20110824020259A

Accident · Substantial damage

FAA accident report · Payne/Foster GLASAIR · Ocala, FL · August 24, 2011

Date
August 24, 2011 · 18:13 local
Place
Ocala, FL
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N250CH
NTSB investigation
NTSBERA11CA471
Reported as
Payne/Foster Glasair
Reported engine
Lycoming 0-320 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
1,550 total3 in this make and model45 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.

During landing rollout on runway 18 at Ocala international airport, aircraft ground-looped to the left and departed the runway. Right main landing gear dug into the grass at the edge of the runway pavement, causing excessive sideload on the gear structure. Such excessive sideload caused the right main landing gear to break away from its attach points within the aircraft fuselage, causing substantial structural damage to the airframe. Post accident onsite investigation of the aircraft revealed that the flight controls and brakes operated properly. However, the tailwheel lock of the free-castering tailwheel assembly failed to keep the tailwheel positively engaged in the locked position. Such failure of the tailwheel locking mechanism accompanied with a direct crosswind of 6 knots caused the aircraft to be exceptionally difficult to control during landing rollout, thus resulting in loss of directional control of the aircraft by the pilot.

As the FAA filed it

DURING LANDING ROLLOUT ON RUNWAY 18 AT OCALA INTERNATIONAL AIRPORT, AIRCRAFT GROUND-LOOPED TO THE LEFT AND DEPARTED THE RUNWAY. RIGHT MAIN LANDING GEAR DUG INTO THE GRASS AT THE EDGE OF THE RUNWAY PAVEMENT, CAUSING EXCESSIVE SIDELOAD ON THE GEAR STRUCTURE. SUCH EXCESSIVE SIDELOAD CAUSED THE RIGHT MAIN LANDING GEAR TO BREAK AWAY FROM ITS ATTACH POINTS WITHIN THE AIRCRAFT FUSELAGE, CAUSING SUBSTANTIAL STRUCTURAL DAMAGE TO THE AIRFRAME. POST ACCIDENT ONSITE INVESTIGATION OF THE AIRCRAFT REVEALED THAT THE FLIGHT CONTROLS AND BRAKES OPERATED PROPERLY. HOWEVER, THE TAILWHEEL LOCK OF THE FREE-CASTERING TAILWHEEL ASSEMBLY FAILED TO KEEP THE TAILWHEEL POSITIVELY ENGAGED IN THE LOCKED POSITION. SUCH FAILURE OF THE TAILWHEEL LOCKING MECHANISM ACCOMPANIED WITH A DIRECT CROSSWIND OF 6 KNOTS CAUSED THE AIRCRAFT TO BE EXCEPTIONALLY DIFFICULT TO CONTROL DURING LANDING ROLLOUT, THUS RESULTING IN LOSS OF DIRECTIONAL CONTROL OF THE AIRCRAFT BY THE PILOT.

NTSB investigation

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

Other reports on N250CH · 3

Matched to the same aircraft by N-number and date.