ASN Wikibase Occurrence # 368812
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Date: | Tuesday 9 May 1989 |
Time: | 15:30 LT |
Type: | Enstrom F-28C |
Owner/operator: | Fair, Fred |
Registration: | N88RA |
MSN: | 344 |
Total airframe hrs: | 688 hours |
Engine model: | LYCOMING HIO-360-E1AD |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Regina, NM -
United States of America
|
Phase: | Landing |
Nature: | Unknown |
Departure airport: | |
Destination airport: | |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:WHILE CONDUCTING A TEST FLT FOLLOWING REPAIRS TO THE TAIL ROTOR DUE TO AN EARLIER ACCIDENT THE PLT STRUCK THE TAIL ROTOR ON THE GROUND WHILE TRANSITIONING FROM FORWARD FLT TO A HOVER. THE GROUND CONTACT CAUSED THE TAIL ROTOR DRIVE SHAFT TO FAIL AND THE HELICOPTER SUSTAINED SUBSTANTIAL DAMAGE IN THE ENSUING CRASH. THE DENSITY ALTITUDE AT THE TIME OF THE ACCIDENT WAS CALCULATED TO BE 10,400 FT. THE ENSTROM F-28C OPERATORS HANDBOOK NOTES THAT THE GROUND EFFECT HOVER CEILING IS 8,800 FT.
Probable Cause: THE PILOT'S POORLY PLANNED APPROACH AND DISREGARD OF THE HELICOPTERS PERFORMANCE DATA. CONTRIBUTING TO THE ACCIDENT WAS THE HIGH DENSITY ALTITUDE CONDITIONS WHICH EXISTED AT THE TIME OF THE ACCIDENT.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | DEN89LA118 |
Status: | Investigation completed |
Duration: | 1 year and 2 months |
Download report: | Final report |
|
Sources:
NTSB DEN89LA118
History of this aircraft
Other occurrences involving this aircraft Location
Revision history:
Date/time | Contributor | Updates |
24-Mar-2024 07:41 |
ASN Update Bot |
Added |
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