Cessna 421C Eagle

US$ 417.554
€ 399.000

概觀

基礎資料
類型:	多螺旋槳飛機
品牌:	Cessna
型號 1:	421C Eagle
製造年:	1981
屬性:	IFR許可 IFR裝備停留在機庫
最後一年的:	3/2024
地點:	德國, Augsburg, EDMA
縂時間（TTAF）:	5250 h
價格:	€ 399.000 (~ US$ 417.554)
歐盟增值稅:	是的
增值稅規定:	是的 (19%)
所有的細節

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細節

基礎資料
類型:	多螺旋槳飛機
品牌:	Cessna
型號 1:	421C Eagle
製造年:	1981
屬性:	IFR許可 IFR裝備停留在機庫
最後一年的:	3/2024
地點:	德國, Augsburg, EDMA
縂時間（TTAF）:	5250 h
價格:	€ 399.000 (~ US$ 417.554)
歐盟增值稅:	是的
增值稅規定:	是的 (19%)
乘客數:	6
著陸:	4700

多個發動機
發動機數量:	2
製造商/型號:	Continental	Continental
功率:	375 PS	375 PS
時間總計:	1200 h	480 h
Time Between Overhaul ？？？大修間隔時間 (hours):	1600 h	1600 h
螺旋槳製造商/型號:	McCaulley	McCaulley
螺旋槳時間總計:	1321 h	1321 h
螺旋槳時間 1:	2000 h	2000 h

航空電子設備

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

裝備

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

外觀

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