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|
Attributes | |
ACN | 954741 |
Time | |
Date | 201106 |
Local Time Of Day | 1201-1800 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | B737-300 |
Operating Under FAR Part | Part 121 |
Flight Phase | Parked |
Flight Plan | IFR |
Component | |
Aircraft Component | Pneumatic Duct Fire/Overheat Warning |
Person 1 | |
Function | Captain |
Experience | Flight Crew Last 90 Days 194 |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural MEL Deviation - Procedural Published Material / Policy Inflight Event / Encounter Weather / Turbulence |
Narrative:
The same aircraft was assigned to us for three legs. We noted a MEL of the left wing body overheat sensor. After reviewing the MEL; I felt there was a potential safety problem; in that one system failure could cause several events; e.g.; if due to the fact we couldn't use APU except for start; and left pack shutdown; loss of right engine would cause de-pressurization for one; bird strike anyone? OAT in one destination was approaching 100 degree. I noted that all passengers leaving the aircraft; were either complaining of the heat in the aircraft (right pack only) and or some were rather pale and sweaty looking. Limited to 25;000 ft; with some thunderstorms along some of our routes; further limited options to us for safety of flight. After conferring with dispatch and the chief pilot; we determined for passenger/crew safety to remove the aircraft from service. Flight was subsequently cancelled. Passengers were accommodated on other flights. Some were upset and I'm sorry about that. However; I made this decision after weighing all parameters for safety of flight. Just because the MEL says it's okay; under certain situations; look a little closer at the implications of system failure related to that MEL.
Original NASA ASRS Text
Title: A Captain refused a B737-300 with a WING BODY OVERHEAT MEL because of passenger comfort with single pack operation in hot weather and a flight restricted to FL250 in thunderstorm conditions.
Narrative: The same aircraft was assigned to us for three legs. We noted a MEL of the left wing body overheat sensor. After reviewing the MEL; I felt there was a potential safety problem; in that one system failure could cause several events; e.g.; if due to the fact we couldn't use APU except for start; and left pack shutdown; loss of right engine would cause de-pressurization for one; bird strike anyone? OAT in one destination was approaching 100 degree. I noted that all passengers leaving the aircraft; were either complaining of the heat in the aircraft (right pack only) and or some were rather pale and sweaty looking. Limited to 25;000 FT; with some thunderstorms along some of our routes; further limited options to us for safety of flight. After conferring with Dispatch and the Chief Pilot; we determined for Passenger/Crew safety to remove the aircraft from service. Flight was subsequently cancelled. Passengers were accommodated on other flights. Some were upset and I'm sorry about that. However; I made this decision after weighing all parameters for safety of flight. Just because the MEL says it's okay; under certain situations; look a little closer at the implications of system failure related to that MEL.
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.