HOWARD BEACH, NY, USA
N24343
Boeing 727-232
The Boeing 727-231 was on final approach with the landing gear down and locked and the flaps at 15 degrees. When the flaps were extended to 30 degrees, the airplane started to roll right. Controllability was assessed and found to be satisfactory for continuation of the approach and landing. Postlanding examination of the airplane revealed the inboard section of the fore flap on the right wing had separated from the airplane. The separated flap section was located in a street of Howard Beach, NY about 2.5 miles from the approach end of runway 13L. Metallurgical examination of the respective attachment fitting revealed a fatigue crack that had originated from grinding marks on the fitting. The source of the grinding marks, (original manufacturer or rebuilder) was not determined. During maintenance, the fitting is inspected visually during a 'C' check (at 1690 hour intervals), which had last occurred 1030 hours before the occurrence.
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.
fatigue failure of the fore flap attachment fitting, due to grinding marks on the fitting.
Source: NTSB Aviation Accident Database
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