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|
Attributes | |
ACN | 928918 |
Time | |
Date | 201101 |
Local Time Of Day | 1801-2400 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Light | Daylight |
Aircraft 1 | |
Make Model Name | B737-800 |
Operating Under FAR Part | Part 121 |
Flight Phase | Parked |
Flight Plan | IFR |
Component | |
Aircraft Component | Rudder Control System |
Person 1 | |
Function | Captain |
Qualification | Flight Crew Air Transport Pilot (ATP) |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural Published Material / Policy |
Narrative:
Rudder balance arm -tungsten metal weight- corroded and pitted. Closer inspection showed surface no longer smooth; [it was] pitted and crumbling. Pieces crumbled into pilot's hand. No samples taken. Upon second request local maintenance would not provide access to get samples. Maintenance control provided detailed guidance and engineering release. Initial logbook release classified the rudder flight control balance arm as a 'nef' (non-essential function) item; applicable to 'paint' on fuselage and limited cabin items. Captain insisted on defining the flight control-rudder balance arm as a stand alone item requiring maintenance as such. Chief pilot on duty consulted with crew and concurred that departure was in compliance with air carrier procedures with an engineering release. Referred to channels for determination on acceleration of rust after teflon coating and paint departs from the rudder balance arm.
Original NASA ASRS Text
Title: A B737-800 Captain reports a rudder balance arm (weight) was found pitted; corroded and pieces crumbled in his hand. Captain refused the Non-Essential Function (NEF) deferral and insisted the rudder balance weight be defined as a stand alone item requiring maintenance.
Narrative: Rudder balance arm -tungsten metal weight- corroded and pitted. Closer inspection showed surface no longer smooth; [it was] pitted and crumbling. Pieces crumbled into pilot's hand. No samples taken. Upon second request local maintenance would not provide access to get samples. Maintenance Control provided detailed guidance and Engineering Release. Initial Logbook Release classified the rudder flight control balance arm as a 'NEF' (Non-Essential Function) item; applicable to 'paint' on fuselage and limited cabin items. Captain insisted on defining the Flight control-rudder balance arm as a stand alone item requiring maintenance as such. Chief Pilot on duty consulted with crew and concurred that departure was in compliance with Air Carrier procedures with an Engineering Release. Referred to channels for determination on acceleration of rust after Teflon coating and paint departs from the rudder balance arm.
Data retrieved from NASA's ASRS site as of April 2012 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.