Accident McDonnell Douglas DC-9-32 N903VJ,
ASN logo
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Thursday 1 February 1996
Time:16:05 LT
Type:Silhouette image of generic DC93 model; specific model in this crash may look slightly different    
McDonnell Douglas DC-9-32
Owner/operator:Valujet Airlines
Registration: N903VJ
MSN: 47261/411
Total airframe hrs:3078 hours
Engine model:P&W JT8D-7B
Fatalities:Fatalities: 0 / Occupants: 80
Aircraft damage: Substantial
Category:Accident
Location:Nashville, TN -   United States of America
Phase: Landing
Nature:Unknown
Departure airport:Atlanta, GA (KATL)
Destination airport:(KBNA)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
During landing, the right main landing gear shock strut cylinder and piston failed which caused the axle, wheels, and tires to separate. Metallurgical examination showed that the fracture surfaces had been damaged after separation. Two areas on the cylinder fracture face were not at an angle to suggest overstress separation, and ratchet marks were present which usually separate initiation sights on offset fracture planes. The piston fracture surfaces had features typical of overstress separation. The right main landing torque links had failed during landing 312 flight hours before this accident. The torque links, shimmy damper, and piston were replaced at that time; the cylinder was not replaced.

Probable Cause: the failure of the right main landing gear shock strut cylinder due to preexisting fractures. Contributing to the accident was: the failure of the operator to inspect the shock strut cylinder for fractures following a previous failure of the torque links, and the absence of specific directives and procedures from the aircraft manufacturer to inspect or replace the shock strut cylinder following torque link failure.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ATL96FA043
Status: Investigation completed
Duration: 1 year and 3 months
Download report: Final report

Sources:

NTSB ATL96FA043

Location

Revision history:

Date/timeContributorUpdates
14-Mar-2024 06:46 ASN Update Bot Added

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org