N296SC

Substantial
None

Boeing 727-224 S/N: 22449

Accident Details

Date
Sunday, September 10, 2000
NTSB Number
CHI00LA296
Location
MINNEAPOLIS, MN
Event ID
20001212X21929
Coordinates
44.879234, -93.220794
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
101
Total Aboard
101

Probable Cause and Findings

The fatigue failure of the wheel assembly. A factor was the inadequate inspection procedures prior to the issuance of a service bulletin.

Aircraft Information

Registration
N296SC
Make
BOEING
Serial Number
22449
Engine Type
Turbo-jet
Year Built
1981
Model / ICAO
727-224 B721
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
3

Registered Owner (Historical)

Name
ART 22449 LLC
Address
4 EMBARCADERO CTR FL 35
Status
Deregistered
City
SAN FRANCISCO
State / Zip Code
CA 94111-4106
Country
United States

Analysis

On September 10, 2000, at 0938 central daylight time, a Boeing 727-224, N296SC, operated by Sun Country Airlines as flight 791, sustained substantial damage when the number 3 wheel and tire assembly failed during taxi at the Minneapolis International Airport, Minneapolis, Minnesota. Pieces of the wheel assembly subsequently impacted the airframe causing the damage. The 14 CFR Part 121 flight was operating in visual meteorological conditions at the time of the accident. No injuries were reported to the 7 crew members or 94 passengers on board. The flight was taxiing to the runway for a departure to the San Francisco International Airport, San Francisco, California.

The wheel components were sent to the NTSB Materials Laboratory in Washington, D.C. for further examination. The examination report indicates that most of the fracture surfaces exhibited signatures consistent with overstress fracture. However, a portion of the fracture surface exhibited signatures consistent with fatigue. The fatigue origin was found to emanate from a point at the inside diameter of one of the brake lugs. A circumferential scratch was found adjacent to the fatigue origin.

The wheel half had been inspected by an approved repair station and shipped to the airline on July 21, 2000. The wheel had accumulated 356.2 hours time in service at the time of the accident. A review of repair station records revealed that the repair station had been rejecting about 4 wheel halves per month. Prior to the accident, the repair station was finding cracks on other wheel halves in the area where the wheel failure occurred. The repair station had been in contact with the wheel manufacturer concerning this matter and had sent representative wheel halves to the manufacturer for evaluation. In a conversation with a representative of the Federal Aviation Administration, the wheel manufacturer stated that one of the returned wheel halves had been examined and that a manufacturing defect had created a stress concentrator, which resulted in a fatigue failure of the wheel half.

On May 04, 2001, the wheel manufacturer issued a Service Bulletin, number 2604561-32-001, to rework the lugs and to provide guidance in inspecting the affected areas of the wheel assembly.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI00LA296