20060529016369A

Accident · Substantial damage

FAA accident report · Piper J3C-65 · Millinocket, ME · May 29, 2006

Date
May 29, 2006 · 15:52 local
Place
Millinocket, ME
Airport
Millinocket Municipal Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1401V
NTSB investigation
NTSBNYC06CA126
Reported as
Piper J3C65
People aboard
1
Fatal injuries
0
Pilot’s flight hours
825 total350 in this make and model16 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 may 29, 2006 the pilot privacy data omitted was pilot-in-command of N1401V a Piper J3C-65 configured for float operations. Upon landing the pilot stated that the front of the right float rotated upwards and was struck by the propeller. The right float did not completely separate from the aircraft. Investigation revealed that the right float rear spreader bar fitting had failed. There was evidence that this fitting was cracked for some time. Pilot admitted that he routinely changed the configuration of his aircraft each year from wheels to floats. He stated that he did this without the aid or supervision of a certificated airframe mechanic.

As the FAA filed it

(-23) ON MAY 29, 2006 THE PILOT ^PRIVACY DATA OMITTED^ WAS PILOT-IN-COMMAND OF N1401V A PIPER J3C-65 CONFIGURED FOR FLOAT OPERATIONS. UPON LANDING THE PILOT STATED THAT THE FRONT OF THE RIGHT FLOAT ROTATED UPWARDS AND WAS STRUCK BY THE PROPELLER. THE RIGHT FLOAT DID NOT COMPLETELY SEPARATE FROM THE AIRCRAFT. INVESTIGATION REVEALED THAT THE RIGHT FLOAT REAR SPREADER BAR FITTING HAD FAILED. THERE WAS EVIDENCE THAT THIS FITTING WAS CRACKED FOR SOME TIME. PILOT ADMITTED THAT HE ROUTINELY CHANGED THE CONFIGURATION OF HIS AIRCRAFT EACH YEAR FROM WHEELS TO FLOATS. HE STATED THAT HE DID THIS WITHOUT THE AID OR SUPERVISION OF A CERTIFICATED AIRFRAME MECHANIC.

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 N1401V · 3

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