1978 Piper PA34 200T Seneca II In South Africa (ZS-KHX) (WITHDRAWN)

Description

PERFORMANCE
Published figures are for standard airplanes flown at gross weight* under standard conditions at sea level, unless otherwise stated. Performance for a specific airplane may vary from published figures depending upon the equipment installed, the condition of engine, airplane & equipment, atmospheric conditions & piloting technique. Each performance figure below is subject to the same conditions as on the corresponding performance chart from which it is taken in the Performance Charts Section.

Gross Weight (pounds): 4570 (2073 kg)
Take-off Run, flaps up, sea level (ft): 1100
Take-off Distance Over 50-ft Obstacle, flaps up, sea level: 1460
Take-off Run (ft) (short field effort, flaps 25°): 900
Take-off Distance Over 50-ft Barrier (ft) (short field effort, flaps 25°): 1240
Minimum Controllable Single Engine Speed (mph): 80 (128 kph)
Rate of Climb, sea level (ft per min): 1340
Rate of Climb, sea level, single engine (ft per min): 225
Best Rate of Climb Speed (mph): 105 (169 kph)
Best Rate of Climb Speed, sea level, single engine (mph): 105 (169 kph)
Best Angle of Climb Speed, sea level (mph): 90 (144 kph)
Best Angle of Climb Speed, sea level, single engine (mph): 93 (150 kph)
Max Speed, sea level (mph): 197 (317 kph)
Max Speed, 12,000 ft. (mph) 225 (362 kph)
Max Speed Optimum Alt, 20,000 ft. 75% power: (TAS) (mph), 218 (351 kph)
Service Ceiling (ft): 25,000**
Service Ceiling, engine out (ft): 13,400
Absolute Ceiling (ft): 25,000**
Absolute Ceiling, engine out (ft): 14,800
Stalling Speed, gear & flaps down, power off (mph): 69 (111 kph)
Stalling Speed, gear down and flaps up, power off (mph): 76 (122 kph)
Fuel Consumption, 15% power, both engines (ephy): 23.6
Landing Roll (flaps down) (ft): 20.5
Landing Over 50-ft Barrier (flaps down) (short field effort) (ft): 1380*
*4342 Ib G.W., Maximum Landing Weight: 2090* (948 kg)

Cruise Speed at best power mixture (mph)
65% power, 24,000 ft: 208 (335 kph)
55% power, 25,000 ft: 189 (304 kph)

Fuel Capacity (Standard / Optional)
Range at best power mixture (mi)
75% power, 16,000 ft With 45 min. reserve: 626 / 900
No reserve: 742 / 1020

55% power, 16,000 ft
With 45 min. reserve: 701 / 1010
No reserve: 830 / 1140

WEIGHTS
Gross Weight (lbs) Max. Take-off: 4570 (2073 kg)
Max. Landing: 4342 (1970 kg)
Max Zero Fuel Weight (Ibs): 4000 (1814 kg)
Standard Empty Weight (lbs): 2788 (1265 kg)
Maximum Useful Load (lbs) (All weight in excess of 4000 lbs must consist of fuel.): 1782 (808 kg)

POWER PLANT
Right Engine (Continental): LTSIO-360-E or LTSIO-360-EB
Left Engine (Continental): TSIO-360-E or TSIO-360-EB
Rated Horsepower (sea level) (12,000 ft): 200
Rated Speed (rpm): 215
Max Manifold Pressure (in. Hg.): 40
Bore (in.): 4.438
Stroke (in.): 3.875
Displacement (cubic in.): 360
Compression Ratio: 7.5:1

FUEL & OIL
Fuel Capacity (U.S. gal)
Standard: 98
Optional (Installed: this Seneca): 128
Unusable fuel (U.S. gal): 5
Fuel, Aviation Grade (minimum octane): 100/130
Oil Capacity (qts) (each engine): 8
Range: 1400-1500 Km
Total Time to Fly on Full tanks: 5.5 Hours

BAGGAGE AREA
Maximum Baggage (Ibs) Forward Compartment: 100 (45 kg)
Maximum Baggage (Ibs) Rear Compartment: 100 (45 kg)
Baggage Space (cubic ft) Forward Compartment: 15.3
Baggage Space (cubic ft) Rear Compartment: 20
Baggage Door Size (in.) Forward Compartment: 24 x 21

DIMENSIONS
Wing Span (ft): 38.9 (11.8 m)
Wing Area (sq ft): 208.7 (19.4 sq m)
Length (ft): 28.5 (8.7 m)
Height (ft): 9.9 (3.0 m)
Wing Loading (lbs per sq ft): 22 (236 lbs per sq m)
Power Loading (Ibs per hp) (sea level): 11.4
(12,000 ft): 10.6
Propeller Diameter (in.): 76
Turn Radius (ft): 33.2

LANDING GEAR
Wheel Base (ft): 7.0
Wheel Tread (ft): 11.1
Tire Pressure (psi): 31
Tire: 50
Nose: 6.00 x 6
Main: 6.00 x 6