JASC 2752
Service difficulty reports · 1,979
Reports filed under 2752 · Trailing Edge Flap Actuator, 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 = '2752' 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 = '2752' 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 CA190515003Actuator · failed(CAN) DURING TAKE-OFF THE CREW REPORTED `FLAPS FAIL` MESSAGE APPEARED ON EICAS AND THE FLAPS COULD NOT BE RETRACTED. AN ATB WAS INITIATED AND UNEVENTFUL LANDING PERFORMED WITH THE FLAPS STUCK IN 20 DEG POSITION. NO EMERGENCY DECLARED. GROUND INSPECTION REVEALESDR CA190514008Motor · failed(CAN) DURING PRE-FLIGHT, TECHNICIAN NOTICED THE #2 FLAP MOTOR C/B (CB2-B5) TRIPPED. PUSH C/B BACK IN AND SELECTED FLAPS TO 20 DEG. ONCE FLAPS STARTED TO MOVE THE C/B TRIPPED AGAIN. FLAP MOTOR REPLACED. (TC# 20190514008)SDR AALA201905029009Gearbox · bindingAIRCRAFT WAS GROUNDED: PILOT REPORTS FLAP RETRACTION AND EXTENSION, BETWEEN UP AND 1 GENERATES A LOUD GRINDING NOISE. SEEMS TO BE ON LEFT (CA) SIDE OF ACFT. INFLIGHT ONLY. MAINTENANCE REPLACED THE LT T/E FLAP OFFSET GEARBOX IAW AMM 27-51-38-401. OPS CHECK OK.SDR 2019FA0000122Actuator · crackedDURING REINSTALLATION OF FLAP AFTER PAINT REFURBISHMENT, FOUND RIGHT OUTBOARD P/N 90-521024-2, S/N 540-M-98 FLAP ACTUATOR ( JACK SCREW DESIGN ) ASSEMBLY WAS CRACKED NEARLY ENTIRE LENGTH OF ACTUATOR SHAFT BARREL( APPROX 4 INCHES ). PART WAS REPLACED WITH OVERHASDR CA190416010Actuator · worn(CAN) AIR TURN BACK CARRIED OUT DUE TO FLAP DRIVE CAUTION LIGHT. MAINTENANCE REPLACED THE #3 FLAP DRIVE ACTUATOR AND RETURNED THE AIRCRAFT TO SERVICE. (TC# 20190416010)SDR CA190405016Roll Pin · migrated(CAN) ON 02-APR-2019 DURING TAXI TO THE RUNWAY, THE AIRCRAFT C/O A GROUND TURN-BACK AND RETURN TO BLOCKS DUE TO FLAPS STUCK BETWEEN 15 AND 35 DEGREES. MAINTENANCE CREW FOUND THE LH #2 FLAP ACTUATOR TO BE SEIZED. UPON FURTHER INSPECTION THE FLAP ACTUATOR ROLL SDR DALA2019032501933Jackscrew · corrodedSHIP 5653 RT WING NR 5 JACKSCREW CORRODED. CORRECTIVE ACTION: REMOVED & REPLACED RT WING NR 5 JACKSCREW ASSY PER AMM 27-51 OPS CHECK TO BE ACCOMPLISHED ON JIC CARD. (0998973)SDR VNAA2019032211102Pdu · failedDURING LANDING FLAPS FAILED AT 8. CREW RAN QRH AND DECLARED EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO GATE 1. 24-MAR-2019 15:27 EST / C/E TO 27-050-004-09 DOF. R/R FLAP PDU IAW AMM 27-52-01-000/400-801. RE RIGGED LT AND RT BPSU'S IAW AMM 27-51-SDR VNAA2019032211101Actuator · failedON APPROACH INTO CLT THE CREW RECEIVED A FLAPS FAIL MSG, DECLARED AN EMERGENCY AND LANDED SAFELY. MX REPLACED RT NR 4 FLAP ACTUATOR OPS CHECK GOOD.SDR AALA2019032109002Motor · failedTHE ALTERNATE FLAPS SYSTEM FAILED DURING AN INFLIGHT CHECK, LEADING EDGE DEVICES EXTENDED, HAD ZERO TRAILING EDGE FLAP MOVEMENT. MAINTENANCE REPLACED THE ELECTRIC FLAP MOTOR IAW AMM 27-51-53-401. OPS CHECKED GOOD IAW AMM 27-51-00-860-802.SDR AALA201903189011Actuator · bindingTHE PILOT REPORTED THAT AFTER LANDING, THE FLAPS WERE RAISED AND THE FLAPS FAIL EICAS MESSAGE ILLUMINATED. THE FLAP INDICATOR INDICATES ZERO WITH AN AMBER BOX. MAINTNENACE FOUND THE RT WING NR 2 FLAP ACTUATOR BINDING AND THE OVER TORQUE INDICATOR DAMAGED. SDR DALA2019031901795Ballscrew · corrodedSHIP 6706 CORROSION ON RT WING INBD FLAP INBD BALL SCREW (AD). CORRECTIVE ACTION: SUMMARY OF NRC 00383: INBD FLAP INBD BALL SCREW WAS REMOVED AND SERVICEABLE INBD FLAP INBD BALL RT WING WAS INSTALLED PER AMM 27-51. TESTS OK. (0978538)SDR R61A201902280208Actuator · smokeSMOKEY SMELL IN MID CABIN, FLAP LOW RATE MESSAGE. UPON FURTHER INSPECTION, SMOKE FOUND IN MID E-BAY COMING FROM SF-ACE 2 IAW AMM 27-53-02. OPS CHECK GOOD.SDR QXEA2019012900053Power Unit · malfunctionedFLAP POWER CAUTION AFTER SELECTING FLAPS 15 FLAPS REMAINED AT FLAPS 10, FLAPS CONT CIRCUIT BREAKER RESET AS PER FLAP POWER CAUTION CHECKLIST. PERFORMED 2ND BREAKER RESET AS PER MAINTENANCE WITH SAME RESULT. PERFORMED MISSED APPROACH THEN RETURNED TO FIELD. LANSDR ABXA20190108002Drive Shaft · disconnectedAFTER TAKEOFF, THE “TE FLAP ASYM” EICAS MESSAGE ILLUMINATED. THE LEFT FLAP INDICATOR SHOWED APPROXIMATELY 4 DEGREES OF FLAPS, AND THE RIGHT FLAP INDICATOR SHOWED 5 DEGREES. MOVING THE FLAP LEVER HAD NO EFFECT ON THE FLAPS. THE CREW PERFORMED AN AIR TURN BACK ASDR DALA2019011000162Nut · corrodedSHIP 6704 INITIAL INSPECTION. CORROSION IN OUTBD BALLSCREW NUT OF INBD FLAP AT LT WING. CORRECTIVE ACTION: REF NRC 00446, OUTBOARD BALL SCREW OF INBD FLAP LT WING WAS REPLACED. (0893121)SDR SWAA2018121227566Drive Shaft · shearedMANUAL FLAP DRIVE SHAFT SHEARED. R&R FLAP POWER DRIVE UNIT MANUAL DRIVE SHEAROUT PER AMM.SDR UIEA2018102902422Actuator · malfunctionedTRAILING EDGE FLAP DISAGREE EICAS ON CLIMB OUT AT INITIAL FLAP RETRACTION MOVEMENT. REMOVED AND REPLACED FLAP LOAD ACTUATOR IAW AMM 27-51-30 OPS CHECK SATISFACTORY.SDR DALA2018103106367Ballscrew · corrodedSHIP 684 CORROSION ON OB BALLSCREW NUT AT LT WING INB FLAP. CORRECTIVE ACTION: R/R O/B BALLSCREW NUT AT LT WING INBD FLAP. OPS TEST OK. (0801497)SDR DALA2018103106360Ballscrew · corrodedSHIP 684 CORROSION ON OB BALLSCREW LARGE SHAFT AT LT WING INBD FLAP. CORRECTIVE ACTION: NRC S/N: 0224: OB BALLSCREW LARGE SHAFT AT LT WING INBD FLAP WAS REPLACED FOR A NEW ONE PER AMM 27-51. OPERATIONAL TEST WAS PERFORMED PER AMM 27-51. (0799257).SDR DALA2018102606320Adapter · corroded(AIRCRAFT 684, L/P 0799260) RII: CORROSION ON OB BALLSCREW ADAPTER AT LT WING INBD FLAP (AI). OB BALLSCREW ADAPTER AT LT WING INBD FLAP WAS REPLACED FOR A NEW ONE PER AMM 27-51-11-424-020 PAR. A TO E.SDR DALA2018102606319Ballscrew · corroded(AIRCRAFT 684, L/P 0799249) RII: CORROSION ON OB BALLSCREW SMALL SHAFT AT LT WING INBD FLAP (AI). OB BALLSCREW SMALL SHAFT AT LT WING INBD FLAP WAS REPLACED FOR A NEW ONE PER AMM 27-51-11-424-020 PAR. A TO E.SDR DALA2018102606318Ballscrew · corroded(AIRCRAFT 684, L/P 0799246) RII: CORROSION ON OB BALLSCREW GIMBAL AT LT WING INBD FLAP (AI). OB BALLSCREW GIMBAL AT LT WING INBD FLAP WAS REPLACED FOR A NEW ONE PER AMM 27-51-11-424-020 PAR. A TO E.SDR DALA2018091805647Ballscrew · corrodedCORROSION ON BALLSCREW NUT IN INBD FLAP OUTBD BALLSCREW AT RT WING. R&R OUTBOARD BALLSCREW OF INBOARD FLAP AT RT WING. TEST OK.SDR JIKA201809100402Actuator · defectiveAFTER T/O FROM KONT AND RETRACTING THE FLAPS AT APPROX 1000 FEET, FLAP DISAGREEMENT LIGHT ILLUMINATED. CREW PERFORMED A SYSTEM CHECK PER QRH AND WAS UNABLE TO CLEAR THE FLAP DISAGREEMENT WARNING. DECLARED AN EMERGENCY, RETURNED TO KONT AND LANDED WITHOUT INCIDSDR O2GA2018090150901Actuator · failedIMMEDIATELY AFTER TAKEOFF EXCESSIVE FORWARD PRESSURE WAS REQUIRED TO PREVENT THE AIRCRAFT FROM PITCHING UP. THE POWER WAS PULLED BACK TO 60% AND TRIM ALMOST FULL FORWARD TO MAINTAIN CONTROLLED CLIMB. EMERGENCY DECLARED AND DIVERTED BACK TO KMCO. LANDING WAS UNSDR REXA201808140684Actuator · failedFLAPS FAILED AT 8. AN EMERGENCY WAS DECLARED. REMOVED AND REPLACED THE RT MID FLAP ACTUATOR IAW AMM 27-52-09. OPS CHECKED GOOD.
SDR DALA2018061203980Ballscrew · corrodedPITTING CORROSION ON BALLSCREW NUT OF RIGHT WING INBOARD TRAILING EDGE FLAP. BALLSCREW ASSY OF INBOARD TRAILING EDGE FLAP AT RT WING WAS REPLACED.SDR DALA2018051503401Ball Screw · corrodedWHILE PERFORMING FLAP BALLSCREW INSPECTION FOUND THE NR 4 FLAP TRACK BALLSCREW TO HAVE CORROSION. REMOVED AND REPLACED LT I/B FLAP I/B BALLSCREW IAW AMM 27-51-10 AND 11.SDR R61A20180423506Actuator · failedFLAPS FAILED DURING DESCENT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R THE NR 2 FLAP ACTUATOR IAW AMM 27-51-03. OPS CHECKED GOOD.SDR B4VR2018032100001Actuator · failedTOTAL FLAP FAILURE IN FLIGHT. FLAP ACTUATOR FAILED IN FLIGHT CAUSING LOSS OF FLAP CONTROL. FLAPS WERE FREE FLOATING AFTER FAILURE.SDR QXEA2018022600071Actuator · malfunctionedON FINAL APPROACH WHILE SELECTING FLAPS 5, THE FLAP INDICATOR, INDICATED BETWEEN 0 DEGREES AND 5 DEGREES AND THE FLAP DRIVE CAUTION LIGHT ILLUMINATED. AFTER RUNNING THE E/A CHECKLIST AND PUTTING THE FLAPS TO 0 DEGREES, THE FLAPS RETRACTED NORMALLY AND THE FLAPSDR SWAA2018022220010Rod · brokenLT INBOARD AFT FLAP ACTUATING MECHANISM ROD BROKEN. R&R ROD IAW AMM AND EA.SDR CVGA20180215001Actuator · leakingCREW NOTICED A DIFFERENCE IN FLAP ANGLE FROM ONE WING VERSUS THE OTHER WHILE EN ROUTE. CREW ELECTED TO PERFORM A NO FLAP LANDING. DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT.SDR DALA2018012200346Transmission · trippedDIVERTED DUE TO A T/E FLAP DISAGREE. TROUBLESHOT IAW FIM. BITE TEST OF FSEU'S AND FSAM NTF. FOUND LEFT OUTBOARD TRANSMISSION TORQUE INDICATOR TRIPPED. SERVICED TRANSMISSION IAW AMM 12-13. RAN FLAPS 7 TIMES AND INDICATOR STAYED IN.SDR 19EA201801120001Actuator · malfunctionedON APPROACH, HAD A FLAP FAIL MESSAGE. DECLARED AN EMERGENCY AND LANDED WITH OUT INCIDENT. TWO FLAP ACTUATORS TESTING CLOSE TO THE LIMITS. REPLACED BOTH FLAP ACTUATORS WITH NO OTHER PROBLEMS NOTED.SDR DALA2017121908739Actuator · corrodedRIGHT WING NR 6 FLAP ROTARY ACTUATOR CORRODED. INSTALLED TEE ANGLE GEARBOX PER AMM 27-51-05. FINAL ADJUSTMENT AND OP CK TO BE C/W ON ROUTINE CARD 2751-01050-02.SDR SWAA2017112117965Transmission · faultyDECLARED EMERGENCY, GOING FROM FLAPS 5 TO 15, FLAPS STAYED IN 5 POSITION WITH ASYMMETRY. FLAPS WOULD NOT RETRACT AFTER LANDING. R&R TRANSMISSION IAW AMM.SDR HALA2017110700268Coupler · failedON FINAL, TRAILING EDGE ASYMMETRY 5 AND 20. FOUND NR 2 OTBD FLAP ROTARY ACTUATOR OVERLOAD TRIP INDICATOR TRIPPED.SDR 2017FA0000607Collar · looseFLAPS FAILED IN FLIGHT: FOUND FLAP SWITCH'S ACTUATING COLLAR UNSCREWED FROM FLAP ACTUATING TUBE ON JACK SCREW.SDR UIEA2017102502016Actuator · corrodedFOUND CORROSION ON ROTARY ACTUATOR POSITION NR 8. REMOVED AND REPLACED ROTARY ACTUATOR.SDR UIEA2017102502091Actuator · corrodedPOSITION 5 FLAP ROTARY ACTUATOR FOUND CORRODED IAW SB 767-27A0229 R1. THE TE FLAP ROTARY ACTUATOR WAS REPLACED.SDR EPUA2017100917001Actuator · seizedPILOT REPORTED AN ODOR OF SMOKE IN COCKPIT DURING TAXI. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THAT THE FLAP ACTUATOR ASSEMBLY HAD SEIZED AND FAILED TO OPERATE FLAPS TO SELECTED SETTING. REPLACED THE FLAP ACTUATOR ASSEMBLY. RETURNED AIRCRAFT TO SSDR DALA2017082106309Actuator · malfunctionedWITH SLATS EXTENDED, THE AIRCRAFT ROLLED TO THE RIGHT, SUBSTANTIALLY. TRIM REQUIRED IS 3 DEGREES LT OF THE TRIM REQUIRED WITH A CLEAN WING. DURING CRUISE THE REQUIRED TRIM IS LESS THAN 1 UNIT RIGHT BOTH RUDDER/AILERON WITH BALANCED POWER & FUEL. FLAP BUSS TSDR A6WA201745168Actuator · failedFLAPS FAILED AT 27 DEGREES DURING APPROACH. EMERGENCY DECLARED. REMOVED AND REPLACED THE LT FLAP ACTUATOR IAW AMM27-53-05. OPS CHECKED GOOD.SDR YENA201707130579Actuator · failedEMERGENCY DECLARED. RECEIVED A FLAP FAIL MESSAGE ON SHORT FINAL SELECTED GEAR DOWN, FLAPS 3. THE FLAPS STUCK AT 2. RAN THE QRH FOR FLAP FAIL AND LANDED UNEVENTFULLY. R & R THE LT & RT NR 2 FLAP ACTUATOR IAW AMM 27-51-01. OPS CHECKED NORMAL. ALL FAULSDR YENA201707130578Actuator · failedEMERGENCY DECLARED. RECEIVED A FLAP FAIL MESSAGE ON SHORT FINAL WHEN WE SELECTED GEAR DOWN, FLAPS 3. THE FLAPS STUCK AT 2. RAN THE QRH FOR FLAP FAIL AND LANDED UNEVENTFULLY. R & R THE LT & RT NR 2 FLAP ACTUATORS IAW AMM 27-51-01. OPS CHECKED NORMAL. ALL SDR UIEA2017053100896Rotary Actuator · corrodedCORRODED NR 2 TE FLAP ROTARY ACTUATOR ON LT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.SDR UIEA2017053100897Actuator · corrodedCORRODED NR 3 TE FLAP ROTARY ACTUATOR ON LT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.SDR UIEA2017053100898Actuator · corrodedCORRODED POSITION NR 4 TE FLAP ROTARY ACTUATOR ON LEFT TE FLAP. REMOVED AND REPLACED IAW 8017-TALLY 1113, AND ENGINEERING ORDER 6727A007_CS.
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