S/N 560-0450

Cessna Citation Ultra

Class	Light
Max. passengers	8
Year of production	1998 PRO
Tail number	PT-XCF

Airframe

TTSN: 3263.3 Hours / 3822 Landings

Engine

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

Avionics

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

Interior

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

Exterior

Overall White with Blue, Green & Gold Stripes

Equipment

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)