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 DALA2015120807476Jackscrew · corrodedINBD FLAP, INBD SCREWJACK END PITTED, CORRODED. R & R JACKSCREW ASSY IAW AMM 27-51-11.SDR O2GA2015121050101Unknown · malfunctionedAFTER TAKEOFF THE FLAPS WOULD NOT RETRACT TO 0*. DURING FLIGHT ALL OTHER HYD SYS WORKED. ACFT DIVERTED BACK & AFTER LANDING THE FLAPS WOULD NOT RETRACT TO 0*. ON POST FLIGHT NOTICED FLAP STUCK IN 7* POSITION. ACFT WAS INSPECTED & FERRIED WITH THE FLAPS AT SDR Q2SA20151203230Flap System · inoperativeTRAILING EDGE FLAPS WOULD NOT EXTEND ON APPROACH. CONDUCTED T/E FLAPS UP LANDING.SDR CA151202007Module · leaking(CAN) ON APPROACH FLIGHT, EXPERIENCED A L/E SLAT ASYMMETRY. A MISSED APPROACH WAS CONDUCTED AND THE QRH WAS CARRIED OUT BEFORE RETURNING FOR LANDING. AN EMERGENCY WAS NOT DECLARED. REPLACED FLAP/SLAT SHUTOFF VALVE MODULE IAW AMM 27-51-48-022-001.SDR AALA20151201004Sensor · faultedFLAPS WOULD NOT DEPLOY PAST 2 DEGREE USING FLAP HANDLE. ALTERNATE FLAP PROCEDURE USED 15 DEGREE LANDING. EMERGENCY DECLARED, LANDING UNEVENTFUL, AND ACFT WAS GROUNDED. MAINTENANCE FOUND A PUSHED BACK PIN IN THE NR 8 FLAP SKEW SENSOR. REMOVED AND REPLACED FLSDR R61A201511280882Torque Tube · failedAS CREW WAS RETRACTING THE FLAPS, RECEIVED A MASTER CAUTION FLAP FAIL MESSAGE. CREW RAN QRH, DECLARED AN EMERGENCY AND ELECTED TO RETURN TO DEPARTURE. LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE RT TORQUE TUBE HAD FALLEN OFF INBD SIDE OF THSDR CALA2015112400955Fseu · unserviceableON APPROACH FLAP 1 WAS SELECTED WITH NO MOVEMENT. QRH ACCOMPLISHED, LANDED WITH ALT FLAP 15D. PERFORMED FSEU BITE IAW TASK 27-51-00-810-80. R & R FSEU IAW AMM 27-51-00-01-400-801. FLAP OPERATIONS CHECKED GOOD AT THIS TIME.SDR QXEA2015112200618Roller · damagedON CLIMBOUT WHILE RETRACTING FLAPS FROM 15 TO 0, FELT A SHUDDERING. AFTER CONSULTING WITH MAINTENANCE CONTROL IT RESULTED IN A RETURN TO FIELD. LANDING UNEVENTFUL. UPON APPROACH, WHILE EXTENDING THE FLAPS FOR LANDING WE FELT THE SAME SHUDDERING WHILE EXTENDSDR FDEA201511223748Fseu · failedDURING DESCENT, RECEIVED EICAS TE ASYM, TE DISCRETE LIGHT & FLAP GAUGE BOTH NEEDLES INDICATED 1/2 WAY BETWEEN UP & 1. SPEED WAS 320 KNOTS & ALTITUDE WAS 21,500. WE SLOWED BELOW 240 KNOTS & READ QRH PROCEDURE. LANDED WITH SLATS EXTENDED & FLAPS UP. ONCE ACFSDR HYIA20151124003Flap · out of rigPILOT REPORTED ACFT ROLLS TO THE RT WHEN FLAPS ARE 15 DEGREES EXTENDED. INSPECTED & FOUND AN ASYMMETRICAL CONDITION WITH FLAPS. RIGGED FLAPS IAW MM CHAPTER 27.SDR FDEA201511213745Flap · stuckFLAP SYS 1 & 2 FAULT, FLAPS STUCK. REMOVED TWO BOLTS FROM RT TORQUE LIMITED COUPLER TO FOM. DRAINED FLUID FROM RT WING NR 1 FLAP DRIVE GEAR BOX FOR INSPECTION PURPOSE. GPS OVERRIDE SWITCH IN COCKPIT, CAPTAINS RIGHT KNEE, REQUIRES SAFETY. FOUND JAM FAULTS OSDR DJFA20151120001Flap System · failedENCOUNTERED A FLAP FAILURE WHEN SELECTING FLAP 10 FROM 0 ON DESCENT. PERFORMED ONE RESET WITH NO CHANGE. DECLARED AN EMER FOR PRIORITY HANDLING & LANDED WITHOUT FURTHER INCIDENT. PERFORMED TROUBLESHOOTING & FOUND FLAP CONTROL HANDLE NEEDED CLEANED. PERFORMSDR CA151116011Ecu · failed(CAN) FLAPS FAILED AFTER TAKE OFF RETURNED TO DEPARTURE. FLAPS WOULD NOT RESET. MX REPLACED FECU.SDR SIMA20151113003Flap · malfunctionedFLAP FAIL ON APPROACH, FAILED AT 0. RESET FLAP SYS & PERFORMED OPERATIONS TEST IAW AMM 27-51-00, WITH NO DEFECTS.SDR CA151113006Ecu · failed(CAN) ATB FLAPS FAIL AT 20, TROUBLESHOT TO FAULTY FECU.SDR SCNA20151112170Control Valve · failedFLAPS WOULD NOT MOVE FROM 25 POSITION DURING GO AROUND AT AIRPORT, WHEN FLAP LEVER WAS MOVED TO FLAPS 15 POSITION. R & R T/E FLAP CONTROL VALVE. R & R FLAP LEVER POSITION SWITCH. ALL TESTS REQUIRED PASSED NORMALLY.SDR YENA20151111551Handle · stuckFLAP HANDLE STUCK AT 2. RETURNED TO FIELD. NO OVERWEIGHT LANDING. R & R FLAP HANDLE IAW AMM 27-51-43, ALL OPS CK OK.SDR SWAA2015120246662Transmission · corrodedLEFT WING NR 4 FLAP TRACK TRANSMISSION BORE BOLT CORRODED. REPAIRED BORE IAW CMM.SDR SWAA2015113046486Transmission · corrodedLEFT WING NR 4 FLAP TRANSMISSION BORE CORRODED. R & R FLAP IAW SRM.SDR VNAA2015111100005Flap System · malfunctionedCREW REPORTED FLAP FAIL AT 30 DEGREES ON FINAL APPROACH. CREW DID A GO-AROUND, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW FIM AND DETERMINED SYS OPERATED NORMALLY AND THAT CAUSE OF DISCREPANCY WAS OPERATOR ERROR. MAINTENASDR HNAA2015111100332Flap System · malfunctionedFLAPS FAILED TO RETRACT FROM 5 TO 0 AFTER APPROXIMATELY 1 MINUTE AND FLAP TRIGGER SELECTED TWICE FLAPS RETRACTED. INSPECTED FLAP SWITCH AND WIRES. NO DEFECTS NOTED. CLEANED THE SWITCH AND CYCLED FLAPS MULTIPLE TIMES ON GROUND, NO DEFECTS FOUND.SDR CALA2015111794820Flap · malfunctionedFLAPS LOCKED AT POSITION 2, WING TIP BRAKES ENGAGED AT 190 KTS, RESET WTB FLAPS IAW AMM 27-50-00-869-006. PREFORMED OPERATIONS FLAP TEST IAW AMM 27-54-00-710-001, TESTED OK. ALSO CFDS SFCC 1 & 2 BITE TESTED OK IAW AMM 27-51-00. FLAPS WTB FAULT MSG CLEARED.SDR SIMA20151109001Controller · failedFLAP FAIL ON EICAS MSG DURING APPROACH. TROUBLESHOOTING IAW FIM TASK 27-51-00-810-817. CMC INDICATED RT TRANSMISSION FAIL. RESET FLAP SYS & PERFORMED OPERATIONAL CHECK. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED OR MSGS NOTED. ON PUSHBACK AFTER NR 1 ENG SSDR DXTA2015110606117Drive Assy · failedDESCENDING THRU 9000 MSL, 245K, ATTEMPTED TO EXTEND FLAPS TO 5 DEGREES, AT WHICH TIME EICAS INDICATED FLAPS FAIL. SLATS WERE FULLY DEPLOYED & FLAPS WERE EXTENDED LESS THAN 5 DEGREES. PER CHECKLIST, ATTEMPTED TO RESET FLAPS WITH NEGATIVE RESULTS. COMPLETED CSDR HYIA20151107001Push-Pull Rod · bentWHEN EXTENDING FLAPS 15 DEGREES, ACFT ROLLS RT UNCOMMANDED. REST OF FLAP DEPLOYMENT AFTER TRIM INITIATED FEELS NORMAL. INSPECTED & FOUND THE RT INBD & OTBD FLAP RODS BENT. R & R RIT INBD & OTBD FLAP PUSH & PULL RODS & RE-RIGGED FLAP CABLES.SDR SIMA20151104002Flap · malfunctionedFLAP FAIL ON EICAS & NO FLAP INDICATION SHOWS A DASH. TROUBLE SHOT FLAP DRIVE TX FAIL CMC MSG IAW FIM 27-51-00. FVS, FDMU & FPTU READINGS CHECK WITHIN LIMITS. RESET FLAP SYS. OPERATIONS TEST FLAP SYS PASSED IAW AMM 27-51-00-700-801-A.SDR CA151105009Cable · broken(CAN) ON APPROACH WHEN THE CREW SELECTED FLAPS FROM 0 TO 15 DEGREES, THE FLAP POSITION INDICATOR DID NOT RESPOND AND WAS NOTED TO BE INCORRECTLY INDICATING THAT THE FLAPS WERE AT 35 DEGREES. CORRESPONDING HYDRAULIC PRESSURE ANNUNCIATION DID NOT OCCUR. THE CRESDR DALA2015110306688Ball Screw · corrodedNR 3 FLAP TRACK BALL SCREW RUSTED. INSTALLED BALL SCREW ASSY IAW AMM.SDR FDEA201510293405Gearbox · lack of lubeSELECTED FLAPS 15 DEGREES AT 200 KTS. FLAPS SYS 1 & 2 FAULT LIGHTS & ON ECAM. CYCLED HANDLE WITH SAME RESULT. FOLLOWED ECAM & QRH. LANDED SLATS 30, FLAPS 0 UNEVENTFULLY & CANCELLED EMERGENCY. LUBED & SERVICED RT ANGLE GEARBOX, TORGUE LIMITER & NR 1 GEARBOSDR DALA2015103006609Shaft · corrodedNR 7 FLAP BALLSCREW SHAFT CORRODED AT DRIVE YOLK CONNECTION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0079:2751-2541-RT/003 00262 REPLACE BALLSCREW ASSY IAW AMM 27-51-21.SDR DALA2015102906589Ball Screw · corrodedNR 1 FLAP BALLSCREW SHAFT CORRODED AT DRIVE YOLK CONNECTION. REPLACED BALL SCREW ASSY IAW AMM 27-51-21.SDR DALA2015102906588Ball Screw · corrodedNR 2 FLAP DRIVE BALL SCREW SHAFT IS CORRODED AT YOLK DRIVE ATTACH POINT. REPLACED BALL SCREW ASSY IAW AMM 27-51-21.SDR CA151029013Control System · contaminated(CAN) ON TAKEOFF, WHEN FLIGHT CREW SET THE FLAP TO 0 FROM 20, "FLAP FAIL" MESSAGE WAS DISPLAYED. THE AIRPLANE CONTINUED FLYING AND LANDED WITH NO FLAP. (NOT EMERGENCY) AS A RESULT OF INSPECTION AFTER THE LANDING BY THE FLIGHT CREW, SNOWY ACCUMULATION WAS CONFISDR 29GA2015102400001Flap System · out of rigFLIGHT 108: AT T/O NOSE TRYING TO LIFT OFF WELL BEFORE ROTATION SPEED. THEN NOTICED TRIM WAS .5 TO .7500 NOSE DOWN ON THE TRIM INDICATOR IN LEVEL FLIGHT, TO HOLD A NORMAL APPROACH/LANDING CONFIGURATION, TRIM INDICATED .7500 TO 1 UNIT NOSE DOWN BELOW GREEN ARC,SDR K11A2015102272201Torque Tube · detachedOTBD T/E FLAPS WENT ASYMMETRIC, FOUND LT T/E OTBD DRIVESHAFT TORQUE TUBE COUPLING CAME OFF.
RESECURED TORQUE TUBE, SAFETY WIRED, PERFORMED ADJUSTMENT AND TEST. NO DEFECTS NOTED AT THIS TIME.SDR DALA2015102206391Ball Screw · corrodedLT INBD T/E FLAP BALLSCREW CORROSION FOUND. SUMMARY, NR FOR ADDITIONAL INFORMATION 001-0067:2751-2539-LT/001 00195. REPLACED BALLSCREW ASSY IAW AMM 27-51-11. OPS TEST C/W ON R/C 2751-2538, STEP 18.SDR CA151020002Handle · failed(CAN) FLAP HANDLE MATERIAL FAILED JUST FWD OF CABLE ATTACHMENT.SDR CA151020001Handle · failed(CAN) FLAP HANDLE MATERIAL FAILED JUST FWD OF CABLE ATTACHMENT. THIS IS OUR 3RD FAILURE OF THIS PART ALONG WITH 1 CRACKED AND REMOVED FROM SERVICE.SDR A6WA201543142Flap · failedFLAPS FAILED IN CRUISE AT FL 290 AT ZERO DEGREES. COMPLIED WITH QRH. HIGHEST BTMS READING WAS 9 UNITS. PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-018G BOX 12. FLAPS RESET, PLACARDED & PLACED ON MEL.SDR HYIA20151019001Rod · severedPILOT REPORTED ON APPROACH, WHEN FLAPS DEPLOYED TO 30 DEGREES THE ACFT ROLLED AGGRESSIVELY TO THE RIGHT. INSPECTED & FOUND THE RT FLAP OTBD FLAP ROD SEVERED. R & R THE FLAP ROD, OPERATIONALLY CHECKED GOOD.SDR 2015FA0000604Selector Valve · failedPILOT REPORTED LANDING GEAR WOULD NOT EXTEND. TROUBLESHOT, FOUND THAT THE HYDRAULIC POWERPACK WOULD CYCLE 5 TIMES, THEN SHUTOFF. ACCORDING TO THE MM THIS IS NORMAL AND IF THIS HAPPENS THE PILOT MUST RESET THE HYD POWERPACK CIRCUIT BREAKER AS THE SYSTEM HAS ASDR DALA2015102206366Mount · corrodedNR 7 BALLSCREW GIMBAL MOUNTS CORRODED INTERNALLY, MARKED. REPLACED BALLSCREW IAW AMM 27-51-21. TO BE INSTALLED ON CARD 2751-2542.SDR SWAA2015102745410Torque Tube · corrodedRIGHT WING SECONDARY TORQUE TUBE ON INBD FLAP CORRODED. REPLACED TUBE IAW CMM.SDR DALA2015101406201Tube · corrodedLT WHEEL WELL INBD FLAP. TUBE THAT CONNECTS THE CARRIAGE TO THE FLAP HAS RUST ON THE FLAP SIDE. REPLACED OUTER TORQUE TUBE, FAIL SAFE TORQUE TUBE AND SUPPORT FITTINGS, REF EA 06-097981-14, REV A.SDR A6WA201543123Flap · failedFLAPS FAILED AT 0, PRIOR TO APPROACH. FLAPS FAILED WHEN SELECTING FLAPS 8. PERFORMED FLAP RESET INCLUDING BREAKER RESET, FLAP FAIL CAUTION REMAINS.SDR DALA2015110506747Gimbal Joint · corrodedNR 8 BALL SCREW GIMBAL MOUNTS CORRODED INTERNALLY, MARKED. REPLACED NR 8 BALL SCREW ASSY IAW AMM 27-51-21.SDR RU3A20151002025Flap · failedFLAP FAIL IN FLIGHT STUCK AT 20'.SDR DALA2015093005886Ball Screw · corrodedNR 5 BALLSCREW ASSY, AFT UNIVERAL JOINT ARM CORRODED INTERNALLY. REPLACED JOINT MM 27-51-11.SDR DALA2015092905859Ballscrew · corrodedNR 6 BALLSCREW ASSY, FWD MOUNT AREA OF JACKSCREW CORRODED INTERNALLY AND BALLSCREW GIMBAL MOUNTS ARE CORRODED INTERNALLY. REPLACED JACKSCREW REF MM 27-51 AND REF NR.SDR DALA2015092905858Ballscrew · corrodedNR 6 BALLSCREW ASSY, AFT UNIVERAL JOINT ARM CORRODED INTERNALLY AND BALLSCREW GIMBAL MOUNTS ARE CORRODED INTERNALLY. REPLACED UNIVERSAL JOINT IAW MM 27-51-11.
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