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 SWAA2015121747252Motor · faultyDECLARED EMER, FLAP HANDLE IN 5, FLAPS WOULD NOT GO PAST POSITION 2 ON INDICATOR. R & R FLAP HYD MOTOR IAW AMM.SDR SWAA2015121647181Transmission · looseDIVERSION, DECLARED EMER. NR 1 FLAP FAIRING CAME OUT OF TRACKS. R & R NR 2 FLAP TRANSMISSION IAW AMM.SDR CA151106006Actuator · binding(CAN) AFTER LANDING THE FLIGHT CREW PERFORMED THE AFTER LANDING CHECKLIST AND SELECTED THE FLAPS TO FULL UP POSITION THEY NOTICED THAT THE INDICATOR STOP AT THE 15 DEGREE SETTING. AFTER PARKING THE ACFT THE FLIGHT CREW CHECKED THE FLAPS AND FOUND THEM AT OR LSDR CA151029026Pdu · failed(CAN) FLAP HALFSPEED MESSAGE ON TAXI OUT - EXTENDING FLAPS FROM ZERO OT 8. CB RESET OK. AFTER TAKEOFF ON RETRACTION FLAP HALFSPEED MESSAGE CAME BACK. DECISION TO RETURN A/C TO AIRPORT. (FLAP SKEW DET. SYSTEM. M TO DEACTIVATE) MAINTENANCE FOUND FLAP POWER DRIVESDR YENA20151018472Actuator · failedDIVERTED DUE TO FLAP FAIL UPON EXTENSION. FLAPS NEVER EXTENDED BEYOND 2. FLAPS LOCKED AT ZERO. FOUND LT SIDE NR 2 FLAP ACTUATOR JAMMED. R & R LT SIDE NR 2 FLAP ACTUATOR IAW AMM 27-51-01. RIG AND OPS FOUND GOOD.SDR DALA2015101606229Actuator · failedAIRCRAFT DIVERTED AFTER TAKEOF DUE TO A FLAP ASYMMETRY MESSAGE L/E SLAT ASYM EICAS APPEARED, FLAP POSITION INDICATOR SHOWS POSITION BETWEEN UP AND 1. COMPLIED WITH QRH PROCEDURE. SWAPPED FSCU NR 2 TO NR 1 IAW AMM. FOUND NR 5 SLAT INBD ROTARY ACTUATOR TRIPPEDSDR DALA2015100806028Mount · corrodedNR 5 BALLSCREW ASSY, FWD MOUNT AREA OF JACKSCREW CORRODED, REF NR00226. REPLACED BALLSCREW REF AMM 27-51-11.SDR CA151002005Drive Shaft · contaminated(CAN) ON DESCENT, FLAP FAIL MESSAGE WAS DISPLAYED. FOUND WET CONDITION WITH CONTAMINATION. (OIL OR GREASE) ON THE DRIVE SHAFT WHICH CONNECT TO THE LT OB FLAP IB ACTUATOR.SDR DALA2015093005887Drive Shaft · corrodedDRIVE SHAFT FOR NR 5 FLAP DRIVE TRANSMISSION IS CORRODED. REPLACED DRIVE SHAFT REF MM 27-51-34.SDR VNAA2015092800028Actuator · bindingCREW REPORTED FLAPS FAIL MESSAGE AT 160 KNOTS AND 40/39 DEGREE ASYMMETRY ON EXTENSION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW ACFT FIM, R & R RT INBD FLAP OTBD ACTUATOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASEDSDR CA150923013Actuator · malfunctioned(CAN) FLAP FAIL CAUTION ILLUMINATED INBOUND THEN ON APPROACH FLAPS SELECTED TO FLAP 8 AND THE FLAPS FAIL CAUTION LIGHT ILLUMINATED IMMEDIATELY. CREW REPORT THAT THEY DID NOT ENCOUNTER AND ICING OR RAIN ON ROUTE. THEY DID PASS THROUGH A CLOUD LAYER. OAT AT TIMESDR CA150911009Flex Drive · damaged(CAN) FLAP FAIL ON APPROACH AT 1800 FT AND APPROXIMATELY 155-160 KIAS. FLAPS STOPPED AT 37 DEGREES. NO EMERGENCY DECLARED. MAINTENANCE REPLACED LT NR 1 AND NR 2 FLEX SHAFTS AND ALSO PDU. RIG CHECK OF THE BPSU COMPLETED.SDR REXA2015090900855Flex Drive · damagedFLAP FAIL ON ARRIVAL, 37 DEGREES, 1800 FEET, SPEED ROUGHLY 155 - 160. R & R LT BPSU IAW AMM 27-51-10, NO FIX. R & R LT NR 1 & 2 FLEX SHAFTS, FLAP IAW AMM 27-53-10. DUE TO DAMAGE, CLEANED NR 3 & 4 FLEX SHAFTS IAW AMM 27-53-10. R & R FLAP PDU IAW AMM 27-52-0SDR CA150825003Shaft · broken(CAN) FLEX FLAP DRIVE FAILED ON THE OUTBD RT OTBD FLAP ACTUATOR .SDR CA150824011Actuator · overheated(CAN) THE CREW PERFORMED A FLAP ZERO LANDING DUE TO A FLAP FAILURE. THERE WAS NO EMERGENCY DECLARED AND THE FA WAS ADVISED OF AN ABNORMAL LANDING. THE FLAPS WERE DEFERRED BY MEL 27-02 AND LATER INVESTIGATED BY MAINTENANCE. IT WAS DETERMINED THAT 2 ACTUATORS SDR CA150814003Motor · failed(CAN) PAN PAN DECLARED WITH ATC DUE TO FLAP FAIL. FAULT CODE 27512014ACE RETRIVED FROM CMC FIM PROCEEDURE 27-51-00 COMPLETED TO BOX NR 8 NIL FAULTS R/H FPDU MOTOR REPLACED AS PER AMM 27-53-03 SYST OPS OK NORMAL.SDR ABXA20150710085Shaft · corrodedREMOVED & REPLACED LT INBD FLAP 6 - 6 PIN IAW AMM 27-51-04-002-134 & 27-51-04-402-135. CORRODED LEVEL 2, PN 113T1216-1, PART NAME SHAFT ASSEMBLY, SN NSN & ACFT WAS GNDED.SDR CA150710021Actuator · worn(CAN) DURING A PHASE INSPECTION, ALL THE FLAP ACTUATORS WHERE REPLACED DUE TO EXCESSIVE WEAR. UPON RIGGING THE FLAPS A LARGE BANG WAS HEARD FROM THE LT OTBD FLAP. THE FLAP FLEX CABLE HAD SNAPPED DURING THE FLAP DOWN TEST. AN INVESTIGATION REVEALED THAT THE SDR 2015F00075Actuator · faultedON LANDING AND CYCLING FLAPS BACK TO THE UP POSITION, A FLAP FAIL CAS MESSAGE ACTIVATED. PILOTS WERE ABLE TO RESET FLAPS AND COMPLETE MOVING FLAPS TO THE FULL UP POSITION. ON TROUBLESHOOTING WITH MAINTENANCE COMPUTER, WE WERE UNABLE TO FIND ANY ACTIVE FAULTSSDR 2015F00083Actuator · faultedAFTER LANDING THE PILOT REPORTED A FLAP FAIL CAS MESSAGE. TRIED TO PERFORM A FLAP RESET PROCEDURE, UPON FIRST CYCLE OF FLAP SAME CAS MESSAGE. UPON TROUBLE SHOOTING WITH MAINTENANCE COMPUTER IT WAS FOUND THAT THE FAILED FLAP ACTUATOR WAS CAUSING LVDT POSITION DSDR AALA20150601009Transmission · faultyEMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH, TE FLAP DISAGREE LIGHT ILLUMINATED WHEN FLAP HANDLE MOVED FROM UP TO 1 DETENT. R & R RT WING FLAP TRANSMISSIONS NR 4 & NR 8 IAW 27-51-17, LT WING INBD FLAP TRANSMISSION IAW 27-51-SDR AALA20150601007Transmission · faultyEMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH, TE FLAP DISAGREE LIGHT ILLUMINATED WHEN FLAP HANDLE MOVED FROM UP TO 1 DETENT. R & R RT WING FLAP TRANSMISSIONS NR 4 & NR 8 IAW 27-51-17, LT WING INBD FLAP TRANSMISSION IAW 27-51-SDR AALA20150529008Transmission · faultyEMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH, TE FLAP DISAGREE LIGHT ILLUMINATED WHEN FLAP HANDLE MOVED FROM UP TO 1 DETENT. R & R RT WING FLAP TRANSMISSIONS NR 4 & 8 IAW 27-51-17, LT WING INBD FLAP TRANSMISSION IAW 27-51-06 SDR CA151002009Cover · cracked(CAN) FOLLOWING INSPECTION AS REQUIRED BY AD 2014-22-09 AND SB 767-27A0229, OUT OF 4 ACFT INSPECTED, 1 AIRCRAFT WAS FOUND WITH A CRACKED COVER ASSY ON THE ACTUATOR FOUND IN POSITION NR 3. THE CONDITION IS NOT SOMETHING THAT THE SB IS LOOKING FOR AS THE SB IS SDR DALA2017041102915Actuator · corrodedRIGHT WING O/B FLAP ROTARY ACTUATOR NR 8 ARM ASSY SHAFT PITTED/CORRODED. REPLACED.SDR DALA2015050403092Actuator · corrodedCORROSION LEVEL: 2, LT OTBD FLAP ROTARY ACTUATOR CORRODED, NR 1 POSITION. REPLACED LT OTBD FLAP ROTARY ACTUATOR DUE TO CORROSION. LP1907932.SDR CA150406003Bushing · migrated(CAN) DURING LT, INBD FLAP REMOVAL, FOUND THE INBD ACTUATOR SCREW BUSHING MIGRATED OUT OF ACTUATOR.SDR A6WA201542592Actuator · failedWHEN SELECTING FLAPS FROM 8 DEG TO 20 DEG, AT 17 LT & 15 RT INDICATED, FLAPS FAILED. COMPLIED WITH FLAP CIRCUIT BREAKER RESET. ON 3RD RETRACTION FLAPS FAILED WHEN SELECTED TO 20 DEG, INDICATION LT 22 & RT 20, FELT SLIGHT RUMBLE WHEN FAILED. FOUND LT NR 3 FLSDR CA150415001Actuator · malfunctioned(CAN) "FLAP FAIL" ANNUNCIATOR ILLUMINATES IN FLIGHT SYSTEM CHECKS SERVICEABLE ON THE GROUND FLIGHT CONDITIONS: AFTER TAKEOFF AND ACFT AT CRUISE ALTITUDE AND SPEED WITH NO FLAP MOVEMENTS AND ABOUT 30 MINS INTO THE FLIGHT, FAULT RE-APPEARS, BUT ONCE THE ACFT LASDR CA150223010Ring · dislodged(CAN) DURING SCHEDULED LUBRICATION OF THE FLAP ACTUATORS, IT WAS NOTICED THAT THE ICE SCRAPER RING WAS PARTIALLY DISLODGED FROM THE LT NR 4 FLAP ACTUATOR. IT WAS NOTICED DUE TO THE EXCESSIVE PLAY BETWEEN THE BALL SCREW SHAFT AND ACTUATOR HOUSING ASSEMBLY.SDR CA150224027Actuator · binding(CAN) ON DEPARTURE IN THE CLIMB, THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE WHEN THE FLAPS WERE SELECTED FROM 8 TO 1 DEGREES. THE FLAPS FAILED AT 8 DEGREES. THE AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT AFTER BURNING OFF FUEL TO REACH THEIR MAX LANDING WEISDR CA150209001Actuator · failed(CAN) ON FINAL APPROACH, FLAPS WOULD NOT GO FROM 20 TO 25 IAW STANDARD OPERATING PROCEDURE, INCREASED SPEED & LANDED WITHOUT INCIDENT. NIL PAX REACTION, NIL EMER DECLARED WITH ATC. FLAP TE LOAD ALLEVIATION ACTUATOR REPLACED IAW AMM 27-51-30-401. TEST OF THE SDR CA150120023Actuator Cable · failed(CAN) UPON LANDING THE PILOT REQUESTED 20 DEGREES FLAP AND THE FLAPS STOPPED/STAYED AT THE 10 DEGREE SETTING. AFTER INSPECTION BY MAINTENANCE THE PRIMARY MOTOR SHAFT SHEAR PIN WAS FOUND SHEARED, THE SYSTEM FUNCTIONED PROPERLY IN STBY MODE, THE FLAP ACTUATOR ASSDR VNAA2015010500005Actuator · failedCREW REPORTED FLAPS FAIL MESSAGE AT ZERO DEGREES ON APPROACH. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW ACFT FAULT ISOLATION MANUAL, R & R NR 1 LT INBD FLAP ACTUATOR AND PERFORMED CHECKS IAW AMM. AFT RELEASED FOR SERVICE.SDR CA150116017Actuator · failed(CAN) FLAP FAIL AFTER TAKE OFF OUT WHEN SEL FLAPS FROM 8 TO 0 SETTING. FLAPS DID NOT MOVE THEY REMAINED AT 8 DEG. DECISION WAS MADE TO DIVERT TO ANOTHER AIRPORT. MAINENANCE DOWNLOADED AND FORWARDED ALL CODES FROM FECU TO FLEET TECH SUPPORT. AS PART OF TROUBLESSDR YENA20141122258Actuator · failedCREW DECLARED AN EMERGENCY DUE TO ON FLAP 1 SELECTION SLAT FAULT ECAM, LANDED WITH FLAPS 3, SLATS 0, FLAP/SLAT ISSUE. SLAT'S FAILED. ACCOMPLISHED SFCC SYSTEM 1 AND 2 RESET PERFORMED OPS CHECK OF SLATS AND FLAPS IAW 27-54-00, NO FAULTS. ON THE FOLLOWING FLIGSDR USAA2014112400006Actuator · failedNO TE FLAPS FLIGHT CONTROL FLAPS FAULT. REPLACED RT FLAP ROTARY ACTUATOR NR 1 IAW JOB CARD 26L00027004 & WORKED IN CONJUNCTION WITH LOG 3092768.SDR USAA2014112400003Actuator · failedNO TE FLAPS FLIGHT CONTROL FLAPS FAULT. REPLACED LT FLAP ROTARY ACTUATOR NR 1 IAW JOB CARD 26L00027004 & WORKED IN CONJUNCTION WITH LOG 3092768.SDR CA141208007Shaft · cracked(CAN) DETAILED INSPECTION OF BOLTED CONNECTION AT RT INBOUND FLAP ACTUATOR - REVEALED A CRACK- RUNNING FROM THE RIVET HOVE DOWN THE LENGTH OF THE SHAFT APPROX. 1 INCH. AN ENTIRE NEW ACTUATOR WAS INSTALLED.SDR USAA2014112100002Actuator · inoperativeEMERGENCY DECLARED FOR FLAP NOT RESPONDING, LANDED WITHOUT INCIDENT. REPLACED NR 1 RT & LT FLAP ROTARY ACTUATOR.SDR R61A201411181194Control Unit · failedCREW RECEIVED A FLAP POWER CAUTION MESSAGE AND RAN QRH. AFTER CYCLING THE CB, 15 SECONDS LATER THE CAUTION LIGHT CAME BACK ON. LANDED AND TAXIED TO GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND R & R THE FCU IAW AMM AND OPS CHECKED GOOD. ACFT IS GOOD SDR CA141121002Actuator · failed(CAN) ON APPROACH, AT 4000 FT, WHEN THE FLAPS WERE SELECTED FROM 0 TO 8 DEGREES, THEY FAILED AT ZERO DEGREES WITH THE FLAP FAIL CAUTION POSTED. OAT AT THE TIME WAS -15C. AFTER CIRCLING TO COMPLETE CHECKLISTS THE ACFT LANDED UNEVENTFULLY WITH FLAPS AT ZERO. CSDR REXA2014111701137Actuator · failedFLAP FAIL CAUTION IN FLIGHT FAILED AT 0 DEGREES DARING EXTENSION AIRSPEED 195 KTS FLIGHT OAT -10 DEGREES C.
DEFERRED FLAPS IAW MEL 27-50-00 IAW DF AT MOC. PLACARD INSTALLED. ENTERED INTO DMR. REPLACE RT NR 1 ACTUATOR, INBD FLAP, INBD ACTUATOR.SDR CA141218013Actuator · cracked(CAN) FLIGHT CREW REPORTED FLUID LEAKING ABOVE LEFT GEAR STRUT. MAINTENANCE FOUND LEFT FLAP ACTUATOR LEAKING & REMOVED ACTUATOR. ACTUATOR HOUSING WAS FOUND CRACKED. SERVICEABLE ACTUATOR WAS INSTALLED & GEAR SWINGS AROUND SERVICEABLE & AIRCRAFT RETURNED TO SSDR HZYR20141028002Actuator · failedFLAPS FAILED TO RETRACT AFTER TAKEOFF. FOUND LT FLAP ACUATOR SWITCH NOT ACTUATING. REPLACED THE ACTUATOR.SDR CA141010013Piston · cracked(CAN) ACTUATOR PISTON FOUND CRACKED WITH APPROXIMATELY A 4.5" CRACK EMANATING FROM THE ROLL PIN HOLE THAT RETAINS PLUG, PN 50-521196-1.SDR CA141009002Piston · cracked(CAN) DURING OPS 1 INSPECTION A CRACK WAS FOUND RUNNING THE LENGTH OF THE PISTON ON THE RIGHT HAND OUTBOARD FLAP ACTUATOR.SDR AALA20140921002Transmission · malfunctionedTRAILING EDGE FLAP DISAGREE INDICATION DURING FINAL APPROACH. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT INBD FLAP TRANSMISSION. SYS GND CHECKED NORMAL OPERATION CLOSED.SDR KX5R20140914003Actuator · crackedLEFT INBD FLAP ACTUATOR FOUND SPLIT LENGTHWISE ALONG LENGTH OF ACTUATOR PISTON DURING ROUTINE PHASE 1 INSPECTION. PHASE 1 INSPECTION CONSISTS OF EMPHASIS ON THE WINGS STRUCTURE AND ASSOCIATED COMPONENTS. FLAPS OPERATED NORMALLY BUT LT INBD FLAP ACTUATOR MADE SDR Y9PA20140916001Actuator · faultyLEFT OTBD FLAP ACTUATOR WAS CHANGED AT A SCHEDULED MX EVENT & UPON ARRIVAL TO HOME BASE FLAPS STUCK AT 20'. FOUND FLAP ACTUATOR EXTREMELY TIGHT ON LANDING. R & R LT OTBD FLAP ACTUATOR.
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