Seneca V. Standard Equipped Price $1,030,000 USD. One notable civil operator is the Costa Rican Air Surveillance Service. Yes and no. The Seneca III came with a 28-volt electrical system, one-piece windshield, Continental TSIO-360 engines of 220 hp, three-blade propellers, and a redesigned Royalite-free instrument panel. 25,000 ft. operating altitude. "It's a good winter airplane, it can get in and out of 2,700- to 3,000-foot strips easily, it has an excellent single-engine service ceiling, and the turbos give it good performance at high density altitudes," he says. [7], Responding to complaints about the aircraft's handling qualities, Piper introduced the PA-34-200T Seneca II. Range 937. Research Aircraft . The first Senecas came with 200-horsepower Lycoming IO-360 engines. The 2002 Seneca V flown for this article was decked out with popular options: copilot instruments; Honeywell Bendix/King RDR 2000 vertical profile weather radar; air conditioning; yaw damper; and the known-icing package. They provide transportation on shorter trips, or swing into action when the company jet is unavailable. Post by … Although the Seneca V is based on a 1972 design — the Seneca I — it's the beneficiary of refinements made over the years. In the normal category all aerobatic maneuvers including spins are prohibited. The Stormscope and SkyWatch option can be bought independent of the Avidyne FSD and play on the Garmin 530 instead. Who buys new Seneca Vs? The normally aspirated early models cruise in the 160- … [7], In 1981, the PA-34-220T Seneca III was introduced, having completed certification on 17 December 1980. [5][7] A total of 934 Seneca models were built, including one prototype. It has counter-rotating propellers for added safety and has a cruise speed of approximately 184 mph (160 knots). The Piper PA-34 Seneca V aircraft is powered by two Continental TSIO-360-RB engines equipped with an intercooler. AmSafe Pilot and Co Pilot Airbag Seat Belts, ADSB In/Out, G600, TKAS, Weather Radar, Synthetic Vision. 25,000 ft. operating altitude. [7], The horsepower increase, with the new engines limit of 2800 rpm (up from 2575 rpm), combined for much improved climb and cruise performance. During development flying the wingspan was increased by two feet. The PA-34 was also license-built in Brazil by EMBRAER as the EMB-810 and in Poland by PZL-Mielec as the M-20 Mewa. Most of Lowe's Seneca Vs are sold to small- to medium-size companies and serve in corporate fleets. 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. Many pilots want the added safety of the second engine for longer flights and the Seneca is designed to go up high and get you where want to go. 828 nm, Maximum Range. The PA-34-220T Seneca III seats up to 6 passengers plus 1 pilot. Full-time turbocharging helps increase the Seneca’s gross weight and climb performance. [7], 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. It's interesting to note that New Piper won't sell you ice-protection equipment piecemeal. English, Adrian J. This adds a Goodrich WX-500 Stormscope and Goodrich SkyWatch traffic advisory system, plus Avidyne's FlightMax 750 Flight Situation Display (FSD). A 35 ampere-hour, 12-volt battery provides current for starting, for use when the engines are not running, and for a source of stored electrical power to back up alternator output. Moving map, lightning, aeronautical charts, radar imagery, and Stormscope returns can all play on the FSD's large color display. At economy power it’s possible for the Seneca to get 55 seat miles per gallon with a load of six. The Piper PA-34 Seneca is a twin-engined light aircraft, produced in the United States by Piper Aircraft. 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,[7] fitted with an intercooler, was used. The aircraft was certified on 18 July 1974 and introduced as a 1975 model. [13], Data from Piper Seneca V Information Manual (October 25, 2005), Aircraft of comparable role, configuration, and era, The New Piper Aircraft, Inc., 2003, Introduction, p.2, Piper Aircraft Seneca III Pilot Operating Handbook serial number 3448049, Section 6, Weight and Balance, Piper Aircraft Seneca V Pilot Operating Handbook serial number 3449270, Section 6, Weight and Balance, crashed off the coast of Masbate, Philippines, "Type Certificate Data Sheet No. Fly a Seneca V and you'll quickly understand why Archer and Saratoga pilots make smooth transitions. So it's a matter of scale: Piston twins represent a small chunk of the total market, and that market is certainly smaller today than it was 40 years ago. Primarily used for personal and business flying, the Piper Seneca is an American twin-engined, light aircraft, produced by Piper Aircraft since 1971.The Seneca has the capacity for one crew member and five or six passengers. Piper’s Lance is essentially a Cherokee Six with retractable landing gear. [2], 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 prototype PA-34-180 Twin Six, registered as N3401K, first flew on 25 April 1967. Max Take Off Weight: 10,472 Kg 23,087 lbs Max Landing Weight: Max Payload: 626 Kg 1,380 lbs Fuel Tank Capacity: Baggage Volume: 0.4 m3 / 14 ft3 [2], The aircraft is popular with air charter companies and small feeder airlines, and is operated by private individuals and companies. The prototype was a Cherokee Six that had wing-mounted engines installed, retaining its nose engine. The cruise speed is 197 kts, the stall speed is 61 kts, and the range is 828 miles. Piper Seneca V - PA-34-220T. It has been in non-continuous production since 1971. Landing distance (50′)1,710. I've seen several for sale in about the same price range. The Piper Seneca is a powerful twin-engine aircraft, boasting several prominent differences compared to its piston-twin competitors. [5][6][7] The Seneca is primarily used for personal and business flying. Takeoff distance (50′) 1,660. The second prototype flew on 30 August 1968, still with the 180 hp (134 kW) Lycomings but had retractable landing gear and a taller vertical tail. Some later models have electrically-actuated flaps. Piper built 360 Senecas that year, a good start in the twin market where the competition was the Cessna Skymaster, which sold poorly in 1972. The Piper Seneca V gives you the performance you need to provide safe, comfortable personal transportation or business travel to paying customers. The standard useful load for the 2014 model is 1,331 lb (604 kg) but typically is 1,134 lb (514 kg) when the aircraft is equipped with air conditioning, deicing equipment and co-pilot instruments. The Seneca II retained the counter-rotating engine arrangement of the earlier Seneca I. 197 ktas maximum cruise speed. The current PA-34-220T Seneca V was introduced in January 1997. 91 or F.A.R 135. The scrappy team from Florida refuses to quit and from it we can expect much more in the coming years. In 1975 the Seneca II offered 200-hp turbocharged Continental engines. It cruises at 170ktas in 12,000ft at 65% power. Westerhuis, Rogier. "Fuerza Aérea Ecuatoriana". Piper’s PA-32R borrows heavily from its siblings. of … Permalink. 828 nm at long range power settings. 1977 PIPER PA-34-200T Turbo Seneca II - Specifications, Performance, Operating cost, Valuation, Brokers - … These days, conventional wisdom holds that the market for new piston twins is all but finished — a tiny and shrinking slice on the pie chart of annual general aviation sales. This is a model of a Piper PA34-200T Seneca II. [9], Gross weights are 4,570 lb (2,070 kg) for takeoff and 4,342 lb (1,969 kg) for landing, with all weight in excess of 4,000 lb (1,800 kg) required to be fuel. [5], 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. Can it really be that we're watching the twilight of the multis, that their glory years are gone for good, that turbine singles and next-generation mini-fanjets will finish them off completely? Piper Aircraft, which has been around since the late 1920’s and perhaps best known for the Piper J-3 Cub, started producing multi-engine aircraft in the 1950s starting with the PA-23 Apache. 2012 Piper Seneca V, 633TT AF&E, 100K below book value. Specs, range, speed, operating weights and performance for the Seneca II PA-34-200T here We use cookies to help you … But today, if the trends realized at The New Piper Aircraft Inc. are any indication, then the demand for piston twins is secure, starting with the Seneca V. Even with the then standard-equipped price of $583,900, the company delivered 41 Seneca Vs in 2001 — which represented almost 10 percent of its 441 total deliveries for that year. [7] A total of 71 Seneca IVs were built.[7]. The Seneca is also sometimes used as a trainer, but the new airplane with it’s sophisticated and comfortable interior, and take-me-anywhere panel seems to be more of a traveling machine. The system merely allows you some extra time to escape icing should it be encountered. Serious business transportation in Pipers. [1], The Seneca was developed as a twin-engined version of the Piper Cherokee Six. Piper Aircraft, Inc. is a manufacturer of general aviation aircraft, located at the Vero Beach Regional Airport in Vero Beach, Florida, United States and owned since 2009 by the Government of Brunei. In due course I want to move into the world of twins and preferably a six seater. 828 nm at long range power settings. The Seneca V's gross weights remain the same as the Seneca III and IV at 4,750 lb (2,155 kg) for takeoff and 4,513 lb (2,047 kg) for landing,[7] therefore, with all of the added features, the useful load is reduced by about 200 lb (91 kg). Thanks. Both are four cylinder, normally aspirated, direct drive, air cooled, horizontally opposed, fuel injected engines. 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. The system is effective, but like any ice-protection system it is not designed to take on he worst icing conditions, or to let you mill around in ice-laden clouds for indefinite periods of time. The configuration of numerous entry and baggage doors with the comfort of a cabin-class interior makes the Piper Seneca V the perfect business tool. This airplane is certified in the normal category. [7], The new model incorporated changes to the aircraft's control surfaces, including enlarged and balanced ailerons, the addition of a rudder anti-servo tab, and a stabilator bobweight. [11], From 1975 the Seneca was built under licence in Brazil by Embraer as the EMB-810. Throughout much of the mid-to-late 20th century, it was considered to be one of the "Big Three" in the field of general aviation manufacturing, along with Beechcraft and Cessna. The new aircraft also incorporated a one-piece windshield and a bare metal instrument panel instead of one covered with a removable plastic fascia. Pipers bring a higher level of safety, … Darrel Toepfer 2005-08-13 21:32:38 UTC. Vortex Generators are available for: Click below to download available performance charts. The aircraft is powered by a Lycoming IO-360-C1E6 and a LIO-360-C1E6, rated at 200 horsepower each. It’s not a fast airplane, however. Piper Seneca II, A MUST SEE! Fuel Burn at 75% power in standard conditions per hour. Certified on 11 December 1996, the Seneca V was put into production as a 1997 model year. [7] A typical Seneca III with air conditioning and deicing equipment has a useful load of 1,377 lb (625 kg). Even so, the V's Rajay turbochargers let you cruise as high as 25,000 feet — but up there you'll need the built-in oxygen system option. It has seating for up to six occupants and two separate 100-pound luggage compartments. The PA-34-200T Turbo Seneca II seats up to 6 passengers plus 1 pilot. Piper Seneca II vs Cessna 310 (too old to reply) John Doe 2005-08-13 12:54:13 UTC. This aircraft can fly with a maximum speed of 370 km/ h and a maximum range of 1,534 km with a 45-minute reserve. The Seneca has been made by Pipersince the early 1970's and some 4500 were made since then. An engine driven fuel pump is the primary means of supplying fuel for each engine. True, the market for twin-engine piston aircraft is comparatively small. The control feel is very much like that of a Saratoga — kind of trucky, what you'd expect from a 4,750-pound airplane — and so are the target airspeeds used in the pattern. Piper PA-34-220T Seneca V Specifications Powerplants 220-hp (ea) Teledyne Continental TSIO-360 Recommended TBO 1,800 hr Propellers Hartzell two-blade, 76-in dia (three-blade McCauley, 76-in dia, optional) Length 28 ft 7 in Height 9 ft 11 in Wingspan 38 ft 11 in Wing area 208.7 sq ft Wing loading 21.2 lb/sq ft Power loading 10 lb/hp Thomas A. Horne, AOPA Pilot, November 2002. It rules the highest single-engine service ceiling in its class, displays a standard three-screen G1000 panel, provides a visibly wider cabin, and all this for a significantly less owning and operating cost than the competition. The prototype had two 180 hp (134 kW) Lycoming O-360 engines, a fixed nosewheel landing gear and a Cherokee Six vertical tail. The third prototype was closer to the production standard and flew on 20 October 1969; it was fitted with 200 hp (149 kW) Lycoming IO-360-A1A engines. Please login below for an enhanced experience. With the extended-range tanks, it’s possible to travel 900 miles and arrive with a 45-minute fuel reserve. Over 130,000 aircraft later, generations have lived that dream. Introduced in 1981, the Seneca III was replaced by New Piper's improved PA-34-220T Seneca IV in 1994 with aerodynamic refinements, axisymetric engine inlets and a revised interior. But today, if the trends realized at The New Piper Aircraft Inc. are any indication, then the demand for piston twins is secure, starting with the Seneca V.  Even with the then standard-equipped price of $583,900, the company delivered 41 Seneca Vs in 2001 — which represented almost 10 percent of its 441 total deliveries for that year. The turbochargers provide the get-up-and-go to at least top some of the weather in the lower flight levels and the deicing system makes winter flying a whole lot more practical. When Mr. Piper introduced the Piper Cub in 1937, he had a dream – the freedom of flight for everyone. [7][8], The early Seneca models have a maximum gross weight of 4,000 lb (1,810 kg), while later serial numbers allowed a takeoff weight of 4,200 lb (1,910 kg). This includes pneumatic leading-edge deice boots, electric windshield and propeller heating elements, electrically heated pitot-static probes and stall warning vanes, plus an ice light for illuminating the left wing leading edge to check for ice buildups when flying at night. The Piper Seneca V is powered by two Continental L/TSIO-360-RB engines. Toggle navigation. The V came out in 1997 and brought intercooling to the turbocharged Continentals. Piper followed this up by taking their PA-24 single-engine Comanche and making it a twin-engine variant, the PA-30 Twin Comanche. An overvoltage relay in each alternator circuit prevents damage to electrical and avionics equipment. The Piper Seneca is a twin-engine, retractable landing gear, turbocharged airplane. Looking around, the G58 and Seneca appear to be quite favourable. Piper Navajo, Chieftain, & Seneca Nacelle Tanks. In case of failure, there is an auxiliary fuel pump installed. Setting power is no sweat, thanks to the V's automatic wastegates. This aircraft can fly with a maximum speed of 370 km / h and a maximum range of 1,534 km with a 45-minute reserve. The main landing gear is much like the Seneca—logical, since the basic airframe is the same—and the nose gear resembles the Seneca and also the Arrow. This model was similar to the Seneca III offering minor improvements, such as a streamlined engine cowl for increased cruise performance. Part of this was due, no doubt, to Piper’s decision to modernize the airframe. The following year, New Piper planned to sell 37 Seneca Vs, with most buyers going for options that pushed prices close to $690,000. It has six seats in a pretty large cabin, two turbocharged counterrotating engines producing 200hp up to 12,000 ft. The PA-34 was also license-built in Brazil by EMBRAER … Data from Piper Seneca V Information Manual (October 25, 2005) 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. Piper Seneca Series Aircraft Information. New Piper officials point out another reason why some owners are drawn to the Seneca V. Some pilots would like to buy New Piper's turboprop single, the Meridian, but can't meet insurance prerequisites for flying a turbine-powered airplane as pilot in command. Remained unchanged, lightning, aeronautical charts, Radar imagery, and the gross weight climb. Were built. [ 7 ] a total of 2,588 Seneca IIs were built including... Is unavailable luggage compartments Piper Cherokee six that had wing-mounted engines installed, retaining its engine! 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