N931AS

MINR
None

MCDONNELL DOUGLAS MD-83 S/N: 49232

Accident Details

Date
Monday, April 18, 1994
NTSB Number
SEA94IA103
Location
SEATTLE, WA
Event ID
20001206X01173
Coordinates
47.439029, -122.280685
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
139
Total Aboard
139

Probable Cause and Findings

THE FATIGUE FRACTURE OF A MAIN GEAR WHEEL HUB.

Aircraft Information

Registration
N931AS
Make
MCDONNELL DOUGLAS
Serial Number
49232
Engine Type
Turbo-jet
Year Built
1985
Model / ICAO
MD-83 MD83
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
SALE REPORTED
Address
NONE
Status
Deregistered
City
XXXX
State / Zip Code
OK 73102
Country
United States

Analysis

On April 17, 1994, approximately 1855 Pacific daylight time (PDT), an Alaska Airlines McDonnell Douglas MD-83, N931AS, experienced a fire in the area of the left main gear while taxiing to the passenger loading gate at Seattle-Tacoma International Airport, Seattle, Washington. After stopping at the gate and requesting fire equipment, the captain ordered an emergency evacuation of the aircraft. There were no reported injuries to the 132 passengers, six crew members, or the single jump seat occupant. The aircraft, which departed San Francisco International Airport on an IFR flight plan at 1655 PDT, was operating in visual meteorological conditions at the time of the incident. This mishap did not involve the activation of an ELT.

According to tower personnel, smoke was seen coming from the area of the left main gear as the aircraft taxied to the gate. The tower notified the aircrew of the situation and, as the aircraft stopped at the gate, flames began coming from the same area, prompting the captain to initiate an emergency evacuation. Approximately half of the occupants evacuated through the normal jetway exit, while the other half exited using the tail cone slide.

The investigation has revealed that the left main gear wheel hub experienced a fatigue fracture which originated in the hub grease dam groove. Subsequent to the hub failure, hydraulic fluid, which was leaking from a damaged brake component, was ignited by a hot brake pad.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA94IA103