20070727016299A

Accident · Substantial damage

FAA accident report · Beech 65-A90 · Wallkill, NY · July 27, 2007

Date
July 27, 2007 · 09:30 local
Place
Wallkill, NY
Airport
Kobelt
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N435A
NTSB investigation
NTSBNYC07CA185
Reported as
Beech 65A90
People aboard
3
Fatal injuries
0
Pilot’s flight hours
3,200 total200 in this make and model25 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Aircraft touched down extremely hard, during landing on rwy 03 at N45, causing the right main gear torque link to break. Aircraft bounced back into air whereupon oleo strut separated from the upper landing gear assembly. Upon reestablishing contact with the runway the aircraft continued northward until it slid to a stop off of the east side of the pavement. The left main gear collapsed under the side loads imposed during the slide. The aircraft sustained damage to the flaps, the nacelles, the fuselage, the tail fin, the right propeller and the nose gear as well as buckling in the skin outboard of the nose gear assembly. A momentary decrease in closure rate perception is likely the primary contributing factor in this accident.

As the FAA filed it

(-23) AIRCRAFT TOUCHED DOWN EXTREMELY HARD, DURING LANDING ON RWY 03 AT N45, CAUSING THE RIGHT MAIN GEAR TORQUE LINK TO BREAK. AIRCRAFT BOUNCED BACK INTO AIR WHEREUPON OLEO STRUT SEPARATED FROM THE UPPER LANDING GEAR ASSEMBLY. UPON REESTABLISHING CONTACT WITH THE RUNWAY THE AIRCRAFT CONTINUED NORTHWARD UNTIL IT SLID TO A STOP OFF OF THE EAST SIDE OF THE PAVEMENT. THE LEFT MAIN GEAR COLLAPSED UNDER THE SIDE LOADS IMPOSED DURING THE SLIDE. THE AIRCRAFT SUSTAINED DAMAGE TO THE FLAPS, THE NACELLES, THE FUSELAGE, THE TAIL FIN, THE RIGHT PROPELLER AND THE NOSE GEAR AS WELL AS BUCKLING IN THE SKIN OUTBOARD OF THE NOSE GEAR ASSEMBLY. A MOMENTARY DECREASE IN CLOSURE RATE PERCEPTION IS LIKELY THE PRIMARY CONTRIBUTING FACTOR IN THIS ACCIDENT.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.