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|
Attributes | |
ACN | 325359 |
Time | |
Date | 199601 |
Day | Sun |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : cvg |
State Reference | OH |
Altitude | agl bound lower : 200 agl bound upper : 1000 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tracon : cvg tower : atl |
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 : captain oversight : pic |
Qualification | pilot : instrument pilot : commercial pilot : cfi pilot : atp |
Experience | flight time last 90 days : 100 flight time total : 4950 flight time type : 65 |
ASRS Report | 325359 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : commercial pilot : instrument |
Events | |
Anomaly | aircraft equipment problem : less severe |
Independent Detector | aircraft equipment other aircraft equipment : unspecified |
Resolutory Action | none taken : unable other |
Consequence | Other |
Supplementary | |
Primary Problem | Aircraft |
Air Traffic Incident | other |
Narrative:
After normal takeoff gear was selected up. After gear retraction the left main indicated that it was not locked up. A red 'unlock' light was illuminated. We executed the checklist procedure on climb out from cvg. We lowered the gear and received 3 green down and locked. We then raised the gear and still the left main showed not locked in up position. We contacted company maintenance control. They had us continue the flight, but divert to pittsburgh. (The checklist authority/authorized continued flight. In pit our maintenance personnel could look at the aircraft.) we landed uneventfully. There was considerable ice, snow, and slush on the txwys at cvg. We feel that the snow/slush covered up the 'proxi' sensors on the main gear. Therefore the sensors couldn't tell that the gear was up. (This aircraft does not use micro switches, and contamination of the main gear from ice/slush, etc, has been a problem with the dornier 328 before.) callback conversation with reporter revealed the following information: proximity sensors on the dornier 328 send indication and warning status information to the pseu (proximity switch electronic unit). The sensors are located on the uplocks and downlocks of the gear, and only 'sense' contact distance, as opposed to the positive mechanical movement of microswitches. The flight crew received a red, 'not locked in selected position' gear warning light which required compliance with a 200 KT airspeed limitation. Reporter states that proximity switches are the primary means of indication and warning signals on the D328. He is concerned that the diverted flts (due to a sensor related problem) contribute to a lowered airline reliability factor. The ceo and poi are apprised, and the company has alerted the manufacturer that there have been many indication and warning problems related to snow and ice accumulation. In order to avert future erroneous signals, a directive has been issued regarding crew member assurance of gear and wheel well deicing prior to departure.
Original NASA ASRS Text
Title: FLT DIVERTED DUE TO AN ERRONEOUS GEAR WARNING INDICATION.
Narrative: AFTER NORMAL TKOF GEAR WAS SELECTED UP. AFTER GEAR RETRACTION THE L MAIN INDICATED THAT IT WAS NOT LOCKED UP. A RED 'UNLOCK' LIGHT WAS ILLUMINATED. WE EXECUTED THE CHKLIST PROC ON CLBOUT FROM CVG. WE LOWERED THE GEAR AND RECEIVED 3 GREEN DOWN AND LOCKED. WE THEN RAISED THE GEAR AND STILL THE L MAIN SHOWED NOT LOCKED IN UP POS. WE CONTACTED COMPANY MAINT CTL. THEY HAD US CONTINUE THE FLT, BUT DIVERT TO PITTSBURGH. (THE CHKLIST AUTH CONTINUED FLT. IN PIT OUR MAINT PERSONNEL COULD LOOK AT THE ACFT.) WE LANDED UNEVENTFULLY. THERE WAS CONSIDERABLE ICE, SNOW, AND SLUSH ON THE TXWYS AT CVG. WE FEEL THAT THE SNOW/SLUSH COVERED UP THE 'PROXI' SENSORS ON THE MAIN GEAR. THEREFORE THE SENSORS COULDN'T TELL THAT THE GEAR WAS UP. (THIS ACFT DOES NOT USE MICRO SWITCHES, AND CONTAMINATION OF THE MAIN GEAR FROM ICE/SLUSH, ETC, HAS BEEN A PROB WITH THE DORNIER 328 BEFORE.) CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING INFO: PROX SENSORS ON THE DORNIER 328 SEND INDICATION AND WARNING STATUS INFO TO THE PSEU (PROX SWITCH ELECTRONIC UNIT). THE SENSORS ARE LOCATED ON THE UPLOCKS AND DOWNLOCKS OF THE GEAR, AND ONLY 'SENSE' CONTACT DISTANCE, AS OPPOSED TO THE POSITIVE MECHANICAL MOVEMENT OF MICROSWITCHES. THE FLC RECEIVED A RED, 'NOT LOCKED IN SELECTED POS' GEAR WARNING LIGHT WHICH REQUIRED COMPLIANCE WITH A 200 KT AIRSPD LIMITATION. RPTR STATES THAT PROX SWITCHES ARE THE PRIMARY MEANS OF INDICATION AND WARNING SIGNALS ON THE D328. HE IS CONCERNED THAT THE DIVERTED FLTS (DUE TO A SENSOR RELATED PROB) CONTRIBUTE TO A LOWERED AIRLINE RELIABILITY FACTOR. THE CEO AND POI ARE APPRISED, AND THE COMPANY HAS ALERTED THE MANUFACTURER THAT THERE HAVE BEEN MANY INDICATION AND WARNING PROBS RELATED TO SNOW AND ICE ACCUMULATION. IN ORDER TO AVERT FUTURE ERRONEOUS SIGNALS, A DIRECTIVE HAS BEEN ISSUED REGARDING CREW MEMBER ASSURANCE OF GEAR AND WHEEL WELL DEICING PRIOR TO 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.