REG NASA-LLIS-0001-1991 Lessons Learned - Implementation of Procedural Controls in Additional Procedures Beyond the Procedure Under Investigation and Correction.pdf
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1、Lessons Learned Entry: 0001Lesson Info:a71 Lesson Number: 0001a71 Lesson Date: 1991-04-10a71 Submitting Organization: JSCa71 Submitted by: L. UnderwoodSubject: Implementation of Procedural Controls in Additional Procedures Beyond the Procedure Under Investigation and Correction Description of Drivin
2、g Event: During prelaunch check out of shuttle orbiter OV-104 for flight STS-36, the AC2 buss phase a voltage fluctuated between 112 and 122V for one minute. The inverter supplying that buss was removed and replaced. The vendors inspection of the failed inverter found loose mounting screws on the el
3、ectrical buss internal to the inverter, which caused the voltage fluctuations. An identical problem had been previously discovered that prompted a change to the manufacturing procedures to include a specified torque for the mounting screws. The failed flight unit had been reworked, but the manufactu
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