N7775C

After takeoff, the aircrew flew to the southern end of Lake winnebago where they made several uneventful water landings. They estimated that the wind was from the northeast at 5 to 6 knots. The water was described as smooth with only small ripples. On the 6th approach, the gear handle was checked in the up position and the amber gear up indicator light was illuminated. The amphibious aircraft touched down on the water with no bounce or porpoise. About 2 or 3 seconds after touchdown, the aircraft yawed violently to the right and rolled left. The left float and wing tip hit the water and the left wing separated. The hull rolled over, but the occupants egresed before the aircraft sank. A diver noted that the right gear was extended. After the aircraft was recovered, the right main gear actuator rod clevis was found to have fractured. The fracture surface had signs of overload failure. The lock nut had been screwed tightly against the clevis and the lock nut threads had produced gouge marks on the unthreaded portion of the shank of the clevis.

Flight / Schedule

N7775C

Aircraft

SCAN-30

Registration

N7775C

MSN

21

Year of Manufacture

1949

Operator

Condor Aviation

Date

August 5, 1983 at 08:37 AM

Type

CRASH

Flight Type

Training

Flight Phase

Landing (descent or approach)

Crash Site

Lake, Sea, Ocean, River

Crash Location

Fond du Lac Wisconsin

Region

North America • United States of America

Coordinates

43.7533°, -88.4494°

Crash Cause

Technical failure

Narrative Report

On August 5, 1983 at 08:37 AM, N7775C experienced a crash involving SCAN-30, operated by Condor Aviation, with the event recorded near Fond du Lac Wisconsin.

The flight was categorized as training and the reported phase was landing (descent or approach) at a lake, sea, ocean, river crash site.

3 people were known to be on board, 0 fatalities were recorded, 3 survivors were identified or estimated. This corresponds to an estimated fatality rate of 0.0%.

Crew on board: 2, crew fatalities: 0, passengers on board: 1, passenger fatalities: 0, other fatalities: 0.

The listed crash cause is technical failure. After takeoff, the aircrew flew to the southern end of Lake winnebago where they made several uneventful water landings. They estimated that the wind was from the northeast at 5 to 6 knots. The water was described as smooth with only small ripples. On the 6th approach, the gear handle was checked in the up position and the amber gear up indicator light was illuminated. The amphibious aircraft touched down on the water with no bounce or porpoise. About 2 or 3 seconds after touchdown, the aircraft yawed violently to the right and rolled left. The left float and wing tip hit the water and the left wing separated. The hull rolled over, but the occupants egresed before the aircraft sank. A diver noted that the right gear was extended. After the aircraft was recovered, the right main gear actuator rod clevis was found to have fractured. The fracture surface had signs of overload failure. The lock nut had been screwed tightly against the clevis and the lock nut threads had produced gouge marks on the unthreaded portion of the shank of the clevis.

Aircraft reference details include registration N7775C, MSN 21, year of manufacture 1949.

Geospatial coordinates for this crash are approximately 43.7533°, -88.4494°.

Fatalities

Total

0

Crew

0

Passengers

0

Other

0

Crash Summary

After takeoff, the aircrew flew to the southern end of Lake winnebago where they made several uneventful water landings. They estimated that the wind was from the northeast at 5 to 6 knots. The water was described as smooth with only small ripples. On the 6th approach, the gear handle was checked in the up position and the amber gear up indicator light was illuminated. The amphibious aircraft touched down on the water with no bounce or porpoise. About 2 or 3 seconds after touchdown, the aircraft yawed violently to the right and rolled left. The left float and wing tip hit the water and the left wing separated. The hull rolled over, but the occupants egresed before the aircraft sank. A diver noted that the right gear was extended. After the aircraft was recovered, the right main gear actuator rod clevis was found to have fractured. The fracture surface had signs of overload failure. The lock nut had been screwed tightly against the clevis and the lock nut threads had produced gouge marks on the unthreaded portion of the shank of the clevis.

Cause: Technical failure

Occupants & Outcome

Crew On Board

2

Passengers On Board

1

Estimated Survivors

3

Fatality Rate

0.0%

Known people on board: 3

Operational Details

Operator

Condor Aviation

Flight Type

Training

Flight Phase

Landing (descent or approach)

Crash Site

Lake, Sea, Ocean, River

Region / Country

North America • United States of America

Aircraft Details

Aircraft

SCAN-30

Registration

N7775C

MSN

21

Year of Manufacture

1949