Aircraft Specifications
1980 Piper Seneca II (PA-34-200T)
Engines: 6 cylinder, horizontally opposed, direct drive, air-cooled, turbo supercharged, fuel injected Continental engines rated @ 200 HP @ 2575 RPM at sea level.
Props: 3 blade McCauley - Constant speed variable pitch, full feathering.
Fuel: 128 Gallon (123 useable) 100LL (BLUE)
Fuel consumption @ 75% BHP - 23.6 GPH
Landing Gear: Retractable, hydraulically activated by an electrically powered reversible pump.
-Landing gear system is equipped with a "gear warning horn" and a "gear unsafe light" that activates when:
Gear selector switch is up while aircraft is on the ground
Gear not down and locked when the throttle is below 14" MP
Electrical: 2 X 65 Ampere, 14 volt Alternators
1 X 35 Ampere, 12 volt Battery
Equipment and Avionics:
| Audio Panel | KMA 20 |
| Nav/Comm1 | KX 155 |
| Nav/Comm2 | KX 155 |
| HSI | KCS 55A |
| ADF | BX 2000 |
| Transponder | BX 2000 |
| RNAV | FMS 5000 / IFR for enroute and terminal |
| DME | KING |
| GPS | *Garmin 430 / Weather Overlay* |
| Auto-Pilot | KFC 200 Autopilot / Flight Director |
| Electric Trim | YES |
| De-Ice | New in 2002 |
| RADAR | WX 10A |
We have upgraded our avionics package by taking out the Loran and installing a Garmin 430 GPS with Weather Data Link Overlay. Stop by the airport for an Intro flight, or just to check out the airplane.
This Seneca II is equipped with Precise Flight Speed Brakes, Merlyn Waste gates, a one piece windshield, all new de-icing boots in 2002, Lo-Presti speed mods for cowl and wing tips, Insight Gemini 1200 graphic engine monitors, air doors seals, and on-board oxygen.
