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. The light aircraft can carry a maximum of 604kg of standard useful load, while its onboard fuel tank is designed to carry 462l of usable fuel. FUEL CAPACITY, USABLE 122 US gal | 462 liters RANGE WITH 45 MINUTE RESERVE . 1- Piper Seneca V conducted tour in Fly! Baggage Capacity Internal / External (CFT) 17.3/15.3. Detailed information, specs, fuel cost, pictures and other features of the Piper Seneca V. All Piper Aircraft Aircraft. The maximum takeoff weight and weight that are equipped with aircraft standards are 2,155 kg and 1,561 kg, respectively. Ownership Costs Engine (x2) Manufacturer: Cont Motor. The PA-34 Seneca is, basically, what you get when you turn a Cherokee Six into a twin, sharing the trademark Hershey-bar wing, stabilator empennage and fuselage of the Cherokee Six. Overhaul (HT): 1,800 Hrs. The Piper PA-34 Seneca has a fairly interesting development history, starting out as a tri-motor and now serving as a popular light twin-engine commuter aircraft. Weights. Height: 11.3 f. Where performance meets efficiency. PA-11 Cub Special | Piper Archer DX | Piper J-2 Cub | Piper J-3 Cub | Piper J-5 Cub Cruiser | Piper Jet | Piper M350 Mirage | Piper M500 Meridian | Piper PA-12 Super Cruiser | Piper PA-14 Family Cruiser | Piper PA-15 Vagabond . Piper Aircraft SENECA V ROTW - Fly.Simvol Do not use for real flight 9 . Powerplant. The Seneca has the capacity for one crew member and five or six passengers. Fuel capacity: 93 GAL. Fuel Capacity: 732 Lb; Payload W/Full Fuel: 444 Lb; Max Payload: 1153 Lb; Range. In October 1969, the next twin-engine prototype PA-34-180 Twin 6 flew . Complete Logs. Fuel System Fuel: Approved Grades 100LL (blue), 100 (green) Total Fuel 98.0 Gal. 93 Gal. PIPER PA-34-220T Seneca III (1981 - 1993) Best Cruise: 178 KIAS . The Seneca is propelled by twin-engine reliability and power, the highest single-engine service ceiling in its class, and a sophisticated TSIO360RB5BN. Piston Twin Aircraft. It has virtually every option that a Seneca can have. SENECA V Piper Aircraft, Inc. 2926 Piper Drive, Vero Beach FL 32960 866-648-1945 FAX 772-978-6592 piper.com PN 767-559 01-2007 Fuel Capacity Volume. Fuel Capacity Volume. best correlation is Vyse for Piper Seneca II (think SETOS) YOU MIGHT ALSO LIKE. Fuel Capacity Usable Fuel: 122 gallons/462 litres Oil Capacity Oil Capacity: 8 quarts/7.6 litres Baggage Volume: Forward Compartment: 15.3 cubic feet/.43 cubic meters FUEl CAPACiTy Usable: 122 US gal | 462 liters MAXiMUM CRUiSing SPEED 200 ktas | 370 km/h . blkhawkplt. Real good performance with the light-weight short cabin B55 Baron. The current Seneca V model is a low-wing, six-seat aircraft equipped with retractable gear and two Continental TSIO-360-RB turbocharged engines. Advertise your PIPER PA-34-200T Turbo Seneca II on this page . The Seneca is primarily used for personal and business flying. the Piper Seneca remains the best value multi-engine aircraft. The original airplane had a 60-gallon fuel system. This listing was posted on May 10, 2022. The turbocharged Piper Seneca allows you to traverse just about any terrain. A $116,250.00 loan over 120 months including $484.38 per month in interest equates to a $5,829.21 per-period payment. Engine 1 Make/Model. Data Sheet - Seneca I (PA34-200) Weights Aircraft Number Empty Weight Empty Moment Useful Load 55908 2786.8 lbs. With the extended-range tanks, it's possible to travel 900 miles and arrive with a 45-minute fuel reserve. PT-VSH - Neiva EMB-810D Seneca III. Description This is the nicest Seneca that will ever be built. View photos, ownership, registration history, and more. It will climb at 1000FPM all the way to the Flight Levels. Piper Aircraft SENECA V ROTW - Fly.Simvol Do not use for real flight 9 . . . Fuel Capacity Useable 122 US gal / 462 liters Cruising Speeds TAS 10,000 ft 18,500 ft Maximum Cruise Power 182 kts / 337 km/h 197 kts / 365 km/h . Seneca V Seminole Archer LX / TX D aher TBM 900 TBM 910 TBM 930 Our interactive graphs demonstrate the relationships between fuel cost and annual flight hour utilization. Quizlet flashcards, activities and games help you improve your grades. Acces PDF Piper Seneca Pa 34 Information Manual SENECA 2 FULL TRAINING PA-34 A Day of CPL Training - Piper Seneca PA34-200 Piper Seneca cockpit view engine start up and takeoff | GoPro HD Piper PA-34 Seneca II Takeoff Piper PA34-200T Seneca II For Sale Beautiful Sunset Landing | Page 6/44. Minimum Octane. Wing Span: 43.0 ft. Endeavor . Fuel capacity (4 x 24.5 gal) 98 gal. 9A-LEM's, for example, reads PA-34-200 with the serial 34 - 73 50 327, which translates to:. Horsepower: 200: . Home > Aircraft Specs > Manufacturers > Piper Aircraft > PA-34-220T Seneca III;IV Performance Information. Piper Seneca. Reply. Price: USD $158,500. Ownership Costs 1971 Total Cost of Ownership: Register For Free Total Fixed Cost Register For Free. Piper Seneca V (letsflysandiego.com) Type: Constant Speed, Full Feathering. Fuel Consumption (Gal./Hr. 100/100LL. Fuel capacity (4 x 24.5 gal) 98 gal. Lester Moreno. PA-34-220T Seneca V - Two 165kW (220hp) Teledyne Continental L/TSIO-360-RB turbocharged, intercooled fuel injected counter rotating flat sixes driving two blade Hartzell or optional three blade McCauley c/s prop. It has been in non-continuous production since 1971. Browse a wide selection of new and used PIPER Aircraft for sale near you at Controller.com, . 2-5 Fuel/Oil - Fuel 100LL - Usable capacity = 122 gal/462 l - Oil capacity = 8 qts/7.6 l . 34-7250001 to 34-7250189 when kit number 760607 . Usable Fuel Capacity. The original Seneca was introduced in 1972, and you can still buy a brand-new Seneca V from Piper today. Fuel capacity: 100 GAL. The Piper Seneca that premiered in the early 1970s also utilized the basic Cherokee Six fuselage. Now, however, the four club seats in the back and the cockpit seats are stitched in soft leather compliments of the Piper Saratoga II HP total makeover back in 1993. Cubic Feet CABIN . Interior Notes: Belted Lav Seat. . Engine 1 Manufacturer. Fuel capacity: 110 US gal (92 imp gal; 420 L), of which 2 US gal (1.7 imp gal; 7.6 L) are unusable; Powerplant: 2 × Lycoming O-360-E1A6 air-cooled flat four (counter rotating), 180 hp (130 kW) each; Fuel Capacity Usable Fuel: 122 gallons/462 litres Oil Capacity Oil Capacity: 8 quarts/7.6 litres Baggage Volume: Forward Compartment: 15.3 cubic feet/.43 cubic meters Aircraft.com is the leading registry for planes, jets, and helicopters. Research, Compare & Buy new Piper Seneca with AIR.ONE. The PA-34 Seneca seats up to 5 passengers plus 1 pilot. Search more Piper airplanes on Hangar67. Range: 828. Low total time, great condition, a perfect 4-seater for private flying! The Seneca had counter-rotating Lycoming IO-360C1E6 engines producing 200 HP each. . Garmin 530W/430W. Minimum Octane. 128 gal (122 gal usable) 768 lb (732 lb usable) Baggage capacity Forward, external 100 lb, 15.3 cu ft Aft, internal 85 lb, 17.3 cu ft Fuel Capacity: 128 Gallons Total Time: Avionics: Garmin GMA-340 Audio Panel Garmin GNS-530W GPS/NAV/COM Garmin GNS-430W GPS/NAV/COM the Piper Seneca remains the best value multi-engine aircraft. The airplane was tanked with an extra 250 gallons of fuel, bringing total capacity to 352 gallons. Search more Piper airplanes on Hangar67. pilots operating handbook and. ITS CLASS, AND A THREE-SCREEN G1000 NXI COCKPIT. Piper PA-34 Seneca V Engine and Performance Dimensions. The Piper M500 Sleek and sexy without sacrificing safety, the M500 is the profile of perfection. 93 Gal. Oil capacity (ea engine . . 2-5 Fuel/Oil - Fuel 100LL - Usable capacity = 122 gal/462 l - Oil capacity = 8 qts/7.6 l . 1010151. pa-34-220t report: vb-1930 faa approved by: linda ü. dicken doa-510620-ce date of approval: the new piper aircraft, inc. october 25, 2005 vero beach, florida 1- Piper Seneca V conducted tour in Fly! . faa approved airplane flight manual. Home > Aircraft Specs > Manufacturers > Piper Aircraft > PA-34-200T C/R Turbo Seneca II Performance Information. AERONAUTICAL INFORMATION MANUAL CHAPTERS 1,2,3,5,6 93 Terms. Engine 1. Rochester Air Center - Part 141 and 61 Flight Training Rochester - GI . The asking price of a new Piper Seneca V is $1,061,000. Total Usable 93.0 Gal. Put six people on board, and the Seneca will carry only about 53 gallons of fuel, enough for 1.5 hours and a 45-minute reserve. . Fuel capacity 122 Gal Baggage capacity Performance Takeoff distance ground roll Takeoff distance over 50-ft obstacle 1,707 ft Rate of climb sea level Service ceiling 25,000 ft Landing distance over 50-ft obstacle 2,180 ft Landing distance ground roll Oil capacity (ea engine) 8 qts. Useable Fuel. Base Price: $739,800: Typically Equipped Price: $845,770: Engines: Austro AE300: Horsepower Per Side: 170 hp turbodiesel: Propellers: MT (3 blade) Seats: 4: Length . The Seneca IV was the last Piper produced under license by Embraer and that agreement terminated in 1996. Reissued : 4/16/2009: SA00944CH Yes. In combination with all my survival gear, HF radio, and other equipment, the HP's total ferry weight was about 4400 pounds—roughly 800 pounds . Piper PA-34-220T Seneca III;IV - Performance Data. Over the years, useful load has declined from over 1700 pounds on the Seneca II that I used to fly to more like 1400 pounds on the later Seneca V. Subtract 122 gallons worth of fuel (732 pounds), and you're left with about 670 paying pounds. Primarily used for personal and business flying, the Piper Seneca is an American twin-engined, light aircraft, produced by Piper Aircraft since 1971. Model: TSIO-360-EB. SAFETY . Height: 9.9 feet Fuel Capacity: 122 US gallons useable Max T/O Weight: 4,750 pounds Max Ramp Weight: 4,773 pounds Standard Empty Weight: 3,442 pounds Useful Load: 1,331 pounds Range: 828 NM including 45 minute reserve Service Ceiling . Fuel . The Seneca II retained the counter-rotating engine arrangement of the earlier Seneca. . Gross Weight: 4750 lbs/2155 kgs *Standard Empty Equipped Weight (b,c,d): 3377 lbs/1532 kgs 1971 - 1974 PIPER PA-34 Seneca View Comparison Twin engine piston aircraft with retractable landing gear. Vortex generators Nayak Nacelle Fuel Tanks, increased fuel capacity from 192 gal to 246 gal Cleve. dirkdj. SENECA V Piper Aircraft, Inc. 2926 Piper Drive, Vero Beach FL 32960 866-648-1945 FAX 772-978-6592 piper.com PN 767-559 01-2007 Piper Seneca V - PA-34-220T. FindAircraft.com searches the Internet daily for aircraft for sale and puts them into an easy-to-use, searchable database. The Piper Seneca V PIPER Page 5/44. Another normally aspirated option would be the Colemill President, a B55 converted with 300hp IO550 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 subsequent.). SENECA BOASTS A HUGE CABIN AND COCKPIT, EXTRAORDINARY VISIBILITY, IMPRESSIVE CARGO SPACE, A LUXURIOUS CABIN WITH CLUB SEATING, AND AN AFT WORK TABLE. Seneca Baron (fuel based on $4.71/gal) Seneca offers an average of 7% less operating cost. The G1000 avionics flight deck and multiple upgrades and refinements make current a classic, . Based on 450 annual owner-operated hours and $5.47-per-gallon fuel cost, the PIPER Seneca V has total variable costs of $157,306.50, total fixed costs of $32,950.00, and an annual budget of $190,256.50. Useable Fuel. Piper Seneca V - PA-34-220T. A 310Q or 310R (with 163 gallon fuel or greater) could make that trip non-stop without a headwind fairly reliably, and also do it at a significantly faster true airspeed. Fuel Capacity Useable: 122 US Gal | 462 Liters; Engines (2) Turbocharged Continental TSIO-360-RB Horsepower: 220 hp each; Dimensions Wingspan: 38 ft 11 . 2 Continental TSIO-360-RB. 2003 PIPER SENECA V Multi Engine Piston for sale located in Sugar Land TX from Hancock Aviation LLC 2405217. The aircraft can carry a maximum of 604 kg of standard useful load, while the fuel tank is designed to carry 462 l of usable fuel. Normal Range: 423 nm; Max Range: 886 nm; VFR Normal Range: 466 nm; VFR Max Range: 911 nm; Service Ceiling: 25000 ft; Distances. Fuel capacity, std . FUEL CAPACITY, USABLE 122 US gal | 462 liters RANGE WITH 45 MINUTE RESERVE . 235743.5 1413.2 lbs. Engine 1. at 75% at 7000 (Mi) 1,025: Cruise Range—Max. PROPELLER ENGINE Hartzell 3-Blade Constant Speed TSIO-360-RB Full-Feathering Counter-Rotating FUEL CAPACITY Usable 122 US gal | 462 L Aircraft Performance Details - FindAircraft.com is the #1 aircraft for sale search engine and trusted online resource for the Aircraft Dealer Network since 1998 with over 18,000 daily listings. The Piper Seneca is a powerful twin-engine aircraft, boasting several prominent differences compared to its piston-twin competitors. Piper PA-34-220T Seneca V's run around $750,000 new, depending on options. 170 US gal . Normal Operating Range. no. FUEL CAPACITY, USABLE 122 US gal | 462 liters Fuel Capacity: 128 Gallons Engines Engine 1 Make & Model: Continental TSIO-360-RB Engine 1 Serial Number: 322461 Engine 1 Time: 288.6 . 1-1 Outside views 1-2 Instruments panel 2- Plane features 3- Performances 3-1 Speeds 3-2 Other performances . Years before overhaul: 12. Piper 1997 Seneca V Base/used Price: $519,900 Engine make/model: Continental TSIO-360-RB Horsepower@altitude: 220 Horsepower for takeoff: 220 TBO hrs. At economy power it's possible for the Seneca to get 55 seat miles per gallon with a load of six. Piper took the first approach with the PA-34 Seneca: it's basically a Saratoga airframe with the 300 hp single engine replaced by two 200 (later 220) hp wing engines. Seats: 6 | Access wholesale aircraft prices with air.one! Unusable fuel (incl in BEW) 5 gal. Earlier models are significantly cheaper than this, of course. 2003 Piper Seneca V - N621LG Asking Price: $550,000 Serial Number: 3449296 Hancock Aviation is proud to represent this 2003 Piper Seneca V. . "Travel at FL250 in the pressurized comfort of the Piper M350, the pressurized turbocharged piston single." Usable Fuel (gal/L) 102/386 OIL CAPACITY (qts/L) 12/11.35 BAGGAGE Volume (ft3/m3) Forward Compartment 7/20 Aft Compartment 17.3/49 Capacity (lbs/kg) Forward Compartment 100/45.4 Aft Compartment 100/45.4 . Fuel Capacity Usable Fuel: 122 gallons/462 litres Oil Capacity Oil Capacity: 8 quarts/7.6 litres Baggage Volume: Forward Compartment: 15.3 cubic feet/.43 cubic meters A $317,500.00 loan over 120 months including $1322.92 per month in interest equates to a $15,920.63 per-period payment. FindAircraft.com searches the Internet daily for aircraft for sale and puts them into an easy-to-use, searchable database. . Performance Specifications Engine Manufacturer: Continental Model: TSI0-360-RB & L/TSIO-360-RB . The 58P is a fairly rare machine, pressurized and turbocharged, lacking the barn doors for passenger and cargo loading. r airplane airplane serial no. The G1000 avionics flight deck and multiple upgrades and refinements make current a classic, . The result is one of the longest-running twins in General Aviation. The empty weight is 3212 lb (1457 kg) and the maximum takeoff weight is 4750 . Unusable fuel (incl in BEW) 5 gal. . Over $500 in Savings! . Piper PA-34-220T Seneca V Specifications Powerplants 220-hp (ea) Teledyne Continental TSIO-360 Recommended TBO 1,800 hr Propellers . . Piper PA-34-200T C/R Turbo Seneca II - Performance Data. 288 SMOH Engines & Props. Search 1000's of Aircraft listings updated daily from 100's of dealers & private sellers. In between the extremes is a lot of payload, loading, and endurance flexibility. Piper Seneca V - PA-34-220T. For Sellers . Seneca developed the upgraded Cherokee Six trimotor, designated PA-32-3M, with two extra Lycoming O-235 and an extra 85kW (115hp) on either wing. 655 . . This listing was posted on May 10, 2022. Piper Seneca Series Aircraft Information. . New Piper continued production of the Seneca V. Certification was under FAA A7SO for: PA-34-200. PA-34-200 Seneca - Two 150kW (200hp) Lycoming IO-360-A1A fuel injected flat fours driving two blade c/s props. Performance Specifications Engine Manufacturer: Continental Model: TSI0-360-RB & L/TSIO-360-RB . 34 - the type designation for the Seneca family The Piper PA-44 Seminole is an American twin-engined light aircraft manufactured by Piper Aircraft. Full tanks provide an endurance of 4.5 hours at a 65-percent-power fuel burn of 23.3 gallons per hour, which yields 175 knots at 10,000 feet. Range remains one of the Comanche's strong points and many have been fitted with even more fuel capacity in tip tanks and fuselage tanks to give it . Cubic Feet CABIN . Annual inspection cost: . It has a maximum payload of 660 kg and a fuel capacity of 120 gallons. at 65% at 10,000' (Mi.) The Piper Seneca is the evolution of the two-engine Cherokee 6. Specifications (Seneca V): . _ seneca v. pa-34-220t sn 3449311, 3449323 and up. Cockpit and avionics 1976 Piper Seneca II MPH -- Limits study guide by tackleberryUSMC includes 70 questions covering vocabulary, terms and more. September 21, 2021, 5:03am #10. Piper's M350 is a direct descendent of the original Malibu of the early 1980s. A rule of thumb for remembering the general performance of the Piper Meridian is the rule of 250 cubed-it will deliver right around 250 knots at Flight Level 250 on 250 pounds of fuel per hour . Not amazing at all. Acces PDF Based on 450 annual owner-operated hours and $5.47-per-gallon fuel cost, the PIPER M350 has total variable costs of $127,422.00, total fixed costs of $32,000.00, and an annual budget of $159,422.00. 1981 PIPER SENECA III. 128 gal. History. : 1800 Fuel type: 100/100LL Propeller type/diameter: … Read More "Piper 1997 Seneca V" That 5.5 hours non-stop is going to be pushing it fuel wise, and so reality is you'll probably find yourself needing a stop in a lot of cases. Based on 450 annual owner-operated hours and $5.47-per-gallon fuel cost, the PIPER Seneca IV has total variable costs of $172,552.50, total fixed costs of $26,650.00, and an annual budget of $199,202.50. Engine 1 Time. Piper M350. Bendix KMD-850 w/ Terrain, Traffic, & Radar. 100/100LL. Fuel Capacity: 732 Lb; Payload W/Full Fuel: 444 Lb; Max Payload: 1153 Lb; PZL104. 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 . Find TC-IMN 2005 PIPER SENECA V on Aircraft.com. 2003 Seneca V 2062 TTAF. I'm working on an installation article for the Piper Flyer which I hope to have completed and submitted to the PFA editor in early March. In 1961, Piper offered an optional 90-gallon system, which gave the Comanche 180 seriously long legs: nine hours, provided it was only loaded with the pilot, one passenger and a little baggage. 2003 PIPER SENECA V For Sale in Baton Rouge, Louisiana at Controller.com. 2003 Piper Seneca I airplane for sale located in Sugar Land, Texas. The Piper M350 is the latest variant of the Piper Malibu Mirage, a pressurized turbocharged piston single aircraft, upgraded with the Garmin G1000 NXi and ESP (Electronic Stability Protection) as standard. . The Lycoming O-360 series engines are four-cylinder, direct-drive, horizontally opposed, air-cooled models, and are approved for use of 93 octane unleaded fuel. Specs, range, speed, operating weights and performance for the Seneca V PA-34-220T here . PIPER PA-32R-301 SARATOGA SP SPECIFICATIONS ENGINE Manufacturer Lycoming Model IO-540-K1G5D . The standard fuel capacity of the PA-24-180 was 60 US gallons (230 L). Like with Soviet aircraft - whose designations and serial numbers amount to pretty much the airframe's entire ID card - you can tell a lot about pre-80s Pipers just by making sense of all the gibberish on their data plates. . Fuel Capacity Useable 122 US gal / 462 liters Cruising Speeds TAS 10,000 ft 18,500 ft Maximum Cruise Power 182 kts / 337 km/h 197 kts / 365 km/h . This breaks down to $354.27 per hour. at 75%) 28: Fuel Consumption (Gal./Hr. The Seneca V measures 8.7m-long and 3m-high, and has a wing span of 11.9m. A total of 4,464 Seneca were delivered by 1 January 1991. 1,200: Cruise Range—Optimum (Mi) 1,400: Minimum Controllable Single Engine speed (MPH) 80 The PA-46-310P Malibu has an exterior length of 8.6 meters, an exterior height of 2.1 meters, a tail height of 3.4 meters, and a fuselage diameter of 1.3 meters. 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 . Horsepower: 200 HP. Contents 1 Development 1.1 PA-34-180 Twin Six 1.2 PA-34-200 Seneca 1.3 PA-34-200T Seneca II 1.4 PA-34-220T Seneca III It is the most successful six-place light twin from its inception. This upgrade will add 30 gallons of fuel to my already tanked 129 giving me almost 160 usable gallons. Seneca v Specifications 2013 Seneca v wing span 38.9 ft/11.9 m | length 28.6 ft/8.7 m | height 9.9 ft/3.0 m Turbocharged Six-Place Piston Twin The Piper Seneca v with the latest in garmin g1000 Avionics, is a powerful twin-engine aircraft, built to . ; regist. Performance Specifications Engine Manufacturer: Continental Model: TSI0-360-RB & L/TSIO-360-RB . The Piper PA-34 Seneca is a twin-engined light aircraft, produced in the United States by Piper Aircraft. Engine 1 Serial Number. Payments as low as 2003 Piper Seneca I airplane for sale located in Sugar Land, Texas. Engine 1 Model. To take some examples of aircraft recently up for sale, a Seneca II will usually sell for something over $100,000, but according to some sources, it is possible to find early Senecas from around 1972 for as little as $35,000. Good economical twin, GPS approved for VFR/IFR enroute, B-RNAV, terminal and instrument approach (GPS, VOR, CONTINENTAL TSIO360RB . The Seneca is propelled by twin-engine reliability and power, the highest single-engine service ceiling in its class, and a sophisticated three-screen G1000 NXi avionics setup. Swiss stability. at 65%) 24: Cruise Range - Max. 322461. The Piper Archer is powered by a single Lycoming O-360-A4M engine generating 180hp. A Little History of the Seneca V. The Seneca V fuselage is a highly upgraded version of the fixed gear PA-32 that debuted with the Cherokee Six in the mid-1960s. Aircraft Performance Details - FindAircraft.com is the #1 aircraft for sale search engine and trusted online resource for the Aircraft Dealer Network since 1998 with over 18,000 daily listings. The PA-46-310P has a maximum takeoff and landing weight of 2,310 kg and 2,199 kg, respectively. Seneca Baron (fuel based on $4.71/gal) Seneca offers an average of 7% less operating cost. Engine 1 Serial Number. CONTINENTAL. FUEL CAPACITY 128 Gallons RENTAL RATE $360 per hour DESCRIPTION Certified on July 18, 1974, the Piper PA-34-200T Seneca II is powered a pair of six cylinder Continental TSIO-360E or EB engines for improved performance, particularly at higher altitudes. At 23 gallons per cruise hour I will have an almost six hour cruise range. Whether you are traveling for business or looking for an escape, the Seneca is equipped to take on the city, mountains, and so much more. Maximum Weights Ramp Weight 4200 lb. Compare. 1-1 Outside views 1-2 Instruments panel 2- Plane features 3- Performances 3-1 Speeds 3-2 Other performances . The maximum take-off weight and standard equipped weight of the aircraft are 2,155kg and 1,561kg respectively. The Seneca V PA-34-220T produced by Piper. . Length: 29.6 ft. Fuel capacity of the Archer is 48 U.S. gallons (182 liters). The 260 was also available as the Turbo Comanche C with a Rajay turbocharger and was introduced in 1970. Airframe Total Time 433 Fuel Capacity Volume 123 gal Complete Logs Yes Engine 1 Engine 1 Manufacturer CONTINENTAL Engine 1 Model TSIO360RB Engine 1 Horsepower 220 HP 128 gal.
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