Accident Aero Commander 500A N9382R,
ASN logo
ASN Wikibase Occurrence # 354504
 
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:Saturday 9 May 1998
Time:12:05 LT
Type:Silhouette image of generic AC50 model; specific model in this crash may look slightly different    
Aero Commander 500A
Owner/operator:Corporate Air
Registration: N9382R
MSN: 500A-899-8
Year of manufacture:1960
Total airframe hrs:15233 hours
Engine model:Lycoming IO-540-E1A5
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Billings, MT -   United States of America
Phase: Initial climb
Nature:Ferry/positioning
Departure airport:
Destination airport:Minot, ND (KMOT)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot reported that, after takeoff, the left-main landing gear would not fully retract. The pilot stated that he then extended the landing gear and performed various emergency procedures in an attempt to fully extend the left-main. The pilot was unable to get the left-main to lock in the down position and elected to land the airplane with the right-main and nosewheel extended. During the landing roll, the left-main gear collapsed and the airplane slid to a stop. Inspection of the left-main landing gear revealed that the upper-main landing gear strut's outer-body to inner-body needle bearing had failed, and the lower needle bearing was near failure. The lack of lubrication in this area was noted, along with evidence of severe corrosion development. The Manufacturer's Inspection Program for this model aircraft does not address a calendar and/or time inspection interval, or lubrication interval for the upper and lower needle bearing.

Probable Cause: Failure of the main landing gear strut outer-body to inner-body needle bearing from the lack of lubrication and the development of corrosion. An inadequate manufacturer's inspection program was a factor.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: SEA98LA073
Status: Investigation completed
Duration: 2 years and 9 months
Download report: Final report

Sources:

NTSB SEA98LA073

Revision history:

Date/timeContributorUpdates
11-Mar-2024 15:13 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