JASC 2750
Service difficulty reports · 10,201
Reports filed under 2750 · Trailing Edge Flap Control System, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2750' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2750' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR EWFA20140402001Control Cable · brokenTHE RT FLAP EXTEND CABLE BROKEN APPROXIMATELY 7.5 INCHES FROM THE TURN BUCKLE JUST UNDER THE HEATER DUCT. THE MALFUNCTION OCCURED ON THE APPROACH TO LANDING; WITH 15 DEGREES OF FLAPS SELECTED. PIC REPORTED HE HEARD A POP AND GRINDING NOISE FOLLOWED BY A 40 DSDR USAA2014033100003Computer · faultyCREW REPORTED A F/CTL FLAPS FAULT ECAM INFLIGHT. DIVERTED TO IAD FOR LONGER RUNWAY & NO FLAPS LANDING, EMERGENCY WAS DECLARED. ACCOMPLISHED TSM 27-51-00-810-810-A. R & R NR 1 1 SFCC IAW AMM 27-51-34. OPERATIONS CHECKED GOOD AT THIS TIME, OK FOR FURTHER FLISDR CA140401020Flap System · failed(CAN) FLAPS WOULD NOT RETRACT FROM THE TAKEOFF SETTING OF 20 DEGREES AFTER BECOMING AIRBORNE. THE CREW ELECTED TO RETURN TO ORIGIN AND LANDED SAFELY WITH ARFF ON STANDBY. ONCE ON THE GROUND THE FLAPS WERE RESET IAW THE FLIGHT INFORMATION MANUAL AND RECYCLESDR GN0A20140327001Flap · malfunctionedAFTER TAKEOFF THE CREW SELECTED THE FLAPS UP, THE INBD & NACELLE PANELS RETRACTED TO 0° WHILE THE OTBD PANELS REMAINED AT 15° TAKEOFF POSITION. THIS CONDITION CAUSED THE FLAP DISAGREEMENT WARNING TO ACTIVATE. THE ACFT RETURNED TO FRG & LANDED WITHOUT INCIDENSDR REXA2014032000308Flap · malfunctionedFLAPS FAIL EICAS, OCCURRED IN FLT ON APPROACH DURING FLAP EXTENSION. FAILED AT FLAP 30 DEG, AIRSPEED 160, TIME INTO FLIGHT 1 HR 10MIN. OAT +5 DEG C TAT. COMPLETED CB RESET OF FLAP SYS. COMPLETED 5 CONSECUTIVE FLAP CYCLES. DEFERRED FLAPS SYS IAW MEL 27-50-SDR CA140318006Flap System · failed(CAN) FLAPS FAIL AFTER T/O ZERO POSITION TOUCHDWON VS LESS THAN 200 FPM THEN FLAPS HALFSPEED STATUS MESSAGE. RESET FLAP SYS IAW AD 200906, 8208,12. RESET SYSTEM IAW FIM 27, PAGE 115.SDR CALA2014031800355Unknown · malfunctionedDURING APPROACH FLAPS LOCKED OUT AT 25 & WOULD NOT EXTEND TO 30. ALL APPLICABLE CHECKLISTS COMPLETED, LANDING WITH INCIDENT IAW FIM TASK 27-51-00-810-801. PERFORMED FSEU BITE NO FAULTS OR PREVIOUS FAULTS LAST 28 LEGS. INSPECTED FLAPS & COMPLIED WITH FLAP LOSDR R61A201403160431Tube · corrodedDURING HEAVY CHECK, RT 6 FLAP DRIVE TUBE IS CORRODED. MAINTENANCE R & R RT 6 FLAP DRIVE TUBE IAW AMM 27-51-03, REF J/C 27-51-01-720-801A2 FOR OPS CHECK, PN 5912949-3 TORQUE TUBE.SDR YADA20140319001Control Cable · brokenPILOT REPORTED FLAPS STUCK AT TAKEOFF POSITION. REPLACED FAILED FLAP DRIVE CABLE.SDR A6WA201441252Flap · malfunctionedRECEIVED FLAPS FAIL CAS MSG WHEN SETTING FLAPS TO 30 ON APPROACH, FLAPS INDICATED 30. RAN QRH & LANDED. PERFORMED FLAP RESET PROCEDURE IAW AWAC SUPP 99-18F BOX 12. FLAPS RESET, PLACARDED & PLACED ON MEL.SDR CA140314014Flap System · failed(CAN) ON APPROACH, "FLAPS FAIL" C UPON SELECTION TO 8 DEGREES. ABORTED APPROACH. AFTER SELECTION BACK TO 0 DEGREES, "FLAPS FAIL", C, DISAPPEARED. SECOND APPROACH PERFORMED AND ACFT LANDED. NO MDC MESSAGES COULD BE RETRIEVED. FLAPS/SLATS SYSTEM OPS TEST PERSDR CHQA20140309077Flap · malfunctionedCREW REPORTED THAT THEY RECEIVED A FLAP FAIL MSG DURING FLIGHT. THE CREW DECLARED AN EMERGENCY & LANDED AT THEIR INTENDED DESTINATION WITHOUT INCIDENT. MX RESET THE FLAP SYS. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.SDR CA140310002Flap System · failed(CAN) FLIGHT CONTROL FAULT ON APPROACH, FLAPS JAMMED AT FLAPS 1, UNABLE TO EXTEND. PERFORMED QRH, RETRACTED GEAR, CIRCLED FOR APPROXIMATELY 15 MINUTES AND SUBSEQUENTLY LANDED AT PARTIAL FLAPS. DID NOT DECLARE PAN PAN WITH ATC, BUT ATC ADVISED THEY WOULD HAVE CSDR CA140514008Torque Tube · grooved(CAN) FOUND RT WING FLAP TORQUE TUBE F6 DAMAGED. GROOVED BY ADJACENT GUARD BRACKET. IT APPEARS THAT THE T TUBE CAME IN CONTACT WITH THE GUARD & DAMAGED BOTH PARTS.SDR GLBA2014030500399Fcu · faultyAFTER SELECTING FLAPS 15, RECEIVED SINGLE CHIME MASTER CAUTION ANNC, FLAPS & ADVANCE SWS ON THE MAP & CONTROL FAULT ON THE OVERHEAD, INBD PAIRS FLASHING. PRESSED RESET BUTTON ON FLAP PANEL IAW CHECKLIST, WHICH WAS UNSUCCESSFUL. IAW QRM EAP -68, EMERGENCY DESDR SIMA20140302002Brake · failedFLAP FAIL MSG WHEN FLAP LEVER MOVED TO 9. INDICATION REMAINED AT 0 ON EICAS. ACFT HAD VERY SLIGHT TENDENCY TO ROLL RIGHT. R & R RT FLAP TRANSMISSION BRAKE IAW AMM 27-51-01, OPERATIONS CHECKED GOOD.SDR REXA2014030100246Shaft · lack of lubeFLAP FAIL AFTER LANDING, STUCK AT 45. CYCLED FLAPS 5 TIMES, NO DEFECTS NOTED. REPLACED NR 1 LT FLAP SHAFT & LUBED LT & RT FLEX SHAFTS. ALL CHECKED GOOD.SDR CALA2014030300248Transmission · trippedTE FLAP ASYMMETRY WARNING CAME ON WHILE CONFIGURING FOR APPROACH. USED ALTERNATE FLAP SELECTOR TO BRING FLAPS TO 20'' INDICATION. DEBRIEFED CAPTAIN & WORDING ABOVE SHOULD READ TE FLAP DISAGREE NOT ASYMMETRY. FSEU 1 SHOWED FAULT 305. PERFORMED FIM TASK 27- SDR CALA2014022790490Flap · malfunctionedAIR RETURN DUE TO FLAP SYS FAULT MESSAGE ON ECAM. FLAPS STUCK IN POSITION NR 2.SDR USAA2014022700005Control Lever · inoperativeFLT 2033, PHL-BOS. WHILE PREPARING TO LAND THE CREW NOTED THAT THE LE DEVICES DID NOT MOVE FROM THEIR POSITION AS COMMANDED IN PREPARATION FOR THE APPROACH. THE CREW EXECUTED A GO AROUND ABOVE 1500 FEET & WERE ABLE TO CLEAR THE DISAGREEMENT. THE FLIGHT LANDSDR CALA2014022590478Fseu · malfunctionedFLAPS PRIMARY FAIL EICAS REPLACED FSEU & FLAP PRIMARY LOW SPEED SOLENOID, MAT GND TEST PASSED HIGH LIFT SYS IAW MM 27-51-05, 27-51-00.SDR REXA2014022100232Flap · obstructedFLAPS FAIL CAUTION MSG. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H B I AMOC DATED JULY 22, 2013 & PHAD 20-052N. REMOVED SNOW & ICE CONTAMINATION FROM FLAPS. OPERATIONS CHECKED IAW AMM 27-54-00 NO DAMAGE NOTED.SDR DXTA2014022405664Pdu · faultyFLAPS FAILED AT APPROXIMATELY 6 DEGREES. RESET PROCEDURES DID NOT WORK. UPON POWER UP, NO FAULTS FOUND ON CONTROLLER, FLAPS WORKING NORMAL. CYCLED FLAPS & VERIFIED ACTUATORS & FLAP DRIVE CABLES OPERATIONS CHECKED GOOD. SYS OPERATIONS CHECKED GOOD WORK DONESDR REXA2014022000230Flap · obstructedFLAPS FAIL PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H 6 I, AMOC DATED JULY 22, 2013 & PA AD 27-052N. REMOVED SNOW & ICE CONTAMINATION FROM FLAPS. OPERATIONS CHECKED GOOD IAW AMM 27-54-00, NO DAMAGE FOUND.SDR 2014FA0000095Control Unit · malfunctionedENROUTE, A FLAPS FAIL EICAS MESSAGE DISPLAYED. AN EMERGENCY WAS DECLARED AND THE ACFT MADE AN UNEVENTFUL LANDING AT ITS INTENDED DESTINATION. SUBSEQUENT TROUBLESHOOTING REVEALED CODES ON THE FLAP CONTROL UNIT INDICATING ITERNAL FAULTS WITHIN THE UNIT ITSELF.SDR AALA20140216001Fseu · inoperativeSFO CREW REPORTED TE FLAP ASYMMETRY. EMERGENCY DECLARED FLIGHT LANDED SFO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RESET LT HAND OTBD TE FLAP TRANSMISSION OVER TORQUE INDICATOR THAT HAD POPPED. REPLACED LT HAND AIR DATA COMPUTER & NR 2 FLAP SLAT ELSDR CA140213005Bellcrank · failed(CAN) PILOT REPORTED FLAPS WOULD NOT COMPLETELY RETRACT AFTER LANDING. MAINTENANCE STAFF FOUND FUSELAGE FLAP BELLCRANK CRACKED, BROKEN AT BASE OF CONTROL ARM FROM THE VERTICAL CRANK BODY.SDR QXEA2014021100113Linkage · brokenFLAP CONTROL HANDLE TRIGGER LINKAGE BROKEN. FLAP POWER CAUTION LIGHT ILLUMINATED. RETURNED TO FIELD, LANDING UNEVENTFUL. PERFORMED GVI AND FOUND FLAP LEVER TRIGGER GROMMET JAMMED INTERROGATED CDS FOUND HYDRAULIC PRESSURE LOSS IN CURRENT FAULTS REPLACED FLAP COSDR AALA20140211008Transmission · trippedLAX CREW REPORTED TRAILING EDGE FLAP DISAGREE MESSAGE RECEIVED WITH FLAP HANDLE AT POSITION 1, WITH FLAPS INDICATING 0. EMERGENCY DECLARED FLIGHT LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. NR 5 FLAP TRANSMISSION OVERLOAD INDICATOR TRIPPED. SDR REXA2014020900196Actuator · failedDURING FLAP EXTENSION, FLAPS FAIL CAUTION MESSAGE DISPLAYED. FLAP POSITION AT FAILURE WAS 0. REPLACED LT FLAP NR 2 & 3 ACTUATORS, RT FLAP NR 1 ,2, 3 & 4 ACTUATORS. RIGGED FLAPS IAW 27-54-00-830-801. OPS CHECKED GOOD.SDR CA140211003Bellcrank · cracked(CAN) DURING PRE-FLIGHT INSTRUCTOR/STUDENT SELECTED T/O FLAP, FLAPS DID NOT RESPOND, SELECTED LANDING FLAP AND FLAPS PARTIALLY EXTENDED. ACFT RETURNED TO BLOCKS. SUBSEQUENT INSPECTION REVEALED FUSELAGE FLAP BELLCRANK WAS CRACKED. REQUEST MADE TO RETURN PART SDR SWIA201436283Flap · defectiveAFTER SELECTING FLAPS TO 45° AIRCRAFT WANTED TO ROLL LT. REQUIRED A SIGNIFICANT AMOUNT OF RWD AILERON TRIM TO COMPENSATE. FLT 6281 REPLACED LT OTBD FLAP IAW AMM. PN 601R14501-841, SN ON SB/RJ/585, PN OFF 601R14501-1 & SN OFF SB/RJ/071.SDR TSAA20140206003Flap · malfunctionedFLIGHT KH1104, ON APPROACH FLAPS WOULD NOT EXTEND. ACFT DECLARED AN EMERGENCY & LANDED IN A NO-FLAP CONDITION. ACFT LANDED UNEVENTFULLY & TAXIED BACK TO PARKING AREA.SDR CALA2014020690314Flap System · malfunctionedFLAP OVER SPEED ON GO AROUND. FLAPS RETRACTED FROM 30 TO 20 & THEN HAD FLAP SHUTDOWN MESSAGE. EG WAS AT 8 KNOTS OVER SPEED. PHASE ONE INSPECTION REQUIRED IAW AMM05-51-08. OPERATED FLAPS IN ALT MODE MESSAGE CLEARED, PERFORMED FLAPS OPERATIONS CHECKED IAW 27SDR OXZS2014022000092Handle · crackedHANDLE CRACKED AND SNAPPED OFF RENDERING THE FLAPS UNUSABLE. THIS OCCURRED AFTER 13 YEARS OF REGULAR USAGE. THE CAUSE WAS PROBABLY RELATED TO DESIGNS OF THE HANDLE WHICH LACKED SUFFICIENT REINFORCEMENT AT THE FULCRUM OF THE HANDLE WHICH MADE THE HANDLE VULNESDR AALA20140204009Switch · inoperativeMSP INFLIGHT ORD-RNO. STANDBY RUDDER LIGHT ILLUMINATED DURING TAKEOFF. EMERGENCY DECLARED FLIGHT DIVERTED MSP LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP SWITCH 51051, SYS GND CHECKED NORMAL OPERATION CLOSED.SDR CALA2014020690321Flap · malfunctionedEICAS MESSAGE TE FLAP DISAGREE DISPLAYED, TE LIGHT ILLUMINATED, WHEN ANY TE FLAP POSITION SELECTED. FLAPS FAIL TO MOVE TO SELECTED POSITION.SDR CA140203021Control Unit · failed(CAN) ON APPROACH WHILE EXTENDING FLAPS , CREW REPORTED THAT THE FLAPS FAILED AT ZERO DEGREES, 200KTS, -20 DEGREES C. LANDING WAS MADE FLAPS UP WITHOUT INCIDENT AND TAXIED TO GATE. EMERGENCY WAS DECLARED. REMOVED AND REPLACED THE FECU, AND LT BPSU.SDR REXA2014020300166Flap · obstructedFLAPS FAIL CAUTION MSG AT GATE. FLIGHT CONTROL SYNOPTIC PAGE SHOWS LT FLAP AT 0 DEGREES & RT FLAP AT 2 DEGREES. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC DATED JULY 22, 2013 & PA AD 27-052N. CLEANED ICE & SLUSH AWAY FROSDR REXA2014020300165Ecu · malfunctionedFLAP FAIL ON DESCENT INTO DTW ABOUT 6000 FEET 200KB. PERFORMED TROUBLE SHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARA H 6 I AMOC DATED JULY 22,2013 & PA AD 27-052N. FOR FECU & LT BPSU R & R, WORK PERFORMED SEE NRCC N60561, N60584, N60600, N60598 & N50826. ASDR REXA2014020200161Flap · obstructedFLAPS FAIL CAUTION MSG UPON ARRIVAL AT ACFT. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARAGRAPH H 6 I. REMOVED IMPACTED ICE & SNOW FROM FLAPS. PERFORMED OPERATIONS CHECK IAW 27-54-00, OPERATIONS CHECKED GOOD.SDR CA140131004Drive Assy · sheared(CAN) THE FLAP SYSTEM WAS BEING ADJUSTED AND FUNCTION TESTED ON THE GROUND AFTER HEAVY MAINTENANCE AND ACFT IMPORT AS PART OF THE RETURN TO SERVICE CHECKS WHEN THE FLAP COMPUTER RECORDED A FAULT AND SHUTDOWN OPERATION OF THE FLAP SYSTEM. AT THIS TIME DURING GSDR R61A201401300178Torque Tube · corrodedDURING HEAVY CHECK, RT WING TE FLAP TORQUE TUBE CORRODED. MAINTENANCE R & R TORQUE TUBE IAW AMM 27-51-03.SDR CA140203022Bpsu · failed(CAN) TSB REPORTED ON FEB 3, 2014, THE FLIGHT CREW RECEIVED A FLAPS FAIL CAUTION INDICATION ON APPROACH AND DECLARED AN EMERGENCY WITH ATC. THE ACFT LANDED UNEVENTFULLY WITH ARFF ON SCENE. MAINTENANCE SUBSEQUENTLY REPLACED THE BRAKE POSITION SENSOR UNIT AND SDR R61A201401280190Torque Tube · corrodedDURING HEAVY CHECK, LEFT WING TE FLAP TORQUE TUBE BEARING SUPPORT CORRODED. MX R & R BEARING SUPPORT IAW AMM 27-51-03,27-51-04.SDR FDEA201401280212Computer · failedDURING FLAP EXTENSION, EXPERIENCED FLAP SYS 1 & 2 FAULT ILLUMINATION, FLAPS FAILED TO EXTEND. PERFORMED QRH PROCEDURE. WHEN FLAP HANDLE MOVED TO 40 DEGREES, FLAPS EXTENDED TO 40. BITE CHECKED BOTH SFCC'S & BOTH PASSED. RESET & TESTED EACH SEGMENT OF BOTH SDR R61A201401280167Torque Tube · corrodedDURING HEAVY CHECK, LT WING TE FLAP TORQUE TUBE CORRODED. MAINTENANCE R & R TORQUE TUBE IAW AMM 27-51-03.SDR CA140128002Flap System · failed(CAN) THE FLIGHT CREW EXPERIENCED A "FLAP FAIL" CAUTION INDICATION WHEN THE FLAPS WERE SELECTED FOR APPROACH INTO. FLAPS REMAINED AT ZERO DEGREES. AN EMERGENCY WAS DECLARED AND A FLAP ZERO APPROACH AND LANDING WAS CARRIED OUT WITHOUT FURTHER INCIDENT. THE ASDR NOZR20140127001Pdu · failedDURING APPROACH, CREW SELECTED FLAP SLAT TO 5 DEGREES, THE SLATS EXTENDED, THE FLAPS MOVE TO 1 TO 2 DEGREES AND STOPPED. CREW ELECTED TO DISCONTINUE THE APPROACH AND COMPLIED WITH THE FLAP FAILURE CHECKLIST. AFTER COMPLETING THE CHECKLIST, THE FLAPS STILL INDSDR CA140219002Control Unit · failed(CAN) TSB REPORTED ON JANUARY 24, 2014 WHEN THE CREW SELECTED FLAPS DOWN A FLAP FAIL MESSAGE WAS GENERATED AND THE FLAPS REMAINED RETRACTED. QRH PROCEDURES WERE FOLLOWED IN PREPARATION FOR A FLAPLESS LANDING AND AN EMERGENCY WAS DECLARED WITH ATC. ACFT LAND
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