2013 Seneca V Specifications and Pricing

Piper PA-34 Seneca V · Specifications

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Overview

The document provides detailed specifications and pricing information for the Piper PA-34 Seneca V, a twin-engine aircraft known for its turbocharged performance and advanced avionics. It is designed for pilots and aviation enthusiasts interested in the technical aspects and operational capabilities of the Seneca V. Key features include engine specifications, dimensions, weights, fuel capacity, performance metrics, and standard equipment. The document also outlines optional equipment and interior/exterior styling options, making it a comprehensive reference for potential buyers and operators.

Engine: 2 x Continental TSiO-360-RB, 220 hp each
Maximum Takeoff Weight: 4,750 lbs (2,155 kg)
Cruising Speed: 200 KTAS (370 km/h)
Range: 828 nm (1,534 km) with 45 min reserve
Maximum Approved Altitude: 25,000 ft (7,620 m)

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Document details

Type: Specifications
Year: 2013
Pages: 4
File size: 372 KB
Publisher: cutteraviation.com

Specifications & performance

Extracted from this document.

Specifications

Range (nm): 828
Engine (hp): 220
Height (ft): 9.9
Length (ft): 28.6
Propeller: McCauley 3 Blade
Wingspan (ft): 38.9
Engine model: Continental TSiO-360-RB
Max speed (kt): 200
Empty weight (lb): 3,442
Fuel capacity (gal): 122
Service ceiling (ft): 25,000
Max takeoff weight (lb): 4,750

Performance

Landing over 50ft: 2,180
Takeoff over 50ft: 1,707
Landing distance (ft): 1,400
Takeoff distance (ft): 1,143

Weight & balance

Useful load (lb): 1,331
Max ramp weight (lb): 4,773
Basic empty weight (lb): 3,442
Max takeoff weight (lb): 4,750

Documentation completeness

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In this document

Engines

The Piper PA-34 Seneca V is powered by two turbocharged Continental TSiO-360-RB engines, each producing 220 horsepower. The engines have a total cylinder count of six and a time between overhaul (TBO) of 1,800 hours.

Dimensions

The aircraft has a wingspan of 38.9 feet (11.9 meters), a length of 28.6 feet (8.7 meters), and a height of 9.9 feet (3.0 meters). These dimensions contribute to its performance and handling characteristics.

Weights

The maximum takeoff weight of the Seneca V is 4,750 pounds (2,155 kg), with a maximum ramp weight of 4,773 pounds (2,165 kg). The standard equipped weight is 3,442 pounds (1,561 kg), providing a standard useful load of 1,331 pounds (604 kg).

Fuel Capacity

The usable fuel capacity of the Seneca V is 122 US gallons (462 liters), allowing for extended range and operational flexibility.

Performance

The maximum cruising speed is 200 knots true airspeed (KTAS) or 370 km/h, with a range of 828 nautical miles (1,534 km) when maintaining a 45-minute reserve. The aircraft can reach a maximum approved altitude of 25,000 feet (7,620 meters) and has a single-engine service ceiling of 16,500 feet (5,029 meters).

Takeoff and Landing Distances

The takeoff distance over a 50-foot obstacle is 1,707 feet (520 meters), with a ground roll of 1,143 feet (348 meters). For landing, the distance over a 50-foot obstacle is 2,180 feet (664 meters), with a ground roll of 1,400 feet (427 meters).

Safety notes

It is the responsibility of the pilot to conduct all operations in accordance with the approved Pilot’s Operating Handbook, which is the only official source of data.

Full document text

2013 Seneca VSpecifications and Pricing PA-34-220T EnginES (2) Turbocharged Continental TSiO-360-RB Horsepower: 220 hp each number of Cylinders: 6 TBO: 1,800 hours PROPEllERS McCauley 3 Blade | Constant Speed | Full-Feathering DiMEnSiOnS Wing Span: 38.9 ft | 11.9 m length: 28.6 ft | 8.7 m Height: 9.9 ft | 3.0 m WEigHTS Maximum Takeoff Weight: 4,750 lbs | 2,155 kg Maximum Ramp Weight: 4,773 lbs | 2,165 kg Standard Equipped Weight: 3442 lbs | 1,561 kg Standard Useful load: 1,331 lbs | 604 kg FUEl CAPACiTy Usable: 122 US gal | 462 liters MAXiMUM CRUiSing SPEED 200 ktas | 370 km/h RAngE WiTH 45 MinUTE RESERvE 828 nm | 1,534 km MAXiMUM APPROvED AlTiTUDE 25,000 ft | 7,620 m SinglE EnginE SERviCE CEiling 16,500 ft | 5,029 m TAkEOFF DiSTAnCE ground Roll: 1,143 ft | 348 m Total Over 50 ft Obstacle: 1,707 ft | 520 m lAnDing DiSTAnCE ground Roll: 1,400 ft | 427 m Total Over 50 ft Obstacle: 2,180 ft | 664 m 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 stand the test of time. it boasts the highest single-engine service ceiling in its class, making it the perfect choice for operations in and around mountainous terrain and over water. With energetic handling and intuitive avionics, the Seneca v is a pleasure to fly. And, with an operating cost averaging 10% less than its competitor, the Seneca v is the more efficient airplane to fly. Seats Engines Horsepower Max Cruise Range Standard Useful Load 4 Lycoming O-360-A1H6 180 hp each 162 ktas / 300 km/h 700 nm / 1,296 km 1,191 lbs / 540 kg SEMINOLE 200 ktas / 370 km/h 828 nm / 1,534 km 1,331 lbs / 604 kg 220 hp each Continental TSIO-360-RB 6 SENECA V SPECIFICATIONS Which Piper Twin is right for you? Standard AviOniCS Garmin G1000 Avionics Suite Dual 10” PFDs, Single 10” MFD, Dual giA63W nAv/COM/gPS, S-TEC 55X Autopilot with Altitude Preselect, Attitude and Heading Reference System, Air Data Computer (ADC), Dual iFR Enroute/Approach and WAAS Certified gPS, Electronic Engine indication System (EiS), garmin FliteCharts, SafeTaxi, gMA 340 Audio Panel, gTX 33 Mode S Transponder, Traffic information Systems (TiS), and Aspen Standby System (EFD-100). ADDiTiOnAl STAnDARD EqUiPMEnT Propeller Synchrophaser AviOniCS EqUiPMEnT OPTiOnS 235: Jeppesen Chartview – $3,950 256: iridium Transceiver (gSR-56) – $15,990 268: gWX 68 Weather Radar – $40,190 269: gDl 69A XM Satellite Radio/Weather – $10,500 330: Stormscope WX-500 – $10,900 (cannot be combined with option 269) 346: Synthetic vision – $17,450 374: 2nd AHRS & ADC – $21,450 450: TAWS-B (Terrain Awareness and Warning System) – $12,000 524: king kR 87 ADF – $7,900 563: king kn 63 DME – $13,650 825: gTS-825 Traffic Advisory System – $32,920 ADDiTiOnAl OPTiOnS 201: PiperAire Air Conditioning with HFC-134a Refrigerant – $21,840 298: Full De-icing group with Annunciators – $49,100 361: 1,999 kg gross Weight kit – $4,350 363: United kingdom lighting Package – $1,350 375: Built-in Oxygen System with kevlar Bottle – $10,600 605: yaw Damper System – $7,600 700: Top Metallic Base Coat – $6,550 710: Bottom Metallic Base Coat – $6,550 715: non-Standard Approved Paint Scheme – quoted Upon Request AMSAFE: AmSafe Aviation Airbag System (crew seats) – $5,700 (installed after aircraft certification at Piper Factory Service Center, vero Beach, Fl) Additional Special Options – quoted Upon Request * Fly-Away-Factory (F.A.F.) vero Beach, Fl – Dealer delivery and local taxes extra. Optional The Seneca v interior is available in four distinct color schemes: Sienna, Sand, and Steel. Each scheme includes seats that are constructed with hand-selected natural leather, tested for maximum quality. Thick-woven and wear-resistant color coordinating carpet lines the floor. Complementary headliner and side panel fabrics are smooth and durable. An entertainment console includes storage room and cup holders. A built-in work table folds seamlessly into the side panel. The 2013 Seneca v exterior styling offers a two-tone scheme in DuPont imron polyurethane paint with a choice of metallic or non-metallic colors. The empennage is full-color. Registration numbers are color coordinated. Custom paint schemes are quoted upon request. interior Styling Exterior Styling Equipment Standard Equipped list Price: $972,400* Sand Steel Sienna Shown in Sand PiPER AiRCRAFT, inC. | 2926 PiPER DRivE | vERO BEACH | Fl | 32960 | 772.567.4361 | PiPER.COM P/n 767-611 Piper Aircraft, inc. reserves the right to make changes, including, but not limited to, changes in specifications, materials, equipment and/or prices at any time without prior notice. it is the responsibility of the pilot to conduct all operations in accordance with the approved Pilot’s Operating Handbook, which is the only official source of data. © 2013 Piper Aircraft, inc.

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