N761HQ

Substantial
None

Cessna T210M S/N: 21062273

Accident Details

Date
Friday, August 29, 1997
NTSB Number
LAX97LA307
Location
SAN MARTIN, CA
Event ID
20001208X08693
Coordinates
37.099727, -121.599052
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Installation of improper connecting hardware by maintenance personnel, and, the inadequate inspection of the installed hardware by inspection personnel resulting in separation of the engine throttle linkage.

Aircraft Information

Registration
N761HQ
Make
CESSNA
Serial Number
21062273
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
T210M C210
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BUSH CHARLES
Address
PO BOX 39
Status
Deregistered
City
FABENS
State / Zip Code
TX 79838-0039
Country
United States

Analysis

On August 29, 1997, at 1510 hours Pacific daylight time, a Cessna T210M, N761HQ, overshot the landing runway and impacted a fence and terrain at South County Airport, San Martin, California. The aircraft was substantially damaged, and the airline transport pilot was not injured. Visual meteorological conditions prevailed for the post-maintenance check flight. The flight departed from the San Jose International Airport about 1430.

The pilot told an inspector from the San Jose Flight Standards District Office that he was conducting the check flight of the aircraft following an annual inspection, which was completed the prior day. While in cruise flight, the engine lost power and he attempted to glide to runway 32 for an emergency landing. He overshot the 3,100-foot-long runway and went off the departure end.

The inspector reported that when the engine was uncowled, the bolt which connects the throttle control to the throttle body actuator arm was missing. The bolt was found in the bottom of the cowling, but the nut was not located. Subsequent investigation revealed that, during maintenance associated with the inspection, the throttle, propeller and mixture control cables had been replaced. The bolt found in the bottom of the cowling was an improper type that did not comply with an applicable Airworthiness Directive.

In his report to the Safety Board, the pilot stated that after the throttle control separated, the engine may not have gone completely to the idle power position and the resulting partial engine power may have contributed to the landing overshoot. The pilot stated that he was wearing a headset and could not hear the engine well enough to detect a partial power condition.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX97LA307