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|
Attributes | |
ACN | 427637 |
Time | |
Date | 199902 |
Day | Wed |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : ord |
State Reference | IL |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tower : stl |
Operator | common carrier : air carrier |
Make Model Name | B757-200 |
Navigation In Use | Other |
Flight Phase | ground : preflight |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
ASRS Report | 427637 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : commercial |
ASRS Report | 427638 |
Events | |
Anomaly | aircraft equipment problem : less severe non adherence : far non adherence other other anomaly other |
Independent Detector | other flight crewa other other : unspecified |
Resolutory Action | none taken : anomaly accepted |
Consequence | Other |
Supplementary | |
Air Traffic Incident | other |
Situations | |
Publication | Unspecified |
Narrative:
Trip ord to sna scheduled for XA50 departure. Logbook was placarded left main fuel quantity gauge. MEL states that after each refueling the total fuel quantity in all tanks containing fuel is verified by measuring sticks. MEL goes on to state that placards will be installed on captain's instrument panel and on the wing fueling panel to read 'fuel quantity in all tanks containing fuel must be verified by measuring sticks and verified by cockpit crew members.' verification by measuring sticks is not a realistic, timely option -- at least in ord and sna. Aircraft must be 0 degrees pitch and roll using aircraft inclinometer and a plumb bob. No such plumb bob could be found in either ord or sna. Using measuring sticks is quick and straight forward but verifying aircraft pitch and roll to 0 degrees is not timely or realistic. I feel the procedure in the MEL is not clear nor necessarily correct. I believe I made a mistake using the xfeed system to empty and refill the left main tank to verify quantity.
Original NASA ASRS Text
Title: A B757-200 PIC RPT ON THE INADEQUACIES OF THE MEL REGARDING MEASURING STICK USE FOR INOP MAIN FUEL GAUGES. NECESSARY GND SUPPORT EQUIP NOT FOUND AT SNA, CA, NOR AT ORD, IL.
Narrative: TRIP ORD TO SNA SCHEDULED FOR XA50 DEP. LOGBOOK WAS PLACARDED L MAIN FUEL QUANTITY GAUGE. MEL STATES THAT AFTER EACH REFUELING THE TOTAL FUEL QUANTITY IN ALL TANKS CONTAINING FUEL IS VERIFIED BY MEASURING STICKS. MEL GOES ON TO STATE THAT PLACARDS WILL BE INSTALLED ON CAPT'S INST PANEL AND ON THE WING FUELING PANEL TO READ 'FUEL QUANTITY IN ALL TANKS CONTAINING FUEL MUST BE VERIFIED BY MEASURING STICKS AND VERIFIED BY COCKPIT CREW MEMBERS.' VERIFICATION BY MEASURING STICKS IS NOT A REALISTIC, TIMELY OPTION -- AT LEAST IN ORD AND SNA. ACFT MUST BE 0 DEGS PITCH AND ROLL USING ACFT INCLINOMETER AND A PLUMB BOB. NO SUCH PLUMB BOB COULD BE FOUND IN EITHER ORD OR SNA. USING MEASURING STICKS IS QUICK AND STRAIGHT FORWARD BUT VERIFYING ACFT PITCH AND ROLL TO 0 DEGS IS NOT TIMELY OR REALISTIC. I FEEL THE PROC IN THE MEL IS NOT CLR NOR NECESSARILY CORRECT. I BELIEVE I MADE A MISTAKE USING THE XFEED SYS TO EMPTY AND REFILL THE L MAIN TANK TO VERIFY QUANTITY.
Data retrieved from NASA's ASRS site as of July 2007 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.