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Aircraft Detail

Administrative Information:
File No. WBC-AV-156751
Adjuster's Name: Peter Kirchen
Bid Closing Date: 07/15/2016
Aircraft Details:
Mfg/Model: Dassault Falcon 20 
Year: 1978 
FAA No: N706SB 
AC SN: 383 
AC TT: 12672.0  
Location of Salvage: Peter Kirchen
Scottsdale, Arizona Airport
Phone: 310-824-1777
pkirchen@kernwooley.com
Description of accident: Right main landing gear collapse during landing roll at the Scottsdale, AZ International Airport  
Cost of storage per day/month $: TBA  
Additional Comments:
Minor scratches caused by ground debris to the lower area of the nose cone and lower nose fuselage.
Heavy impact damage caused by terrain debris in the form of large dents, scratches and some punctures throughout the lower fuselage beginning at the aft portion of the nose section continuing aft to the forward tail section.
Two communication/navigation antennas have been crushed due to impact with terrain.
Minor impact damage to the fuselage fore and aft of the left and right wing to body fairings can be seen due to lifting of the aircraft with large cargo straps during retrieval from the end of the runway.
Heavy debris markings can be seen throughout the right side of the main fuselage starting at the forward section of the right wing on the upper and lower sides of the winged body fairings. Debris from the right fuselage can be seen entering into the right engine.
The right wing appears to have come into contact with the terrain while the aircraft was in motion. The right wing shows much material loss for the leading edge fixed wing area including flaps and ailerons. The inboard flap is crushed and bent due to impact with terrain as well as retrieval of the aircraft. The right wing appears to be punctured into the fuel cell areas. The wing is not likely repairable given the amount of material loss to flight controls and fixed wing structures.
The left wing appears to have sustained minimal impact damages isolated to the lower surface panels of the fixed wing and flaps as well as aileron in the form of minor dents and bending.
All main landing gear tires were caused to burst due to impact with the rough terrain on the runway overrun area which is a mix of rocks and other aggregate material. All main landing gear struts appear to be in the normal down and locked position and revealed no fluid loss or other discrepancies.
The right main landing gear door revealed minor bending and several dents likely caused by impact of terrain debris and minor bending.
The left main landing gear door appears to have suffered minor impact damage due to terrain debris.
The left engine revealed small amounts of sand that may have entered into the bypass inlet.
The right engine appears to have sustained substantial damages from ingestion of terrain debris. All first stage fan blades exhibit impact damage including material loss.

The interior is new in 12/15 and the landing gear is new condition in 6/15  
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Engine Information

Model Information Total Hours Since
Eng# Make and Model: TBO Hours New Reman Overhaul
2 Honeywell TFE 731 6080.0
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Prop Information

Prop# Make and Model: Present Hours: TBO Hours:
There are currently no props for this aircraft.
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Instrument Information

Instrument Make Model Serial No Helicopter Data
Hours
Remaining
Time
Life
#1 Nav/Com           
Transponder           
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Questions

Question Answer Comments
Is the aircraft stored in a secure area? Yes Yes, Open air ramp
Are the avionics stored in a secure area? Yes Yes, In aircraft
Is the title free and clear of liens? No TBA
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Documents and logbooks available

Item
A/W Certificate Included
AD's Included
Airframe Logs Included
Bill of Sale Included
Clear Title Not Available
Engine Logs Included
Equipment List Not Available
Photos Included
POH Included
Registration Certificate Included
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Images

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