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Piper PA-31T-620 Cheyenne II Blackhawk |
zł 5.661.170 CHF 1.200.000 |
Przegląd
| Informacje podstawowe | | Typ: | Samolot jednośmigłowy | | Producent: | Piper | | Model: | PA-31T-620 Cheyenne II Blackhawk | | Rok produkcji: | 1981 | | Nr. rejestracyjny: | HB-LUF | | Numer seryjny: | 31T-8120015 | | Lokalizacja: | Szwajcaria, Bern | | Całkowity czas (TTAF): | 9 h | | Cena: | CHF 1.200.000 (~ zł 5.661.170) | | Wszystkie szczególy |
| Sprzedawca |
Aeromeccanica S.A Aeroporto Cantonale di Locarno 6596 Gordola Szwajcaria
Tel.: +41-91-2103128 Fax: +41-91-7450037 |
| Kontakt do Sprzedawcy |
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Szczególy
| Informacje podstawowe | | Typ: | Samolot jednośmigłowy | | Producent: | Piper | | Model: | PA-31T-620 Cheyenne II Blackhawk | | Rok produkcji: | 1981 | | Nr. rejestracyjny: | HB-LUF | | Numer seryjny: | 31T-8120015 | | Lokalizacja: | Szwajcaria, Bern | | Całkowity czas (TTAF): | 9 h | | Cena: | CHF 1.200.000 (~ zł 5.661.170) |
| Awionika | | ADS-B, WAAS and LPV equipped. Dual Garmin GTN750 with WAAS; Garmin GTX 330 D transponder; Garmin GMA 347 Audio/MKR; Garmin GWX 68 weather radar; King KN 63 DME; King KDI 572 DME; King KR 87 ADF; King KA 44B antenna; King KI 229 RMI; King KAS 297A ALT/Preselect; Sandel SN4500 EHSI; King KPI 552 HSI R/H; Avidyne TAS 620 TCAD and antenna; L3 WX 500 Stormscope; L3 NY 163 antenna; Sandia SAE5-35 B encoder filter; ATR 833 COM3; Garmin GAD 42 interface; radar altimeter; Kannad ELT 406AF. Copilot panel: airspeed indicator, attitude indicator, vertical speed indicator, altimeter, turn coordinator, HSI. |
| Zewnętrze | | In good condition. 2007 paint; white with blue and gold stripes. |
| Wnętrze | | In good condition. 2007 interior; 1 pilot and 7 passengers; grey leather, grey carpet, toilet, rear cabinets, courtesy tables. |
| Inne uwagi | Very clean, privately onwed and hangared Piper Cheyenne II with recent Blackhawk Conversion and 5 Bladed Composite Propellers
Blackhawk Conversion 620 HP Pratt & Whitney PT6A-135A (FAA STC SA00863SE; EASA STC 10031462); MT-Propeller five-composite-blade propellers (EASA STC 10038174 R2; FAA STC SA03249NY), described by Controller as vibration-damping, nickel-leading-edge, 5% take-off/climb and 3 kt cruise improvement at 1,900 rpm, unrestricted ground operation in low idle, unlimited blade life/FOD-repairable, increased ground clearance, reduced cabin noise/vibration, and compliant with the stated German noise regulations; wet-splines starter generators; Whelen LED wing-tip-tank recognition lights (EASA STC IM.21O.10045878); LED strobe/position, taxi and landing lights; cargo net; engine inlet plugs; engine exhaust covers; rear cabinet; toilet seat; first-aid kit. Pressurized; inadvertent ice protection; Includes Floats: Yes.
Specifications subject to verification by purchaser |
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