19951010036679I

Incident · Minor damage

FAA incident report · Amtrad Buccaneer · Fort Pierce, FL · October 10, 1995

Date
October 10, 1995 · 17:53 local
Place
Fort Pierce, FL
Airport
St Lucie County International
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N234HM
Reported as
Amtrad Buccaneer
Reported engine
ROTAX ROTAX912
People aboard
1
Fatal injuries
0
Pilot’s flight hours
3,500 total14 in this make and model14 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.

Narrative: the airworthiness certificate was issued 10-6-95 by j.l. murphy (DAR-38-FS-SO) and the aircraft appeared to be in good condition. When inspector casado and I arrived the aircraft was positioned so that we could observe the retraction of the landing gear. The cables from the rudder control horn to the water rudder had been removed but it was demonstrated how the water rudder cables became tangled in the tail wheel control horns. When the tail wheel was extended the tail wheel was deflected 90 degrees from the trail position. Upon touch down the aircraft made an abrupt turn causing a ground loop. Only one main wheel was damaged and no part of the aircraft contacted the ground.

As the FAA filed it

NARRATIVE: THE AIRWORTHINESS CERTIFICATE WAS ISSUED 10-6-95 BY J.L. MURPHY (DAR-38-FS-SO) AND THE AIRCRAFT APPEARED TO BE IN GOOD CONDITION. WHEN INSPECTOR CASADO AND I ARRIVED THE AIRCRAFT WAS POSITIONED SO THAT WE COULD OBSERVE THE RETRACTION OF THE LANDING GEAR. THE CABLES FROM THE RUDDER CONTROL HORN TO THE WATER RUDDER HAD BEEN REMOVED BUT IT WAS DEMONSTRATED HOW THE WATER RUDDER CABLES BECAME TANGLED IN THE TAIL WHEEL CONTROL HORNS. WHEN THE TAIL WHEEL WAS EXTENDED THE TAIL WHEEL WAS DEFLECTED 90 DEGREES FROM THE TRAIL POSITION. UPON TOUCH DOWN THE AIRCRAFT MADE AN ABRUPT TURN CAUSING A GROUND LOOP. ONLY ONE MAIN WHEEL WAS DAMAGED AND NO PART OF THE AIRCRAFT CONTACTED THE GROUND.

Other reports on N234HM · 1

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