1982 Cessna 414A

The Cessna 414 is an American light, pressurized, twin-engine transport aircraft built by Cessna.
 
AIRFRAME
TOTAL TIME 5135.8 HRS.
PROP 1 LH HARTZEL 192.0 HRS. SOVH
PROP 2 RH HARTZEL 192.0 HRS. SOVH
 
AVIONICS
COMMUNICATIONS EQUIPMENT
GPS/NAV/COM 1 GARMIN GNS 530W
 NAV/COM 2 BENDIX KING KX 155A
TRANSPONDER 1 GARMIN GTX 345 ADS-B
TRANSPONDER 2 GARMIN GTX 327
 DME BENDIX KING DME KN62
RADAR SCREEN MFD EX 500
 AUTOPILOT ARC 800B
 ELT 406 ARTEX

ADDITIONAL EQUIPMENT
RAM WINGLETS KIT
POWER PAC SPOILERS (SPEED BRAKES)
 DUAL STRAKE KIT
RAM BORTEX GENERATOR KIT

SPECIFICATIONS
 CREW: ONE OR TWO
 CAPACITY: 2-8 PASSENGERS
 LENGTH: 36 FT 4.5 IN (11.087 M)
WINGSPAN: 44 FT 1.5 IN (13.449 M)
HEIGHT: 11 FT 5.5 IN (3.493 M)
WING AREA: 225.80 SQ FT (20.978 M2)
EMPTY WEIGHT: 4,365 LB (1,980 KG)
GROSS WEIGHT: 6,750 LB (3,062 KG)
POWERPLANT: 2 × CONTINENTAL TSIO-520-NB FLAT
SIX TURBOCHARGED PISTON, 310 HP (230 KW) EAC

This aircraft is offered in "AS IS" condition. All information contained here in was derived from sources believed correct, but is not guaranteed. Buyers shall rely entirely on their own information, judgment and ispection of the aircraft and record. Aircraft is subject to prior sale and reaction from the market. 
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Phone: +52 55 4633 6303
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