ASN Wikibase Occurrence # 38557
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: | Tuesday 1 March 1994 |
| Time: | 13:15 LT |
| Type: |  Cessna P210R |
| Owner/operator: | Weiser, Joel J. |
| Registration: | N55MM |
| MSN: | P21000874 |
| Total airframe hrs: | 882 hours |
| Engine model: | CONTINENTAL TSIO-520-CE1F |
| Fatalities: | Fatalities: 4 / Occupants: 4 |
| Aircraft damage: | Destroyed |
| Category: | Accident |
| Location: | Bay Minette, AL -
 United States of America
|
| Phase: | En route |
| Nature: | Executive |
| Departure airport: | New Orleans, LA (NEW |
| Sarasota, FL (61X) | |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
THE PILOT RECEIVED A FULL WEATHER BRIEFING BEFORE THE IFR FLIGHT. CONVECTIVE THUNDERSTORM ACTIVITY WAS FORECAST FOR THE ROUTE OF FLIGHT, THERE WERE NUMEROUS THUNDERSTORMS IN THE AREA AT THE TIME OF DEPARTURE, AND A TORNADO WATCH WAS IN EFFECT AT THE TIME OF THE ACCIDENT. AFTER LEVELING AT FL210, HE REPORTED THAT CONDITIONS WERE 'GETTING ROUGH.' SHORTLY THEREAFTER, HE REPORTED PROBLEMS WITH THE AIRCRAFT GYRO SYSTEM, THEN SAID ALL GYRO'S WERE 'OUT.' HE ELECTED TO DESCEND IN AN ATTEMPT TO LOCATE VFR WEATHER. AS THE AIRCRAFT DESCENDED, RADIO & RADAR CONTACT WERE LOST. WRECKAGE WAS FOUND DISTRIBUTED OVER AN AREA ABOUT 4-1/2 MILES IN LENGTH. AN EXAM OF THE WRECKAGE REVEALED EVIDENCE THAT THE WINGS HAD FAILED IN AN UPWARD DIRECTION. DURING AN EXAM OF THE VACUUM POWERED ATTITUDE GYRO, NO ROTATIONAL SCRATCHING WAS FOUND ON THE GYRO OR IN THE GYRO HOUSING. AN EXAM OF THE LEFT VACUUM PUMP REVEALED THAT THE PLASTIC DRIVE COUPLING HAD SIGNS OF HEAT STRESS & MELTING, THAT THE INTERNAL VEINS WERE BROKEN & CRACKED & THAT THERE WAS A DEPOSIT OF CARBON MATERIAL INSIDE THE HOUSING. THE RIGHT VACUUM PUMP HAD EVIDENCE OF ROTATIONAL SCRATCHING. THE GYROS SHOULD HAVE OPERATED WITH 1 VACUUM PUMP IN OPERATION.
Probable Cause: THE PILOT'S FAILURE TO MAINTAIN CONTROL OF THE AIRCRAFT DUE TO SPATIAL DISORIENTATION, AND EXCEEDING THE DESIGN STRESS LIMITS OF THE AIRCRAFT. FACTORS RELATED TO THE ACCIDENT WERE: THE PILOT'S FLIGHT INTO KNOWN ADVERSE WEATHER CONDITIONS, OVERCONFIDENCE IN HIMSELF AND THE AIRPLANE, FAILURE OF THE LEFT VACUUM PUMP, PARTIAL LOSS OF THE VACUUM SYSTEM, AND AN INOPERATIVE ATTITUDE INDICATOR.
Accident investigation:
 |
|
Sources:
NTSB ATL94FA056
Location
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 24-Oct-2008 10:30 | ASN archive | Added |
| 21-Dec-2016 19:23 | ASN Update Bot | Updated [Time, Damage, Category, Investigating agency] |
| 10-Apr-2024 08:41 | ASN Update Bot | Updated [Time, Operator, Other fatalities, Departure 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:
| ASN Home | Send Correction / Feedback |
| FSF Home | Disclaimer | Copyright |
| Contact Us | Privacy Policy |
| Press / Media |
CONNECT WITH US:
©2024 Flight Safety Foundation