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|
Attributes | |
ACN | 891440 |
Time | |
Date | 201005 |
Local Time Of Day | 0601-1200 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | B737 Next Generation Undifferentiated |
Operating Under FAR Part | Part 121 |
Flight Phase | Final Approach |
Flight Plan | IFR |
Component | |
Aircraft Component | Flap Control (Trailing & Leading Edge) |
Person 1 | |
Function | Captain Pilot Flying |
Qualification | Flight Crew Air Transport Pilot (ATP) |
Person 2 | |
Function | Pilot Not Flying First Officer |
Events | |
Anomaly | Aircraft Equipment Problem Critical |
Narrative:
On approach flaps would not extend beyond 25 degrees. Autopilot and autothrottles were engaged and using VNAV procedures. Passing FAF checked speed below 200 KTS and called for gear down and flaps 15. Checked speed below 190 and called for flaps 25. Checked speed below 175 and called for flaps 30 followed by flaps 40 when speed below 162. I noticed it took an unusually long time for the speed to bleed below 162. Then noted that the auto speed bug was still indicating flaps 25 speed and noted the flaps were still indicating 25 degrees. Reselected flap handle to flaps 25 position momentarily and then back to flaps 40 position. Flaps remained indicating 25 degrees. Executed a missed approach and due to our low fuel state elected an immediate divert to [a nearby airport] for flaps 15 landing. Landed normally using flaps 15 landing procedures. This aircraft had two previous flap problem write-ups and flap maintenance had been performed on this aircraft prior to the previous leg. Aircraft was signed off after this event as could not duplicate (on ground). Upon review of the flap load relief system; I believe the system on this airplane may be malfunctioning causing a flap lockout at higher than intended speeds. Check the load relief system on this aircraft.
Original NASA ASRS Text
Title: A B737NG Flight Crew reported problems with their flap load relief system on approach; leading to a deviation to a nearby airport with a longer runway.
Narrative: On approach flaps would not extend beyond 25 degrees. Autopilot and autothrottles were engaged and using VNAV procedures. Passing FAF checked speed below 200 KTS and called for gear down and flaps 15. Checked speed below 190 and called for flaps 25. Checked speed below 175 and called for flaps 30 followed by flaps 40 when speed below 162. I noticed it took an unusually long time for the speed to bleed below 162. Then noted that the auto speed bug was still indicating flaps 25 speed and noted the flaps were still indicating 25 degrees. Reselected flap handle to flaps 25 position momentarily and then back to flaps 40 position. Flaps remained indicating 25 degrees. Executed a missed approach and due to our low fuel state elected an immediate divert to [a nearby airport] for flaps 15 landing. Landed normally using flaps 15 landing procedures. This aircraft had two previous flap problem write-ups and flap maintenance had been performed on this aircraft prior to the previous leg. Aircraft was signed off after this event as could not duplicate (on ground). Upon review of the flap load relief system; I believe the system on this airplane may be malfunctioning causing a flap lockout at higher than intended speeds. Check the load relief system on this aircraft.
Data retrieved from NASA's ASRS site as of April 2012 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.