N124LR

Substantial
None

Cessna A185E S/N: 159507-9-D

Accident Details

Date
Monday, August 30, 1999
NTSB Number
ANC99LA126
Location
ANCHORAGE, AK
Event ID
20001212X19413
Coordinates
61.110744, -149.900360
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
4
Total Aboard
4

Probable Cause and Findings

The total loss of engine power for an undetermined reason.

Aircraft Information

Registration
Make
CESSNA
Serial Number
159507-9-D
Engine Type
Reciprocating
Year Built
1970
Model / ICAO
A185E C185
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
6
FAA Model
A185E

Registered Owner (Current)

Name
WILSON DAVID J
Address
PO BOX 4183
City
PALMER
State / Zip Code
AK 99645-4183
Country
United States

Analysis

On August 29, 1999, about 1815 Alaska daylight time, a float equipped Cessna A185E airplane, N124LR, sustained substantial damage during a forced landing, about 4 miles east of Anchorage, Alaska, at 61.06.37 north latitude, 149.51.80 west longitude. The airplane was being operated as a visual flight rules (VFR) personal flight under Title 14, CFR Part 91, when the accident occurred. The certificated private pilot, and the three passengers aboard, were not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated about 1743, from an off airport site located on Eleanor Island, Alaska.

During an on-site interview with the National Transportation Safety Board (NTSB) investigator-in-charge on August 29, the pilot reported that during the initial descent to the Lake Hood Seaplane Base, all engine power was lost. The pilot said that after performing the engine emergency procedures, he was unable to restore engine power. The pilot stated that he selected a forced landing area in a slough that was surrounded by trees. During the forced landing, the left wing struck a stand of trees, and the airplane pivoted to the left.

The airplane sustained substantial damage to the wings and fuselage.

An on-site inspection of the airplane by the NTSB investigator-in-charge (IIC) on August 29, revealed the presence of fuel in both wing tanks, fuel lines, and the fuel manifold assembly. No mechanical defects were found with the engine. The cockpit fuel selector valve was found in the "both" position.

On September 7, 1999, the engine, while still mounted on the accident airplane's airframe, was operated under the direction of the IIC. The engine ran without any observed anomalies, and produced full factory specified rpm.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC99LA126