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 AALA2019111429018Control Unit · faultyAIRCRAFT WAS GROUNDED: CREW DECLARED AN EMERGENCY INTO EWR ON ACCOUNT OF FLAP PROBLEM. FLAPS WOULD NOT LOWER NORMALLY HAD TO LOWER THEM USING THE ALTERNATE SYSTEM. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE TROUBLESHOT AND FOUND CODE 27SDR CALA2019111101964Warning Message · false activationTE FLAP DISAGREE TE FLAP LOCKOUT AT 22 DEGREES PERFORMED BITE OF FSEU REF FIM 27-50-00. MAINT CODE 217. FLA FAIL. CYCLED FLAPS SLATS SEVERAL TIMES . OPS CK NORMAL. PERFORMED FLA TEST REF FIM 27-51-00. OPS CK NORMAL. REMOVED AND REPLACED #1 AND #2 FSEU, GET HARSDR J7SA2019120918001Flap System · malfunctionedSWPS FAULT, FLAP FAIL, PTRIM BKP FAIL AND SPOILER FAULT CAS MESSAGES RESULTING IN AUTO PILOT UNUSABLE AND FLAPS INOP. COMPLIED WITH FOL # PHE505-01/19 PERFORMED ELECTRICAL RESET AND COMPLIED WITH FLAP EXTENSION AND RETRACTION CHECK - NO DEFECT NOTED AND COMPLISDR C77A2019111100001Warning Message · illuminatedFLAP FAIL MSG IN FLIGHTSDR R61A2019110871221Warning Message · false activationFLAP LOW RATE EICAS MESSAGE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED FIM 27-53-0081-802-A. MESSAGE CLEARED.SDR R61A201911051219Actuator · failedFLAP FAIL ON APPROACH WITHOUT ACTUATING THE FLAP HANDLE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R&R SF-ACE 1 IAW AMM 27-53-02. PERFORMED ELECTRONIC RIGGING IAW AMM 27-50-00-820-802. OPS CHECK GOOD.SDR SWIA2019110546706Potentiometer · out of tolerancePOTENTIOMETER 5,6,7 AND 8 OUT OF TOLERANCE (READING .011) ON FECU. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX.SDR SWIA2019110546704Potentiometer · out of toleranceRH BPSU POTENTIOMETER OUT OF TOLERANCE. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX,SDR SWIA2019110546703Potentiometer · out of toleranceLH BPSU POTENTIOMETER OUT OF TOLERAANCE. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX.SDR MASA2019110512121Unknown · malfunctionedFLAPS FAIL, EMERGENCY DECLARED. CYCLE FLAPS CND OPS GOOD, NO DEFECTS FOUND.SDR DALA2019110406412Torque Tube · worn(AIRCRAFT 5807, L/P 6423330) WHILE CONFIGURING TO LAND WE GOT THE TE FLAP DISAGREE EICAS MESSAGE THE FLAP LEVER POSITION WAS SET AT 25 DEGREES, THE INDICATED POSITION WAS GREATER THAN 20 DEGREES, BETWEEN 20 AND 25, AFTER ENGINE SHUTDOWN FLAP'S MOVED TO INDICATSDR IPXA2019103098453Relay · malfunctionedINSPECTION TYPE:N/A** EMERGENCY DECLARED ** ON APPROACH WENT TO FLAPS 30 RECIEVED TRAILING EDGE FLAP DISAGREEPERFORMED BITE OF FSEU 1, 2, AND 3 IAW AMM 27-51-01. NO FAULTS NOTED. OP CHECK OF TE FLAP SYSTEM THROUGH MULTIPLE CYCLES IAW AMM 27-51-00-715-001. NO FSDR SWIA2019103046631Flap System · malfunctionedFLAP FAIL CAUTION MESSAGE DURING APPROACH FLAPS DID NOT EXTEND BEYOND ZERO ON EICAS DISPLAY. FLAPS FAIL QRH PERFORMED AND COMPLIED WITH. FLAP FAIL CAUTION MESSAGE DURING APPROACH FLAPS DID NOT EXTEND BEYOND ZERO ON EICAS DISPLAY. FLAPS FAIL QRH PERFORMED AND CSDR AALA201910319001Module · faultyAIRCRAFT WAS GROUNDED: CAPTAIN REPORTED FLAPS DID COME DOWN TO 15 DEGREE VERY VERY SLOWLY WITH TE DISAGREE LIGHT FLAPS RETRACTED BACK TO ZERO NORMALLY BUT THEN LOCKED AT 1 DEGREE WHEN CALLED FOR 15 DEGREEREMOVED AND REPLACED FLAP/SLAT SHUT OFF VALVE MODULE ISDR DALA2019102506180Module · malfunctionedSHIP 1808 -ATB- DUE TO FLAP TE FLAP DISAGREE EICAS MESSAGE. RAN QRH CHECKLIST AND LANDED FLAPS 20, WEIGHT 395,000 AND APPROACH SPEED 183 KNOTS. DECLARED EMERGENCY. CORRECTIVE ACTION: COMPLIED WITH OVERWEIGHT LANDING CHECK PER AMM. BITE OF FESU HAD FAULT MESSAGSDR AALA2019102329003Flap System · malfunctionedAIRCRAFT NOT GROUNDED: PILOT REPORTS ON APPROACH, FLAPS SELECTED 25 DEGREES, AIRCRAFT ROLLED RIGHT REQUIRING 2 UNITS LEFT AILERON TO FLY LEVEL. MAINTENANCE DEPLOYED ALL FLIGHT CONTROL DEVICES AND INSPECTED FOR DAMAGE, NO DEFECTS FOUND. ACCOMPLISHED BITE TEST SDR SWAA2019102238111Electronic Unit · faultyDECLARED EMERGENCY--------------------------------------------------------------DURING FLAP EXTENSION TRAILING EDGE FLAPS STOPPED EXTENDING BETWEEN 10 AND 15 WITH FLAP HANDLE AT 30. / R&R FLAP SLAT ELECTRONIC UNIT IAW MM.SDR AALA201910219030Control Unit · unreliableAIRCRAFT WAS GROUNDED: CREW DECLARED AN EMERGENCY ON FINAL APPROACH INTO DFW ON ACCOUNT OF FLAP DISAGREE. MAINTENANCE ACCOMPLISHED FIM TASK 27-51-00-810-820 RH FLAPS POSTED TRANSMITTER DISAGREE PROBLEM FOR MAIN MESSAGE 27-52260. REMOVED AND REPLACED FSEU IAW ASDR AALA201910189001Flap System · malfunctionedAIRCRAFT WAS GROUNDED: PILOT REPORTS LANDING FLAPS ONLY EXTENDED TO 15 WHEN SELECTED MORE THAN 15. MAINTENANCE RESET C/BS AT P6-2 C/B A11 AND P6-4 C/B D14 EXTENDED FLAPS AND SLATS, OPS CK NORMAL. ACCOMPLISHED FSEU BITE IAW FIM 27-51-00-810-801. OPS CHECK NORMASDR DALA2019101875984Flap System · malfunctioned(LOG 6222494) FLAP DISAGREEMENT ON FINAL AT 1800' FLAP HANDLE AT 30 DEG WHILE INDICATOR SHOWED STUCK AT 25 DEG. PERFORMED INSPECTION PER B737 AMM AND WDM 27-51 OF FLAPS, FLAP HANDLE SWITCHES, FLAP XMITTER WIRING AND PLUG. NO TROUBLE FOUND. RAN TRAILING EDGE FLSDR SWIA2019101146460Pdu · malfunctionedFLAPS HALF SPEED STATUS MSG DURING CLIMB OUT, AFTER FLAPS UP. FLAPS FAIL CAUTION MSG DURING APPROACH, WITH FLAPS STOPPING AT 36. (FLT#5153) RESET AND OPERATED FLAPS 5 FULL CYCLES. OK TO CONTINUE IN SERVICE. REMOVED AND REPLACED THE FLAPS PDU IAW AMM. OPS CHECSDR 2020F00084Bellcrank · brokenUPON LANDING LH OUTBOARD AFTER FLAP, INBOARD BELLCRANK BROKEN. CORRECTIVE ACTION: BELLCRANCK MECHANISM OUTBOARD AFT FLAP LH REMOVED AND REPLACEDSDR DALA2019100985806Module · leakingDIVERTED DUE TO LOSS OF LT HYDRAULIC FLUID. FOUND LEAKS AT FLAP/SLAT DEPRESSURIZATION MODULE AND LT EDP. REPLACED DAMAGED SEAL AT FLAP/SLAT DEPRESSURIZATION MODULE AND LT EDP. R & R LT ACMP AND CASE DRAIN FILTER, LT RTN FILTER MODULE, AND PTU AS PRECAUTIONARSDR JJBA201910097005Control Unit · inoperativeDURING DESCENT TO 230 SPS ADVANCED AND FLAP LOW SPEED PRESENTED WHEN FLAP 9 SELECTED FLAP FAIL. R&R FECU. OPS CHECK NO DEFECTS NOTED.SDR QXEA2019100700377Power Unit · inoperativeUPON SETTING FLAPS 15 DEG ON APPROACH FLAP DRIVE CAUTION ILLUMINATED WHEN FLAPS REACHED 15 DEG FLAP DRIVE CAUTION CHECK LIST COMPLETED FLAP 15 DEG LANDING ACCOMPLISHED. REMOVED FROM SERVICE. INTERROGATED CDS FOR FLAP DRIVE FAULT NO FAULTS REPORTED PERFORMED OPSDR CALA2019100701709Fseu · intermittentFLAPS FAILED TO EXTEND BEYOND 5. UNABLE TO CORRECT. LANDED WIT H FLAPS 5. PSEU ILLUM. ACCOMPLISHED BITE TEST OF PSEU, FOUND FAULTS 32-62009 AND 32-62010. MOVED FLAPS TO 40 AND BACK TO 0, FAULTS WENT AWAY AND PSEU LIGHT EXTINGUSHED. T/S REF FIM 27-81-00-810-SDR IPXA201910047515Bearing · failedINSPECTION TYPE:12YR, LT WING NR 5 FLAP JACK SCREW AFT BEARING GRINDING. REMOVED AND REPLACED THE LT WING NR 5 FLAP JACK SCREW IAW AMM 27-54-24-04. (MINOR REPAIR)SDR FDEA201909162253Handle · obstructedON APPROACH TO JFK WHEN FLAPS 25 SELECTED, "TE FLAP DISAGREE" EICAS MESSAGE. EXECUTED GO-AROUND, COMPLIED WITH QRH LANDED UNEVENTFUL @ JFK. EMERGENCY DECLARED. T/S PER FIM 27-51 FAULT TREE 805 AND 27-51 FAULT TREE 808. FOUND SLIGHT DEBRIS ON FLAP HANDLE DETENTSDR I5EA20190920002Jackscrew · lack of lubeDURING INITIAL CLIMB DURING RT TURN FELT A SERIES OF RAPID THUMPS LASTING ABOUT 1 SECOND FELT AS WELL IN THE CONTROL COLUMN THEN AFTER LEVEL OFF AT 3000' ANOTHER SERIES OF THUMPS AUTO PILOT DISENGAGED YAW DAMPER DIENGAGED RETURNED TO MIA FOR LANDING. SERVICEDSDR SCNA20190907176Screw · unsecure#3 SPOILER DAMAGED DUE TO SCREW POPPED OUT FROM THE TRAILING EDGE OUTBOARD FLAP. REMOVED #3 SPOILER IAW AMM 27-61-11. INTERFACE INSPECTION OF #3 SPOILER COMPLIED WITH, OK TO INSTALL. INSTALLED #3 SPOILER IAW AMM 27-61-11. PERFORMED SPOILER SYSTEM TEST AND ADJUSDR SCNA20190907174Screw · brokenTE OB FWD FLAP DAMAGED DUE TO SCREW BROKEN FROM 10FT OB OF THE FLAP. DAMAGE PAST LIMITS FOR SRM 57-53-01-01-03. REMOVED LT OUTBOARD FLAP PER AMM 27-51-22. INSTALLED SERVICEABLE LT OB MAIN FLAP REF AMM 27-51-21-400-801. FLAP ADJUSTMENT PERFORMED PER AMM 27-51-2SDR DALA2019090605195Flap · lack of lubeSHIP 670 - DIV - TO LAX DUE TO FLAPS DISAGREE ON APPROACH. CORRECTIVE ACTION: FOUND LT O/B FLAP TRANSMISSION TRIPPED. DRAINED AND RE-SERVICED. C/W FLAP LUBE PER AMM 12-24. PERFORMED FLAP SYS TRANSMITTER CK, ALL CK OK.SDR AALA201909069003Unknown · malfunctionedAIRCRAFT NOT GROUNDED: PILOT REPORTS AT 3000 ON APPROACH, FLAPS 30, SPEED INCREASED TO 180 KTS. FLAPS BLEW BACK TO 25, CORRECTED TO APPROACH SPEED FLAPS 30. LANDED UNEVENTFUL. MAINTENANCE ACCOMPLISHED PHASE 1 CHECK FOR FLAP OVERSPEED IAW AMM 05-51-08. NO DAMAGSDR UIEA2019083005405Module · leakingITEM 1: LEFT HYDRAULIC SYSTEM EICAS MESSAGE QTY ON, AFTER GEAR UP. LOSS OF INDICATION VALVE, PRESSURE WAS 3000+. ITEM 2: CENTER HYDRAULIC SYSTEM EICAS MESSAGE QTY CAME ON AFTER GEAR UP. QTY WAS +-50. PRESSURE WAS 200. T/S PER FIM 29-11 FT 831, FOUND MONITOR UNSDR VNAA2019083011102Bpsu · failedDURING APPROACH TO PHL THE CREW RECEIVED A FLAPS FAIL AND DECLARED AN EMERGENCY. TRUCKS ROLLED. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. THE AIRCRAFT WILL BE FERRIED TO A MAINTENANCE BASE FOR REPAIR. FOUND BOTH RT OB ACTUATORS NOT SUFFICIENTLY LUSDR VNAA2019083011101Warning Message · false activationDURING LANDING, THE CREW RECEIVED A FLAPS FAIL AT 40 DEGREES. DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE WITHOUT INCIDENT. CLEARED INHIBITS AND C/W ELECTRICAL EXTENSION AND RETRACTION OF FLAP/SLAT SYS IAW AMM 27-52-00-864-801/SDR A6WA2019083046811Warning Message · illuminatedDURING CRUISE FLIGHT, THE FLIGHT CREW RECEIVED A FLAP FAIL MESSAGE. THE CREW NOTIFIED DISPATCH, DECLARED AN EMERGENCY AND DIVERTED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO INJURIES OR ADVERSE PASSENGER REACTION.SDR VNAA2019082611101Warning Message · false activationDURING APPROACH TO PHL THE CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE AND DECLARED AN EMERGENCY. TRUCKS ROLLED. THE AIRCRAFT LANDED SAFELY AND TAXIED TO THE GATE. CLEARED INHIBITS THROUGH MDC AND OPERATIONAL TEST OF THE FLAPS AND SLATS SYSTEM WAS PREFORMED IASDR WX0A2019082673417Flap System · faulted(EMERGENCY DECLARED) ON APPROACH, RECEIVED ECAM FOR FLAP & SLAT FAULT. PERFORMED EXTENSION AND RETRACTION ON GROUND OF THE FLAP/SLAT SYS. NO ACTIVE FAULTS AT THIS TIME.SDR A6WA2019082746805Warning Message · illuminatedCLIMBING OUT OF 17,000 FLAP FAIL CAUTION MESSAGE, C/W QRH, MESSAGE REMAINED, LANDED FLAPS 0, NORMAL T/D, NORMAL LANDING, PERFORED FLAP RESET PROCEDURE IAW 98-18G BOX 12,SDR DALA2019082654952Limiter · faultedSHIP 3149 - ATB - DUE TO FLAP FAILURE TO RETRACT AFTER TAKE-OFF. ECAM WARNING: F/CTL FLAPS FAULT. SLATS AT ZERO, FLAPS AT 1. CORRECTIVE ACTION - FLAP R/H SIDE MECHANICAL DRIVE JAM, R/H INBOARD FLAP DRIVE ROTARY ACTUATOR NR 1 TORQUE LIMITER TRIPPED, FLAP CARRIASDR VNAA2019082211101Warning Message · false activationDUE TO INTERSECTING RUNWAYS ATC INSTRUCTED THE CREW TO DO A GO AROUND AT WHICH TIME THE CREW RECEIVED A FLAPS FAIL MSG AND FOLLOWED THE FLAPS FAIL CHECKLIST. FLAPS STUCK AT 8 DEGREES. THE CREW DID A FLAPS 8 LANDING ON RUNWAY 27L. THE AIRCRAFT LANDED SAFELYSDR SIMA201908221003Control Unit · failedFLAP FAIL ON EICAS CAUTION MESSAGE AFTER SELECTING FLAPS 9 FLAPS STAYED UP. RESET FLAPS SYSTEM IAW FIM TASK 27-51-00-810-801-A, RECEIVED FLAPS AT 9 DEGREES FOR FERRY FLIGHT PERFORMED GVI OF FLAPS NO DEFECTS NOTED. PERFORMED CMC DOWNLOAD IAW AMM 45-45-00, CSDR SIMA201908221004Warning Message · false activationFLAP FAIL MSF WHEN SELECTING FLAPS 22. RESET SYSTEM C/W OPERATIONAL CHECK IAW E140 AMM 27-51-00-700-801-A. NO FAULTS FOUND. A/C OK FOR SERVICESDR FDEA201908201954Flap System · malfunctionedON APPROACH (ABOUT 1500') CALLED FOR FLAPS 25 DEGREES AND THE TRAILING EDGE FLAPS DISAGREE LGT ILLUMINATED. BROKE OFF THE APPROACH, RAN THE QRH AND LANDED FLAPS 20 DEGREES WITHOUT FURTHER INCIDENT. FIM 27-51 FT 803 CARRIED OUT, NO FAULTS EVIDENT, ON EITHSDR A6WA2019082046794Warning Message · illuminated"RECIEVED FLAP FAIL CAUTION MESSAGE DURING INTIAL CLIMB. FLAPS WERE SET AND INDICATED ZERO" CREW DID NOT DECLARE AN EMERGENCY. AIRCRAFT LANDING WENT WELL THE BTMS WAS READING A LITTLE HIGH. THE BTMS WAS READING "NORMAL" AT 6-8.SDR IPXA2019081445623Flap System · faultedEMERGENCY DECLARED, SLAT AND FLAP FAULT SYS 1 AND 2 ILLUMINATED ON EXTENSION FROM F20 TO F40. FOLLOWED ECAM PROCEDURE AND SELECTED F40 WITH NO FURTHER FAULTS. PERFORMED BITE TEST IAW TSM 27-50-00, NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE.SDR FDEA201908091820Restrictor · malfunctionedAFTER TAKEOFF WHEN RETRACTING FLAPS RECEIVED LEVEL 2 FLAP DISAG. FLAP INDICATED 6,6,7,7 WITH HANDLE IN UP/0 EXT POSITION. RAN QRH. (DUMPED FUEL FROM 75.2 TO 50.0 POUNDS.) MATCHED UP FLAP HANDLE TO 7 MARK, BUT FLAP INDICATED 0. NORMAL LANDING. IDENTIFIED PARTS SDR CA190806006Bearing · damaged(CAN) DURING THE MANUFACTURERS SCHEDULED 5000HR/5 YEAR FLAP INSPECTION IT WAS FOUND THAT THE AIRCRAFT WAS NOT IN COMPLIANCE WITH AN AD THAT WAS SHOWING AS PREVIOUSLY COMPLIED WITH IN THE AIRCRAFT RECORDS. AD99-01-03 WAS SHOWING AS BEING PREVIOUSLY COMPLIED WITSDR 2019FA0000249Control Cable · severedLEFT INBOARD FLAP EXTEND CABLE BROKE AT INBOARD WING BELL CRANK CAUSING BOTH LEFT FLAPS TO NOT EXTEND AND CREATED ASYMMETRIC FLIGHT WHEN FLAP SWITCH WAS SELECTED IN 20 DEGREE AND 40 DEGREE DOWN POSITIONS.
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