Chiama per sapere i costi
Posizione dell' Aereomobile:Guilford, Connecticut, Stati Uniti
Informazioni sul venditore
Visualizza le informazioni sul venditoreGenerale
Anno
2005
Produttore
Modello
Numero di serie
560-5581
Registrazione #
N577PS
Condizione
Usati
Fondata
GMU
Descrizione
** DEAL PENDING **
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)
Struttura velivolo
Tempo totale
4,770
Sbarchi totali
3,876
Autonomia
1,989 Nm
Peso massimo della rampa
9,253.28 kg
Peso massimo al decollo
9,162.57 kg
Peso massimo di atterraggio
8,482.18 kg
Peso massimo del carburante zero
6,849.24 kg
Peso vuoto di base
5,701.91 kg
Monitoraggio di mantenimento
Camp
Engine Program
Engine 1 Maintenance Program
Nessuna
Engine 1
Engine 1 Make/Model
PRATT & WHITNEY PW545B
Motore 1 - Numero di serie
PCE-DD0171
Engine 1 Time
4,770 SNEW
Motore 1 TBO
5500
Engine 1 Cycles Since Overhaul
3,879
Motore 1 Note
Enrolled on Trend Monitoring Program which extends TBO to 5500
Engine 2
Engine 2 Make/Model
PRATT & WHITNEY PW545B
Motore 2 - Numero di serie
PCE-DD0170
Engine 2 Time
4,770 SNEW
Motore 2 TBO
5500
Engine 2 Cycles Since Overhaul
3,879
Motore 2 Note
Enrolled on Trend Monitoring Program which extends TBO to 5500
Auxiliary Power Unit
APU
Si
Durata unità di potenza ausiliaria
2,135
Programma APU
Nessuna
Note APU
APU is currently undergoing the 4,000 Cycle Rotor Overhaul
Avionica
Flight Deck Manufacturer/Model
HONEYWELL
Sistema ADS-B
Si
WAAS
Si
Avionica/Radio
Avionics: 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
Attrezzatura Aggiuntiva
Wifi
Si
Attrezzature aggiuntive
WIFI (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)
Esteriore
Anno dipinto
2015
Esteriore
Overall Jet Glo Express Matterhorn White w/Metallic Columbia Blue, Steel Blue & Antique Silver Stripes (Repainted in 2015)
Interno
Anno Interno
2018
Numero di posti a sedere
9
Configurazione della cambusa
Forward
Interiore
The 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 Ispezione
Stato di ispezione
Operated & 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 aerea
Si

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