N6669L

Substantial
None

LAKE LA04 S/N: 431

Accident Details

Date
Saturday, August 7, 1993
NTSB Number
ANC93LA136
Location
BLAIR LAKE, AK
Event ID
20001211X13026
Coordinates
64.769905, -147.329910
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
3
Total Aboard
3

Probable Cause and Findings

THE PILOT'S INADVERTANT ENTRY INTO A PORPOISE AND SUBSEQUENT LOSS OF CONTROL WHILE STEP-TAXIING PRIOR TO TAKEOFF. A FACTOR IN THE ACCIDENT WAS THE ROUGH WATER CONDITIONS.

Aircraft Information

Registration
N6669L
Make
LAKE
Serial Number
431
Engine Type
Reciprocating
Year Built
1969
Model / ICAO
LA04 SA04
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
TIMM KATHLEEN M
Address
HC 36 BOX 2909
Status
Deregistered
City
WASILLA
State / Zip Code
AK 99654-8789
Country
United States

Analysis

HISTORY OF FLIGHT

On August 6, 1993, at approximately 1930 Alaska daylight time, a Lake Amphibian LA04 airplane, N6669L, porpoised, dragged a wing and waterlooped while conducting a high speed on-the-step taxi. The airplane sank on Blair Lake, 30 miles SE of Fairbanks. The flight had originated at Wrights Field, North Pole, Alaska at 1730 on a personal flight in visual meteorological conditions, under 14 CFR Part 91. No flight plan was filed. The commercial pilot and two passengers escaped without injury and the aircraft was substantially damaged.

In a statement to the NTSB the pilot said that the airplane developed a porpoise while taxiing on the step at 60 MPH which progressed to wing oscillations and loss of control.

DAMAGE TO AIRCRAFT

The aircraft sustained hull damage and loss of wing floats, consistent with sideloads experienced in a waterloop.

AIRCRAFT INFORMATION

In boat hull seaplanes, a porpoise is a pitch into and out of the sea by the bow of the aircraft about the lateral axis. The magnitude of the oscillations relate to the energy needed to displace the water under the bow and the resultant upward force by the water on the hull. The frequency of the oscillation relates to aircraft speed and period of the sea (distance between swell crests). The oscillations can be pilot-induced or sea-condition-induced. Typically, this porpoise is followed by rolls about the longitudinal axis which, as the wingtip floats alternately enters the water, and exacerbates the rolling moment by porpoising themselves. A final turn (waterloop) is typically a result of the hydrodynamic center of drag becoming forward of the aerodynamic center of gravity, leading to a destabilized loss of control and sudden sideload on the forward hull. Damage to cantilever mounted wing floats by these sideloads is typical.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC93LA136