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|
Attributes | |
ACN | 485802 |
Time | |
Date | 200009 |
Day | Tue |
Local Time Of Day | 1801 To 2400 |
Place | |
Locale Reference | airport : zzz.airport |
State Reference | US |
Altitude | msl single value : 24000 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | artcc : zzz.artcc tower : gso.tower |
Operator | common carrier : air carrier |
Make Model Name | B727-200 |
Operating Under FAR Part | Part 121 |
Flight Phase | cruise : level |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : multi engine pilot : atp |
Experience | flight time last 90 days : 150 flight time total : 9500 flight time type : 3300 |
ASRS Report | 485802 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : commercial pilot : instrument pilot : multi engine |
Events | |
Anomaly | aircraft equipment problem : critical maintenance problem : improper maintenance non adherence : far non adherence : published procedure |
Independent Detector | other flight crewa |
Resolutory Action | none taken : detected after the fact |
Consequence | other other |
Factors | |
Maintenance | contributing factor : schedule pressure performance deficiency : inspection performance deficiency : installation performance deficiency : repair |
Supplementary | |
Problem Areas | Flight Crew Human Performance Aircraft Maintenance Human Performance |
Primary Problem | Maintenance Human Performance |
Narrative:
On sep/xa/00 at approximately XA30Z at FL240, approximately 80 DME from sac VOR on the 070 degree radial, the aircraft shuddered as if passing through an inversion level or a possible bird strike. No apparent structural problems, flight control malfunctions, no warning light indications in the cockpit, nor was there any sign or indication of damage to the aircraft. The possibility of a bird strike at FL240, though remote, was assumed. Upon landing, walkaround revealed no indications of a bird strike. However, upon preflight, the flight engineer found the left gear door missing and structural damage to the underside of the left wing. Maintenance was notified and the missing gear door was recorded in the logbook. The cause of the gear door separating from the aircraft is not exactly known at this time. The flight engineer did inspect the gear door on his walkaround and it appeared to be properly attached. A tire change was accomplished previously in the day before the flight, and it is suspected that the attaching bolts were in place but retaining nuts to hold the bolts in place were not properly attached. Callback conversation with reporter revealed the following information: the reporter stated the aircraft was a B727-200 and the left main gear tire and wheel had been replaced the day before the flight. The reporter said the inboard flap jackscrew fairing was gouged and dented by the gear door departure.
Original NASA ASRS Text
Title: A B727-200 IN CRUISE AT FL240 INCURRED THE LOSS OF THE L MAIN LNDG GEAR DOOR DUE TO INCORRECT INSTALLATION AFTER TIRE AND WHEEL REPLACEMENT.
Narrative: ON SEP/XA/00 AT APPROX XA30Z AT FL240, APPROX 80 DME FROM SAC VOR ON THE 070 DEG RADIAL, THE ACFT SHUDDERED AS IF PASSING THROUGH AN INVERSION LEVEL OR A POSSIBLE BIRD STRIKE. NO APPARENT STRUCTURAL PROBS, FLT CTL MALFUNCTIONS, NO WARNING LIGHT INDICATIONS IN THE COCKPIT, NOR WAS THERE ANY SIGN OR INDICATION OF DAMAGE TO THE ACFT. THE POSSIBILITY OF A BIRD STRIKE AT FL240, THOUGH REMOTE, WAS ASSUMED. UPON LNDG, WALKAROUND REVEALED NO INDICATIONS OF A BIRD STRIKE. HOWEVER, UPON PREFLT, THE FE FOUND THE L GEAR DOOR MISSING AND STRUCTURAL DAMAGE TO THE UNDERSIDE OF THE L WING. MAINT WAS NOTIFIED AND THE MISSING GEAR DOOR WAS RECORDED IN THE LOGBOOK. THE CAUSE OF THE GEAR DOOR SEPARATING FROM THE ACFT IS NOT EXACTLY KNOWN AT THIS TIME. THE FE DID INSPECT THE GEAR DOOR ON HIS WALKAROUND AND IT APPEARED TO BE PROPERLY ATTACHED. A TIRE CHANGE WAS ACCOMPLISHED PREVIOUSLY IN THE DAY BEFORE THE FLT, AND IT IS SUSPECTED THAT THE ATTACHING BOLTS WERE IN PLACE BUT RETAINING NUTS TO HOLD THE BOLTS IN PLACE WERE NOT PROPERLY ATTACHED. CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING INFO: THE RPTR STATED THE ACFT WAS A B727-200 AND THE L MAIN GEAR TIRE AND WHEEL HAD BEEN REPLACED THE DAY BEFORE THE FLT. THE RPTR SAID THE INBOARD FLAP JACKSCREW FAIRING WAS GOUGED AND DENTED BY THE GEAR DOOR DEP.
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.