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|
Attributes | |
ACN | 1514077 |
Time | |
Date | 201801 |
Local Time Of Day | 1801-2400 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Light | Night |
Aircraft 1 | |
Make Model Name | Caravan 208B |
Operating Under FAR Part | Part 135 |
Flight Phase | Taxi |
Flight Plan | IFR |
Component | |
Aircraft Component | Throttle/Power Lever |
Person 1 | |
Function | Captain Pilot Flying |
Qualification | Flight Crew Commercial Flight Crew Flight Instructor Flight Crew Multiengine Flight Crew Instrument |
Experience | Flight Crew Last 90 Days 200 Flight Crew Total 2500 Flight Crew Type 1000 |
Events | |
Anomaly | Aircraft Equipment Problem Less Severe |
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.
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.