1967 DEHAVILLAND DHC 2T
Aircraft Summary
General
Year
1967
Manufacturer
DEHAVILLAND
Model
DHC-2T
Condition
New
Total Time
0
Description
BX Conversion DHC-2T
Maximum gross weight 5,999 LBS
Basic aircraft weight* 4,300 LBS
Main wings fuel capacity 148.2 USG
Auxiliary tanks capacity 64 USG
Max wing loading 23.5 LB/SQ FT
Stall speed (FLAP 35) 68 MPH
Take off ground roll (runway) at sea level, gross weight, ISA 453 FT
Landing ground roll (runway) at sea level, gross weight, ISA 474 FT
Take off ground roll (water) at sea level, gross weight, ISA 570 FT
Landing ground roll (water) at sea level, gross weigt, ISA 582 FT
Max rate of climb at sea level, gross weight 1,922 FT/MIN
Max rate of climb at 12,000 FT, gross weight 1,704 FT/MIN
Engine 1
Engine 1 Time
0
Engine 1 Time Since
SMOH
Engine 1 TBO
3600
Engine 1 Notes
Factory New PT6A-34
Props
Prop Notes
Factory new Hartzell 106’’ three bladed propeller, reversible, full feathering, start locks and spinner kit
Modifications/Conversions
Modifications/Conversions
Factory new BX wings per SA97-88
Avionics
Avionics/Radios
New avionics and redesigned instrument panel
Factory new electronics international MVP-50T engine monitoring
Panel can be customized to buyers need.
Additional Equipment
Additional Equipment
Factory new BX wings per SA97-88
Carbon fiber air inlet
Electrical actuated inertial particle separator & ice bypass
New lightweight & fire-resistant carbon fiber cowlings
Custom heavy duty engine mount Oil system with oil cooler & hoses
Hutchinson engine isolators
Completely redesigned fuel system
200 AMP Ametek starter generator & generator control unit
New bleed air cabin heat
Propeller and overspeed governor
Np & Nf tachometer generator
Concorde lead-acid stainless steel encapsulated battery
Recommended For You
View All(Recommended For You)Aircraft.com does not own the rights to the images displayed on this site. We do not have information regarding the original seller or source of these images unless explicitly stated.


