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$4,200,000
Aircraft Location:Guilford, Connecticut
Seller Information
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General
Year
2005
Manufacturer
Model
Serial Number
560-5581
Registration #
N577PS
Condition
Used
Based at
GMU
Description
Available for immediate delivery
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)
Airframe
Total Time
4,770
Total Landings
3,876
Range
1,989 NM
Max Ramp Weight
20,400 lb
Max Takeoff Weight
20,200 lb
Max Landing Weight
18,700 lb
Max Zero Fuel Weight
15,100 lb
Basic Empty Weight
12,570.56 lb
Maintenance Tracking
CAMP
Engine Program
Engine Maintenance Program
None
Engine 1
Engine 1 Make/Model
PRATT & WHITNEY PW545B
Engine 1 Serial Number
PCE-DD0171
Engine 1 Time
4,770 SNEW
Engine 1 TBO
5500
Engine 1 Cycles
3,879
Engine 1 Notes
Enrolled on Trend Monitoring Program which extends TBO to 5500
Engine 2
Engine 2 Make/Model
PRATT & WHITNEY PW545B
Engine 2 Serial Number
PCE-DD0170
Engine 2 Time
4,770 SNEW
Engine 2 TBO
5500
Engine 2 Cycles
3,879
Engine 2 Notes
Enrolled on Trend Monitoring Program which extends TBO to 5500
Auxiliary Power Unit
APU
Yes
APU Time
2,135
APU Maintenance Program
None
APU Notes
APU is currently undergoing the 4,000 Cycle Rotor Overhaul
Avionics
Flight Deck Manufacturer/Model
HONEYWELL
ADS-B Equipped
Yes
WAAS
Yes
Avionics/Radios
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
Additional Equipment
Wifi
Yes
Additional Equipment
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)
Exterior
Year Painted
2015
Exterior Notes
Overall Jet Glo Express Matterhorn White w/Metallic Columbia Blue, Steel Blue & Antique Silver Stripes (Repainted in 2015)
Interior
Year Interior
2018
Number of Seats
9
Galley Configuration
Forward
Interior Notes
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
Inspection Status
Inspection Status
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
Airworthy
Yes
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