A cruise speed is the speed of a plane in relation to the air masses surrounding it. The Piper Seneca V. Standard Equipped Price $1,030,000 USD. Rate of climb (1 engine out): 190 FPM. 25,000 ft. operating altitude. 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. It has seating for up to six occupants and two separate 100-pound luggage compartments. Correct answer is... 348 km/h. It is equal to 188 kn or 216 mph. Pipers bring a higher level of safety, technology and performance to enhance the lives of owners. SENECA OPERATING INSTRUCTIONS PREFLIGHT If you are planning a flight in the Seneca: 1. The prototype was a Cherokee Six that had wing-mounted engines installed, retaining its nose engine. During development flying the wingspan was increased by two feet. Serious business transportation in Pipers. Piper PA-34-200T I-CNTY Il Piper PA-34 Seneca è un bimotore, 6 posti, sviluppato e prodotto dalla Piper a partire dal 1971, e che, mantenendo la stessa linea di base, è ancora in produzione oggi. Seneca development began when Piper flew a converted trimotor Cherokee Six, designated PA-32-3M, fitted with two additional 85kW (115hp) Lycomings O-235 on either wing. [10], In 1994, the "New" Piper Aircraft company introduced the Seneca IV, having achieved certification on 17 November 1993. A new generation twin-engine aeroplane, suitable for multi-engine ratings training, the IR multi-engine extensions, turbo differences training, and for the VFR night rating. [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. Enjoy freedom as only the Seneca provides. Over 130,000 aircraft later, generations have lived that dream. The prototype was flown as a tri-motor aircraft in the initial stages of the test-flying program. 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. Twenty years later, it’s one of only four piston multis still in production. More Senecas are powered by twin Teledyne Continental counter-rotating engines with full-time turbocharging. This model was similar to the Seneca III offering minor improvements, such as a streamlined engine cowl for increased cruise performance. The prototype had two 180 hp (134 kW) Lycoming O-360 engines, a fixed nosewheel landing gear and a Cherokee Six vertical tail. 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 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. Laminar Flow Systems, Inc. - Manufacturing & Selling Piper Aircraft Sped Modifications Since 1984. 828 nm at long range power settings. Westerhuis, Rogier. 1977 PIPER PA-34-200T Turbo Seneca II - Specifications, Performance, Operating cost, Valuation, Brokers - … Piper PA-34 Seneca V I-CEPU. What is the wingspan of Piper PA-34 Seneca? Max Speed: 204 kts; Normal Cruise: 200 kts; Economy Cruise: 170 kts; Cost per Hour: $ 414.76 What is the stall speed of Piper PA-34 Seneca? What is the max speed of Piper PA-34 Seneca? 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. [7] A typical Seneca III with air conditioning and deicing equipment has a useful load of 1,377 lb (625 kg). [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. 1981 SENECA II (PA-34-200T) Estimated Aircraft Ownership and Operating Expense. 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. [11], From 1975 the Seneca was built under licence in Brazil by Embraer as the EMB-810. [7] A total of 71 Seneca IVs were built.[7]. The day of our visit to New Piper, five Seneca Vs and seven Seminoles were being readied for delivery. Piper Seneca V Photo Gallery. "Air Power Analysis:Central America and the Caribbean:Panama". 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 It has counter-rotating propellers for added safety and has a cruise speed of approximately 184 mph (160 knots). Rate of climb: 1,360 FPM. [5][6][7] The Seneca is primarily used for personal and business flying. (See weight and balance section of this manual.) Maximum speed: 204 kn (235 mph, 378 km/h) at 23,000 ft (7,000 m) Cruise speed: 188 kn (216 mph, 348 km/h) econ cruise at 25,000 ft (7,600 m) Stall speed: 61 kn (70 mph, 113 km/h) wheels and flaps down; Never exceed speed: 204 kn (235 mph, 378 km/h) [2], The aircraft is popular with air charter companies and small feeder airlines, and is operated by private individuals and companies. Right up front, at the risk of compromising my alleged objectivity, I have to confess to a soft spot for the Piper Seneca. A cruise speed is the speed of a plane in relation to the air masses surrounding it. Correct answer is... 348 km/h. [5][7] A total of 934 Seneca models were built, including one prototype. [5] A total of 2,588 Seneca IIs were built. The Seminole also figures prominently in New Piper's … [7], Responding to complaints about the aircraft's handling qualities, Piper introduced the PA-34-200T Seneca II. The Piper Seneca V gives you the performance you need to provide safe, comfortable personal transportation or business travel to paying customers. A Flight in a Twin-Engine Piper Seneca. The Piper Seneca is a twin-engine, retractable landing gear, turbocharged airplane. When Mr. Piper introduced the Piper Cub in 1937, he had a dream – the freedom of flight for everyone. We are very picky to select an reliable data providers, but we cannot guarantee that everything is 100% error-proof. Piper Seneca Spectacular High Speed Low Pass Hernan Acevedo. Certification for flights into known icing conditions and the nice single engine behaviour made the Seneca a popula… The Piper PA-61 Aerostar was designed by Ted R. Smith as a twin-engined propeller-driven aircraft produced from 1967 to 1984. Loading ... 1980 Piper Seneca II for Sale from WildBlue - N711SC (SOLD!) We recommend for any serious purpose - as a rule of thumb - to request offical data about cruise speed from manufacturer of Piper PA-34 Seneca. 1981 Seneca II Operating Economics Guide - Piper Aircraft Corporation. (See performance section of this manual.) What is the length of Piper PA-34 Seneca? Piper PA-34-220T Seneca III;IV - Performance Data. Thousands of Satisfied Customers Worldwide! The PA-34-200T Turbo Seneca II seats up to 6 passengers plus 1 pilot. 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. It has been in non-continuous production since 1971. With the wind, it will equal 318 km/h. Home > Aircraft Specs > Manufacturers > Piper Aircraft > PA-34-220T Seneca III;IV Performance Information. English, Adrian J. [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. When I heard we had a Piper Seneca II twin-engine plane in our hangar, it needed to return to its home in Rochester, and we were allowed to get instruction in the plane, I volunteered to take an hour of multi-engine instruction time and fly it up to Rochester. Disclaimer: Our articles and data connected to cruise speed of Piper PA-34 Seneca are based on public data from various sources. 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. 3. [1], With the decision to abandon the three-engined design tested on the PA-32-3M, the PA-34 was developed as a twin-engined design. [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). [7], In 1981, the PA-34-220T Seneca III was introduced, having completed certification on 17 December 1980. [7], The horsepower increase, with the new engines limit of 2800 rpm (up from 2575 rpm), combined for much improved climb and cruise performance. 30"mp and 2300 rpm yields 70.5% power at 10,000 feet - lean to 1475 egt and no hotter than 1500. Horsepower: 200 Gross Weight: 4570 lbs Top Speed: 196 kts Empty Weight: 2841 lbs Cruise Speed: 177 kts Fuel Capacity: 93 gal Stall Speed (dirty): 62 kts Range: 725 nm Takeoff: Landing: Ground Roll: 870 ft Ground Roll 1380 ft: Over 50 ft obstacle: 1240 ft Over 50 ft obstacle: 2110 ft Rate Of Climb: 1340 fpm Rate of Climb (One Engine): 225 fpm Ceiling: 25000 ft Ceiling (One Engine): 13400 ft Total Operating Expense (Schedule I) Type Aircraft: 1981 SENECA II (PA-34-200T) Business Usage: 100% Assumed Hours Per Year: 500 Assumed Years of Ownership: 7 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 [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. The engines are rated at 200 hp at sea level and develop 215 hp at 12,000 feet, which allows for a 75-percent cruise speed of 218 mph. Make sure the weather is suitable. Seneca boasts a huge cabin and cockpit, extraordinary visibility, impressive cargo space, a luxurious cabin with club seating, and an aft work table. It continued to use the counter-rotating Continental TSIO-360-KB engines and gross weights remained unchanged. Plan the navigation (if going cross-country). 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). 828 nm, Maximum Range. 197 ktas maximum cruise speed. Six Seat, Club Seating (2) Turbocharged Continental TSIO-360-RB | 220 hp (each) 200 KTAS, Maximum Cruise Speed. The Seneca II retained the counter-rotating engine arrangement of the earlier Seneca I. What is the climb speed of Piper PA-34 Seneca? Seneca V Little Big Twin When most twins disappeared in the ‘80s, the Piper Seneca soldiered on. Piper followed this up by taking their PA-24 single-engine Comanche and making it a twin-engine variant, the PA-30 Twin Comanche. It has six seats in a pretty large cabin, two turbocharged counterrotating engines producing 200hp up to 12,000 ft. 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. [1], The Seneca was developed as a twin-engined version of the Piper Cherokee Six. - Duration: 2:35. flywildblue 12,487 views. 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). "Fuerza Aérea Ecuatoriana". The light transport aircraft was initially built by Ted Smith Aerostar Company before it became Piper Aircraft Corporation. 2. Certified on 11 December 1996, the Seneca V was put into production as a 1997 model year. Piper Fly-Away 2 Year Warranty on Airframe, Systems, and … One notable civil operator is the Costa Rican Air Surveillance Service. [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. Not too long after that, Piper took their popular PA-32 Cherokee Six, installed a 115 hp Lycoming O-235 on each win… The Seneca has been made by Pipersince the early 1970's and some 4500 were made since then. Some later models have electrically-actuated flaps. 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. [2] The PA-34-200T was produced as the EMB-810C Seneca (452 built) and the PA-34-220T as the EMB-810D (228 built). 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 ($7,406). 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. once the props are set- reduce manifold to - 30" mp. The Piper Seneca V gives you the performance you need to provide safe, comfortable personal transportation or business travel to paying customers. 828 nm at long range power settings. What is the cruise speed of Piper PA-34 Seneca? Cruise- close the cowl flaps- reduce props to 2300 for normal cruise, 2200 for economy cruise and 2350 for max cruise. If there is a side wind, the speed will vary between 318 and 378 km/h, depending on whether it’s more against or with the wind. 25,000 ft. operating altitude. Piper PA-34-200T I-CNTL. Stall Speed: 60 KIAS. Ceiling: 17,900 FT The aircraft was certified on 18 July 1974 and introduced as a 1975 model. 4. However, the higher the plane flies the stronger the wind. Aircraft = Piper Aerostar 700P Cruise speed (no mods) = 264 KT Cruise speed (with mods) = 268 KT Difference in time for 300 NM trip = 1 min 1 sec Difference in time for 500 NM trip = 1 min 42 sec. 197 ktas maximum cruise speed. This is a model of a Piper PA34-200T Seneca II. It cruises at 170ktas in 12,000ft at 65% power. Find a Local Dealer Download Brochure 200 ktas | 370 km/h Max Cruise Speed To give an example, the cruise speed of Piper PA-34 Seneca flying at 400 meters against the wind of 30 km/h will equal 318 km/h. This page was last edited on 21 December 2020, at 19:41. Training in Pipers. The Seneca II PA-34-200T produced by Piper. [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. Piper Seneca V - PA-34-220T. It is equal to 188 kn or 216 mph. [7], The change in model designation reflected an engine upgrade. Le sue linee derivano dal Piper Cherokee Six, che è un monomotere., a cui aggiunsero due motori sulle ali, facendolo divenire un tri-motore per i test di volo. In windless weather the cruise speed equals the speed in relation to earth. 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=995569956, 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. Il Piper PA-34 Seneca è un bimotore, 6 posti, sviluppato e prodotto dalla Piper a partire dal 1971, e che, mantenendo la stessa linea di base, è ancora in produzione oggi.Le sue linee derivano dal Piper Cherokee Six, che è un monomotere., a cui aggiunsero due motori sulle ali, facendolo divenire un tri-motore per i test di volo. Check weight and balance for the flight. Investigate performance and range. [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. What is the empty weight of Piper PA-34 Seneca. Specs, range, speed, operating weights and performance for the Seneca II PA-34-200T here We use cookies to help you … The prototype PA-34-180 Twin Six, registered as N3401K, first flew on 25 April 1967. A total of 1,010 aircraft were produced. The new aircraft also incorporated a one-piece windshield and a bare metal instrument panel instead of one covered with a removable plastic fascia. 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