Accident Boeing 727-247 N2809W,
ASN logo
ASN Wikibase Occurrence # 182066
 
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:Sunday 6 July 1997
Time:16:50 LT
Type:Silhouette image of generic B722 model; specific model in this crash may look slightly different    
Boeing 727-247
Owner/operator:Delta Air Lines, Inc.
Registration: N2809W
MSN: 20581/890
Year of manufacture:1972
Total airframe hrs:9198 hours
Engine model:P&W JT8D-15A
Fatalities:Fatalities: 0 / Occupants: 156
Aircraft damage: Substantial
Category:Accident
Location:Albuquerque International Airport, NM (ABQ/KABQ) -   United States of America
Phase: Landing
Nature:Unknown
Departure airport:Dfw Airport, TX (DFW
Destination airport:(KABQ)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The Captain reported a normal flight and that the landing approach was stabilized. He stated that the wind was 'right down the runway for the landing.' As the airplane decelerated through 70 KIAS, the first officer reported hearing a 'loud bang,' and the airplane began 'listing heavily to the right and drifting to the right.' The pilots determined that the right main landing gear (MLG) had collapsed and an evacuation was ordered. The right MLG was last removed (18,188 cycles before the accident) for overhaul on April 8, 1988, and the right MLG forward trunnion bearing support fitting (FTBSF) was last ultrasonically inspected in May 1993 (7,634 cycles before the accident). A Service Bulletin, dated March 8, 1990, recommended that the MLG FTBSFs be ultrasonically inspected after 12,000 flight cycles every 6 months or 1,500 flight cycles, whichever occurred first. Operators were to continue this inspection cycle until the part was replaced or the preventative modification was done. The NTSB Materials Laboratory examined the broken right MLG FTBSF and determined that the failure was the result of stress corrosion cracking.

Probable Cause: The inadequate inspection of the right main landing gear forward trunnion bearing support fitting. Factors were the failure of the right main landing gear forward trunnion bearing support fitting and the subsequent right main landing gear failure.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: FTW97FA255
Status: Investigation completed
Duration: 2 years and 5 months
Download report: Final report

Sources:

NTSB FTW97FA255

Location

Revision history:

Date/timeContributorUpdates
07-Dec-2015 16:08 JINX Added
26-Nov-2016 21:34 TB Updated [Location, Narrative]
21-Dec-2016 19:30 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
08-Apr-2024 14:19 ASN Update Bot Updated [Time, Operator, Total occupants, Other fatalities, Nature, Departure airport, Destination airport, Source, Narrative, Category, Accident report]

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