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Attributes | |
ACN | 121375 |
Time | |
Date | 198908 |
Day | Sun |
Local Time Of Day | 1801 To 2400 |
Place | |
Locale Reference | airport : 2w6 |
State Reference | MD |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Operator | general aviation : personal |
Make Model Name | Small Aircraft, High Wing, 1 Eng, Fixed Gear |
Flight Plan | None |
Aircraft 2 | |
Make Model Name | Small Aircraft |
Flight Phase | ground : parked |
Flight Plan | None |
Person 1 | |
Affiliation | Other |
Function | flight crew : single pilot oversight : pic |
Qualification | pilot : private |
Experience | flight time last 90 days : 17 flight time total : 305 flight time type : 33 |
ASRS Report | 121375 |
Events | |
Anomaly | aircraft equipment problem : less severe conflict : ground critical non adherence : far other anomaly |
Independent Detector | other flight crewa |
Resolutory Action | none taken : unable |
Consequence | other |
Supplementary | |
Primary Problem | Flight Crew Human Performance |
Air Traffic Incident | Pilot Deviation |
Narrative:
My airplane is a vintage small aircraft tail dragger and is not equipped with a starter. During preflight, I untied the airplane and left a chock in front of the left main wheel. I was alone during this incident. As soon as the engine started, the RPM increased to well above idle although the throttle control in the cockpit was definitely at the idle position. The airplane jumped the chock and began a turn to the left. My airplane hit another airplane before I could get to the cockpit and secure the engine. No one was injured. The cause of the high RPM at engine start was as follows. Earlier in the day I had removed the engine cowling to take measurements for a new throttle cable. I noticed that the clamp which secures the throttle cable was loosening and I tightened the clamp. The cable must have slipped forward, however, so that when the throttle control in the cockpit was at the idle position, the throttle arm on the carburetor was well above the idle position. My contributions to this incident were not having the airplane tied down for starting and not having an a&P mechanic inspect the throttle linkage after I noticed that the clamp was loosening.
Original NASA ASRS Text
Title: PLT OF VINTAGE TAIL DRAGGER WITHOUT STARTER WAS HANDPROPPING ACFT WITH ONLY THE LEFT MAIN WHEEL CHOCKED, RESULTING IN RUNAWAY ACFT WHICH DAMAGED ANOTHER PARKED ACFT.
Narrative: MY AIRPLANE IS A VINTAGE SMA TAIL DRAGGER AND IS NOT EQUIPPED WITH A STARTER. DURING PREFLT, I UNTIED THE AIRPLANE AND LEFT A CHOCK IN FRONT OF THE LEFT MAIN WHEEL. I WAS ALONE DURING THIS INCIDENT. AS SOON AS THE ENGINE STARTED, THE RPM INCREASED TO WELL ABOVE IDLE ALTHOUGH THE THROTTLE CONTROL IN THE COCKPIT WAS DEFINITELY AT THE IDLE POSITION. THE AIRPLANE JUMPED THE CHOCK AND BEGAN A TURN TO THE LEFT. MY AIRPLANE HIT ANOTHER AIRPLANE BEFORE I COULD GET TO THE COCKPIT AND SECURE THE ENGINE. NO ONE WAS INJURED. THE CAUSE OF THE HIGH RPM AT ENGINE START WAS AS FOLLOWS. EARLIER IN THE DAY I HAD REMOVED THE ENGINE COWLING TO TAKE MEASUREMENTS FOR A NEW THROTTLE CABLE. I NOTICED THAT THE CLAMP WHICH SECURES THE THROTTLE CABLE WAS LOOSENING AND I TIGHTENED THE CLAMP. THE CABLE MUST HAVE SLIPPED FORWARD, HOWEVER, SO THAT WHEN THE THROTTLE CONTROL IN THE COCKPIT WAS AT THE IDLE POSITION, THE THROTTLE ARM ON THE CARBURETOR WAS WELL ABOVE THE IDLE POSITION. MY CONTRIBUTIONS TO THIS INCIDENT WERE NOT HAVING THE AIRPLANE TIED DOWN FOR STARTING AND NOT HAVING AN A&P MECHANIC INSPECT THE THROTTLE LINKAGE AFTER I NOTICED THAT THE CLAMP WAS LOOSENING.
Data retrieved from NASA's ASRS site as of August 2007 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.