AN MD88 WAS DISPATCHED IN NON COMPLIANCE WITH THE INCORRECT RUDDER LIMITER ACTUATOR INSTALLED.
Synopsis
AN MD88 WAS DISPATCHED IN NON COMPLIANCE WITH THE INCORRECT RUDDER LIMITER ACTUATOR INSTALLED.
Narrative
WHILE WORKING ACFT Y INBOUND WRITE-UP 'UNRESTR RUDDER LIGHT FAILS TO COME ON UNTIL BELOW 144 KTS.' -- REMOVED AND REPLACED RUDDER LIMITER ACTUATOR ASSEMBLY. -- INSTALLED INCORRECT MANUFACTURER PART NUMBER Z EFFECTIVE FOR SHIPS X THROUGH Z. SHOULD HAVE INSTALLED MANUFACTURER PART NUMBER X OR Y. EFFECTIVE FOR SHIPS A-B. -- ADJUSTMENT TEST OF RUDDER SYSTEM MAINT MANUAL 27-20-06-201-2 WAS USED EFFECTIVE FOR A-B. -- THERE IS VISUALLY NO DIFFERENCE IN THE PARTS. -- THE ACR X REPAIR SHOP FOR THIS PART NOTICED THE EFFECTIVITY DIFFERENCES WHEN REPAIRING THE REMOVED ASSEMBLY. -- THE ACFT WAS RETURNED TO SVC WITH NO OTHER TROUBLE FROM THE RUDDER SYS. -- THE ACFT WAS ROUTED BACK FOR LIMITER ASSEMBLY REPLACEMENT UPON THE DISCOVERY OF THE INEFFECTIVE ASSEMBLY ON THE ACFT. ON AUG/FRI/03; I WAS INFORMED OF THE DISCREPANCY ON THIS DATE. SUPPLEMENTAL 591385: TO MY UNDERSTANDING; MY COMPANY IS CURRENTLY WORKING ON SOLUTIONS WITH THE COMPUTER PROGRAMS USED FOR THE M/M; IPC; AND PARTS ORDERING SYS TO AID IN PREVENTING THIS TYPE OF EVENT FROM HAPPENING. IN THE FUTURE; I WILL PERSONALLY REQUIRE THE IPC REF TO BE AVAILABLE DURING R11 OK TO INSTALL INSPECTIONS.
Source: NASA Aviation Safety Reporting System (public domain). Reports are voluntary submissions and are not verified by NASA.