ASN Wikibase Occurrence # 355533
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Date: | Saturday 19 July 1997 |
Time: | 14:30 LT |
Type: | Revolution Mini-500 |
Owner/operator: | Private |
Registration: | N500XM |
MSN: | 180 |
Year of manufacture: | 1997 |
Total airframe hrs: | 23 hours |
Engine model: | Rotax 582 |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Ava, MO -
United States of America
|
Phase: | Landing |
Nature: | Private |
Departure airport: | Cabool, MO (KTVB) |
Destination airport: | (KAOV) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot was completing a series of flight tests that involved transitions from cruise flight into a hover. The pilot reported the exhaust gas temperature (EGT) was higher in cruise flight than when hovering and that the EGT cooled rapidly when the helicopter went from cruise flight into the hovering maneuver. The pilot stated that approximately two miles from his destination, at 2,500 feet mean sea level (msl), he began a 200 to 300 foot/min descent to reach the airport's traffic pattern altitude. He said that as soon as the descent was initiated he experienced unusual engine noises and an abrupt loss of engine power. He lowered the collective and applied full power, but received no indication of engine power. He then initiated an autorotation to landing on a field with a 30-degree slope. Upon landing, the aircraft rolled over and came to rest on its port side causing the rotor to impact the tail boom. Examination of the engine showed evidence that the engine had seized during flight. Inspection of the fuel metering system showed that the accident airplane had not complied with Revolution Helicopter Service Information Letter number 042696, which requires the original factory carburetor jet setting to be adjusted to insure that the EGT be between 1,000 and 1,150 degrees Fahrenheit. No engine coolant was found in the coolant tank and the coolant hose tee was found to be deformed and leaking fluid.
Probable Cause: Loss of engine power due to loss of engine cooling fluid. Related factors were maintenance service bulletin not complied with by the owner/pilot mechanic resulting in low output of the carburetor, and unsuitable terrain.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | CHI97LA222 |
Status: | Investigation completed |
Duration: | 2 years and 6 months |
Download report: | Final report |
|
Sources:
NTSB CHI97LA222
Location
Revision history:
Date/time | Contributor | Updates |
12-Mar-2024 13:00 |
ASN Update Bot |
Added |
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