Specs, range, speed, operating weights and performance for the Seneca II PA-34-200T here. Probably not the case with a Meridian in operating costs, but certainly cheaper if you factor in purchase price. Piper Navajo, Chieftain, & Seneca Nacelle Tanks. 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. Yes it takes a few minutes to get it setup. Landing gear is much better in the Seneca II Seneca II is easier for the passengers to enter (club seating) Seneca II will give you a good honest 165 knots and burn a total of 21 to 23 GPH. I do have an endorsement from one flight in a 235 HP C-182, and I wouldn't be flying the Seneca solo, so it's mostly just a trivia point.) Advertisement Seneca II Seneca V STANDARD DATA: Seneca II Seats 6. Considering our 100 hour-per-year average, that’s $12,200. Additionally, the PA-34-200"T" was powered by turbocharged, six cylinder Continental TSIO L/TSIO-360E engines for improved performance, particularly at higher altitudes. Add that up and a TP twin might be on par with the bigger single turboprops. By: Norm Goyer. System Description: The airplane is equipped with a standard fuel system consisting of four vented fuel tanks, fuel tank selector valves, fuel strainer, engine driven fuel pump, auxiliary electric fuel pump, and fuel injection system. The Piper Seneca is more rubust and performs better than the smaller Seminole, able to maintain training altitudes on one engine even in the desert heat. It has six seats in a pretty large cabin, two turbocharged counterrotating engines producing 200hp up to 12,000 ft. At best power, the consumption is: 10.0 GPH at 75% power. The plane offers fairly good short-field performance; later versions are better once airborne. 3's have wastegate hooked to throttle lever. 4,570. The 310 is a much faster plane - on the same fuel burn as the Aztec I'm about 25 KTAS faster in the 310, but keep in mind the 310 I fly has 520s and I've spent a lot of time optimizing it. The pilot had the left fuel selector set to the left main tank and the right fuel selector was set to the right main tank. Piper Seneca Series Aircraft Information. The ’74 version had twin 200-hp Lycoming four-cylinder engines. Installation of replacement fuel cell assemblies (FFC replacement part number 573 is eligible for installation on Piper Seneca II models Pa-34-200T serial numbers 34-757001 and subsequent and Piper Seneca III models PA-34-200T serial numbers 34-8133001 and … Fuel Burn @ 75% power: 10.5 GPH. Merlyn wastegates are automatic AFAIK. We use cookies to help you get the best experience when using our website. It is a six place plane, the fuel tanks hold 128 gallons (123 usable) total, and the max gross weight is 4500 pounds. 7.5 GPH at 65% power. Lined up on Vero Beach’s Runway R11, I put the power to the TSIO-360s and rotated in no time. 8.8 GPH at 65% power. It s not a fast airplane, however. This is a model of a Piper PA34-200T Seneca II.The Seneca has been made by Piper since the early 1970's and some 4500 were made since then. “Simplicity is another outstanding attribute. The Piper Twin Comanche can fly at 160 kts on 50 litres per hour and carry 4 or even 6 people if you fly on reduced fuel load. At best economy cruise, fuel consumption for a Warrior II (PA28-161) is: 8.5 GPH at 75% power. Seneca II has a user friendly fuel system compared to a C-310. Location: Blacksburg, Va. Aircraft damage: Substantial. That, more than anything, may explain why it endures in Piper s line. Piper 34-200 Seneca school flight around Roskilde Airport (EKRK) with various simulated engine failures. Empty wt. Useful Load: 1,559 lbs. Ergonomic controls, seats built for comfort, avionics placement and design, coupled with built-in durability and components chosen for reliability. 2017 Piper M350 , One owner since new always Piper maintained, Warranty remaining thru Oct. 22, 2020, No Damage History, shows as near new. 930 Seneca IIIs were produced before Piper Aircraft filed for Chapter 11 bankruptcy in 1991. PIPER PA-34 SENECA SPECS. Pilot report - Piper Seneca series [Reprinted from Fliteguide / Imperial Aviation] Piper's Seneca is the archetypal light twin. 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 aircraft was certified in July 1974 and introduced as a 1975 model. Bear in mind that they also have the capability to fly for 5.5 hrs without tip tanks and 7.5 hours with tip tanks so reducing the fuel load still gives you more endurance than the average single. More changes were made to the control system to improve handling. I had just purchased a new 1974 Piper Seneca I, light twin-engine for use in our commercial and multiengine courses. Injuries: None. Seneca II With a strong if not a hot seller on its hands, Piper continued to improve the Seneca with the PA-34-200T Seneca II. That requires about 30-gph fuel consumption, while 70% power of 25 inches and 2,300 rpm knocks around 10 knots off the speed but lowers fuel burn to 24 gph. Handling at cruise speed requires more muscle than during climb and approach, but the Seneca V is properly responsive and quite stable, even when flown manually. I've done research on the Piper Seneca's and it just so happens a good friend of mine is selling his, gonna get a great deal on it as well. Horsepower: 220 Gross Weight: 4750 lbs Top Speed: 196 kts Empty Weight: 2852 lbs Cruise Speed: 178191 kts Fuel Capacity: 93123 gal Stall Speed (dirty): 64 kts Range: 725 nm Takeoff: Landing: Ground Roll: 920 ft Ground Roll 1400 ft: Over 50 ft obstacle: 1210 ft Over 50 ft obstacle: 1978 ft Rate Of Climb: 1400 fpm Rate of Climb (One Engine): 240 fpm Ceiling: 25000 ft Ceiling (One Engine): 12000 ft 2,839. Griggs Aircraft is the holder of the STCs for the Piper PA-31, 31-325, 31-350 (Navajo & Navajo Chieftain) and PA-200T & PA-220T (Seneca) Auxiliary Nacelle Fuel Tanks, previously produced by Nayak Aviation. It was the first version of this long-lived Piper introduced in 1973. Piper Seneca II PA-34-200T Technical Data* ENGINES Lycoming TSIO-360E Lycoming LTSIO-360E 200 HP Each SEATS 6 CRUISE SPEED 177 KIAS RANGE (75% POWER) 900 NM FUEL BURN (75% POWER) 23.6 Gallons / Hour MAX GROSS WEIGHT 4,570 lbs SERVICE CEILING 25,000 feet FUEL CAPACITY 128 Gallons RENTAL RATE $350 per hour DESCRIPTION Enjoy the videos and music you love, upload original content, and share it all with friends, family, and the world on YouTube. Travel. Seneca II has counter rotating propellers. Test Flight For Piper Seneca V PA-34. Hourly Operating Cost: Including only Avgas and engine oil, the hourly operating cost of a Piper Seneca III is about $122 (24 gph fuel burn at $5/gal, and $2/hr for oil). The PA-34-220T Seneca III upgraded the engines to the Continental TSIO-360-KB, now with 220 hp for even better performance, and included three-blade props. The Seminole was built in 1979–1982, in … ): 1800 Horsepower: 220 Fuel type: 100/100LL Propeller type/diameter: Hartzell CS/2-blade … Read More "2007 Piper PA34-220T Seneca V" The Piper PA-44 Seminole is an American twin-engined light aircraft manufactured by Piper Aircraft.. Pitching for the Seneca’s best angle airspeed of 83 knots, I retracted the gear once a positive rate was established, and the useable runway slipped away below us. 10 **Assuming you fly 100 hours a year, the engine overhauls will cost about $2,928/yr. Seneca I's are 200 hp/side. Price $1,047,000 Contact Cody Ramsey at 928-775-3832 Apply for Financing Operating Costs Get Insurance Advertisement 2007 Piper PA34-220T Seneca V New price: $756,500 Engine make/model: Continental TSIO-360-RB TBO (hrs. 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 Gross wt. I used to run at 75% most of the time when I was doing cross-country flights in a Warrior II. Piper Aircraft would add one more model to the Seneca line in 1981 before going bankrupt. Total Usable 93.0 Gal. Piper also introduced a new limitation: a zero-fuel weight of 4000 pounds, meaning that any weight over 4000 pounds had to be in fuel, not payload. Aircraft: Piper Comanche. The fuel burn is lowest of any single-engine turboprop on the market,” said Jackie Carlon, senior director of marketing at Piper Aircraft. ... Piper introduced the PA-34-200T Seneca II. Fuel capacity 98-128. Base Price: $1,491,000: Engine: 2 x Continental IO-550-N: Seats: 6: Max Takeoff Weight: 5,500 lbs. The engine began to lose power during the approach. Garrett's have 5400hr TBO, cost less to overhaul, burn about 20-30% less fuel than the PT6's. The Mooney's engine is exactly 200 HP, so it doesn't count. Piper’s engineering and design teams lead the industry in designing aircraft for the owner-flown class of aircraft. Fuel System Fuel: Approved Grades 100LL (blue), 100 (green) Total Fuel 98.0 Gal. The Seneca maintains the same simplicity of handling and systems as other retractable-gear Pipers. By continuing to use this website, you are agreeing to our Cookie Policy. 7.8 GPH at 55% power. Engines two 200-hp turbocharged counter-rotating … Read More "PIPER SENECA /II/III/IV/V" With a strong if not a hot seller on its hands, Piper continued to improve the Seneca with the PA-34-200T Seneca II. Piper also introduced a new limitation: a zero-fuel weight of 4000 pounds, meaning that any weight over 4000 pounds had to be in fuel, not payload. It also has a smaller cabin and is worse in icing conditions (thinner, hotter wing) which is how it achieves this. The Seneca II PA-34-200T produced by Piper. Seneca II. This lofty achievement is shared by one other - Beechcraft's long-enduring Baron - and whilst between them they account for nearly one hundred percent of the current new twin market, they have occupied diametrically opposite ends of the price spectrum. The PA-44 is a development of the Piper Cherokee single-engined aircraft and is primarily used for multi-engined flight training.. Every lever effects every lever. Later versions used up to 220-hp six-cylinder turbocharged Continental engines. I'm a low time pilot (135hrs) all in a PA-28 235, so while I have the HP endorsement I'm gonna need to get the complex as well as the Multi Add On. 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