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Attributes | |
ACN | 1302734 |
Time | |
Date | 201510 |
Local Time Of Day | 1801-2400 |
Place | |
Locale Reference | EMT.Airport |
State Reference | CA |
Environment | |
Flight Conditions | VMC |
Light | Dusk |
Aircraft 1 | |
Make Model Name | Cessna 150 |
Operating Under FAR Part | Part 91 |
Flight Phase | Initial Approach |
Route In Use | Visual Approach |
Flight Plan | None |
Component | |
Aircraft Component | Intake Ice System |
Person 1 | |
Function | Instructor Pilot Flying |
Qualification | Flight Crew Commercial Flight Crew Flight Instructor Flight Crew Instrument Flight Crew Multiengine |
Experience | Flight Crew Last 90 Days 191 Flight Crew Total 700 Flight Crew Type 65 |
Events | |
Anomaly | Aircraft Equipment Problem Less Severe Inflight Event / Encounter Weather / Turbulence |
Narrative:
I was providing primary flight instruction in a cessna 150. We were inbound to the airport from the south; and were directed by tower to enter left traffic for runway 19.at approximately 1400 feet MSL on the descent to traffic pattern altitude (1300 feet); I encountered a loss in RPM of approximately 500-600 RPM. At the time of the power loss; I had full power (2400 RPM) selected. Due to my low proximity to the ground; and the fact that runway 01 was almost directly in front of me; I elected to request a landing straight in to runway 01. I believed it to be carburetor icing; and I applied full carburetor heat. I knew that the carburetor on the O-200 engine on the cessna 150 is very susceptible to carb icing; and the relative humidity on this day was also unusually high (approx 80%). The conditions to form carburetor icing were set.following my landing on runway 01; I ran the engine up to full power; and the engine ran smooth; both with carb heat on and off. This confirmed by suspicion of carb ice. We taxied to the transient parking to shut down; and call the flight school to report it. We decided to go to the run up area and do another run up to check engine function. Engine ran fine; both with carb heat on and off. It was determined that the carb ice had been eliminated and the engine was running normally. I've encountered carburetor icing before. However; this is the first time I've encountered it at pattern altitude.having noticed that the humidity level was higher than normal; I should have been more proactive with use of the carburetor heat on descent; even while operating the engine within the parameters where the poh says it is normally not required.
Original NASA ASRS Text
Title: C150 Instructor Pilot reported encountering carburetor ice that resulted in a power loss in the pattern at EMT.
Narrative: I was providing primary flight instruction in a Cessna 150. We were inbound to the airport from the south; and were directed by Tower to enter left traffic for runway 19.At approximately 1400 feet MSL on the descent to traffic pattern altitude (1300 feet); I encountered a loss in RPM of approximately 500-600 RPM. At the time of the power loss; I had full power (2400 RPM) selected. Due to my low proximity to the ground; and the fact that runway 01 was almost directly in front of me; I elected to request a landing straight in to runway 01. I believed it to be carburetor icing; and I applied full carburetor heat. I knew that the carburetor on the O-200 engine on the Cessna 150 is very susceptible to carb icing; and the relative humidity on this day was also unusually high (approx 80%). The conditions to form carburetor icing were set.Following my landing on runway 01; I ran the engine up to full power; and the engine ran smooth; both with carb heat on and off. This confirmed by suspicion of carb ice. We taxied to the transient parking to shut down; and call the flight school to report it. We decided to go to the run up area and do another run up to check engine function. Engine ran fine; both with carb heat on and off. It was determined that the carb ice had been eliminated and the engine was running normally. I've encountered carburetor icing before. However; this is the first time I've encountered it at pattern altitude.Having noticed that the humidity level was higher than normal; I should have been more proactive with use of the carburetor heat on descent; even while operating the engine within the parameters where the POH says it is normally not required.
Data retrieved from NASA's ASRS site and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.