SPEC SHEET

Piper PA-34 Seneca V · Specifications

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Overview

This document provides detailed specifications for the Piper PA-34-220T Seneca V, a twin-engine aircraft known for its performance and versatility. It is intended for pilots, aviation enthusiasts, and those interested in the technical aspects of the aircraft. Key information includes powerplant specifications, performance metrics, and dimensional data, all of which are crucial for understanding the aircraft's capabilities and operational limits. The specifications are based on standard conditions and provide insights into the aircraft's design and operational efficiency.

Powerplants: 220-hp (each) Teledyne Continental TSIO-360 engines.
Max takeoff weight: 4,750 lb.
Cruise speed at 25,000 ft: 200 kt with a range of 645 nm.
Takeoff distance over 50-ft obstacle: 2,180 ft.
Max demonstrated crosswind component: 17 kt.

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Document details

Type: Specifications
Pages: 3
File size: 47 KB
Publisher: airmart.com

Specifications & performance

Extracted from this document.

Specifications

Range (nm): 635
Engine (hp): 220
Height (ft): 9
Length (ft): 28
Propeller: Hartzell two-blade
Wingspan (ft): 39
Engine model: Teledyne Continental TSIO-360
Max speed (kt): 200
Cruise speed (kt): 182
Empty weight (lb): 3,413
Fuel capacity (gal): 128
Rate of climb (fpm): 1,460
Service ceiling (ft): 25,000
Max takeoff weight (lb): 4,750

Performance

Fuel burn (gph): 28
Landing over 50ft: 2,180
Max crosswind (kt): 17
Takeoff over 50ft: 2,180
Landing distance (ft): 1,143
Takeoff distance (ft): 2,180
Stall speed clean (kt): 67
Stall speed landing (kt): 61

V-speeds

VA: 139
VR: 81
VX: 83
VY: 88
VFE: 113
VNE: 204
VNO: 164
VS1: 67
VSO: 61

Weight & balance

Useful load (lb): 1,337
Max ramp weight (lb): 4,773
Baggage allowance (lb): 185
Basic empty weight (lb): 3,413
Max landing weight (lb): 4,513
Max takeoff weight (lb): 4,750

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In this document

Powerplants

The Piper PA-34-220T Seneca V is equipped with two Teledyne Continental TSIO-360 engines, each producing 220 horsepower. The recommended time between overhaul (TBO) for these engines is 1,800 hours.

Dimensions and Weights

The aircraft has a length of 28 feet 7 inches, a height of 9 feet 11 inches, and a wingspan of 38 feet 11 inches. The standard empty weight is 3,413 pounds, with a maximum ramp weight of 4,773 pounds and a maximum takeoff weight of 4,750 pounds.

Performance

The Seneca V has a takeoff distance of 1,143 feet over ground and 2,180 feet over a 50-foot obstacle. It can climb at a rate of 1,460 feet per minute at sea level, with a maximum operating altitude of 25,000 feet.

Airspeeds

Key airspeeds include V R (rotation) at 81 KIAS, V X (best angle of climb) at 83 KIAS, and V Y (best rate of climb) at 88 KIAS. The stall speed in a clean configuration is 67 KIAS.

Fuel and Baggage Capacity

The standard fuel capacity is 128 gallons, with 122 gallons usable, weighing 768 pounds (732 pounds usable). The baggage capacity includes 100 pounds forward external and 85 pounds aft internal.

Safety notes

All performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.

Full document text

SPEC SHEET 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 Seats 6 Cabin length 10 ft 4 in Cabin width 4 ft 1 in Cabin height 3 ft 6 in Standard empty weight 3,413 lb Max ramp weight 4,773 lb Max takeoff weight 4,750 lb Max zero fuel weight 4,479 lb Max useful load 1,337 lb Max payload w/full fuel 605 lb Max landing weight 4,513 lb Fuel capacity, std 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 Performance Takeoff distance, ground roll 1,143 ft Takeoff distance over 50-ft obstacle 2,180 ft Accelerate-stop distance, 0 flaps 2,650 ft Max demonstrated crosswind component 17 kt Rate of climb, sea level 1,460 fpm Single-engine ROC, sea level 253 fpm Cruise speed/range w/45-min rsv (fuel consumption) @ High-speed cruise, 10,000 ft 182 kt/635 nm (28 gph) @ Normal cruise, 25,000 ft 200 kt/645 nm (24 gph) Max operating altitude 25,000 ft Service ceiling 25,000 ft Single-engine service ceiling 16,500 ft Landing distance over 50-ft obstacle 2,180 ft Landing distance, ground roll 1,143 ft Limiting and Recommended Airspeeds V R (rotation) 81 KIAS V X (best angle of climb) 83 KIAS V Y (best rate of climb) 88 KIAS V XSE (best single-engine angle of climb) 83 KIAS V YSE (best single-engine rate of climb) 88 KIAS V MC (min control w/one engine inoperative) 66 KIAS V SSE (min intentional one-engine operation) 85 KIAS V A (design maneuvering) 139 KIAS V FE (max flap extended) 113 KIAS V LE (max gear extended) 128 KIAS V LO (max gear operating) Extend 128 KIAS Retract 107 KIAS V NO (max structural cruising) 164 KIAS V NE (never exceed) 204 KIAS V S1 (stall, clean) 67 KIAS V SO (stall, in landing configuration) 61 KIAS For more information, contact The New Piper Aircraft Inc., 2926 Piper Drive, Vero Beach, FL 32960; telephone 561/567-4361; fax 561/778-2144; or visit the Web site ( www.newpiper.com). All specifications are based on manufacturer's calculations. All performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.

All Piper PA-34 Seneca V specifications