20241117018829I

Incident · Minor damage

FAA incident report · Clay E Hartley AIRCAM · Suwannee, FL · November 17, 2024

Date
November 17, 2024 · 10:30 local
Place
Suwannee, FL
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N511PH
Reported as
Clay E Hartley Aircam
Reported engine
ROTAX 912ULS series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
14,883 total

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.

Aircraft was coming in for a water landing. Pilot checked the gear indicator light on dash and it showed retracted (up) and locked. The pilot failed to check the secondary indicator located on the floats themselves which were working properly and showed the gear being extended (down). The bellcrank rod end on both landing gear retraction assemblies were corroded and had snapped, leaving the gear in the down and locked position, though the actuators retracted properly, prompting dash indicator light to show up and locked. When the aircraft contacted the water, it contacted the extended gear and caused aircraft to flip forward.

As the FAA filed it

AIRCRAFT WAS COMING IN FOR A WATER LANDING. PILOT CHECKED THE GEAR INDICATOR LIGHT ON DASH AND IT SHOWED RETRACTED (UP) AND LOCKED. THE PILOT FAILED TO CHECK THE SECONDARY INDICATOR LOCATED ON THE FLOATS THEMSELVES WHICH WERE WORKING PROPERLY AND SHOWED THE GEAR BEING EXTENDED (DOWN). THE BELLCRANK ROD END ON BOTH LANDING GEAR RETRACTION ASSEMBLIES WERE CORRODED AND HAD SNAPPED, LEAVING THE GEAR IN THE DOWN AND LOCKED POSITION, THOUGH THE ACTUATORS RETRACTED PROPERLY, PROMPTING DASH INDICATOR LIGHT TO SHOW UP AND LOCKED. WHEN THE AIRCRAFT CONTACTED THE WATER, IT CONTACTED THE EXTENDED GEAR AND CAUSED AIRCRAFT TO FLIP FORWARD.

Other reports on N511PH · 1

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