2005 CESSNA CITATION XLS
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Standort des Flugzeugs:Guilford, Connecticut, USA
Verkäuferinformation
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Beschreibung
Spezifikation
Jahr2005
HerstellerCESSNA
ModellCITATION XLS
Seriennummer560-5581
Registration #N577PS
ZustandGebraucht
Based atGMU
Total Time4,770
Total Landings3,876
Range1,989 Nm
Max Ramp Weight9,253.28 kg
Max Takeoff Weight9,162.57 kg
Max Landing Weight8,482.18 kg
Max Zero Fuel Weight6,849.24 kg
Basic Empty Weight5,701.91 kg
Maintenance TrackingCamp
Engine 1 Maintenance ProgramKeine
Engine 1 Make/ModelPRATT & WHITNEY PW545B
Engine 1 Serial NumberPCE-DD0171
Engine 1 Time4,770 SNEW
Engine 1 TBO5500
Engine 1 Cycles Since Overhaul3,879
Engine 1 NotesEnrolled on Trend Monitoring Program which extends TBO to 5500
Engine 2 Make/ModelPRATT & WHITNEY PW545B
Engine 2 Serial NumberPCE-DD0170
Engine 2 Time4,770 SNEW
Engine 2 TBO5500
Engine 2 Cycles Since Overhaul3,879
Engine 2 NotesEnrolled on Trend Monitoring Program which extends TBO to 5500
APUJa
APU Time2,135
APU Maintenance ProgramKeine
APU NotesAPU is currently undergoing the 4,000 Cycle Rotor Overhaul
Flight Deck Manufacturer/ModelHONEYWELL
ADS-B EquippedJa
WAASJa
Avionics/RadiosAvionics: Honeywell Primus 1000 Suite
Flight Displays: Three Honeywell Primus 1000 Liquid Crystal Displays
Global Positioning System: Dual Universal UNS 1ESPW FMS w/ GPS
Communications: Dual Honeywell 850 Integrated Comms
Navigation: Dual Honeywell 850 Navs
Cockpit Voice Recorder: Fairchild FA2100 CVR (120 minute)
Flight Management System: Dual Universal UNS 1ESPW FMS w/ GPS
Attitude Heading Reference Unit: Honeywell LCR-93 AHRS
Distance Measuring Equipment: Dual Honeywell DM 850 DME
Autopilot System: Honeywell Primus 1000 IFCS
Transponders: Dual Honeywell XS 850 / Mode S Transponders w/ ADS-B Out and Enhanced Surveillance
Traffic Alert and Collision Avoidance System: Honeywell TPU-678 TCAS II
Weather Radar: Honeywell WU-880 Weather Radar
Terrain Awareness Warning System: Honeywell Mark V TAWS
Radio Altimeter: Honeywell ALT-55B Radio Altimeter
Emergency Locator Transmitter: Artex 406-N ELT w/ navigation interface
SATCOM: AirCell ST-3100 Iridium w/ dual cordless handsets
High Frequency Radio: Honeywell HF 1050 w/ SELCAL
WifiJa
Additional EquipmentWIFI (GoGo AVANCE L5)
WAAS
ADS-B Out
Garmin GMX-200 MFD w/ XM Weather
Garmin GDL-69 Datalink
HF Radio w/ SELCAL
2nd UNS 1ESPW FMS
Cockpit Speaker Mute Switch
RAAS (Runway Awareness & Advisory System)
Year Painted2015
ExteriorOverall Jet Glo Express Matterhorn White w/Metallic Columbia Blue, Steel Blue & Antique Silver Stripes (Repainted in 2015)
Year Interior2018
Number of Seats9
Galley ConfigurationForward
InteriorThe 9-passenger executive interior with new carpet in 2018 and wood veneers refinished in 2015 and is configured as follows:
Entryway: Two-place side-facing divan
Cabin: Mid-cabin double club and two forward-facing seats in the aft cabin portion of the aircraft
Aft Lavatory: Lavatory with externally serviceable flushing toilet and aft closet storage
Left Hand Forward Refreshment Center: Insulated ice drawer, trash compartment, and storage
Inspection StatusOperated & Maintained per FAR §135
Date of Manufacture: 2005
Certification Date: September 24, 2005
Maintenance tracked by CAMP
Engines Enrolled on Trend Monitoring
Inspection Doc. Description Last Completed Next Due Date (Date/Hours)
Document 1 (12 M) Nose, Cockpit, Fuselage May 23, 2025 April 30, 2026
Document 3 (24 M) Cabin, Lavatory, Windshields, Windows May 23, 2025 April 30, 2027
Document 6 (48 M) Complete Inspection May 19, 2023 April 30, 2027
Document 8 (2400 Hrs) Complete Inspection 3,955.9 6,355.9
Document 11 (48 M) Flight Control Inspection April 28, 2025 April 30, 2027
Document 13 (72 M) CVR, Hydraulic, Cockpit, Empennage April 21, 2021 April 30, 2027
Document 16 (96 M) Nose, Cabin, Cockpit, Horizontal, Vertical May 19, 2023 May 31, 2031
Document 17 (6000 Hrs) Vertical Stabilizer Pivot Fitting n/a 6,000.0
Engine 1 & 2 Inspection 4,732.4 / 4,732.4 5,532.4 / 5,532.4
Engine 1 & 2 Overhaul Inspection n/a 5,500.0
AirworthyJa