ASN Wikibase Occurrence # 263551
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| Date: | Wednesday 2 June 2021 |
| Time: | 07:00 LT |
| Type: |  Cessna 172G Skyhawk |
| Owner/operator: | Alexander J. Hyatt Jr |
| Registration: | N3871L |
| MSN: | 17254040 |
| Year of manufacture: | 1965 |
| Total airframe hrs: | 3981 hours |
| Engine model: | Continental O-300-D |
| Fatalities: | Fatalities: 0 / Occupants: 2 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | Nevada County NW of Immigrant Gap, CA -
 United States of America
|
| Phase: | En route |
| Nature: | Private |
| Departure airport: | Yuba City, CA (O52) |
| Reno/Tahoe International Airport, NV (RNO/KRNO) | |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
The pilot reported that he was climbing the airplane at full engine power and an airspeed of 80 mph, and he had progressively leaned the fuel/air mixture during the climb. About 6,000 ft mean sea level (msl), he noted that the the engine oil temperature was indicating its maximum limit of 240°F. The pilot lowered the nose to increase airspeed and reduced engine power to cool the engine. About 10 minutes later, the engine oil temperature decreased below redline and he resumed his climb with a slightly richer mixture setting. About 8,500 ft msl, the engine produced a “backfire' sound, the engine rpm decreased, and a loss of engine power ensued. The pilot declared an emergency and performed a forced landing to mountainous terrain, during which the airplane sustained substantial damage.
Examination of the engine revealed that the No. 2 cylinder's piston exhibited a stuck top compression ring. The No. 3 cylinder exhibited a stuck exhaust valve, and the No. 3 piston's top compression ring had separated into two. The No. 5 intake valve exhibited excessive clearance within its guide. The No. 6 cylinder's piston top compression ring had separated into four pieces.
A review of the airframe and engine maintenance logbooks indicated that the last annual inspection was completed 6 months before the accident. At the time of the annual inspection, the engine had amassed a total time of 4,027 hours, and 1,896 hours since major overhaul. The engine tachometer indicated 2,277 hours during the last annual inspection and indicated 2,288.8 at the time of the accident. The engine-manufacturer recommended overhaul interval is 1,800 hours or 12 years, whichever occurs first.
Probable Cause: A total loss of engine power during an enroute climb due to a stuck exhaust valve and multiple failed piston compression rings.
Accident investigation:
 |
|
Sources:
NTSB WPR21LA224
FAA register: https://registry.faa.gov/aircraftinquiry/Search/NNumberResult?NNumberTxt=3871L
https://flightaware.com/live/flight/N3871L
History of this aircraft
Other occurrences involving this aircraft
| 21 November 1986 | N3871L | Private | 0 | Evansville, IN | |
sub |
Location
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 02-Jun-2021 21:29 | Geno | Added |
| 03-Jun-2021 02:11 | Geno | Updated [Aircraft type, Registration, Cn, Operator, Departure airport, Destination airport, Source] |
| 03-Jun-2021 14:01 | RobertMB | Updated [Registration, Nature, Source, Narrative] |
| 06-Jun-2021 20:14 | Geno | Updated [Source, Narrative] |
| 16-Jun-2023 12:35 | ASN Update Bot | Updated [[Source, Narrative]] |
Corrections or additions? ... Edit this accident description
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