N24343

MINR
None

Boeing 727-232 S/N: 21630

Accident Details

Date
Friday, August 16, 1996
NTSB Number
NYC96IA169
Location
HOWARD BEACH, NY
Event ID
20001208X06598
Coordinates
40.660758, -73.840118
Aircraft Damage
MINR
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
112
Total Aboard
112

Probable Cause and Findings

fatigue failure of the fore flap attachment fitting, due to grinding marks on the fitting.

Aircraft Information

Registration
N24343
Make
BOEING
Serial Number
21630
Engine Type
Turbo-jet
Year Built
1980
Model / ICAO
727-232 B721
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
3

Registered Owner (Historical)

Name
PACIFIC AIRCORP 21630 INC
Address
4 EMBARCADERO CTR FL 35
Status
Deregistered
City
SAN FRANCISCO
State / Zip Code
CA 94111-4106
Country
United States

Analysis

On August 15, 1996, about 2325 eastern daylight time, TWA flight 782, N24343, Boeing 727-231, had a separation of flap section during approach to John F. Kennedy Airport, Jamaica, New York. Visual meteorological conditions prevailed and an instrument flight rules plan was filed. There were no injuries to the 112 occupants. The airplane received minor damage. The departure point was Orlando, Florida. The flight was conducted under 14 CFR Part 121.

Flight 782 conducted the VOR approach to runway 13L, and according to the captain, when landing flaps (30 degrees) were selected, the airplane rolled to the right. The roll was corrected with aileron input, and airplane control was regained. In addition, there were no abnormal cockpit indications, and the reference speed was increased 15 knots for safety. The approach continued to a normal landing.

Post flight examination of the airplane revealed a portion of the right wing outboard trailing edge flap had separated. An eight foot long section remained attached to the airplane. The separated flap section was located in a street of Howard Beach, New York, about 2.5 miles from the approach end of runway 13L. The section was about 16 inches wide and 9 feet long. There was no property damage associated with the separation.

Metallurgical examination of the failed fitting in the NTSB Laboratory found a fatigue crack that emanated from gouge marks. The gouge marks were found on multiple locations on the fitting. In addition, the metallurgical report stated that the maximum roughness allowed was 125 microinches (0.000125 inches), and the gouge marks measured as deep as 0.002 inches. The source of the gouges, original manufacturer, or rebuild was not determined.

The fittings P/N 69-26255, are inspected at "C" checks. The last "C" check was conducted on April 4, 1996, at the TWA maintenance base located at John F. Kennedy Airport 1030 hours prior to the occurrence. The interval between "C" checks was 1690 hours. According to the work card, the inspection is a visual inspection conducted without removal of the fitting.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# NYC96IA169