1987 PIPER CHEYENNE 400LS

Technische Daten

Zelle

Motor & Propeller

Gewichte & Kraftstoff

Beschreibung

Impressive turbo-prop performance. Certified to 41,000 ft. in pressurized comfort. More than 5 hours endurance with near 350 kt cruise speed. One owner airplane, same pilot since 1993. Originally a factory demonstrator.

Avionik & Ausstattung

Avidyne EX-500 MFD
Garmin GNS-530AW (16 watt transmitter) Nav/Com/GPS
L-3 (Goodrich) WX-1000 Stormscope interfaced w/ EX-500 MFD & 530W
Heads Up XM WX Weather Datalink interfaced w/ EX-500 MFD
Garmin GAD-42 Interface Adapter
Sandel SN 4500 Primary Navigation Display
Collins APC-65 Autopilot
Kulite oil pressure/temperature gauges/pressure transducers
Flight Stream - talk to Nav from iPad.(send flight plan from ipad to airplane)
to allow connection to an EFB

Spares and tools included with sale:
Honeywell OEM Audio Panel (Serviceable and working when removed/replaced) (2)
Incandescent digital display capsules for Collins Proline Nav/com Radio (3)
Garrett/Honeywell Integrated Engine Control (IEC) Service Analyzer and Diagnostic Tool (1)
OEM Engine Oil Pressure/Temperature Indicator (2)
OEM Engine Oil Pressure Transducer (1)
Nosewheel Rim and Tire (Serviceable when removed) (1)
400LS Tail Jack Pad Appliance (1)
M-T Propeller Service and Removal Tool (2)

Zelle

Aircraft has been professionally flown since new.
* Piper states it determines year by date of airworthiness certificate. 3/12/1987. Prior was experimental category with1983 Special airworthiness certificate

I/R/W Piper Progressive Inspection Program. Event 1 completed 10/2023. Next due in 98 hrs. or 3/2026. Event 2 completed 3/2025. Next due in 198 hrs.