N4646B

Substantial
None

CESSNA 180 S/N: 31544

Accident Details

Date
Wednesday, March 30, 1994
NTSB Number
FTW94LA112
Location
AUSTIN, TX
Event ID
20001206X00913
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

THE LOSS OF ENGINE POWER FOR UNDETERMINED REASONS. FACTORS WERE THE WIRE STRIKE AND LACK OF SUITABLE TERRAIN.

Aircraft Information

Registration
Make
CESSNA
Serial Number
31544
Engine Type
Reciprocating
Model / ICAO
180 C180
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
180

Registered Owner (Current)

Name
BRAVO 300 LLC
Address
PO BOX 477
City
COWETA
State / Zip Code
OK 74429-0477
Country
United States

Analysis

On March 30, 1994, at 1554 central standard time, a Cessna 180, N4646B, was substantially damaged during a forced landing near Austin, Texas. The commercial pilot and passenger were not injured. Visual meteorological conditions prevailed for the personal flight.

In an interview with a Federal Aviation Administration inspector, the pilot stated that on final approach the aircraft lost engine power. He further stated that he could not reach the runway and impacted the ground approximately a quarter of a mile short of the runway. At the time of the loss of engine power the fuel selector was in the both position and was switched to the left tank. During the interview the pilot further stated that he attempted to restart the engine but was unable to do so.

An inspection of the accident scene revealed that the airplane struck a power line. The pilot reported following the wire strike the aircraft turned left and impacted the ground.

An inspection of the airplane revealed that the left wing contained 6.5 gallons of fuel and the right contained 2.5 gallons of fuel. The inspection also revealed that the engine exhibited no damage and there was no evidence of a fuel leak. A check of the manufacturer's specifications revealed that each wing had 2.5 gallons of unusable fuel. During the inspection it was determined that the wings and structural portions of the aircraft had sustained damage.

Followup testing included an engine run. The engine started without problems. The engine was cycled through the RPM ranges and it continued to run without any malfunctions.

The aircraft was released to the owner.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW94LA112