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|
Attributes | |
ACN | 401115 |
Time | |
Date | 199804 |
Day | Fri |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : cvg |
State Reference | OH |
Altitude | agl bound lower : 50 agl bound upper : 100 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tracon : cvg tower : cvg |
Operator | common carrier : air carrier |
Make Model Name | Commercial Fixed Wing |
Operating Under FAR Part | Part 121 |
Navigation In Use | Other Other |
Flight Phase | climbout : takeoff climbout : initial |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : atp |
Experience | flight time last 90 days : 225 flight time total : 8500 flight time type : 1800 |
ASRS Report | 401115 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : atp |
Events | |
Anomaly | aircraft equipment problem : critical other anomaly other |
Independent Detector | aircraft equipment other aircraft equipment : unspecified other flight crewa |
Resolutory Action | other |
Consequence | Other |
Supplementary | |
Primary Problem | Flight Crew Human Performance |
Air Traffic Incident | other |
Narrative:
We were scheduled to depart cvg for aup at XA10. Our aircraft was having the main landing gear bay overheat sensor replaced and we departed 63 mins late. After maintenance was completed I conducted my walkaround and noticed no irregularities. There were 3 gear pin flags on the holders on the flight deck bulkhead. Start and taxi were normal. On takeoff when gear were selected up the nose gear retracted and the mains remained down. We selected the gear handle down and got 3 green indicators. We switched to departure and informed them of the problem (after informing tower and telling them that we needed to remain in the local area). While being vectored to burn down to maximum landing weight we informed the passenger and company. Upon reaching maximum landing weight we made an uneventful approach and landing. After landing we discovered that the aircraft had flown a revenue flight from gsp to cvg with the main gear pinned because the main landing gear bay overheat system would not test. The flags were removed from the gear pins and placed in the holders in the cockpit. There was no maintenance write-up to indicate the aircraft had been flown with the gear pinned. The mechanics who replaced the warning element were not aware of the gear pins being installed and neither were we. Without the flags on the gear pins, it is nearly impossible to tell that they are installed. Obviously, this incident was completely avoidable had the proper maintenance procedures been followed. I share a portion of the blame for not looking closely during my preflight.
Original NASA ASRS Text
Title: FLC RETURNED TO LAND AFTER NOT BEING ABLE TO RETRACT LNDG GEAR. MAIN GEAR PINS WERE LEFT IN FOR TKOF BY MISTAKE.
Narrative: WE WERE SCHEDULED TO DEPART CVG FOR AUP AT XA10. OUR ACFT WAS HAVING THE MAIN LNDG GEAR BAY OVERHEAT SENSOR REPLACED AND WE DEPARTED 63 MINS LATE. AFTER MAINT WAS COMPLETED I CONDUCTED MY WALKAROUND AND NOTICED NO IRREGULARITIES. THERE WERE 3 GEAR PIN FLAGS ON THE HOLDERS ON THE FLT DECK BULKHEAD. START AND TAXI WERE NORMAL. ON TKOF WHEN GEAR WERE SELECTED UP THE NOSE GEAR RETRACTED AND THE MAINS REMAINED DOWN. WE SELECTED THE GEAR HANDLE DOWN AND GOT 3 GREEN INDICATORS. WE SWITCHED TO DEP AND INFORMED THEM OF THE PROB (AFTER INFORMING TWR AND TELLING THEM THAT WE NEEDED TO REMAIN IN THE LCL AREA). WHILE BEING VECTORED TO BURN DOWN TO MAX LNDG WT WE INFORMED THE PAX AND COMPANY. UPON REACHING MAX LNDG WT WE MADE AN UNEVENTFUL APCH AND LNDG. AFTER LNDG WE DISCOVERED THAT THE ACFT HAD FLOWN A REVENUE FLT FROM GSP TO CVG WITH THE MAIN GEAR PINNED BECAUSE THE MAIN LNDG GEAR BAY OVERHEAT SYS WOULD NOT TEST. THE FLAGS WERE REMOVED FROM THE GEAR PINS AND PLACED IN THE HOLDERS IN THE COCKPIT. THERE WAS NO MAINT WRITE-UP TO INDICATE THE ACFT HAD BEEN FLOWN WITH THE GEAR PINNED. THE MECHS WHO REPLACED THE WARNING ELEMENT WERE NOT AWARE OF THE GEAR PINS BEING INSTALLED AND NEITHER WERE WE. WITHOUT THE FLAGS ON THE GEAR PINS, IT IS NEARLY IMPOSSIBLE TO TELL THAT THEY ARE INSTALLED. OBVIOUSLY, THIS INCIDENT WAS COMPLETELY AVOIDABLE HAD THE PROPER MAINT PROCS BEEN FOLLOWED. I SHARE A PORTION OF THE BLAME FOR NOT LOOKING CLOSELY DURING MY PREFLT.
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.