PIPER SENECA III AIRCRAFT SERIAL # 34 – 8533018 FULLY AIR-CONDITIONED OUR COMPANY IS THE FIRST OWNER SINCE NEW
Piper Seneca III PA34 220T AIR-CONDITIONED VINTAGE – 1985 Specifications
Aircraft Serial # 34-8533018 DIMENSIONS Total Aircraft Hours 8602 Wing Span (ft./m) 38.9/11.9 Total Aircraft Hours since Last C of A 07 Length (ft./m) 28.6/8.7 Height (ft./m) 9.9/3.0 ENGINES Cabin Length (Instrument panel to rear bulkhead)
Manufacturer Continental (in./cm.) 125.0/317.5 Model TSIO-360-KB Cabin width (in./cm.) 49.0/124.5 Rating (hp @ rpm) & LTSIO-360-KB Cabin Height (in./cm.) 42.0/1067 Take-off Power (5 Min. Limit) 220 @ 2800 Headroom (Seat to Ceiling) Maximum Continuous Power 200 @ 2600 Front Seats (in./cm.) 38/96.5 Number of Cylinders 06 Middle Seats (in./cm.) 36.5/90.8 Recommended TBO (hrs.) 1800 Rear Seats (in./cm.) 34.5/87.6 Left Engine hours 456 Forward Baggage Door Size (in./cm.) 21/53.3 x 24/61.0 Rt. Engine hours 650 Aft Baggage/Utility Door Size (in./cm.) 20.5/52.1 x 26/66.0 Forward cabin Door Size (in./cm.) 35/88.9 x 36/91.4 PROPELLERS Wheel Base (ft./m) 7/2.13
Manufacturer McCauley Wheel Treated (ft./m) 11.1/3.39
Number of Blades 3 Type Constant Speed, FUEL CAPACITY Full Feathering Diameter (in./cm.) 76/193 Total Capacity (gal./L) 128/484 1039 / 65 months Useable Fuel (gal./L) 123/466 Right Propeller Hours/Cal Life 858 / 38 months WEIGHTS Ramp Weight (lbs./kg) 4773/2165 OIL CAPACITY (qts./L) 8/7.57 Gross Take-off weight (lbs./kg) 4750/2154 Gross Landing Weight (lbs./kg) 4513/2047 BAGGAGE Empty Weight (lbs./kg) 3243/1474 Volume (ft.³/m³) (Includes: unusable fuel, full oil and full Forward Compartment 15.3/.43 operating fluids) Aft Compartment 17.3/.49 Useful Load (lbs./kg) 1530/695 Capacity (lbs./kg) Zero Fuel Weight (lbs./kg) 4470/2028 Forward Compartment 100/45.4 Aft Compartment 100/45.4 Performance FUEL CONSUMPTION
MAXIMUM SPEED 196 / 363 High Speed Cruise Power (75%) 29.0/110
Kts / kmh (TAS at Mid-Cruise Weight) Economy Cruise Power (65%) 23.3/88 ( OPT. ALTITUDE 10.000 FT ) (gph/lph)
ECONOMY CRUISE 175 / 324 (Fuel Cons: 191 gph) RAT E OF CLIMB Takeoff Power Continuous Power LONG RANGE CRUISE 143 / 265 (Fuel Cons: 168 gph) (At see Level and Gross Wt.)
Two Engine (fpm/mpm) 1400/427 1300/396 High Speed Cruise Power (75%) 179/332 193/358 Single Engine (fpm/mpm) 240/73 200/61
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|
Name of Equipment |
Quantity |
Manufacturer |
Model |
|
i. HF Communication |
- |
- |
- |
|
ii. VHF Communication-3 |
02 |
King |
KY-197 |
|
iii. ADF |
01 |
King |
KR-87 |
|
iv. ILS/VOR |
01/02 |
King |
KNS-80/KN53 |
|
v. Marker |
01 |
King |
KMA24 |
|
vi. DME |
01 |
King |
KNS80 |
|
vii. Radio Altimeter |
- |
- |
- |
|
viii. Airborne Radar System |
- |
- |
- |
|
ix. ATC Transponder |
01 |
King |
KT76A |
|
x. Intercommunication |
01 |
King |
KMA24 |
|
xi. SELCAL |
- |
- |
- |
|
xii. ELT |
01 |
ACK Technologies Inc |
ELT- 01 |
|
xiii. GPWS |
N/A |
- |
- |
|
xiv. TCAS - II |
N/A |
- |
- |
|
xv. GPS |
01 |
Garmin |
GPS-100 |