1996 PIPER SENECA IV
Aircraft Summary
General
Year
1996
Manufacturer
PIPER
Model
SENECA IV
Condition
Used
FlightRules
IFR
Based at
EDAZ
Description
A great trainer or family commuter. Max Take Off Weight 4407lbs (1999kg) no airway fees in Europe. 1021lbs (463kg) Useful load Fuel Capacity 128 USG 22-30 GPH in cruise with 160-180KT. The Max range is 800 miles (1481km).
Airframe
Total Time
1010
Range
900 NM
Max Takeoff Weight
4,404.84 lb
Useful Load
1,020.74 lb
Complete Logs
Yes
Engine 1
Engine 1 Manufacturer
CONTINENTAL
Engine 1 Model
TSIO360A
Engine 1 Horsepower
210 HP
Engine 1 Time
144
Engine 1 Time Since
SMOH
Engine 1 TBO
1800
Engine 1 Turbocharged
Yes
Engine 2
Engine 2 Manufacturer
CONTINENTAL
Engine 2 Model
TSIO360A
Engine 2 Horsepower
210 HP
Engine 2 Time
144
Engine 2 Time Since
SCMOH
Engine 2 TBO
1800
Engine 2 Turbocharged
Yes
Engine 2 Notes
Turbocharged Continental engines. Reliable, smooth, and efficient. TSIO-360 210hp with only 144 hours on each engine. Counter-rotating engines for safety. Propeller McCauley 3AF32C509-C/L82NFA-6 with only 75 hours on each
Props
Prop 1 Manufacturer
MCCAULEY
Prop 1 Model
3AF32C509
Prop 2 Manufacturer
MCCAULEY
Prop 2 Model
3AF32C509
Number of Blades
3
Blade Composition
Aluminum
Props Sync
Yes
Avionics
WAAS
Yes
Avionics/Radios
Reliable classic equipment: Kings KX 165A NAV/COMS with 8.33KHz GPS KLN 90B BR/NAV DME KN62A Stormscope L3 Radar Altimeter Kind Weather Radar Auto Pilot KFC 150 Transponder KT79 and KT73 Tablet mount with cooling fans
Additional Equipment
Oxygen System
Yes
Flight Into Known Icing (FIKI)
Yes
Exterior
Year Painted
1996
Interior
Year Interior
1996
Number of Seats
6
Configuration
Passenger
Inspection Status
Inspection Status
Current under all required inspections under EASA, ready to fly
Airworthy
Yes
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