ASN Wikibase Occurrence # 37255
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 19 December 1992 |
Time: | 09:39 LT |
Type: | Beechcraft 65 Queen Air |
Owner/operator: | Edwards, William J. |
Registration: | N555GC |
MSN: | LC-164 |
Year of manufacture: | 1965 |
Total airframe hrs: | 3700 hours |
Engine model: | Lycoming IGSO-480-A1E6 |
Fatalities: | Fatalities: 5 / Occupants: 5 |
Aircraft damage: | Destroyed |
Category: | Accident |
Location: | 30 km from Orlando-Sanford, FL -
United States of America
|
Phase: | En route |
Nature: | Private |
Departure airport: | Sanford, FL (KSFB) |
Destination airport: | Fort Lauderdale, FL |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:PLT REPORTED LEVEL AT 6,000 FT; NO FURTHER TRANSMISSIONS WERE RECEIVED. RADAR DATA SHOWS THAT AFTER 5 MIN AT CRUISE FLT GROUNDSPEED BEGAN TO SLOW, AND AS SPEED REACHED 85 KTS (VMC IS 83 KTS) ACFT MADE A RAPID TURN TO THE LEFT AND THE SPEED DROPPED TO 74 KTS. RADAR CONTACT WAS THEN LOST. WITNESSES REPORTED HEARING AND SEEING ACFT WITH AN ENG SPUTTERING AND QUITTING, AT WHICH TIME NO ENG NOISE WAS AUDIBLE. ENG WOULD THEN RESTART, AND AT ONE POINT ACFT WAS OBSERVED INITIATING A CLIMB AFTER ENG START. ENG RESTARTED AND OBTAINED NEAR FULL POWER, AND A SHORT TIME LATER SOUND OF IMPACT WAS HEARD. THE LEFT ENG FUEL SERVO WAS FOUND CONTAMINATED WITH CORROSION AND DIRT, AND WOULD NOT ALLOW FUEL FLOW TO THE ENG. THE FUEL STRAINER FOR THIS ENG WAS INSTALLED BACKWARDS ALLOWING UNFILTERED FUEL TO ENTER THE ENG. THE LEFT PROPELLER WAS NOT FEATHERED AND HAD NO SIGNS OF ROTATION UNDER POWER. RIGHT ENG FUEL SERVO ALSO CONTAINED CORROSION & CONTAMINATION. THE AIRCRAFT DID NOT HAVE A CURRENT ANNUAL INSPECTION.
Probable Cause: THE PILOT'S FAILURE TO FEATHER THE PROPELLER TO MAINTAIN ALTITUDE FOLLOWING A LOSS OF POWER OF THE LEFT ENGINE. THE POWER LOSS WAS DUE TO AN IMPROPERLY MAINTAINED FUEL SYSTEM. IN ADDITION, THE RIGHT ENGINE LOST POWER FOR AN UNDETERMINED REASON(S).
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | MIA93FA031 |
Status: | Investigation completed |
Duration: | 9 months |
Download report: | Final report |
|
Sources:
NTSB MIA93FA031
Revision history:
Date/time | Contributor | Updates |
24-Oct-2008 10:30 |
ASN archive |
Added |
13-Mar-2015 21:45 |
wf |
Updated [Operator, Location, Phase, Source] |
21-Dec-2016 19:23 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
10-Apr-2024 16:16 |
ASN Update Bot |
Updated [Time, Operator, Other fatalities, Phase, Departure airport, Destination airport, Source, Narrative, Accident report] |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation