ASN Wikibase Occurrence # 385891
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Date: | Friday 18 May 2001 |
Time: | 10:00 LT |
Type: | Robinson R22 |
Owner/operator: | Private |
Registration: | N7087X |
MSN: | 2829 |
Year of manufacture: | 1998 |
Total airframe hrs: | 488 hours |
Engine model: | Lycoming O-360 |
Fatalities: | Fatalities: 0 / Occupants: 2 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Raymondville, TX -
United States of America
|
Phase: | Manoeuvring (airshow, firefighting, ag.ops.) |
Nature: | Private |
Departure airport: | Raymondville, TX (NONE) |
Destination airport: | |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The helicopter had been in flight for approximately 5 minutes when the main rotor rpm began to decrease. The "clutch light" illuminated and the "low rotor horn sounded." The pilot initiated an autorotation to an open field; however, he did "not have enough altitude" to clear some trees. The helicopter contacted the trees and impacted the ground "hard." The main rotor drive belts were found separated from the drive wheels. An examination of the helicopter by an aircraft mechanic and an FAA inspector revealed that the drive belts were "frayed and ripped." No anomalies were noted with the rest of the drive system. The helicopter was issued an airworthiness certificate on May 27, 1998. Review of the helicopter's maintenance records revealed that it had undergone its last annual inspection on February 10, 2001, at an aircraft total time of 409.2 hours. There was no record of the drive belts being replaced during the life of the helicopter. According to the helicopter manufacturer, the drive belts are to be changed on condition, and there is no life limit on the belts; however, the belts usually get replaced during the helicopter's 2,200-hour overhaul. At the time of the accident, the helicopter had accumulated a total of 488 hours.
Probable Cause: the failure of the main rotor drive belts while maneuvering which resulted in a loss of main rotor drive. A contributing factor was the lack of suitable terrain for the forced landing.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | FTW01LA124 |
Status: | Investigation completed |
Duration: | 4 months |
Download report: | Final report |
|
Sources:
NTSB FTW01LA124
History of this aircraft
Other occurrences involving this aircraft Location
Revision history:
Date/time | Contributor | Updates |
05-Apr-2024 08:58 |
ASN Update Bot |
Added |
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