20000407019579A

Accident · Substantial damage

FAA accident report · Tcraft BC12-D · Dameron, MD · April 7, 2000

Date
April 7, 2000 · 12:00 local
Place
Dameron, MD
Phase of flight
Takeoff Ground Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N43459
NTSB investigation
NTSBIAD00FA034
Reported as
Tcraft BC12D
Reported engine
Continental C8512
People aboard
2
Fatal injuries
0
Pilot’s flight hours
171 total6 in this make and model20 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)On April 7, 2000, FAA inspector privacy data omitted was conducting a private pilot additional rating certification test. While the pilot/applicant was performing a normal approach and landing task, the floats separated the airplane sank in approximately seven to eight feet of water. During the initial response and investigation of the incident, only the floats had been recovered. The rear float spreader bar was missing. The attach points for the rear spreader bar showed evidence of severe corrosion. On April 8, 2000 the aircraft was recovered from the water by the owner. On April 14,2000 I was able to inspect the aircraft and did not find any other significant damage.

As the FAA filed it

(-23)ON APRIL 7, 2000, FAA INSPECTOR ^PRIVACY DATA^ WAS CONDUCTING A PRIVATE PILOT ADDITIONAL RATING CERTIFICATION TEST. WHILE THE PILOT/APPLICANT WAS PERFORMING A NORMAL APPROACH AND LANDING TASK, THE FLOATS SEPARATED THE AIRPLANE SANK IN APPROXIMATELY SEVEN TO EIGHT FEET OF WATER. DURING THE INITIAL RESPONSE AND INVESTIGATION OF THE INCIDENT, ONLY THE FLOATS HAD BEEN RECOVERED. THE REAR FLOAT SPREADER BAR WAS MISSING. THE ATTACH POINTS FOR THE REAR SPREADER BAR SHOWED EVIDENCE OF SEVERE CORROSION. ON APRIL 8, 2000 THE AIRCRAFT WAS RECOVERED FROM THE WATER BY THE OWNER. ON APRIL 14,2000 I WAS ABLE TO INSPECT THE AIRCRAFT AND DID NOT FIND ANY OTHER SIGNIFICANT DAMAGE.

NTSB investigation

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