20160711020529A

Accident · Substantial damage

FAA accident report · Canadian Car & Foundry Harvard MK IV · Somerset, KY · July 11, 2016

Date
July 11, 2016 · 12:30 local
Place
Somerset, KY
Airport
Lake Cumberland Regional Airpo
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N99CV
NTSB investigation
NTSBGAA16CA373
Reported as
Canadian Car & Foundry Harvard MK IV
Reported engine
Pratt & Whitney R-1340-AN-1
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
14,500 total1,000 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.

Pilot statement: wheel landing performed iaw formation procedures. When the tail came down the aircraft wanted to go right. Aircraft was corrected left, went right again. Left rudder and brake applied and aircraft exited right side of the runway, making contact with a 3000' remaining marker.

Taxied to ramp and shutdown. Later, pushing aircraft into the hangar with a brake rider; tailwheel steeering was effective and tailwheel unlocked per usual. Brakes worked when activated and didn't drag or bind. ''''''End'''''''

Iic investigation of landing area and markings indicated the aircraft departed to the right with evidence of left brake application. The brakes, rudder, and tailwheel indicated no defects existed. Aircraft had substantial damage to the RH wing rear spar and ailerion.

Weather reported calm winds. A witness described the winds to be calm during the time of accident.

As the FAA filed it

PILOT STATEMENT: WHEEL LANDING PERFORMED IAW FORMATION PROCEDURES. WHEN THE TAIL CAME DOWN THE AIRCRAFT WANTED TO GO RIGHT. AIRCRAFT WAS CORRECTED LEFT, WENT RIGHT AGAIN. LEFT RUDDER AND BRAKE APPLIED AND AIRCRAFT EXITED RIGHT SIDE OF THE RUNWAY, MAKING CONTACT WITH A 3000' REMAINING MARKER.

TAXIED TO RAMP AND SHUTDOWN. LATER, PUSHING AIRCRAFT INTO THE HANGAR WITH A BRAKE RIDER; TAILWHEEL STEEERING WAS EFFECTIVE AND TAILWHEEL UNLOCKED PER USUAL. BRAKES WORKED WHEN ACTIVATED AND DIDN'T DRAG OR BIND. ''''''END'''''''

IIC INVESTIGATION OF LANDING AREA AND MARKINGS INDICATED THE AIRCRAFT DEPARTED TO THE RIGHT WITH EVIDENCE OF LEFT BRAKE APPLICATION. THE BRAKES, RUDDER, AND TAILWHEEL INDICATED NO DEFECTS EXISTED. AIRCRAFT HAD SUBSTANTIAL DAMAGE TO THE RH WING REAR SPAR AND AILERION.

WEATHER REPORTED CALM WINDS. A WITNESS DESCRIBED THE WINDS TO BE CALM DURING THE TIME OF 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.