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ASN Wikibase Occurrence # 44926
Last updated: 3 June 2020
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Date:23-FEB-2004
Time:08:49
Type:Silhouette image of generic PA46 model; specific model in this crash may look slightly different
Piper PA-46-310P Malibu
Owner/operator:Private
Registration: N9103Z
C/n / msn: 4608028
Fatalities:Fatalities: 2 / Occupants: 2
Other fatalities:0
Aircraft damage: Written off (damaged beyond repair)
Category:Accident
Location:Arlington, AL -   United States of America
Phase: Manoeuvring (airshow, firefighting, ag.ops.)
Nature:Private
Departure airport:Panama City, FL (PFN)
Destination airport:Tulsa, OK (RVS)
Investigating agency: NTSB
Narrative:
The pilot received a preflight briefing from the Gainesville Automated Flight Service Station before departing on the instrument flight. The briefer advised the pilot of the potential for occasional moderate turbulence between 24,000 and 37,000 feet and on the current Convective SIGMET for embedded thunderstorms over southern Mississippi. The flight was in cruise flight at 24, 000 feet when the airplane encountered moderate to severe turbulence and heavy rain. The airplane descended from 24,000 feet to 3,100 feet in a descending right turn in 2 minutes and 10 seconds before radar contact was lost. The airplane was located 8 hours 26 minutes after the accident along a crash debris line that extended between 1.31 miles and 1.53 miles northwest of Arlington, Alabama. Airframe components recovered from the accident site were submitted to the NTSB Materials laboratory for examination. The examinations revealed all failures were consistent with overstress fracturing and there was no evidence of pre-existing conditions or fatigue damage. Examination of the airframe revealed that the airframe design limits were exceeded. The Pilot's Operating Handbook states the maximum structural cruising speed is 173 knots indicated airspeed or 170 knots calibrated airspeed. The co-pilot airspeed indicator at the crash site indicated 180 knots calibrated airspeed. The design maneuvering speed is 135 knots indicated airspeed or 133 knots calibrated airspeed.




Probable Cause: The pilots inadequate in-flight planning/decision and his failure to maintain aircraft control, resulting in an in-flight encounter with a thunderstorm and exceeding the design limits of the aircraft.

Sources:

NTSB: https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20040305X00268&key=1


Revision history:

Date/timeContributorUpdates
28-Oct-2008 00:45 ASN archive Added
21-Dec-2016 19:24 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
07-Dec-2017 17:41 ASN Update Bot Updated [Operator, Source, Narrative]

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