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|
Attributes | |
ACN | 412227 |
Time | |
Date | 199808 |
Day | Sun |
Local Time Of Day | 0001 To 0600 |
Place | |
Locale Reference | airport : zzz |
State Reference | US |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Light | Night |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | DC-10 10 |
Operating Under FAR Part | Part 121 |
Flight Phase | other |
Flight Plan | None |
Person 1 | |
Affiliation | company : air carrier |
Function | other personnel other |
Qualification | other other : other |
ASRS Report | 412227 |
Person 2 | |
Affiliation | company : air carrier |
Function | other personnel other |
Qualification | other other : other |
Events | |
Anomaly | non adherence : published procedure other anomaly other |
Independent Detector | other other : unspecified |
Resolutory Action | none taken : detected after the fact |
Consequence | Other |
Supplementary | |
Air Traffic Incident | other |
Narrative:
During a normal service check of a DC10 aircraft, the #2 hydraulic accumulator was found to be leaking internally requiring replacement. This unit is in the left main landing gear well and accessing it requires lowering the fuselage mounted landing gear door. The accumulator was replaced and I proceeded to resvc the system fluid. I understood my lead mechanic to advise servicing with the system pressurized. In order to gain access to the service point, also in the left gear well, I climbed into the wheel well above the now open door with pressure on the hydraulic system and no downlock on the door actuator. This was a very dangerous act and in doing so put myself at risk of injury or death if the door had closed for any reason.
Original NASA ASRS Text
Title: A MECH WORKING IN THE L WHEEL WELL OF A DC10 WITH NO DOOR LOCKS INSTALLED AND ACFT HYD SYS PRESSURIZED ENDANGERED THE RPTR'S SAFETY AND OTHERS WORKING NEARBY.
Narrative: DURING A NORMAL SVC CHK OF A DC10 ACFT, THE #2 HYD ACCUMULATOR WAS FOUND TO BE LEAKING INTERNALLY REQUIRING REPLACEMENT. THIS UNIT IS IN THE L MAIN LNDG GEAR WELL AND ACCESSING IT REQUIRES LOWERING THE FUSELAGE MOUNTED LNDG GEAR DOOR. THE ACCUMULATOR WAS REPLACED AND I PROCEEDED TO RESVC THE SYS FLUID. I UNDERSTOOD MY LEAD MECH TO ADVISE SVCING WITH THE SYS PRESSURIZED. IN ORDER TO GAIN ACCESS TO THE SVC POINT, ALSO IN THE L GEAR WELL, I CLBED INTO THE WHEEL WELL ABOVE THE NOW OPEN DOOR WITH PRESSURE ON THE HYD SYS AND NO DOWNLOCK ON THE DOOR ACTUATOR. THIS WAS A VERY DANGEROUS ACT AND IN DOING SO PUT MYSELF AT RISK OF INJURY OR DEATH IF THE DOOR HAD CLOSED FOR ANY REASON.
Data retrieved from NASA's ASRS site as of July 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.