Are you ready to step up to a practical and efficient jet? 777 Aircraft Sales presents a low-time Eclipse jet that’s practically new, with only 343 hours of flight time. This sleek and stylish jet burns just 59 GPH and can cruise at over 400 MPH, ready to take you anywhere within a 1,100 NM range on a single trip.
|
Registration |
N112EA | |
| Year of construction | 2007 | |
| Country | Denmark | |
| City/Aerodrome | RKE | |
| Price | US$ 1,450,000 Vat free | |
Key Features:
Flight Management Capabilities:
Engines and Maintenance:
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.
Airplane Time State
Avionics
Logbook
Manufacture Eclipse Aerospace Registration No: N112EA
Model EA500 Serial No: 0038
Total Hour TSN 314 Cycle Since New CSN 312
Workorder ref. N112EA-OCT20 Maintenance ref. EA500AMM rev 020
Engine(s)
Manufactor / Model P&W PW610F-A Manufactor / Model P&W PW610F-A
Position L/H – #1 Position R/H – #2
Serial No PCE-LA0069 Serial No PCE-LA0070
TSN/TSO 416 TSN/TSO 422
CSN/CSO (starts) 375 CSN/CSO (Starts) 379
I certify that the work specified except as otherwise specified
was carried out in accordance with FAA airworthiness
regulations, and in respect to that work the aircraft is
considered airworthy condition and hereby approved for
return to service
Name:
Hans E. Hemmingsen
Date:
04/DEC/2020
FAA A&P 2413867 IA
Signature:
Work Performed:
• 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.
Not Performed:
• Overhaul on Pilot and Co-Pilot mask due iaw. AMM 05-10. Condition checked ok.
• Passenger mask in cabin area due for overhaul iaw. AMM 05-10. Condition checked ok.
• Pitot/Static check iaw. FAR 91.411 not a requirement as aircraft does not flies in US.
• Transponder check iaw. FAR 91.413 not a requirement as aircraft does not flies in US.
LOGBOOK CERTIFICATE
FAA A&P 2413867 IA
Aircraft
Manufacture Eclipse Aerospace Registration No: N112EA
Model EA500 Serial No: 0038
Total Hour TSN 314 Cycle Since New CSN 312
Workorder ref. N112EA-OCT20 Maintenance ref. EA500AMM rev 020
Engine(s)
Manufactor / Model P&W PW610F-A Manufactor / Model P&W PW610F-A
Position L/H – #1 Position R/H – #2
Serial No PCE-LA0069 Serial No PCE-LA0070
TSN/TSO 416 TSN/TSO 422
CSN/CSO (starts) 375 CSN/CSO (Starts) 379
I certify that the work specified except as otherwise specified
was carried out in accordance with FAA airworthiness
regulations, and in respect to that work the aircraft is
considered airworthy condition and hereby approved for
return to service
Name:
Hans E. Hemmingsen
Date:
04/DEC/2020
FAA A&P 2413867 IA
Signature:
Maintenance Next Due
• Airframe 24mth/300hrs inspection next due DEC/2022 or 614hrs
• Airframe 48mth/1200hrs inspection next due MAR/2022 or 1.480hrs
• Engine 12mth/300hrs inspection next due DEC/2021 or 614hrs
• Engine 600hrs inspection next due 880hrs
Chapter 04 (Airworthiness Limitations) Next due:
Fuselage and associated structure – Wing structure – Empennage structure
• Recurring structural inspection due at 3.300 FH
• Life limit for structure due at 10.000 FH
Airframe Component Limitations
• Aircraft Start battery due for capacity check at 04/June/2020
• Aircraft System battery due for capacity check at 04/June/2020
• Starter Generator due for overhaul at 1.600 FH
• Engine Fire Extinguisher Canister due for overhaul at 30/April/2023
• Pitch Trim Actuator due for overhaul at 2.000 FH
• Rudder Force Spring Assy due for overhaul at 10.000 FH
• Main Landing Gear due for overhaul at 20.000 FH or 20.000 CYC
• Left/Right MLG Side Stay Assy due for overhaul at 7.500 Landings
• Nose Landing Gear due for overhaul at 20.000 FH or 20.000 CYC
• Landing Gear Actuators due for overhaul at 2.000 Landings
• Oxygen Cylinder (40 cu ft.) due for overhaul at April/2023
• Oxygen Cylinder (40 cu ft.) Life limit at October/2020
• Left/Right Windshield recurring inspection at 900 FH
• Left/Right Windshield life limit at 2.700 FH
• Left/Right Cockpit side window recurring inspection at 900 FH
• Engine mount isolator assy discard at 3.600 FH
Engine Components Limitations
• Engine components life limit next due at 10.500 CYC
• Engine HP Turbine life limit next due at 5.250 CYC
