2007 ECLIPSE 500
Aircraft Summary
General
Year
2007
Manufacturer
ECLIPSE
Model
500
Serial Number
343
Condition
Used
Based at
Denmark RKE
Description
777 Aircraft Sales can assist an interested buyer in relocation of the airplane as well as registration in their country, making it easy to buy internationally.
Contact us for more details, to schedule a viewing, or to submit an offer.
AIRCRAFT KEY FEATURES:
• Advanced Avionics: Equipped with top-quality avionics, this jet ensures maximum pilot awareness and minimizes workload.
• Avio IFMS: Includes an Integrated Flight Management System, Class 3 E-Charts, and XM Satellite Weather.
• IS&S Displays: Thirteen microprocessors control all major aircraft systems, with flight data presented on a high-resolution 15” LCD multifunction display.
• Intuitive Interface: Simplified data entry with integrated bezel pushbuttons, encoders, and an externally mounted keyboard.
CAPABILITIES:
• Coupled WAAS/LPV Approaches
• Performance-Based Top of Descent
• RNP 0.1 nm Precision
• Coupled Enroute GPS Navigation
• Coupled Missed Approach and Procedure Turn
• Coupled Holding Patterns
• Automated Airway Entry
• Coupled Offsets
• Storage of up to 99 Flight Plans
Airframe
Total Time
314
Total Landings
312
Range
1,100 NM
Engine Program
Engine Maintenance Program
ESP Gold
Engine Program Notes
Fully Paid
Engine 1
Engine 1 Manufacturer
PRATT & WHITNEY
Engine 1 Model
PW610F
Engine 1 Serial Number
LA0069
Engine 1 Time
416
Engine 1 Time Since
SNEW
Engine 1 Cycles
375
Engine 2
Engine 2 Serial Number
LA0070
Engine 2 Time
416
Engine 2 Time Since
SNEW
Engine 2 Cycles
375
Avionics
WAAS
Yes
LPV
Yes
Avionics/Radios
Avio NG Integrated Avionics Suite
Dual AoA Indicators
Dual Air Data Computers
Dual Magnetometers
Dual GPS Receivers
Integrated Autopilot
IFMS
Inspection Status
Inspection Status
Annual: Due September 2024
ARC: Due September 2024
300hrs/24 months airframe inspection iaw. AMM 05-20-081-801
Engine(s) LH and RH 12 months inspection iaw. LMM 3070895 chapter 05-20
DSU and FADEC Fault interrogation performed by Eclipse, no faults.
System battery capacity iaw. AMM 24-32-24-071-801
Start battery capacity iaw. AMM 24-32-24-071-801
FWD Fuselage skin insp (RVSM) iaw. AMM 53-10-10-021-801
ELT inspection iaw. FAR91.207 and AMM 25-60-00-071-801 (ELT bat exp. 04/2023)
Portable fire extinguisher check iaw. AMM 25-60-00-021-801
Condition of passenger oxygen mask performed. OH not performed, owner request
Condition of pilot/Co-pilot oxygen mask performed. OH not performed, owner request
SB500-52-010 Door Lock Pin O-Ring.
Transponder system #1 and #2 checked iaw. EASA 2011-15R2
AD(s) checked true Bi-Weekly 2020-24
Findings / Rectification:
System battery failed cap test. Start battery moved to system battery position, and new start battery with improved capacity installed iaw. RAS IM E50-IN-2418-050. Special ICA applies from RAS. E50-ICA-2418-050.
System battery P/N F0773-3005 S/N: 132840031, Start battery P/N: 24-1100-2000-1 S/N: 92-096
L/H Main gear shock absorber leaking. All O-rings renewed and hydraulic/Nitrogen re-fill iaw.
AMM 32-10-13 / 12-10-06-061-801.
All life vest replaced with P/N HS3701-SWA as due for overhaul. Next Overhaul 30/06-2030
Oxygen refilled iaw. AMM 12-10-05-061-801.
DSU no valid readout. Recovery performed by Eclipse and re-installed iaw. AMM
All De-Ice boots treated with Ice-X.
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