NOTES:
No damage history
Fireblocking
Original Airworthiness Certificate Issued 08/04/2000


WEIGHTS (Lbs):
MAX RAMP: 20,400MAX TAKEOFF: 20,200MAX LANDING: 18,700
MAX ZERO FUEL: 15,100EMPTY WEIGHT: 12,129
(GROSS WEIGHT INCREASE: SB560XL-32-28 accomplished)


Airframe:
TOTAL TIME: (Times as o 08/24/2008)
TTAF:2723.3
LANDINGS: 2697

Engine Specs:
ENGINES: Pratt & Whitney Canada PW545A LeftRight
SNEW:2723 2723Cycles:26972697
Serial Number:PCE-DB0209PCE-DB0206

Modifications/Conversions:
CAPABILITIES:
RVSM: Yes
GROSS WEIGHT INCREASE: SB560XL-32-28

Avionics/Radios:
AVIONICS: (Integrated Primus II Package ¡V Honeywell ¡V 3 tube EFIS)
Provides a dual Primus II SRZ-850 Integrated Radio System. The Primus II System consists of dual Radio Management Units (RM-850), dual digital audio control panels (AV-850), dual navigation Units (RNZ-850), and dual communication units (RCZ-833). The RNZ-850 navigation system meets FM Immunity requirements and provides dual VOR, ILS, G/S, DME, and a single ADF. The RCZ-833 communication system provides dual Mode S Transponders and dual VHF Comm¡¦s capable of supporting 8.33 kHz and 25 kHz channel spacing.
VHF COMMUNICATION: (2) Honeywell TR-33 transceivers contained in RCZ-850 integrated communication unit (ICU)
VHF NAVIGATION: (2) Honeywell NV-850 systems contained in RNZ-850 integrated navigation unit (INU) include VOR, LOC, GS and marker beacon receivers
FLIGHT MANAGEMENT SYSTEM: (2) Universal UNS-1 CSP+ with Permanent Data Transfer Unit
FLIGHT DIRECTOR/AUTOPILOT /EFIS: Honeywell P-1000 Integrated Avionics System includes display and flight guidance functions. The system features dual Integrated Avionics Computers (IAC) which combines the Electronic Flight Instrument Display System (EFIS) with flight guidance functions of flight director and autopilot. The EFIS system is comprised of two 8¡¨x7¡¨ Primary Flight Displays (PFD) and (1) 8¡¨x7¡¨ Multifunction Display (MFD).
WEATHER RADAR: Honeywell Primus WU-880
TRANSPONDER: (2) Honeywell XS-852 Mode S
AUTOMATIC DIRECTION FINDER: Honeywell DF-850
DISTANCE MEASURING EQUIPMENT: (2) Honeywell DM-850
MARKER BEACON: (2) integrated in the Honeywell NV-850 navigation system
HIGH FREQUENCY RADIO: Honeywell KHF-950
RADIO ALTIMETER: Honeywell ALT-55 displayed on both PFD¡¦s
AIR DATA COMPUTER: (2) AZ-850
ALTITUDE HEADING REFERENCE SYSTEM: Dual digital LITEF LCR-93 AHRS
GLOBAL POSITIONING SYSTEM: (2) Integrated into Universal UNS-1CSP+
TERMINAL COLLISION AVOIDANCE SYSTEM: Honeywell TCAS 2000 TCAS-II
TERRAIN AWARENESS AND WARNING SYSTEM*: Universal TAWS A with bank limits and minimums
*[NOTE:Class B TAWS required for Part 91 ops in a/c with 6 seats by March 29, 2005] „Ï
COCKPIT VOICE RECORDER: Fairchild A200S
ELT*: ARTEX 110-4 ELT
*[NOTE: ELT is required 1/1/2004 of all nonscheduled N-registered jet aircraft] „Ï
OTHER AVIONICS:
COCKPIT SPEAKER MUTE: Audio Inhibit Switch (Optional Equipment)
STANDBY HSI: Meggit Mark 1 Model HIS 315B
FLIGHT DATA RECORDER: L3 Communications F1000 Solid State FDR records 17 parameters for 25 hours

Additional Equipment:
ADDITIONAL EQUIPMENT / OPTIONS:
CABIN DISPLAY: B&D Cabin Display on right bulkhead
PULSE LIGHT SYSTEM: Precise Flight
AIR LINK: Universal UL-601UniLink with uplink
OXYGEN SYSTEM: 76 cubic foot O2 bottle
AIR TELEPHONE: Magnastar C-2000 phone system with 2 handsets and data port
OTHER: EROS Crew Oxygen Masks
Remote Cabin Temperature Control
(2) 110-volt AC Outlets
Fax/Data Port
In-Direct Lighting
Right Side Externally Serviceable Toilet
Spare Center Aisle Carpet
43 Amp/Hr SAFT Nicad battery
Life Raft

Exterior:
EXTERIOR:
Overall Snow White with Commercial Green and Tovar (Gold) accent stripes.

Interior:
INTERIOR:
Interior condition is outstanding. The main cabin is arranged with 6 swivel pedestal passenger seats arranged with forward club configuration, two forward facing swivel pedestal seats at the rear of cabin and RH forward two-place side facing couch across from the main entry door, all with fireblocking. The rail tracks for the aft seats in the forward club area have been extended to permit full aft travel. Two full size executive tables in forward club section and individual stowable slimline tables at both aft forward facing seat. Aft divider accent and dropped aisle lighting. Pleated fabric window shades. LH forward refreshment center includes a heated liquid container, wine bottle storage, divided ice drawer, trash container, pull-out work surface and numerous storage drawers. RH fwd closet for coat or general storage. All woodwork is Figured Walnut. Leather seats are Cappuccino Townsend Leather Traditional Cow. Hardware plating is Satin Blush White Gold. Window reveals color is Champagne. The upper sidewall is Cappuccino Townsend Leather. The lower sidewall color is Rosemary and the carpet is Pine colored Cut Pile. Pilots¡¦ seats have sheepskin covers.

Inspection Status:
MAINTENANCE & INSPECTION:
Enrolled in CESCOM
Enrolled in ProParts
Most major maintenance accomplished by the Citation Service Centers at Wichita and Toledo

INSPECTIONLAST COMPLETEDNEXT DUE
Phase 1 (Every 300 hrs / 24 mo)2467 hrs / 06-08-20072767/ 06-30-2009
Phase 2 (Every 300 hrs / 24 mo)2855 hrs / 11-01-20072855 / 11-30-2009
Phase 3 (Every 300 hrs / 24 mo)2605 hrs / 01-08-082905 / 01-31-2010
Phase 4 (Every 300 hrs / 24 mo)2444 hrs / 05-02-20072744 / 05-31-2009
Phase 5 (Every 1200 hrs / 36 mo)2226 hrs / 05-23-20063426 / 05-31-2009
HOT SECTIONS (both engines)2518 hrs / 08-21-20075018