2012 DEHAVILLAND DHC 6 400
Aircraft Summary
General
Year
2012
Manufacturer
DEHAVILLAND
Model
DHC-6-400
Condition
Used
FlightRules
IFR
Airframe
Total Time
893.0
Airframe Notes
Configuration and Construction:
All metal, non pressurized, high-wing
monoplane with fixed tricycle (steerable
nose) landing gear.
Engine Program
Engine Program Notes
Two, Pratt & Whitney Aircraft of
Canada Limited, PT6A-34, single
stage, freeturbine engines.
Props
Prop Notes
Two Hartzell HC-B3TN three bladed
reversible pitch, constant speed, fully
feathering propellers.
Avionics
Avionics/Radios
Dual DME
Dual Mode S EHS Transponders with
ADS-B Out Capability
Radar Altimeter
Class AT errain Warning
(Honeywell MK VI EGPWS)
TCAS I Traffic Advisory System
Honeywell RDR 2000 Weather Radar
Crew Intercom
Dual David Clark Noise Cancelling
Headsets
Jacks for Third (Observer) Headset at
Flight Compartment
Cabin Public Address System
406 Mhz ELT with Latitude and
Longitude Transmission
L3 Electronic Integrated Standby
Instrument System
Thommen Chronometer
Eye Height Reference Device
Integrated Central Maintenance
Computer Function
4 Channel CVR
Dual14 Volt Convenience Outlets in
Flight Compartment
Flight Director (delayed
Additional Equipment
Additional Equipment
CVR, FDR, HF RADIO, DUAL GPS Installation, ELT with navigation interface and remote switch, Dual Audio Panels, Vertical Depiction of Terrain on Route Ahead, Mk 6 Class A TAWS, Radar Altimeter, TCAS
Exterior
Year Painted
2012
Exterior Notes
NEW
Interior
Year Interior
2012
Number of Seats
19
Interior Notes
NEW
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