Cessna 421 Golden Eagle

We are pleased to offer to the market this stunning Cessna 421 with tip tanks and comfortable interior. 

The Cessna 421 was first produced in May 1967 and production continued until 1985. 

Maximum take-off weight 6,840 lb (3,103 kg)

Airframe

TTSN – 3878.7 hrs

Engines

Continental GTSIO – 540D with 375 HP 

Left – 1004.8 hrs

Right – 600 hrs

Propellers

McCauley 

TTSO 9.5 hrs

Avionics

KX 155 TSO radio and Nav

KMA 24 

Transponder Garmin GTX 327 

GPS Apollo 2001 NMS

Garmin GNS 530

Specifications

Crew: One or two
Capacity: Six passengers
Length: 36 ft 4+5⁄8 in (11.09 m)
Wingspan: 41 ft 1+1⁄2 in (12.53 m)
Height: 11 ft 5+3⁄8 in (3.49 m)
Wing area: 215 sq ft (20.0 m2)
Empty weight: 4,501 lb (2,042 kg)
Max takeoff weight: 7,450 lb (3,379 kg)
Fuel capacity:  262 US gal (218 imp gal; 990 L) with optional wing tanks
Powerplant: 2 × Continental GTSIO-520-D turbocharged, fuel injected and geared flat-six engines, 375 hp (280 kW) each
Propellers: 3-bladed McCauley constant-speed propellers

Performance : Maximum speed: 256 kn (295 mph, 474 km/h) at 20,000 ft (6,100 m)

Cruise speed: 240 kn (280 mph, 440 km/h) at 25,000 ft (7,600 m) (75% power)

Range: 1,487 nmi (1,711 mi, 2,754 km) at 25,000 ft (7,600 m), econ cruise speed
Service ceiling: 30,200 ft (9,200 m)
Rate of climb: 1,940 ft/min (9.9 m/s)
Takeoff distance to 50 ft (15m): 2,323 ft (708 m)
Landing distance from 50 ft (15 m): 2,293 ft (699 m)