N699DT

Destroyed
None

CESSNA 421B S/N: 421B0540

Accident Details

Date
Thursday, June 10, 1993
NTSB Number
ATL93LA108
Location
ATTALLA, AL
Event ID
20001211X12533
Coordinates
34.010334, -86.100730
Aircraft Damage
Destroyed
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

THE FAILURE OF THE LEFT ENGINE TURBOCHARGER DUE TO ROTOR SHAFT SEIZURE, WHICH RESULTED IN A LOSS OF ENGINE POWER.

Aircraft Information

Registration
N699DT
Make
CESSNA
Serial Number
421B0540
Engine Type
Reciprocating
Model / ICAO
421B C421
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
FIVE STAR AVIATION CO
Address
PO BOX 503 US BUSINESS 30 E
Status
Deregistered
City
COLUMBIA CITY
State / Zip Code
IN 46725
Country
United States

Analysis

On June 10, 1993, at about 1827 central daylight time, a Cessna 421B, N699DT, collided with trees and terrain following a reported engine power loss near Attalla, Alabama. The aircraft was destroyed by impact forces and fire. The airline transport pilot was not injured. The aircraft was operated under 14 CFR Part 91 by the pilot. Visual meteorological conditions existed at the time, and no flight plan was filed for the flight from Gadsden, Alabama to Huntsville, Alabama. The flight originated at about 1825.

The pilot reported the following: Shortly after lifting off from runway 36 at the Gadsden Airport, he heard a loud noise from the left engine, and observed smoke trailing from the left engine nacelle. He confirmed that the left engine had lost power, and he feathered the propeller. He was unable to maintain altitude, and prepared for a forced landing in an open field. The aircraft collided with trees prior to reaching the field. The aircraft impacted the ground, and caught fire. The pilot exited the aircraft without injury.

The left engine was sent to the manufacturer's facility in Mobile, Alabama, where a disassembly and inspection were performed. A copy of the inspection report is included as an attachment to this report (see Teledyne Continental Motors Analytical Inspection Report).

The left engine turbocharger was sent to the manufacturer's facility in Torrence, California, where a disassembly and inspection were performed. The inspection revealed that the turbocharger rotor could not be manually rotated. The rotor shaft was extracted from the centerbody, and both bearings were fused to the shaft. The bearings were removed from the shaft, exposing evidence of metal transfer to the bearing journals. For a detailed description of the turbocharger disassembly and inspection, refer to "NTSB Turbocharger Group Chairman Factual Report", attached to this report.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL93LA108