Descrizione
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)Specifiche
Anno2005
ProduttoreCESSNA
ModelloCITATION XLS
Numero di serie560-5581
Registrazione #N577PS
CondizioneUsati
FondataGMU
Tempo totale4,770
Sbarchi totali3,876
Autonomia1,989 Nm
Peso massimo della rampa9,253.28 kg
Peso massimo al decollo9,162.57 kg
Peso massimo di atterraggio8,482.18 kg
Peso massimo del carburante zero6,849.24 kg
Peso vuoto di base5,701.91 kg
Monitoraggio di mantenimentoCamp
Engine 1 Maintenance ProgramNessuna
Engine 1 Make/ModelPRATT & WHITNEY PW545B
Motore 1 - Numero di seriePCE-DD0171
Engine 1 Time4,770 SNEW
Motore 1 TBO5500
Engine 1 Cycles Since Overhaul3,879
Motore 1 NoteEnrolled on Trend Monitoring Program which extends TBO to 5500
Engine 2 Make/ModelPRATT & WHITNEY PW545B
Motore 2 - Numero di seriePCE-DD0170
Engine 2 Time4,770 SNEW
Motore 2 TBO5500
Engine 2 Cycles Since Overhaul3,879
Motore 2 NoteEnrolled on Trend Monitoring Program which extends TBO to 5500
APUSi
Durata unità di potenza ausiliaria2,135
Programma APUNessuna
Note APUAPU is currently undergoing the 4,000 Cycle Rotor Overhaul
Flight Deck Manufacturer/ModelHONEYWELL
Sistema ADS-BSi
WAASSi
Avionica/RadioAvionics: 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
WifiSi
Attrezzature aggiuntiveWIFI (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)
Anno dipinto2015
EsterioreOverall Jet Glo Express Matterhorn White w/Metallic Columbia Blue, Steel Blue & Antique Silver Stripes (Repainted in 2015)
Anno Interno2018
Numero di posti a sedere9
Configurazione della cambusaForward
InterioreThe 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
Stato di ispezioneOperated & 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
Idoneo alla navigazione aereaSi
Anno2005|
ProduttoreCESSNA|
ModelloCITATION XLS|
Numero di serie560-5581|
Registrazione #N577PS|
CondizioneUsati|
FondataGMU|
Tempo totale4,770|
Sbarchi totali3,876|
Autonomia1,989 Nm|
Peso massimo della rampa9,253.28 kg|
Peso massimo al decollo9,162.57 kg|
Peso massimo di atterraggio8,482.18 kg|
Peso massimo del carburante zero6,849.24 kg|
Peso vuoto di base5,701.91 kg|
Monitoraggio di mantenimentoCamp|
Engine 1 Maintenance ProgramNessuna|
Engine 1 Make/ModelPRATT & WHITNEY PW545B |
Motore 1 - Numero di seriePCE-DD0171|
Engine 1 Time4,770 SNEW |
Motore 1 TBO5500|
Engine 1 Cycles Since Overhaul3,879|
Motore 1 NoteEnrolled on Trend Monitoring Program which extends TBO to 5500|
Engine 2 Make/ModelPRATT & WHITNEY PW545B |
Motore 2 - Numero di seriePCE-DD0170|
Engine 2 Time4,770 SNEW |
Motore 2 TBO5500|
Engine 2 Cycles Since Overhaul3,879|
Motore 2 NoteEnrolled on Trend Monitoring Program which extends TBO to 5500|
APUSi|
Durata unità di potenza ausiliaria2,135|
Programma APUNessuna|
Note APUAPU is currently undergoing the 4,000 Cycle Rotor Overhaul|
Flight Deck Manufacturer/ModelHONEYWELL|
Sistema ADS-BSi|
WAASSi|
Avionica/RadioAvionics: 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|
WifiSi|
Attrezzature aggiuntiveWIFI (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)|
Anno dipinto2015|
EsterioreOverall Jet Glo Express Matterhorn White w/Metallic Columbia Blue, Steel Blue & Antique Silver Stripes (Repainted in 2015)|
Anno Interno2018|
Numero di posti a sedere9|
Configurazione della cambusaForward|
InterioreThe 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|
Stato di ispezioneOperated & 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|
Idoneo alla navigazione aereaSi|