20090509006329A

Accident · Substantial damage

FAA accident report · Jihlav KP 5 ASA · Crete, NE · May 9, 2009

Date
May 9, 2009 · 19:04 local
Place
Crete, NE
Airport
Crete Municipal
Phase of flight
Takeoff
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N21KP
NTSB investigation
NTSBCEN09CA289
Reported as
Jihlav KP5ASA
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s flight hours
114 total46 in this make and model54 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) At approximately 1910 local time, the light sport pilot and the lone passenger were taking off on runway 35 at cek. Wind direction was 280 at 6 knots: visibility 10SM with barometric pressure at 3011. During takeoff roll the aicraft started moving left center with the pilot countering with right aileron and rudder. At approximately 519 feet from the beginning of 35 the aircraft rudder came in contact with the runway with a heading of approximately 320. The aircraft became airborn for a short time before the left wing touched down in the grass on the left side of the runway between a runway light and the VASI. Approximatley 34 feet from the side of the runway, the nose landing gear impacted the terrain causing it to buckle under the airframe spinning the aircraft 175 degrees before coming to rest with a heading of 145 degrees magnetic. All three landing gear assemblies were folded to the left but still attached. The aircraft was substantially damaged consisting of; all three landing gear folded under; left wing tip and aileron; right wing and aileron; right elevator; rudder; aft fuselage; forward fuselage; propellers; canopy and firewall. The pilot in command and the lone passenger were not injured.

As the FAA filed it

(-23) AT APPROXIMATELY 1910 LOCAL TIME, THE LIGHT SPORT PILOT AND THE LONE PASSENGER WERE TAKING OFF ON RUNWAY 35 AT CEK. WIND DIRECTION WAS 280 AT 6 KNOTS: VISIBILITY 10SM WITH BAROMETRIC PRESSURE AT 3011. DURING TAKEOFF ROLL THE AICRAFT STARTED MOVING LEFT CENTER WITH THE PILOT COUNTERING WITH RIGHT AILERON AND RUDDER. AT APPROXIMATELY 519 FEET FROM THE BEGINNING OF 35 THE AIRCRAFT RUDDER CAME IN CONTACT WITH THE RUNWAY WITH A HEADING OF APPROXIMATELY 320. THE AIRCRAFT BECAME AIRBORN FOR A SHORT TIME BEFORE THE LEFT WING TOUCHED DOWN IN THE GRASS ON THE LEFT SIDE OF THE RUNWAY BETWEEN A RUNWAY LIGHT AND THE VASI. APPROXIMATLEY 34 FEET FROM THE SIDE OF THE RUNWAY, THE NOSE LANDING GEAR IMPACTED THE TERRAIN CAUSING IT TO BUCKLE UNDER THE AIRFRAME SPINNING THE AIRCRAFT 175 DEGREES BEFORE COMING TO REST WITH A HEADING OF 145 DEGREES MAGNETIC. ALL THREE LANDING GEAR ASSEMBLIES WERE FOLDED TO THE LEFT BUT STILL ATTACHED. THE AIRCRAFT WAS SUBSTANTIALLY DAMAGED CONSISTING OF; ALL THREE LANDING GEAR FOLDED UNDER; LEFT WING TIP AND AILERON; RIGHT WING AND AILERON; RIGHT ELEVATOR; RUDDER; AFT FUSELAGE; FORWARD FUSELAGE; PROPELLERS; CANOPY AND FIREWALL. THE PILOT IN COMMAND AND THE LONE PASSENGER WERE NOT INJURED.

NTSB investigation

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