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100% Bonus Depreciation Is Here to Stay! Learn more.

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Performance & Specifications · Piper

Piper Seneca V PA-34-220T Performance and Specifications

Specifications, performance and limiting airspeeds, including single-engine figures, for the twin-engine Piper PA-34-220T Seneca V.

Piper Seneca V
Engines
2 × TSIO-360, 220 hp ea
Normal cruise
200 kt @ 25,000 ft
High-speed cruise
182 kt @ 10,000 ft
Service ceiling
25,000 ft
Single-engine ceiling
16,500 ft
Max useful load
1,337 lb
Piper PA-34-220T Seneca V

Specifications

Engines & Propellers

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)

Dimensions

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

Cabin

Seats
6
Cabin length
10 ft 4 in
Cabin width
4 ft 1 in
Cabin height
3 ft 6 in

Weights

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

Capacities

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

Questions About the Piper Seneca V?

Talk with an AirMart aircraft specialist about the Piper Seneca V: performance, ownership and what to look for when you buy.

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Piper PA-34-220T Seneca V

Performance

Ground rollTotal distance over a 50-ft obstacle50-ft obstacle
Takeoff
Ground roll 1,143 ftOver 50-ft obstacle 2,180 ft
Accelerate-stop0 flaps
Over 50-ft obstacle 2,650 ft
Landing
Ground roll 1,143 ftOver 50-ft obstacle 2,180 ft
Airspeed Limits at a GlanceKIAS · from the figures on this sheet
406080100120140160180200220VNE 204Vmc 66Vyse 88Vr 81Vsse 85Vle 128Va 139
Flap operating range (61–113)Normal operating range (67–164)Caution range (164–204)Never exceed (204)Vmc 66: min control speed, one engine inoperativeVyse 88: best single-engine rate of climb
With One Engine InoperativeTwin-engine figures from the sheet

Rate of climb, sea level

Both engines
1,460 fpm
One engine
253 fpm

Service ceiling

Both engines
25,000 ft
One engine
16,500 ft

Takeoff & Landing

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
Landing distance over 50-ft obstacle
2,180 ft
Landing distance, ground roll
1,143 ft

Climb & Ceilings

Rate of climb, sea level
1,460 fpm
Single-engine ROC, sea level
253 fpm
Max operating altitude
25,000 ft
Service ceiling
25,000 ft
Single-engine service ceiling
16,500 ft

Cruise

@ High-speed cruise, 10,000 ft
182 kt/635 nm (28 gph)
@ Normal cruise, 25,000 ft
200 kt/645 nm (24 gph)

Cruise speed/range w/45-min rsv (fuel consumption).

Limiting and Recommended Airspeeds

Vr (rotation)
81 KIAS
Vx (best angle of climb)
83 KIAS
Vy (best rate of climb)
88 KIAS
Vxse (best single-engine angle of climb)
83 KIAS
Vyse (best single-engine rate of climb)
88 KIAS
Vmc (min control w/one engine inoperative)
66 KIAS
Vsse (min intentional one-engine operation)
85 KIAS
Va (design maneuvering)
139 KIAS
Vfe (max flap extended)
113 KIAS
Vle (max gear extended)
128 KIAS
Vlo (max gear operating)
Extend
128 KIAS
Retract
107 KIAS
Vno (max structural cruising)
164 KIAS
Vne (never exceed)
204 KIAS
Vs1 (stall, clean)
67 KIAS
Vso (stall, in landing configuration)
61 KIAS

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.

Talk to an AirMart Aircraft Specialist

Call us to discuss the Piper Seneca V, or send a message through our contact page and we'll get back to you.

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Elevate Your Journey â„¢

Specifications for this aircraft are believed to be accurate but are not warranted. It is the responsibility of the buyer to confirm all specifications, equipment, and times. AirMart does not represent or warrant the working order, merchantability, or operability of any equipment. Airplanes are dynamic assets whose condition, availability, and details may change without notice. All information is subject to independent verification and inspection by the buyer. Availability cannot be guaranteed, as the aircraft may be sold, leased, or withdrawn from the market at any time.
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