N533CA

Substantial
Minor

CESSNA T-210M S/N: T21062161

Accident Details

Date
Saturday, October 29, 1994
NTSB Number
FTW95LA035
Location
TYLER, TX
Event ID
20001206X02455
Coordinates
32.580665, -94.730606
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

LOSS OF ENGINE POWER DUE TO INADEQUATE FUEL MANAGEMENT AND FUEL STARVATION. A FACTOR WAS THE LACK OF SUITABLE TERRAIN AVAILABLE FOR THE FORCED LANDING.

Aircraft Information

Registration
N533CA
Make
CESSNA
Serial Number
T21062161
Engine Type
Reciprocating
Model / ICAO
T-210M C210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
KIRK JOHN
Address
600 E WHALEY
Status
Deregistered
City
LONGVIEW
State / Zip Code
TX 75601
Country
United States

Analysis

On October 29, 1994, at 1347 central daylight time, a Cessna T-210M, N533CA, was substantially damaged during a forced landing in the vicinity of Tyler, Texas. The private pilot and one passenger received minor injuries. Visual meteorological conditions prevailed for the local personal flight.

The pilot reported, in his endorsed statement, that while on a practice ILS approach to runway 13 at Tyler's Pounds Field, the "engine sputtered" during the outbound leg to procedure turn. He then switched fuel tanks from RIGHT to LEFT. Inside the outer marker, the "engine sputtered" again and lost power. The pilot then switched fuel tanks from LEFT to RIGHT, operated the boost pump, but could not restart the engine. The pilot further reported that the RIGHT fuel gauge indicated FULL and the LEFT gauge indicated "a little less than" 1/2 FULL while he was switching tanks. The airplane then descended into trees approximately 3/4 mile from the approach end of the runway and came to rest approximately wings level and slightly nose down.

During aircraft recovery, 19 hours after the accident, the right fuel tank was observed to be empty and approximately 27 gallons of fuel was found in the left fuel tank. No evidence of fuel spillage was noted at the site. The right wing fuel tank was filled with water to check for leaks. It was noted that water seeped at a rate of 1 drop per second near a damaged area of the wing leading edge which was crushed back to the spar. No previous fuel stains were noted near the crushed area.

Two engine runs were performed after the accident. One using the fuel selector valve on the RIGHT TANK position, and one using the LEFT TANK position. The engine started normally on both runs and was operated normally to 2500 RPM each time. Manifold pressure was observed as 23 inches on the LEFT TANK fuel selector, and 25 inches on the RIGHT selector. The main fuel screen was examined and found to be clean and clear.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95LA035