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 DALA1149700695Gear · defectiveTRAILING EDGE FLAP TRANSMISSION GEAR REPLACED IAW EA 06-097281-03, ME04.SDR SIMA201015204Ecu · malfunctionedON FLIGHT 4580 THE CREW RECEIVED A FLAP FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED WITH 0 FLAPS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT AND FOUND FLAP ELECTRONIC CONTROL UNIT FAIL, RIGHT SENSORSDR AALA20100528LAX01Fseu · faultyLAX - CREW REPORTED FLAP PROBLEMS ON APPROACH. USED ALTERNATE FLAP EXTENSION. EMERGENCY DECLARED LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 2 FLAP SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DJFA2010013Cable · brokenDURING A SCHEDULED INSPECTION, MX FOUND THE LT FWD FLAP FOLLOW-UP CABLE SEVERELY CORRODED AND SEVERED AT THE MID BELL CRANK FERRULE. THE CABLE WAS REPLACED.SDR CALA2010052700228Fitting · corrodedNR 3 MID FLAP O/B TORQUE TUBE HOUSING HAS CORROSION. REMOVED AND INSTALLED NEW FITTING PER SRM 51-40-02 PARAGRAPH 7 AND 51-20-02 PARAGRAPH 8.SDR CA100531008Rod · broken(CAN) FLAPS FAULT - BROKEN RT INBD FLAP ACTUATOR FAIRING ROD. RECEIVED CALL STATING THAT THE CREW REPORTED A FLAPS FAULT AMBER MESSAGE IN FLIGHT. PILOTS SELECTED FLAPS 20 DURING APPROACH AND THE FLAP STOPPED AT 17 DEGS WHEN THE FLAP FAULT MESSAGE POSTED. UPSDR FDKA2010052000119Flap · malfunctionedFLAP FAIL IN FLT ZERO DEGREES, EMERGENCY DECLARED. MX RESET FLAP SYS, OPS CHECKED GOOD.SDR HYIA764EA52010Control Cable · brokenON FINAL DECENT, CREW REPORTED FLAP MALFUNCTION ( SPLIT FLAPS ). PILOT DECLARED AN EMERGENCY, LANDING WAS UNEVENTFUL. MX FOUND (1) OF (2) FLAP EXTEND CABLES BROKEN. MX R & R BOTH EXTEND AND RETRACT CABLES.SDR MASA2010051800518Flap · malfunctionedFLAPS WOULD NOT DEPLOY FOR LANDING, FLIGHT CREW PERFORMED A GO-AROUND AND LANDED WITH NO FLAPS. MX RESET SYSTEM, OPS CHECKS GOOD.SDR 2010FA0000606Flap System · separated((F8ER)) ON APPROACH, THE RT INBD, FORE FLAP, OTBD SECTION SEPARATED FROM THE ACFT, STRIKING THE RT SIDE OF FUSELAGE AND PUNCTURING SEVERAL AREAS OF EXTERIOR SKIN CAUSING DAMAGE TO SEVERAL FUSELAGE FRAMES AND STRINGERS IN FUSELAGE SECTIOON 46 WITH DAMAGE BEINGSDR AALA20100515LAX01Transmission · faultyLAX - CREW REPORTED "TRAILING EDGE FLAPS DISAGREE" EICAS MESSAGE. FOLLOWED QRH PROCEDURES LANDED FLAPS 20. EMERGENCY DECLARED LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT INBOARD TRAILING EDGE FLAP TRANSMISSION. SYSTEM GROUND SDR UALA2010051401637Fseu · faultyREPEAT ALT FLAP CHECK FAIL. REPLACED 3 PINS ON ALT FLAP EXTEND MOTOR M547 CONNECTOR, REPLACED FSEU & ALT FLAP EXTEND RELAY, OPS TESTED GOOD.SDR 2010FA0000463Control Cable · frayedFOUND FLAP CABLE STRANDS BROKEN.SDR 2010FA0000462Control Cable · frayedFOUND FLAP CABLE STRANDS BROKEN.SDR 2010FA0000461Control Cable · frayedFOUND FLAP CABLE STRANDS BROKEN.SDR QXEA2010051700303Bpsu · failedUPON FLAPS 20 SELECTION DURING APPROACH, GOT A FLAPS FAIL CAUTION MESSAGE. PERFORMED CHECKLIST WITH NO CHANGE. FLT CTRL SYNOPITIC PAGE INDICATED L FLAPS AT 16 DEG AND NO INDICATION ( 2 DASHES )FOR RT FLAPS. SLATS INDICATED 20 DEG. DIVERTED AND LANDING WAS USDR REXA201000075Ecu · malfunctionedCREW REPORTED A FLAPS FAIL AT 20. MISSED APPROACH, RAN QRH. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FECU IAW AMM 27-51-05.SDR FDEA201005041437Control Valve · inoperativeON CLIMB OUT STARTED NORMAL FLAP RETRACTION-GOT A FLAP DISAG. FLAPS INDICATED 14- 17 IN AMBER BOXES ON CONFIG PAGE.PUT FLAP/SLAT HANDLE TO 15 DETENT,FLAPS THEN MOVED TO 10,THEN 4, FLAP HANDLE STILL AT 15. MOVED HANDLE TO 0 DEGS,FLAPS EVENTUALLY MOVED TO 0 DSDR A6WA201040340Bpsu · failedAIR RTN- AFTER T/O FLAPS RETRACTED 20 TO 8, FLAPS FAILED AS 10 (LT = 8/RT=10) C/W QRH. NORMAL LANDING AT 46400 LBS GROSS. R & R LT AND RT BRAKE POSITION SENSOR UNIT.SDR A6WA201040336Control Lever · failedAFTER T/O, FLAPS FAILED AT 20 DEGREES. COMPLIED WITH QRH. PERFORMED FLAP RESET PROCEDURE IAW SUPP 98-18D, BOX 12. FLAPS RESET. PLACARDED AND PLACED ON MEL. PERFORMED OPS TEST OF FLAPS SYS IAW AMM 27-51-05. ALL CHECKS GOOD, REMOVED FROM MEL. M/C REF 2018SDR A6WA201040335Ecu · failedFLAPS FAILED AT 12 DEGREES DURING RETRACTION AFTER TAKEOFF. C/W QRH DIVERTED, LANDED AT 44360. C/W FLAP RESET PROCEDURE (98-018D) FLAPS FAILED AGAIN. REPLACED FECU IAW AMM 27-51-05. OPS AND FUNCTIONAL TEST CK OK.SDR ASOA201000661Bpsu · failedFLAP FAIL AT 0 DEG ON APPROACH. (EMERGENCY DECLARED). R & R LT BPSU ASSY IAW AMM-27-51-10. PERFORMED RIGGING TEST AND POSITION TEST IAW 27-51-10-830-801. OPS CHECKS GOOD NO DEFECTS NOTED C/W AD 2009-06-12. MCO CLEARED. (CLOSED)SDR USAA2010042890859Strut · out of adjustFLT 1420 - PHL-CLT - EMERGENCY LANDING - FLAPS LOCKED - ALIGNMENT FAULT. ACCOMPLISHED A MCDU WING TIP BRAKE (WTB) RESET. ACCOMPLISHED A LEFT AND RIGHT WING INTERCONNECTING STRUT ADJUSTMENTS IAW AMM 27-51-44-05. OPERATIONAL CHECKS WAS GOOD.SDR MASA2010042600406Control Lever · failedFLAPS FAIL AT 20 DEGREES, NO EMERGENCY DECLARED. PLACED ON MEL. REMOVED AND REPLACED CONTROL LEVER REPLACED FLAP CONTROL LEVER.SDR A6WA201040302Control Unit · failedFLAPS FAIL MSG DURING CLIMB-OUT. FAILED AT 13 DEGREES. C/W QRH, DIVERTED, LANDED AT 46370 LBS. ATTEMPTED FLAP RESET IAW SUPP 98-018C (AMOC) FLAPS FAILED AGAIN. R & R FLAP ELECTRONIC CONTROL UNIT.SDR REXA201000054Bpsu · failedFLAPS FAIL AT 0 IN CRUISE, PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I) PER AMOC DATED MARCH 27, 2009 AND PA AD27-052F. REMOVED AND REPLACED RT BPSU IAW AMM 27-51-10. PERFORMED OP/C OF FLAPS IAW AMM 27-50-00. OP/SDR CALA2010042600157Flap · malfunctionedT/E FLAP DISAGREE LT ON APPROACH PERFORMED FIM TASK 27-51-00 FIG 104, NO FAULTS FOUND ALL INDICATIONS NORMAL. PERFORMED AMM 27-58-00 501, OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME.SDR MASA2010042100378Flap · failedFLAPS FAIL AT ZERO DEGREES, EMERGENCY DECLARED BRACE COMMAND GIVEN. PLACED ON MEL THEN COMPLIED WITH EO OPS GOOD.SDR KPVA 201001Rvdt · out of adjustT/O WARNING HORN SOUNDED WITH THE ADVANCEMENT OF THE POWER LEVERS WITH THE AIRCRAFT PROPERLY CONFIGURED FOR T/O. FOUND THE RIGHT FLAP RVDT OUT OF ADJUSTMENT. RE-ADJUSTED THE RIGHT RVDT. OPS CHECK GOOD.SDR UC2R10FA0000502Spring · brokenTHE PILOT REPORTED THAT WHEN USING THE FLAP HANDLE TO EXTEND THE FLAPS SHE HEARD A LOUD BANG. THE ACFT LANDED WITHOUT INCIDENT. THE PILOT ALSO REPORTED THE THE FLAPS WENT TO THE FULL EXTENSION POSITION AFTER LANDING. WHILE INSPECTING THE FLAP SYSTEM AFTER TSDR E81R_TT40283Relay · stickingINVESTIGATED REPORT OF FLAPS NOT EXTENDING FROM RETRACTED POSITION. FOUND K105 FLAP MOTOR DYNAMIC BRAKE RELAY STICKING AND FLAP GEARBOX MOTOR BINDING. REPLACED K105 DYNAMIC BRAKE RELAY AND FLAP GEARBOX MOTOR, FLAP SYSTEM OPERATIONAL CHECKS NORMAL. SUSPECT DSDR A6WA201040289Flap System · failedFLAPS FAILED AT 6 DEGREES AFRER TAKEOFF ON BOTH SIDES DURING G FLAP RETRACTION RETURNED TO DEPARTURE AND LANDED AT 47000 LBS. COMPLIED WITH SUP 98-018C.1 (AMOC) TROUBLESHOT IAW FIM 27-50-00. PLACED SKEW ON MEL.SDR CHQA201000082Control Lever · faultyCREW REPORTED THAT THE AIRCRAFT WOULD NOT ACCELERATE AND A RUMBLE COULD BE HEARD AND FELT. THE CREW INSPECTED THE WINGS DURING FLIGHT AND FOUND THE FLAPS SLIGHTLY EXTENDED WITH A ZERO INDICATION IN THE COCKPIT. THE FLAP HANDLE WAS CYCLED AND THE FLAPS FULLY SDR CHQA201000080Brake · faultyTHE CREW REPORTED THE FLAP POSITION INDICATION WAS INOP ON APPROACH. MAINTENANCE REPLACED THE LEFT FLAP WING BRAKE DUE TO FAIL MESSAGES FOUND ON THE CMC WITH NO FURTHER DEFECTS NOTED.SDR AALA20100415TUL02Torque Tube · wornINBOARD FLAP PRIMARY DRIVE TORQUE TUBE HAS A WORN SPOT JUST INBOARD OF INBOARD FLAP. REMOVED AND REPLACED PRIMARY TORQUE TUBE PER SB 737-53-1264.SDR E81R_JT22794_35Lever · chafedDURING SCHEDULED IFA 200 HR IFA "A", AND IFA "B" INSP, NOTED LT AND RT FLAP FOLLOW-UP SWITCHES ACTUATING LINKAGE LEVERS POSITIONED TOO LOW AND CHAFING INTO ADJACENT LOWER WING T/E ACCESS PANELS 512TB AND 612TB. ADJUSTED SWITCH ACTUATING LEVERS HIGHER ON FOLLOWSDR USAA2010041290759Strut · wornFLT 819 CLT-GCM - DIV - WHILE JUST SOUTH OF GCM, CREW RECEIVED 'F/CTL FLAP LOCK SYS 1' FAULT - LOCKED BETWEEN POSITIONS 0 AND 1. CREW DECLARED AN EMERGENCY AND DIVERTED TO MBJ. MAINTENANCE FOUND LEFT FLAP INTERCONNECT STRUT WORN BEYOND LIMITS. REMOVED AND RSDR MYWA100063Unknown · flutterETOPS SIGNIFICANT ITEM - DURING APPROACH, FLUTTERING WAS FELT WITH FLAPS EXTENDED.SDR COMA2010040950089Detection Sys · malfunctionedON APPROACH INTO JFK RECEIVED FLAPS FAILED CAUTION MSG, FLAPS FAILED AT 30 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY AT JFK. RESET BOTH THE SKEW DETECTION SYSTEM AND THE FLAP FECU. PERFORMED OPERATIONAL CHECK OF THE FLAP SYSTEM, OPS CHECK GOOD.SDR COMA2010040550081Flap · failedON APPROACH INTO IAD FLAPS FAILED AT 3 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION.SDR E81RPT600772Limit Switch · intermittent( E81R) INVESTIGATED REPORT OF FLAPS NOT EXTENDING FROM APPROACH POSITION TO FULL DOWN POSITION. FOUND ONE SET OF CONTACTS INSIDE OF S76 14 DEGREE LIMIT SWITCH TO BE INTERMITTENTLY OPEN. REPLACED S76 14 DEGREE LIMIT SWITCH AND ADJUSTED FLAP 14 DEGREE AND 16 SDR IPXA10159073Jackscrew · bindingDIVERSION - FLAP 1 AND 2 SYS FAULT. FLAPS STUCK AT 20 ON T/O. AT 3500 FT CYCLED FLAPS IAW ECAM NO HELP. ESTIMATED FLAP OVERSPEED OF 10 KNOTS DURING LEVEL OFF ESTIMATED DURATION OF OVERSPEED 5 SEC. FOUND NR 5 JACKSCREW SUPPORT ASSY BINDING. R & R NR 5 JACKSCSDR USAA2010033190684Actuator · malfunctionedFLT 1911 PHL-NAS - DIVERSION - ON DESCENT INTO NAS, CREW WAS UNABLE TO DEPLOY THE FLAPS - COULD ONLY EXTEND THE SLATS. AIRCRAFT DIVERTED TO FLL AND REGAINED FLAPS ON APPROACH. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND INBOARD FLAP TORQUE LIMITER INDSDR RYNA2010000330000Fseu · malfunctionedDURING FLIGHT, AIR / GROUND DISAGREE STATUS MESSAGE. AFTER TAKEOFF ON FLAP RETRACTION FLAP LEVER O* - INDICATOR 1 * (BOTH L/R)- NO EICAS MESSAGE, NO WARNING LIGHTS. T/S PER FIM 32-09-03/101 BLOCKS 1, 2, 3, 14, 35, 7 AND BLOCK 8. PER THE FIM THE PSEU IS OK FSDR COMA2010032950071Control Handle · failedFLAPS FAILED AT 30 DEG ON APPROACH INTO JFK. EMERGENCY DECLARED, A/C LANDED SAFELY AT JFK. REMOVED AND REPLACED FLAP CONTROL LEVER.SDR QXEA2010032900205Flap System · failedON TAXI IN THE FLAPS FAIL CAUTION ILLUMINATED. ACFT DOWN FOR REPAIRS.SDR CALA2010032600105Flap · malfunctionedON FINAL APPROACH DURING SELECTION OF FLAPS 30 OVERSHOT TO BEYOND 30 DEG THEN SELECTED 30 DEG FLAPS STOPPED AT FLAPS 25. WENT AROUND & PERFORMED CHECK LIST & RETURNED FOR NORMAL APPROACH & LANDING. PERFORMED FSEU FLAP LOAD RELIEF TEST IAW FIM TASK 27-51-00-8SDR SIMA201008401Flap System · malfunctionedON FLIGHT 44262 DURING TAKEOFF THE CREW REPORTED FLAP FAIL AT 9 DEGREES. THE CREW ELECTED TO RETURN TO RDU. THE AIRCRAFT LANDED OVERWEIGHT BUT WAS UNDER THE 360 FEET PER MINUTE AT TOUCHDOWN, AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICESDR VNAA2010032600013Ecu · malfunctionedCREW REPORTED A FLAPS FAIL AMBER CAS MESSAGE ON DESCENT INTO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT (FECU) AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE SDR AALA20100320JFK01Fseu · faultedJFK - CREW REPORTED TRAILING EDGE FLAP DISAGREE MESSAGE ON APPROACH. QRH PROCEDURE ACCOMPLISHED. EMERGENCY DECLARED LANDED JFK WITHOUT INCIDENT. FOUND FLAP SLAT ELECTRONIC UNIT AT FAULT. REPLACED UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
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