Serious incident Boeing 767-232 N111DN,
ASN logo
ASN Wikibase Occurrence # 352309
 
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:Monday 6 December 1999
Time:17:55 LT
Type:Silhouette image of generic B762 model; specific model in this crash may look slightly different    
Boeing 767-232
Owner/operator:Delta Air Lines
Registration: N111DN
MSN: 22223/74
Year of manufacture:1983
Total airframe hrs:51977 hours
Engine model:GE CF6-80A2
Fatalities:Fatalities: 0 / Occupants: 85
Aircraft damage: Minor, repaired
Category:Serious incident
Location:Salt Lake City, UT -   United States of America
Phase: Initial climb
Nature:Passenger - Scheduled
Departure airport:Salt Lake City International Airport, UT (SLC/KSLC)
Destination airport:Dallas/Fort Worth International Airport, TX (DFW/KDFW)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The crew heard a loud noise and felt a vibration when the landing gear was retracted after takeoff. An emergency was declared, and the flight returned to Salt Lake City. When the landing gear was lowered, the nose and right main landing gear DOWN AND LOCKED lights illuminated, but a GEAR UNSAFE light illuminated for the left main landing gear. Following a low pass over the airport, maintenance personnel advised the landing gear appeared to be down and locked. An uneventful landing was made. Maintenance personnel informed the crew that the landing gear actuator had sheared and could not be pinned for towing. The part was later removed and examined. Stress corrosion cracking had occurred through 75% of the piston, followed by ductile separation. The corrosion had formed when a faulty fillet seal around the base of the rod end allowed moisture to enter the joint. The retract actuator was an original part, but it was determined that it had previously been reworked.

Probable Cause: Total failure of the main landing gear retract actuator due to stress corrosion caused by the use of a faulty sealant by company maintenance personnel that allowed moisture to enter the joint. A factor was the use of an improper fillet seal.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: DEN00IA023
Status: Investigation completed
Duration: 1 year and 8 months
Download report: Final report

Sources:

NTSB DEN00IA023

Revision history:

Date/timeContributorUpdates
07-Mar-2024 08:00 ASN Update Bot Added
07-Mar-2024 08:01 ASN Updated [Operator, Nature, Departure airport, Destination airport, Narrative]

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