N900LH - 1994 DORNIER 328 120

1994

DORNIER

328-120

3014

Used

N900LH

Equipped with Honeywell Primus 2000 Integrated Avionics Suite

16343.6

Total Airframe Hours Since New: 16,343.6 Total Airframe Cycles Since New: 19,222 Empty Weight: 21,252 lbs

Pratt & Whitney PW-119C Left Engine: S/N 116026 TSN: 15,864 CSN: 20,178 TSO: 5,947.7 CSO: 6,813 TSHSI: 5,947.7 CSHSI: 6,813 Right Engine: S/N 116040 TSN: 16,682.9 CSN: 20,503 TSO: 5,439.7 CSO: 5,814 TSHSI: 5,439.7 CSHSI: 5,814

Left Prop: S/N HL-118 TSN: 9,740.2 CSN: 9,495 TSO: 3,772.7 CSO: 4,552 Right Prop: S/N HL-25 TSN: 10,751 CSN: N/A TSO: 556.3 CSO: N/A

Equipped with Honeywell Primus 2000 Integrated Avionics Suite which includes the following: Flight Director: Built into the Integrated Avionics Computer (IAC) Auto-Pilot: Built into the Integrated Avionics Computer (IAC) COMMS: Dual Honeywell Units NAVS: Dual Honeywell Units ADF: Integrated into the Honeywell NAV Units DME: Integrated into the Honeywell NAV Units XPONDER: Mode "S" diversity transponder RADAR: Primus 650 Weather Radar TCAS: Honeywell RT-910 TCAS EGPWS: Honeywell Mark VI EGPWS RMI: Built into the Multi-Function Displays (MFD) HSI: Built into the Multi-Function Displays (MFD) ALTIMETER: Built into the Multi-Function Displays (MFD) RAD ALT: Dual Honeywell RT-300 CVR/FDR: Honeywell CVR & FDR Features: 5 Tube DU-870 EFIS Displays Dual 855B Radio Management Units (RMU) Dual Honeywell DA-800 Data Acquisition Units Dual Honeywell IC-800 Integrated Avionics Computer (IAC) Single AHZ-800 Attitude Heading Reference System (AHRS) with Single Inertial Reference System (IRS) Dual ADZ-840 Air Data Computers AI-330K Standby Horizon AV-850A Audio Control Panel JETPACK Emergency Power Supply PS-838C 115 Cubic Foot Oxygen Bottle Curtain for Passenger Door Cockpit Observer Seat Propeller Reverse Standby Compass

2008

Fresh Paint in 2008

2008

12

New 12 Passenger Corporate Interior in 2008