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Let 410UVP-E20 |
zł 10.029.279
US$ 2.550.000 |
Przegląd
| Informacje podstawowe | | Typ: | Samolot turbośmigłowy | | Producent: | Let | | Model: | 410UVP-E20 | | Rok produkcji: | 2005 | | Cechy charakterystyczne: | Certyfikat IFR
Wpisany do rejestru handlowego | | Lokalizacja: | Honduras | | Całkowity czas (TTAF): | 12027 h | | Cena: | US$ 2.550.000
(~ zł 10.029.279) | | Wszystkie szczególy |
| Sprzedawca |
Greece Aviation
Apostolos Chrysafidis
Marinou Antipa 40
57001 Thessaloniki
Grecja
Tel.: +30 6955193957 |
| Kontakt do Sprzedawcy |
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Szczególy
| Informacje podstawowe | | Typ: | Samolot turbośmigłowy | | Producent: | Let | | Model: | 410UVP-E20 | | Rok produkcji: | 2005 | | Cechy charakterystyczne: | Certyfikat IFR
Wpisany do rejestru handlowego | | Lokalizacja: | Honduras | | Całkowity czas (TTAF): | 12027 h | | Cena: | US$ 2.550.000
(~ zł 10.029.279) | | Lądowania: | 13813 |
| Silnik(i) | | Liczba silników: | 2 | | Producent/Model: | GEM601E | GEM601E | | Numer seryjny: | 901035 | 882046 | | Czas całkowity: | 6008 h | 7043 h | | SOH: | 1031 h | 1156 h | | Śmigło - Producent/Model: | V510/90A/C | V510/90A/C | | Śmigło - Czas całkowity: | 3759 h | 3484 h | | Śmigło - Czas 1: | 518 h SOH | 518 h SOH |
| Opis/Charakterystyka silnika | Last Flight Time Mar, 2012, well preserved. Aircraft beginning major airframe, propeller and engine maintenance to return to service, delivered in perfect airworthiness, with good time remaining on the main components.
Estimated delivery time 105 days.
Year Of Manufacture 1990, Rebuilt at the factory in 2005
Excelent history, No Damage History. |
| Awionika | AVIONICS & RADIOS
1 Magnetic compass LUN 1221.1-8 1
2 Dimmer Lights of Instrument Gyro RL-10 3
3 Turn and Sleep Indicator LUN 1215.03 2
4 Airspeed Indicator 8025 2
5 Gyro Horizon Indicator LUN 1205.31-8 2
6 Altimeter Indicator 5934P-3 2
7 Triple Indicator (Oil, Pressure, oil
Temp, Fuel Pressure) LUN 1538-8 2
8 Dual Hydraulic Pressure Indicator UI 2-240 K 1
9 Torque Indicator LUN 1539.02-8 2
10 Inter turbine indicator ( ITT) LUN 1370.02-8 2
11 Gas Turbine Indicator NG LUN 1347.03-8 2
12 Propeller Indicator NP LUN 1348.01 2
13 Fuel Quantity Indicator LUN 1674.8 4
14 Vertical Speed Indicator 7000 2
15 Clock ACHS-1M 1
16 Load Meter Indicator RH /VA LUN 2743.01-8 1
17 Load Meter Indicator LH /VA LUN 2743.01-8 1
18 AC Volt Meter VF.0.4-150 1
19 DC Volt Meter VF.0.4-45 1
20 Emergency Statistic Lock N/A 2
21 Break Pressure Indicator LUN 1446.02-8 1
22 Parking Brake Indicator MA 100 1
23 Pneumatic Deicer Indicator N/A 1
24 Landing Gear Indicator LUN 1694.8 1
25 Rudder Indicator LUN 1687-8 N/A
26 Emergency Hydraulic Control
Panel LUN 6577-8 -
27 Cockpit Voice Recorder N/A N/A
28 Flight Data Recorder S800-2000-00 1
29 EGPWS KGP-860 N/A
30 Standby Gyro Horizon AZRGK-2 1
31 Air Temperature Indicator LUN 5810.01-8 1
32 Navigation Glide Slope Indicator
L/H 066-3056-112 Navigation Glide Slope Indicator R/H 066-3056-01
33 Directional Gyro Indicator LRG-331 Same as #38
34 AD & RMI Indicator ARK-15M & IKU-IA 2
35 Radio Altimeter A-037 N/A
36 Fire Extinguisher MA16K 2
37 AC/DC Voltmeter Selector Valve LUN 7375.01-8 1
38 Combine Indicator URG-4 UK 2
39 Correcting Mechanism KM-8 1 |
| Wnętrze | | 18 seats in good condition |
| Modifications/Conversions | | Converted TC9401-05 |
| Inne uwagi | | While the information presented in this document is given in good faith based upon the most current information available, changes or modifications with respect to the subject aircraft, the associated records and/or lease documentation may be made at any time. No express or implied warranty or representation is made and this document may not be regard as establishing any obligation on the part of Seller or any of its affiliates. It is expected that interested parties will conduct an independent physical inspection of the aircraft and associated record and/or any lease documentation. |
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