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 KPV2002F00000Drive Unit · slowNR 2 ADI PITCH/ROLL MISMATCH, AHRS DATA INVALID, YAW DAMPNER FAILED ON BOTH CHANNELS. FLAPS VERY SLOW MOVING AND STUCK AT 10 PERCENT. FLAPS WOULD NOT RETRACT ABOVE 5 DEGREE. DECLARED EMERGENCY AND RETURNED TO AIRPORT. LANDED WITHOUT INCIDENT. CORRECTIVE ASDR DHL2002366004Limiter · malfunctionedON SELECTING FLAPS 8 DEGREES, FLAPS JAMMED AT ABOUT 0 DEGREES, SLATS WERE 16 DEGREES. COMPLETED ABNORMAL PROC FOR JAMMED FLAPS & LANDED. FOUND FLAPS OVERTRAVELED TO UP POSITION. DISCONNECTED TORQUE LIMITER RIG FLAP TO UP POSITION. RECONNECTED TORQUE LIMITESDR GAIA02040OPJackscrew · damagedFLT 879 - FWA-SJC - DURING CLIMB-OUT WHEN FLAPS SELECTED TO RETRACT. THE OUTBOARD FLAPS WHERE SPLIT. THE CREW DECLARED AND EMERGENCY LANDING, DUMPED FUEL AND RETURNED TO FWA. THE LANDING WAS UNEVENTFUL. REMOVED AND REPLACED THE LEFT OUTBOARD FLAP OUTBOARD SDR DL76G020490Fseu · malfunctionedT/E FLAP DISAGREE LIGHT WHEN FLAPS 25 SELECTED, EICAS MSG ALSO. FLAPS DID NOT MOVE TO 25 DEGS POSITION. USED ALT FLAP PROC. INSPECTED FLAP, NO DISCREPANCIES NOTED. FSEU BITE SHOWED M603 FLAP LEVER RVDT. REPLACED FSEU PER AMM. OPS CHECKED NORMAL. NO HISTSDR 02119663Flap · malfunctionedAFTER TAKEOFF, THE CREW REPORTED THAT THE FLAPS HAD STUCK AT 20 DEGREES AND WOULD NOT RETRACT. THE CREW FOLLOWED THE QRH PROCEDURES, RETURNED TO CAE, AND LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL PERFORMED EXTENSIVE TESTS OF THE FLAP SYSTEM AND FECU, CYSDR COMA0260289FlapFLAPS FAIL MESSAGE AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0260287Fcu · malfunctionedFLAPS FAIL MESSAGE. REPLACED THE FECU.SDR COMA0260286FlapFLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0260290Pdu · failedFLAPS FAILED AT 20 DEGREES. REPLACED THE FLAP PDU.SDR REXA02006Flap · malfunctionedFLAPS FAILED ON APPROACH WHEN SELECTED DOWN. QRH PROCEDURES FOLLOWED AND AN UNEVENTFUL 0-FLAP LANDING WAS PERFORMED. SYSTEM WAS RESET PER FAULT RESET PROCEDURES OF THE BOMBARDIER FIM AND IAW AD 98-20-01. SYSTEM OPERATIONALLY CHECKED GOOD. (M)SDR CA020507018Control Cable · frayed(CAN) LT AND RT FLAP UPPER CABLES FRAYED AT WING ROOT PULLEYS.SDR REXA02007Flap · malfunctionedFLAPS FAILED ON APPROACH WHEN SELECTED DOWN. QRH PROCEDURES FOLLOWED AND AN UNEVENTFUL 0 FLAP LANDING WAS PERFORMED. SYSTEM WAS RESET PER FAULT RESET PROCEDURES OF THE BOMBARDIER FIM AND IAW AD 98-20-01. SYSTEM OPERATIONALLY CHECKED GOOD. (M)SDR COMA0260277FlapFLIGHT 5801 FLAPS FAILED WHEN SELECTED UP AFTER LANDING.RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR C2XA02SH004Spring · corrodedSHV - DURING C-CHECK INSPECTION, THE LEFT HAND INBOARD AND OUTBOARD LOWER FLAP SHROUD SPRINGS WERE FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPRINGS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR COMA0260255Fcu · malfunctionedFLIGHT 5797 FLAPS FAIL MESSAGE, FLAPS STUCK AT 20 DEGREES.REPLACED THE FECU.SDR CA020502008Control Cable · failed(CAN) FLAPS FAIL MESSAGE ON EICAS AFTER TAKEOFF WITH FLAPS SELECTED AT 8, AIR TURN BACK. REPLACED FLEX CABLE ACTUATOR BETWEEN NR 1 AND 2 ACTUATORS ON THE LT SIDE.SDR DHL2002807554Fitting · crackedITEM: REF.: N/R 1124 RT. WING FLAP ACTUATOR (LWR) ATTACH FITTING CRACKED 1" @ STA. 339.000CORR: R/R RH FLAP ACTUATOR LOWER ATTCH FITTING IAW OHM27-28-8 PG. 3 REFER TO N/R 2387 FOR OP'S CHECKSDR DL76S020434Flap · malfunctionedON APPROACH TRAILING EDGE FLAP DISAGREE EICAS WITH T/E FLAP. SHUT DOWN STATUS MSG LANDED WITH FLAPS AT 23 DEG. T/S PER FIM 27-51-00 FIG 114B. SYS TEST NORMAL. MSG CLEARED, NO FAULTS.SDR CA020416006Torque Tube · sheared(CAN) THE EMERGENCY FLAP HANDLE FAILED AT 3 DEGREES. THE TORQUE TUBE WAS FOUND SHEARED AT THE UPPER CRANK ADAPTER FITTING JUST BELOW THE FLOORBOARD. THE TORQUE TUBE WAS REPLACED AND THE SYSTEM WAS TESTED SERVICEABLE.SDR COMA0260248Fcu · malfunctionedFLIGHT 5903 FLAPS FAIL MESSAGE WHILE A/C AT GATE. REPLACED THE FECU.SDR GTIA020288Flap · lack of lubeLGA - FLT 1864 - FLAPS DID NOT FULLY RETRACT AFTER LANDING. CLEANED AND INSPECTED RIGHT TRAILING EDGE FLAP LUBED FLAPS, OPS NORMAL. (M)SDR CA020416002Rod · loose(CAN) AFTER COMPLETING AD CF-80-03 & SB6/390 THE TRIM ROD WAS BEING ADJUSTED AT INSTALLATION WHEN IT WAS FOUND THAT THE FORWARD SWAG WAS ALLOWING THE ROD END FITTING TO ROTATE. THE ROD WAS REPLACED.SDR DL738020429Fseu · malfunctionedTRAILING EDGE FLAPS EXTENDED AT 240 KTS TO FIVE DEGREES, FLAPS STOPPED AT MID POSITION BETWEEN UP AND 1. T/S-READ FSEU BITE, NO FAULTS. REPLACED FSEU PER M/M, NO FAULTS. INSPECTED FLAPS AND FLAPS OPERATE NORMALLY. OK FOR SERVICE.SDR GAIA02032OPConnector · dirtyFLT 713 - HSV-FWA - ON APPROACH, THE AIRCRAFT HAD OUTBOARD SPLIT FLAP INDICATION. THE CREW USED THE EMERGENCY CHECKLIST AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED AT HSV UNEVENTFUL. CLEANED THE CONNECTOR PLUG AT THE OUTBOARD FLAP TRANSMITTERS. CYCLED TSDR COMA0260246PaintFLIGHT 5012 AIRCRAFT ROLLS RIGHT WHEN FLAPS EXTENDED.SANDED ROUGH PAINT ON R/H OUTBD FLAP.SDR AUS20020334Control Cable · misrouted(AUS) FLAP CABLE RUN NR 244B BROKEN. FLAP CABLE RUN NO 242B FRAYED. INVESTIGATION FOUND THE CABLES HAD BEEN INCORRECTLY ROUTED ON THE WRONG SIDE OF THE PULLEY CABLE KEEPER. SUSPECT CAUSED DURINGAIRCRAFT MANUFACTURE. PERSONNEL/MAINTENANCE/MANUFACTURING ERROR.SDR COMA0260240FlapFLIGHT 5083 FLAPS FAILED AT 30 DEGREES DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR COMA0260238Actuator · bindingFLIGHT 5234 FLAPS FAILED MESSAGE. R/H OUTBD FLAP IS TWISTED.REPLACED R/H OUTBD FLAP ACTUATORS,SDR CA020507017Control Cable · frayed(CAN) LT AND RT UPPER FLAP CABLES FRAYED AT WING ROOT PULLEY.SDR COMA0260235Bpsu · malfunctionedFLIGHT 5297 FLAPS FAILED AT 0 DEGREES.REPLACED THE R/H BPSU.SDR C2XA02CL091Lever · faultyCLE FLIGHT NR 3052 THE CREW REPORTED UPON GEAR RETRACTION RECEIVED A LANDING GEAR WARNING AND THE WARNING WOULD NOT CANCEL UNTIL THE GEAR WAS EXTENDED. MAINTENANCE INSPECTED AND REPLACED THE FLAP SELECTOR LEVER. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WASDR COMA0260233FcuFLIGHT 5471 FLAPS FAIL MESSAGE.ADJUSTED THE FECU POTENTIOMETERS.SDR 2002FA0000525Cable · brokenON FINAL APPROACH, AIRCRAFT EXPERIENCED A SPLIT FLAP CONDITION, CAUSED BY BROKEN CABLE ASSEMBLY. FLAP ACTUATOR INBOARD (PN 14601007). CABLE HAD BROKEN ON RIGHT SIDE, 1 INCH FROM CABLE END, AT BELLCRANK ENTRY POINT. INSPECTION OF LEFT SIDE FLAP CABLE ASSEMBLSDR 2002F00360Control Cable · brokenWHILE ON APPROACH THE PILOT SELECTED HIS APPROACH FLAP SETTING OF 15 DEGREES. UPON DOING SO HE HEARD A BANG AND THE AIRCRAFT BEGAN A SLIGHT ROLL TO THE RIGHT. HE THEN RETRACTED THE FLAPS, WHICH CORRECTED THE SITUATION. HE CONTINUED HIS APPROACH AND MADE AN UNESDR DL738020388Sensor · inoperativeAFTER SELECTING FLAP SETTING 2 DEGREES AT AIRSPEED 210 KNOTS THE FLAPS SPLIT ASYMMETRICALLY. THE RIGHT TRAILING EDGE FLAP WAS AT 1.75 DEGREES AND THE LEFT TRAILING EDGE FLAP INDICATED 1.3 DEGREES. PROCEDURE FOLLOWED IAW QR HANDBOOK. LANDING ACCOMPLISHED NOSDR 2002FA0000539Motor · inoperativeFLAPS INOPERATIVE, TROUBLESHOOTING, FOUND FLAP MOTOR INOPERATIVE. REPLACED MOTOR ASSEMBLY.SDR MALA020216Control Valve · failedON APPROACH OF FLIGHT 3250 INTO MQT, FLAPS WOULD NOT COME DOWN, VERY LITTLE BRAKING WAS USED DURING ROLLOUT. MAINTENANCE REMOVED AND REPLACED FLAP CONTROL VALVE AND REMOVED AND REPLACED FLAP CONTROLLER. ALL CHECKS GOOD AT THIS TIME.SDR CA020326009Arm · cracked(CAN) SMALL CRACK FOUND IN RADIUS OF THE BASE OF THE MASS BALANCE ARM.SDR 02FDEA00218Flap · malfunctionedWRI 27-50-7942 WITH FLAPS SEL AT 50 DEG LEFT TAPE IND 45 DEG IN FLT ON GRD FLAP TAPE GO TO 50 DEG. REMOVED AND REPLACED O/B FLAP PER MM 27-50-02-4.SDR COMA0260219FlapFLIGHT 5654 FLAPS FAILED AFTER T/O.COULD NOT DUPLICATE. INSPECTED FLAP SYSTEM, NO DEFECTS FOUND.SDR COMA0260213FlapFLIGHT 5360 FLAPS FAILED AT 20 DEGREES DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR SWIA200210756Fcu · malfunctionedFLAP CONTROL FAULT, INBOARD FLAPS STUCK. REPLACED FCU WITH SERVICEABLE UNIT. OPS CHECK GOOD.SDR COMA0260209FlapFLIGHT 5921 FLAPS FAILED AT 27 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.SDR COMA0260207FlapFLIGHT 5820 FLAPS FAILED AT 0 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0260206Bpsu · malfunctionedFLIGHT 5295 FLAPS FAILED AT 20 DEGREES.REPLACED THE R/H BPSU.SDR 02FDEA00209Control Valve · faultyAFTER T/O 9L FLL FLAP TAPES REMAIN IN T/O POS WITH HANDLE 0 EX. REMOVED AND REPLACED INBOARD FLAP CONTROL VALVE PER MM 27-52-02-2.SDR 02FDEA00204Indicator · failed02-71 ASYMMETRICAL INBD FLAPS DUR RETRACT STOPPED BETWEEN 5 DEG & 2 DEG. R&R INBD FLAP IND PER MM 27-52-021-2.SDR 2002UALA00502Bellcrank · fracturedBELL CRANK FOUND FRACTURED ALONG WITH ADJACENT 113W1452-X PUSH ROD WITH ROD END FRACTURED. FOUND DAMAGED OVERWING FAIRING SPRT MLG BODY DOOR STOP STRUCTURE INSTL (49W4172-2,149W4175-1). MINOR DAMAGE (GOUGE TO INSIDE WALL OF I/B FLAP TRACK ON I/B FLAP). CLIPSDR COMA0260197Bpsu · malfunctionedFLIGHT 5234 - FLAPS FIALED AT 0 DEGREES.REPLACED THE L/H BPSU.SDR COMA0260198Fcu · malfunctionedFLIGHT 5436 FLAPS FIALED AT 0 DEGREES.REPLACED THE FECU
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