Accident Rockwell Aero Commander 690A N55JS,
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ASN Wikibase Occurrence # 43985
 
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Date:Sunday 15 October 2006
Time:13:03
Type:Silhouette image of generic AC90 model; specific model in this crash may look slightly different    
Rockwell Aero Commander 690A
Owner/operator:Private
Registration: N55JS
MSN: 11195
Year of manufacture:1974
Total airframe hrs:7943 hours
Engine model:Honeywell Aerospace TPE33110T515K
Fatalities:Fatalities: 4 / Occupants: 4
Aircraft damage: Destroyed
Category:Accident
Location:Antlers, OK -   United States of America
Phase: En route
Nature:Private
Departure airport:Oklahoma City, OK (PWA)
Destination airport:Orlando, FL (ORL)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
Approximately 37 minutes after departing on a 928-nautical mile cross-country flight under instrument flight rules, the twin-engine turboprop airplane experienced an in-flight break-up after encountering moderate turbulence while in cruise flight at the assigned altitude of FL230. In the moments preceding the break-up, the airplane had been flying approximately 15 to 20 knots above the placarded maximum airspeed for operations in moderate turbulence. The airplane was found to be approximately 1,038 pounds over the maximum takeoff weight listed in the airplane's type certificate data sheet (TCDS). The last radar returns indicated that the airplane performed a 180-degree left turn while descending at a rate of approximately 13,500 feet per minute. There were no reported eyewitnesses to the accident. The wreckage was located the next day in densely wooded terrain. The wreckage was scattered over an area approximately three miles long by one mile wide. An examination of the airframe revealed that the airplane's design limits had been exceeded, and that the examined fractures were due to overload failure.
Probable Cause: The pilot's failure to reduce airspeed while operating in an area of moderate turbulence, resulting in an in-flight break up. Contributing factors were the pilot's decision to exceed the maximum takeoff weight, and the prevailing turbulence.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: DFW07FA004
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB: https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20061024X01554&key=1

Location

Revision history:

Date/timeContributorUpdates
28-Oct-2008 00:45 ASN archive Added
12-Feb-2012 01:24 Gwydd Updated [Aircraft type]
21-Dec-2016 19:24 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
05-Dec-2017 10:14 ASN Update Bot Updated [Operator, Other fatalities, Departure airport, Destination airport, Source, Narrative]

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