20000608020729I

Incident · Minor damage

FAA incident report · Shelton Tom AVID FLYER IV · Troutdale, OR · June 8, 2000

Date
June 8, 2000 · 11:12 local
Place
Troutdale, OR
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N60TS
Reported engine
AMTR EA81
People aboard
1
Fatal injuries
0
Pilot’s flight hours
1,500 total5 in this make and model5 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) Weather factors: aircraft is equipped with floats. Landing was attempted on the columbia river in rough water as described by the pilot. Witness stated there was some swells and waking. Witnesses also stated that the aircraft bounced once and then landed hard. According to the pilot, after a hard landing he noticed the right wing drop and could not hold it up with aileron control. As the aircraft slowed the outer three to four feet of the right wing became submerged in the water. The pilot unsuccessfully attempted to taxi to shore. The aircraft was towed to shore by a couple of boats. Inspection of the aircraft revealed the right aft strut broken just below the fuselage attach point. The aft cross brace wire that attaches to the right float was severed or pulled apart. The forward cross brace wire that attaches to the right float was pulled from its mounting bracket, which was damaged as well. The right wing tip sustained minor damage.

As the FAA filed it

(-23) WEATHER FACTORS: AIRCRAFT IS EQUIPPED WITH FLOATS. LANDING WAS ATTEMPTED ON THE COLUMBIA RIVER IN ROUGH WATER AS DESCRIBED BY THE PILOT. WITNESS STATED THERE WAS SOME SWELLS AND WAKING. WITNESSES ALSO STATED THAT THE AIRCRAFT BOUNCED ONCE AND THEN LANDED HARD. ACCORDING TO THE PILOT, AFTER A HARD LANDING HE NOTICED THE RIGHT WING DROP AND COULD NOT HOLD IT UP WITH AILERON CONTROL. AS THE AIRCRAFT SLOWED THE OUTER THREE TO FOUR FEET OF THE RIGHT WING BECAME SUBMERGED IN THE WATER. THE PILOT UNSUCCESSFULLY ATTEMPTED TO TAXI TO SHORE. THE AIRCRAFT WAS TOWED TO SHORE BY A COUPLE OF BOATS. INSPECTION OF THE AIRCRAFT REVEALED THE RIGHT AFT STRUT BROKEN JUST BELOW THE FUSELAGE ATTACH POINT. THE AFT CROSS BRACE WIRE THAT ATTACHES TO THE RIGHT FLOAT WAS SEVERED OR PULLED APART. THE FORWARD CROSS BRACE WIRE THAT ATTACHES TO THE RIGHT FLOAT WAS PULLED FROM ITS MOUNTING BRACKET, WHICH WAS DAMAGED AS WELL. THE RIGHT WING TIP SUSTAINED MINOR DAMAGE.