20190622007809A

Accident · Substantial damage

FAA accident report · Maule M-7-235B · Sunriver, OR · June 22, 2019

Date
June 22, 2019 · 10:00 local
Place
Sunriver, OR
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N118G
NTSB investigation
NTSBWPR19FA178
Reported as
Maule M-7-235B
Reported engine
Lycoming IO-540 series
People aboard
2
Fatal injuries
1
Other injuries
1
Pilot’s certificates
Airline transport, commercial pilot, flight instructor

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.

Arrived on scene approx. 1930 local. Located deputy who was securing scene. Observed aircraft in the river floats up with amphibious wheels extended. Aircraft remained in the river until Thursday 6/27. When aircraft was recovered, damage to front of aircraft and wing leading edges was consistent with aircraft doing a water landing with wheels extended and flipping inverted immediately. Wing support struts sheared at fuselage attach points and obstructed cabin door opening. Upon gaining access to the cockpit. Verified landing gear selector position was in the down position. Magneto selector was in the left position only not both. Fuel selector was selected to the left tank. Teardown results indicated both magnetos were functional. Both exhaust mufflers had internal damage to the baffle tube. Left hand baffle tube was broken and moving freely inside the muffler. Right hand baffle tube was broken and blocking the exhaust exit.

As the FAA filed it

ARRIVED ON SCENE APPROX. 1930 LOCAL. LOCATED DEPUTY WHO WAS SECURING SCENE. OBSERVED AIRCRAFT IN THE RIVER FLOATS UP WITH AMPHIBIOUS WHEELS EXTENDED. AIRCRAFT REMAINED IN THE RIVER UNTIL THURSDAY 6/27. WHEN AIRCRAFT WAS RECOVERED, DAMAGE TO FRONT OF AIRCRAFT AND WING LEADING EDGES WAS CONSISTENT WITH AIRCRAFT DOING A WATER LANDING WITH WHEELS EXTENDED AND FLIPPING INVERTED IMMEDIATELY. WING SUPPORT STRUTS SHEARED AT FUSELAGE ATTACH POINTS AND OBSTRUCTED CABIN DOOR OPENING. UPON GAINING ACCESS TO THE COCKPIT. VERIFIED LANDING GEAR SELECTOR POSITION WAS IN THE DOWN POSITION. MAGNETO SELECTOR WAS IN THE LEFT POSITION ONLY NOT BOTH. FUEL SELECTOR WAS SELECTED TO THE LEFT TANK. TEARDOWN RESULTS INDICATED BOTH MAGNETOS WERE FUNCTIONAL. BOTH EXHAUST MUFFLERS HAD INTERNAL DAMAGE TO THE BAFFLE TUBE. LEFT HAND BAFFLE TUBE WAS BROKEN AND MOVING FREELY INSIDE THE MUFFLER. RIGHT HAND BAFFLE TUBE WAS BROKEN AND BLOCKING THE EXHAUST EXIT.

NTSB investigation

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