Accident Piper PA-46-350P Malibu Mirage N133MA,
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ASN Wikibase Occurrence # 38465
 
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Date:Thursday 22 December 1994
Time:13:52 LT
Type:Silhouette image of generic PA46 model; specific model in this crash may look slightly different    
Piper PA-46-350P Malibu Mirage
Owner/operator:Ryders Replica Fighter Museum
Registration: N133MA
MSN: 4622133
Total airframe hrs:106 hours
Engine model:Lycoming TIO-540-AE2A
Fatalities:Fatalities: 3 / Occupants: 3
Aircraft damage: Destroyed
Category:Accident
Location:Rochester, MN -   United States of America
Phase: En route
Nature:Private
Departure airport:
Destination airport:Guntersville, AL (8A1
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
THE AIRPLANE DEPARTED ON RUNWAY 31 IN INSTRUMENT METEOROLOGICAL CONDITIONS (IMC) AND TURNED RIGHT TO A HEADING OF 090 DEGREES. RADAR CONTACT (ARTS TAG) WAS ACQUIRED ABOUT 1 TO 2 MILES NORTH OF THE AIRPORT. REPORTEDLY, THE ARTS TAG WOULD TYPICALLY BE ACQUIRED AS THE AIRPLANE CLIMBED THROUGH AN ALTITUDE OF ABOUT 700 FEET AGL. SUBSEQUENTLY, THE AIRPLANE CRASHED ABOUT 2 MILES NORTH OF THE AIRPORT. A WITNESS REPORTED HEARING A LOUD ENGINE NOISE BEFORE THE PLANE CRASHED. THE WRECKAGE PATH WAS ORIENTED ALONG A WESTERLY HEADING AND OVER AN AREA OF ABOUT 380 FEET. THERE WAS EVIDENCE OF AN IN-FLIGHT BREAKUP. AN OUTBOARD PORTION OF THE RIGHT WING WAS FOUND ABOUT 150 FEET FROM THE MAIN IMPACT CRATER. AN EXAMINATION REVEALED THE RIGHT WING HAD FAILED NEAR THE PRODUCTION SEAM. THE RIGHT SPAR EXHIBITED FEATURES 'TYPICAL OF AN UPWARD BENDING OVERSTRESS SEPARATION.' EXAMINATION REVEALED NO OTHER EVIDENCE OF PREIMPACT AIRCRAFT OR ENGINE MALFUNCTION. THE AIRPLANE'S GROSS WEIGHT WAS ESTIMATED TO BE ABOUT 4696 POUNDS; ITS MAX LIMIT WAS 4300 POUNDS. THE PILOT'S LOGBOOK INDICATED THAT HE HAD FLOWN ONLY 2 INSTRUMENT APPROACHES IN THE PREVIOUS 14 MONTHS.

Probable Cause: FAILURE OF THE PILOT TO MAINTAIN CONTROL OF THE AIRPLANE, WHILE CLIMBING IN INSTRUMENT METEOROLOGICAL CONDITIONS (IMC) AFTER TAKEOFF. FACTORS RELATED TO THE ACCIDENT WERE: FOG, LOW CEILING, THE PILOT'S LACK OF RECENT INSTRUMENT EXPERIENCE, AND THE EXCESSIVE GROSS WEIGHT OF THE AIRPLANE.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CHI95FA061
Status: Investigation completed
Duration: 7 months
Download report: Final report

Sources:

NTSB CHI95FA061

Location

Revision history:

Date/timeContributorUpdates
24-Oct-2008 10:30 ASN archive Added
21-Dec-2016 19:23 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
09-Apr-2024 17:42 ASN Update Bot Updated [Time, Other fatalities, Destination airport, Source, Narrative, Category, Accident report]

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