Class | Light |
Max. passengers | 8 |
Year of production | 1998 PRO |
Tail number | PT-XCF |
Airframe
TTSN: 3263.3 Hours / 3822 LandingsEngine
Engine 1: 3263 Hours / 3771 CyclesEngine 2: 3263 Hours / 3771 Cycles
Avionics
PRIMUS® 1000 SYSTEMPrimus® 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
Interior
Eight Passenger Executive ConfigurationForward 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
Exterior
Overall White with Blue, Green & Gold StripesEquipment
RNZ-850 Integrated Navigation UnitRCZ-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)
Notifications
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