Narrative:

Reference engine #1 thrust reverser inoperative. MEL. The procedure requires sync lock; thrust reverser control and indication circuit breakers to be pulled. Engine sync lock circuit breaker is labeled indicating which engine #1 or #2; but cont and ind circuit breakers are not labeled which engine they belong to on the P6-2 panel. If the incorrect circuit breaker was inadvertently pulled; both reversers wouldn't work. After talking with line maintenance we both felt the MEL card should be more descriptive and the P6-2 panel should be placarded to indicate which engine is associated with the cont and ind circuit breakers. I also just talked to maintenance headquarters and he also said this deferral is confusing. Just something to consider from a safety perspective.

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Original NASA ASRS Text

Title: THE B737-300 MEL PROC FOR DEFERRING A THRUST REVERSER REQUIRES CIRCUIT BREAKERS TO BE PULLED AND LOCKED. ALL BREAKERS LABELED PER ENG EXCEPT CTL AND INDICATION ON P6-2 PANEL.

Narrative: REF ENG #1 THRUST REVERSER INOP. MEL. THE PROC REQUIRES SYNC LOCK; THRUST REVERSER CONTROL AND INDICATION CIRCUIT BREAKERS TO BE PULLED. ENG SYNC LOCK CIRCUIT BREAKER IS LABELED INDICATING WHICH ENG #1 OR #2; BUT CONT AND IND CIRCUIT BREAKERS ARE NOT LABELED WHICH ENG THEY BELONG TO ON THE P6-2 PANEL. IF THE INCORRECT CIRCUIT BREAKER WAS INADVERTENTLY PULLED; BOTH REVERSERS WOULDN'T WORK. AFTER TALKING WITH LINE MAINT WE BOTH FELT THE MEL CARD SHOULD BE MORE DESCRIPTIVE AND THE P6-2 PANEL SHOULD BE PLACARDED TO INDICATE WHICH ENG IS ASSOCIATED WITH THE CONT AND IND CIRCUIT BREAKERS. I ALSO JUST TALKED TO MAINT HEADQUARTERS AND HE ALSO SAID THIS DEFERRAL IS CONFUSING. JUST SOMETHING TO CONSIDER FROM A SAFETY PERSPECTIVE.

Data retrieved from NASA's ASRS site as of January 2009 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.