N350SW

MINR
None

BOEING 737-300 S/N: 24409

Accident Details

Date
Wednesday, September 8, 1993
NTSB Number
CHI93IA354
Location
ST. LOUIS, MO
Event ID
20001211X13362
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
144
Total Aboard
144

Probable Cause and Findings

a failure of the left outboard foreflap due to the loss of the bolts that hold the inboard sequencing carriage to the foreflap attach lug.

Aircraft Information

Registration
N350SW
Make
BOEING
Serial Number
24409
Engine Type
Turbo-jet
Year Built
1989
Model / ICAO
737-300 B733
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
SOUTHWEST AIRLINES CO
Address
2702 LOVE FIELD DR # HDQ-4GC
Status
Deregistered
City
DALLAS
State / Zip Code
TX 75235-1908
Country
United States

Analysis

On September 8, 1993, at 1740 central daylight time, a Boeing 737-300, N350SW, operated by Southwest Airlines, Inc., as revenue flight 282, sustained an in-flight structural failure of the left outboard flap assembly, while on approach to the Lambert-St. Louis International Airport, St. Louis, Missouri. There were no injuries to the 5 crewmembers or 139 passengers aboard the airplane. The flight, conducted under 14 CFR Part 121, originated at Kansas City, Missouri. An IFR flight plan was filed, and visual meteorological conditions prevailed at the time.

The airplane was on final approach to runway 12R when the controller requested a go-around for traffic separation. The first officer was the pilot flying. The first officer stated in an interview the go-around was normal until he called for flaps 1 about 500 feet. He said the airplane had a rolling tendency to the left, and required a lot of right aileron. The cockpit crew received notification from the cabin attendants that there was a problem with the flaps on the left side. The Captain sent a Southwest Airlines Captain who was riding in the cockpit observers seat to the cabin to investigate. He reported pieces of the outboard flap were hanging loose.

The Captain took control of the airplane and extended the flaps to 5. He made an uneventful landing and taxied to the gate. Inspection of the airplane was conducted by Federal Aviation Administration Inspectors who reported the left outboard foreflap was broken into two pieces and had damaged two sections of spoiler. The two forward bolts which hold the inboard sequencing carriage to the foreflap attach lug were fractured, and the two aft bolts were missing their nuts.

The left outboard flap assembly was removed and sent to the NTSB Materials Laboratory for examination. A copy of the report of the examination of the flap assembly is appended.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI93IA354