Boeing 757-200 N921UW incident near Richmond, Virginia

Mar 22, 2008 · NTSB number DCA08IA048 · Final report

Probable cause

The installed wing panel clips failed due to fatigue, likely caused by the incorrect installation of the fasteners in response to SB 757-57-0027. Contributing to the incorrect installation was the SB's lack of clarity in the instructions and figures on the correct orientation of the clips and spacers.

NTSB analysis

NTSB materials laboratory examined the wing-side portions of the left wing trailing edge panel clips from the inboard, middle and outboard positions, with fasteners. Analysis indicated that the wing panel clips fractured due to fatigue. The fatigue region of the inboard clip covered the largest area fraction and was smoothest among the three clips, indicating that fatigue initiated first in the inboard clip. No evidence of corrosion or material anomalies was observed at the fatigue origin. The shape of the fatigue crack in this clip is consistent with fatigue crack propagation primarily under out-of-plane (inboard-outboard) bending loads.

Boeing Service Bulletin (SB) 757-57-0027 was issued April 28, 1988, to address fatigue cracking of attach clips at the location of the fracture in the incident airplane clips. Thickness of the middle clip from the incident airplane indicates that the clips were replaced using kit number 012N8546-1 clips. However, the clips were installed on the incorrect side of the vertical stiffener, and the clips were not installed with spacers as required in SB. Installing the clip on the outboard side of the rear spar vertical stiffener instead of the inboard side would be expected to put additional tensile stress on the inboard side of the clip, which is where fatigue initiation was observed. It is likely that this incorrect installed increased stresses on the clips, which would increase the likelihood of failure due to fatigue.

Patterns in the sealant and filled holes on the inboard clip indicate that it was repositioned to a lower position at some time. The middle clip showed sealant filling areas where the white paint was missing, indicating that the middle clip might have been removed and reinstalled at some time as well.

Text from the NTSB. Open the NTSB docket for DCA08IA048 for the full record.

Event

Date
Mar 22, 2008
Type
Incident
Place
Richmond, Virginia
Highest injury
None
Weather
Visual (VMC)
Light
Day

Boeing 757-200

N-number
N921UW
Category
Airplane
Damage
Minor
Operating rule
Part 121 (airline)

From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.