ASN Wikibase Occurrence # 141926
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Date: | Friday 13 January 2012 |
Time: | 17:50 |
Type: | Cessna 150M |
Owner/operator: | Prairie Air Service Inc |
Registration: | N714BS |
MSN: | 15079055 |
Year of manufacture: | 1976 |
Total airframe hrs: | 10375 hours |
Engine model: | Continental O-200 SERIES |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | El Dorado, KS -
United States of America
|
Phase: | En route |
Nature: | Private |
Departure airport: | Benton, KS (1K1) |
Destination airport: | Benton, KS (1K1) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot was on a local flight and the airplane had climbed to an altitude of about 10,700 feet. The pilot reduced the power and established a glide. At an altitude of about 8,000 feet, he advanced the throttle, but the engine only reached about 1,500 rpm. He checked the throttle and mixture controls and applied carburetor heat; however, the engine rpm kept getting lower. During the forced landing in a field, the airplane impacted an embankment and nosed over, coming to rest inverted. An examination of the engine failed to identify any anomalies that would account for a loss of power. A review of the carburetor icing probability chart revealed that the weather conditions were just outside favorable conditions for the formation of carburetor icing. Additionally, the air temperature and moisture content at 8,000- to 12,000-feet altitude were not conducive to carburetor icing. A review of Transport Canada’s publication, TP10737, “The use of automobile gasoline (Mogas) in Aviation,” dated March 31, 1993, noted that, “Mogas is generally higher in volatility than Avgas [aviation gas]. Mogas will thus absorb more heat from the mixing air when vaporizing, resulting in ice accumulation at higher ambient temperatures. The likelihood of carburetor icing while flying on Mogas is higher.” Despite the low power setting during the glide and the use of Mogas, the weather conditions near the accident site did not appear to be favorable for the formation of carburetor icing. The reason for the loss of engine power could not be determined.
Probable Cause: The loss of engine power for reasons that could not be determined because postaccident examination of the airframe and engine did not reveal any anomalies that would have precluded normal operation.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | CEN12LA135 |
Status: | Investigation completed |
Duration: | 11 months |
Download report: | Final report |
|
Sources:
NTSB
Location
Revision history:
Date/time | Contributor | Updates |
17-Jan-2012 17:08 |
Geno |
Added |
20-Jan-2012 17:26 |
Geno |
Updated [Time, Phase, Nature, Source, Narrative] |
21-Dec-2016 19:26 |
ASN Update Bot |
Updated [Time, Damage, Category, Investigating agency] |
27-Nov-2017 17:53 |
ASN Update Bot |
Updated [Operator, Other fatalities, Nature, Departure airport, Destination airport, Source, Narrative] |
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