This aircraft is undergoing evaluation and familiarization with the CEFS staff and is anticipated to be available for service beginning 1-Dec-2025

General Description:

• 6-Seat.
• Two 6-Cylinder, turbocharged 200 HP fuel injected engine(s), the Continental TSIO-360.
• Variable pitch 3-blade Hartzell propeller(s).
• 165 knot cruise @ 75% power @ 8,500 ft. Service ceiling 26,000 ft.
• Retractable wheels (complex).
• Day/Night VFR/IFR certified.
• A roomy aircraft for complex multi-engine training or instrument certification.
• Good condition 7/10 interior, 7/10 exterior.

Accessories:

• Rosen visors.
• Wired for conventional 2-plug headsets, all seats.

Avionics:

• Fully ADS-B in/out compliant utilizing a Garmin GDL-88 UAT and Garmin GNS-430 GPS. No Bluetooth(R) data link for customer accessories such as Foreflight(TM) or Garmin Pilot (TM).
• PS Engineering 7000B Audio Panel.
• Garmin GNS-430W GPS (3.3"W x 1.8"H screen), subscribed all US (east, central, west)  as NAV1/COM1 coupled to a Bendix-King KCS-55 HSI (VOR/LOC/GS #1).
• Bendix-King KX-155A (NAV/COM 2) coupled to a Bendix-King KI-209 CDI (VOR/LOC/GS #2).
• Bendix-King KT-76 Transponder.
• Narco DME 890

Engine Instruments:

• JPI-EDM-790 Engine(s) monitor.

Specifications:

• 100LL fuel, 92 gal total, 88 useable.
• ~26 gallons/hr fuel burn at 75% power.
• Max Gross Take-off Weight: 4570 lbf.
• Max empty fuel weight: 4000 lbf.
• Serial number: 34-7570221.

CEFS Pilot Qualifications:

• To receive instruction in N1142X there are additional Insurance Requirements not typical to the other aircraft in the CEFS fleet.

• For solo rental the Renter must have as a minumum:
  • An Instrument rating.
  • 500+ total PIC hours in all aircraft.
  • 100+ PIC hours in retractable gear aircraft.
  • Have not less than 100 hours instructed time specifically in the Piper Seneca II.

Advantages:

• Fast. A powerful and sleek airplane.
• Multi-engine, complex airplane.
• Retractable landing gear.
• Variable pitch prop(s).
• GNS-430 GPS with ADS-B In/out Installed.
• Six seat, club seating. The useful load before any usable fuel is added is 1605 lbf per the weight and balance cert.
• The Seneca II has left rear cargo/passenger doors for easier passenger entry/exit.

Disadvantages:

• No air conditioning.
• No de-ice boots, propeller heating or pilot window heat plate
• No O2 system on board.
• The autopilot is an early version of the Altimatic IIIc. This unit however, does feature altitude hold.

To be Determined:

• Determine if the GTX-330 has Bluetooth connectivity.

Fuel State:

• This aircraft is routinely fueled/refueled to ~60 gal at or before the beginning of the operational day though this is not guaranteed. The Pilot In Command is fully and solely responsible for determining the pre-flight fuel state and weight/balance limits.