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Cessna 421C Eagle |
US$ 507.407
€ 457.000 |
Обзор
| Список альбомов | | Тип: | многопропеллерний | | Производитель: | Cessna | | модель: | 421C Eagle | | год выпуска: | 1981 | | Свойства: | IFR сертификат
IFR установлено
Всегда в ангаре | | Jahresnachpr.: | 3/2024 | | местонахождение: | Германия, Augsburg, EDMA | | Общее время (TTAF): | 5250 h | | цена: | € 457.000
(~ US$ 507.407) | | ЕС облагаются налогом: | да | | Налога с оборота: | да (19%) | | Полные сведения |
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Подробности
| Список альбомов | | Тип: | многопропеллерний | | Производитель: | Cessna | | модель: | 421C Eagle | | год выпуска: | 1981 | | Свойства: | IFR сертификат
IFR установлено
Всегда в ангаре | | Jahresnachpr.: | 3/2024 | | местонахождение: | Германия, Augsburg, EDMA | | Общее время (TTAF): | 5250 h | | цена: | € 457.000
(~ US$ 507.407) | | ЕС облагаются налогом: | да | | Налога с оборота: | да (19%) | | Количество пассажиров: | 6 | | Посадки: | 6500 |
| Мотор (en) | | Количество моторов: | 2 | | Марка / Модель: | Continental | Continental | | Представление: | 375 PS | 375 PS | | общее время: | 1200 h | 480 h | | TБО (hours): | 1600 h | 1600 h | | Пропелер производитель / модель: | McCaulley | McCaulley | | Пропелер общее время: | 1321 h | 1321 h | | Пропелер время 1: | 2000 h | 2000 h |
| Авионика | NAV/COM1: Garmin GNS430W
NAV/COM2: Garmin GNS430W
Bluetooth/W-LAN: Flight Stream 210
Radar Altimeter: KRA10
DME: Bendix King KN62A
PFD/MFD LH: Garmin G600
MFD: Avidyne EX500
Weatherradar: Bendix RDR160
Transponder: Garmin GTX330 (mode S)
TCAS: GTS800
Audio Panel: GMA340
ELT: Artex ME406
Autopilot: S-TEC55x
Emergency COM: King KY196A
Instruments:
Garmin G600 LH.
2 x Airspeed indicator, 2 x Altimeters, 2 x Variometers, 2 x Horizons, HSI,
Prop synchronizer |
| оборудование | Club seating
VIP seating
Pressurized cabin
air conditioner
Retractable landing gear
high payload (approx. 1,000 kg)
Very spacious cabin
General characteristics
Crew: One or two
Capacity: Six passengers
Length: 11,090 m
Wingspan: 12,535 m
Altitude: 3,489 m
Curb weight: 2,042 kg
Maximum takeoff weight: 7,450 lb (3,379 kg)
Performance
Maximum speed: 256 kn (295 mph, 474 km/h) at 20,000 ft (6,100 m)
Cruising speed: 240 kn (280 mph, 440 km/h) at 25,000 ft (7,600 m) (75% power)
Range: 1,487 nautical miles (1,711 miles, 2,754 km) at 25,000 feet (7,600 m), Econ cruise speed
Service altitude: 30,200 feet (9,200 m)
Climb speed: 1,940 ft/min (9.9 m/s)
Launch distance to 50 feet (15 m): 2,323 feet (708 m)
Landing distance from 50 feet (15 m): 2,293 feet (699 m)
Story
The prototype of the Cessna 421, designed as a low-wing aircraft, completed its first flight in October 1965, and deliveries began in May 1967. The aircraft received two Continental GTSIO-520-D piston engines.
The improved version 421A has existed since 1969. In 1970, production of the 421B began with a larger wingspan and higher performance. The 421C from 1975 received new wings with modified tanks. Since 1980, the 421C has been delivered with a revised chassis.
In 1985, Cessna stopped producing propeller aircraft including the 421 |
| внешний вид | Retractable landing gear
high payload (approx. 1,000 kg)
Very spacious cabin
General characteristics
Crew: One or two
Capacity: Six passengers
Length: 11,090 m
Wingspan: 12,535 m
Story
The prototype of the Cessna 421, designed as a low-wing aircraft, completed its first flight in October 1965, and deliveries began in May 1967. The aircraft received two Continental GTSIO-520-D piston engines.
The improved version 421A has existed since 1969. In 1970, production of the 421B began with a larger wingspan and higher performance. The 421C from 1975 received new wings with modified tanks. Since 1980, the 421C has been delivered with a revised chassis.
In 1985, Cessna stopped producing propeller aircraft including the 421
Main information:
Location Germany
Year of construction: 1981
TTAF: 5258
C421c, well equipped, no damage history, A-SID performed. Actually in German CAMO
Model engine 1:
Teledyne Continental GTSIO-520-N
TSO: 1201/399 hours remaining
Year of overhaul 2011
Model engine 2:
Teledyne Continental GTSIO-520-N
TSO:467h/remaining 1133h
Year of overhaul 2016
Model propeller 1:
Year of overhaul 2018
Propeller 2 model:
Year of overhaul 2018 |
| интерьер | Club seating
VIP seating
Pressurized cabin
air conditioner
Retractable landing gear
high payload (approx. 1,000 kg)
Very spacious cabin |
Фотографии
Контакт с продавцом
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