TTSN: 3263.3 Hours / 3822 Landings

JT15D-5D

Engine 1: 3263 Hours / 3771 Cycles
Engine 2: 3263 Hours / 3771 Cycles

PRIMUS® 1000 SYSTEM
Primus® 650 Weather Radar
Primus® II Radio System
EFIS consists of the following elements:
• IC-600 Integrated Avionics Computer (IAC) Included within each IAC are the following:
• Flight Director Computer
• Autopilot Computer (No. 1 only)
• Symbol Generator
• Sensor Interfaces
• DU-870 Display Units (DUs),PFDs, and MFD
• BL-870 PFD Bezel Controllers (2)
• BL-871 MFD Bezel Controller
• DC-550 Display Controllers (2)
• RI-553 Instrument Remote Controller
• MC-800 MFD Controller
COM 1, NAV 1, ADF 1, X-PDR1, are controlled by the left RMU
COM 2, NAV 2, ADF 2, X-PDR2 are controlled by the right RMU
Secondary Flight Display System (MEGGITT TUBE)
2 Altitude-Reporting Transponders
Flight Director System which incorporates the Autopilot
GNS-XL FMS with VPU/GPS
ELT
CVR

RNZ-850 Integrated Navigation Unit
RCZ-850 Integrated Communication Unit
DF-850 ADF Receiver Module, which is a Component of the RNZ-850
HONEYWELL PRIMUS® REMOTE RADIO SYSTEM— DME-850
CD-850 HONEYWELL PRIMUS® II RADIO SYSTEM—AUXILIARY COM 1/NAV 2 CDU
HONEYWELL PRIMUS® II REMOTE RADIO SYSTEM—AUDIO CONTROL UNIT
Single-Point Pressure Refueling
Tail Flood Lights
Indexer Lights AOA
KHF-950 HF
Universal EGPWS
Traffic Alert and Collision Avoidance System (TCAS I)
AirShow (INOP)

Eight Passenger Executive Configuration
Forward 4-Place Center Club Seating with Dual Executive Tables
Single Aft Facing Seat Opposite Entrance Door
Aft 2 Forward Facing Seats
Aft Lav with Belted Potty
Seats are Brown Rawhide Leather

Overall White with Blue, Green & Gold Stripes