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SF340 flight crew reports anti-skid inoperative light after gear extension and flight idle stop must be manually overridden after landing before reverse can be selected.
| Attributes | |
| ACN | 769634 |
| Time | |
| Date | 200801 |
| Local Time Of Day | 1801 To 2400 |
| Place | |
| Locale Reference | airport : zzz.airport |
| State Reference | US |
| Environment | |
| Flight Conditions | VMC |
| Light | Night |
| Aircraft 1 | |
| Controlling Facilities | tower : mcn.tower |
| Operator | common carrier : air carrier |
| Make Model Name | SF 340B |
| Operating Under FAR Part | Part 121 |
| Flight Phase | descent : approach |
| Flight Plan | IFR |
| Person 1 | |
| Affiliation | company : air carrier |
| Function | flight crew : captain oversight : pic |
| Qualification | pilot : commercial |
| ASRS Report | 769634 |
| Person 2 | |
| Affiliation | company : air carrier |
| Function | flight crew : first officer |
| Qualification | pilot : commercial |
| ASRS Report | 769638 |
| Events | |
| Anomaly | aircraft equipment problem : less severe non adherence : company policies |
| Independent Detector | aircraft equipment other aircraft equipment : cwp other flight crewa |
| Resolutory Action | none taken : anomaly accepted none taken : insufficient time |
| Supplementary | |
| Problem Areas | Flight Crew Human Performance Aircraft |
| Primary Problem | Aircraft |
Narrative:
While on short final the landing gear was extended. When it locked into place; the anti-skid light illuminated on the control wheel panel. We made the decision to continue the landing and upon landing; the flight idle stop did not disengage. We pulled the flight idle stop light and were able to bring the aircraft to a stop and taxi to the gate without incident. We had reviewed the landing distance and determined that we had the required demonstrated landing distance with the anti-skid inoperative but not the required factored. We only had 1600 pounds of fuel on board so landing was our decision. All of this was figured in hindsight. The anti-skid failure caused the flight idle stop release to fail requiring the flight idle stop override to be pulled. We could have gone around and reviewed our situation more closely. Ultimately we would have had to land in ZZZ anyway because we only had 1600 pounds of fuel on board.
Original NASA ASRS Text
Title: SF340 FLT CREW REPORTS ANTI-SKID INOP LIGHT AFTER GEAR EXTENSION AND FLIGHT IDLE STOP MUST BE MANUALLY OVERRIDDEN AFTER LANDING BEFORE REVERSE CAN BE SELECTED.
Narrative: WHILE ON SHORT FINAL THE LNDG GEAR WAS EXTENDED. WHEN IT LOCKED INTO PLACE; THE ANTI-SKID LIGHT ILLUMINATED ON THE CTL WHEEL PANEL. WE MADE THE DECISION TO CONTINUE THE LNDG AND UPON LNDG; THE FLT IDLE STOP DID NOT DISENGAGE. WE PULLED THE FLT IDLE STOP LIGHT AND WERE ABLE TO BRING THE ACFT TO A STOP AND TAXI TO THE GATE WITHOUT INCIDENT. WE HAD REVIEWED THE LNDG DISTANCE AND DETERMINED THAT WE HAD THE REQUIRED DEMONSTRATED LNDG DISTANCE WITH THE ANTI-SKID INOP BUT NOT THE REQUIRED FACTORED. WE ONLY HAD 1600 LBS OF FUEL ON BOARD SO LNDG WAS OUR DECISION. ALL OF THIS WAS FIGURED IN HINDSIGHT. THE ANTI-SKID FAILURE CAUSED THE FLT IDLE STOP RELEASE TO FAIL REQUIRING THE FLT IDLE STOP OVERRIDE TO BE PULLED. WE COULD HAVE GONE AROUND AND REVIEWED OUR SIT MORE CLOSELY. ULTIMATELY WE WOULD HAVE HAD TO LAND IN ZZZ ANYWAY BECAUSE WE ONLY HAD 1600 LBS OF FUEL ON BOARD.
Data retrieved from NASA's ASRS site as of May 2009 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.