Descrição
Aircraft is enrolled on an engine monitoring program that extends the TBO to 5,500 hours
APU is currently undergoing the 4,000 Cycle Rotor Overhaul
Many desirable options that include:
- WIFI (GoGo AVANCE L5)
- WAAS
- ADS-B Out
- Garmin GMX-200 MFD w/ XM Weather
- Garmin GDL-69
- RAAS (Runway Awareness & Advisory System)Especificações
Ano2005
FabricanteCESSNA
ModeloCITATION XLS
Número de Série560-5581
Cadastro #N577PS
CondiçãoUsado
Com base emGMU
Tempo total4,770
Total de desembarques3,876
Alcance1,989 Nm
Peso máximo da rampa9,253.28 kilos
Peso máximo de decolagem9,162.57 kilos
Peso Máximo de Aterrissagem8,482.18 kilos
Peso Zero Máximo Combustível6,849.24 kilos
Peso Vazio Básico5,701.91 kilos
Rastreamento de manutençãoCamp
Engine 1 Maintenance ProgramNão Possui
Engine 1 Make/ModelPRATT & WHITNEY PW545B
Número de série do motor 1PCE-DD0171
Engine 1 Time4,770 SNEW
Motor 1 TBO5500
Engine 1 Cycles Since Overhaul3,879
Motor 1 NotasEnrolled on Trend Monitoring Program which extends TBO to 5500
Engine 2 Make/ModelPRATT & WHITNEY PW545B
Número de série do motor 2PCE-DD0170
Engine 2 Time4,770 SNEW
Motor 2 TBO5500
Engine 2 Cycles Since Overhaul3,879
Motor 2 NotasEnrolled on Trend Monitoring Program which extends TBO to 5500
APUSim
Tempo APU2,135
Programa de Manutenção de APUNão Possui
Notas APUAPU is currently undergoing the 4,000 Cycle Rotor Overhaul
Flight Deck Manufacturer/ModelHONEYWELL
Equipado com ADS-BSim
WAASSim
Aviônicos/RádiosAvionics: 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
Wi-fiSim
Equipamento adicionalWIFI (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)
ano pintado2015
ExteriorOverall Jet Glo Express Matterhorn White w/Metallic Columbia Blue, Steel Blue & Antique Silver Stripes (Repainted in 2015)
Ano Interior2018
Número de assentos9
Configuração da cozinhaForward
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
Status da InspeçãoOperated & 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
AeronavegávelSim
Ano2005|
FabricanteCESSNA|
ModeloCITATION XLS|
Número de Série560-5581|
Cadastro #N577PS|
CondiçãoUsado|
Com base emGMU|
Tempo total4,770|
Total de desembarques3,876|
Alcance1,989 Nm|
Peso máximo da rampa9,253.28 kilos|
Peso máximo de decolagem9,162.57 kilos|
Peso Máximo de Aterrissagem8,482.18 kilos|
Peso Zero Máximo Combustível6,849.24 kilos|
Peso Vazio Básico5,701.91 kilos|
Rastreamento de manutençãoCamp|
Engine 1 Maintenance ProgramNão Possui|
Engine 1 Make/ModelPRATT & WHITNEY PW545B |
Número de série do motor 1PCE-DD0171|
Engine 1 Time4,770 SNEW |
Motor 1 TBO5500|
Engine 1 Cycles Since Overhaul3,879|
Motor 1 NotasEnrolled on Trend Monitoring Program which extends TBO to 5500|
Engine 2 Make/ModelPRATT & WHITNEY PW545B |
Número de série do motor 2PCE-DD0170|
Engine 2 Time4,770 SNEW |
Motor 2 TBO5500|
Engine 2 Cycles Since Overhaul3,879|
Motor 2 NotasEnrolled on Trend Monitoring Program which extends TBO to 5500|
APUSim|
Tempo APU2,135|
Programa de Manutenção de APUNão Possui|
Notas APUAPU is currently undergoing the 4,000 Cycle Rotor Overhaul|
Flight Deck Manufacturer/ModelHONEYWELL|
Equipado com ADS-BSim|
WAASSim|
Aviônicos/RádiosAvionics: 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|
Wi-fiSim|
Equipamento adicionalWIFI (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)|
ano pintado2015|
ExteriorOverall Jet Glo Express Matterhorn White w/Metallic Columbia Blue, Steel Blue & Antique Silver Stripes (Repainted in 2015)|
Ano Interior2018|
Número de assentos9|
Configuração da cozinhaForward|
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|
Status da InspeçãoOperated & 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|
AeronavegávelSim|