Narrative:

After landing and taxi; the fuel condition lever slipped past the detent when low idle was selected. Fuel flow decreased to the point that the engine flamed-out. Smoke was then observed from the engine cowling so airport rescue and fire fighting; (arff) was requested and the passenger was escorted to the terminal building. The inadvertent engine shutdown after landing has highlighted a hazard with the condition lever in that it does not position into the notch (which is worn) on the detent. Additionally; the lever arm rests in the middle of the travel and strikes the left edge of the detent and halfway across the lever arm. In a video of what happens when the condition lever is moved quickly from high to low idle; a secondary movement of the condition lever is not required to bypass the detent. The condition lever easily rides smoothly over the detent essentially unnoticeable. To exacerbate the hazard; there is a rubber shield covering the travel that needs to be lifted out of position to visibly confirm position in relation to the detent.this airplane does not have a positive low idle stop/lever; as do other aircraft in our fleet. Had one been installed this event would not have occurred. There should be continuity in equipment within our fleet. Otherwise; this hazard will be present itself in the future.

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Original NASA ASRS Text

Title: Cessna Caravan Captain reported that the fuel condition lever slipped past the detent when low idle was selected; causing the engine to shut-down; and the engine cowling filling with smoke.

Narrative: After landing and taxi; the fuel condition lever slipped past the detent when low idle was selected. Fuel flow decreased to the point that the engine flamed-out. Smoke was then observed from the engine cowling so Airport Rescue and Fire Fighting; (ARFF) was requested and the passenger was escorted to the terminal building. The inadvertent engine shutdown after landing has highlighted a hazard with the condition lever in that it does not position into the notch (which is worn) on the detent. Additionally; the lever arm rests in the middle of the travel and strikes the left edge of the detent and halfway across the lever arm. In a video of what happens when the condition lever is moved quickly from high to low idle; a secondary movement of the condition lever is not required to bypass the detent. The condition lever easily rides smoothly over the detent essentially unnoticeable. To exacerbate the hazard; there is a rubber shield covering the travel that needs to be lifted out of position to visibly confirm position in relation to the detent.This airplane does not have a positive low idle stop/lever; as do other aircraft in our fleet. Had one been installed this event would not have occurred. There should be continuity in equipment within our fleet. Otherwise; this hazard will be present itself in the future.

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.