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 SIMA201132001Ecu · malfunctionedON FLIGHT 3527 DURING DESCENT THE CREW REPORTED THAT A FAIL PRESENTED ON EICAS WHEN FLAP LEVER SET TO 9 DEGREES. THE FLAPS REMAINED AT 0 DEGREES. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO PNS. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMSDR UALA2011111506262Module · faultyFLAT-SLAT EICAS STATUS MSG. DUE TO UNABLE TO CLEAR 'SLAT ISLN VLV' MAINT MSG. REPLACED FLAP-SLAT SHUTOFF VALVE MODULE PER AMM. MSGS CLEARED AND ALL NORMAL.SDR 2011FA0000742Control Cable · frayedREMOVED LT & RT INBD FLAP EXTEND CABLES FROM BOTH INBD FLAP BELLCRANKS TO INSPECT FOR WEAR OR DAMAGEDURING 100HR, ANNUAL INSPECTON PROCESS. FOUND APPROX 1" BEHIND CABLE END THREADED FITTINGS BOTH CABLES HAD SIGNIFICANT BROKEN WIRE STRANDS WHICH UNDETECTED, WOSDR CVGA113191Flap · malfunctionedFLAPS FAILED AT 17 DEGREES WHEN SELECTING "FLAPS 20" ON APPROACH TO KISO. RECEIVED AUDIBLE WARNING AND EICAS "FLAPS FAIL" AMBER MESSAGE.SDR HALA2011111000511Flap System · malfunctionedON APPROACH, SELECTED FLAPS 15 DEGREE, GOT EICAS FLAP DISAGREE MSG HANDLE IN DETENT AND FLAP GAUGE SHOWED APPROX 10 DEGREE. FOLLOWED PROCEDURE AND LANDED WITHOUT INCIDENT, ON FINAL ALL ALERTS OFF AND SEL FLAP 25 DEGREE, FLAPS MOVED TO 25 DEGREE NORMALLY. TROSDR USAA2011111100020Unknown · malfunctionedCONFIGURING AIRCRAFT ON APPROACH TO PVD - WITH FLAPS AT 10 DEGREES, GEAR SELECTED DOWN, FLAP HANDLE POSITIONED TO 25 DEGREES - RIGHT FLAP NEEDLE INDICATED 15 DEGREES AND LEFT FLAP NEEDLE INDICATED 25 DEGREES. ACCOMPLISHED GO-AROUND TO DOWNWIND AND POSITIONED SDR CA111118001Motor · failed(CAN) DURING A ROUTINE FLIGHT, IT WAS NOTED DURING THE APPROACH THE FLAP SYS BECAME UNSERVICEABLE BEING STUCK AT APPROACH, THE FLIGHT AND LANDING CONTINUED WITHOUT COMPLICATIONS. MAINTENANCE DISCOVERED THE FLAP MOTOR WAS HOT AND SMELLED BURNED. THE MOTOR WAS SDR CA111110002Control Cable · frayed(CAN) WE FOUND DURING AN INSPECTION THAT THE FLAP CABLE, UNDER THE REAR SEATS WAS "FRAYED" DUE TO IMPROPER INSTALLATION OF FLAP CLIP, PN: 62701-185. THE CLIP WAS INSTALLED UPSIDE DOWN WHICH CAUSED THE CABLE TO NOT BE OPERATED IN A LINEAR PATH. THE CABLE FRAYEDSDR AALA20111109ORD01Fseu · malfunctionedORD - CREW REPORTED FLAPS STUCK AT 15 DEGREES. FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP SLAT ELECTRONICS UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.SDR CALA2011110800724Flap · malfunctionedFLAPS STUCK BETWEEN 0 AND 1. PERFORMED APPROPRIATE CHECKLIST. PERFORMED FIM TASK 27-51-00-810-836. PERFORMED FSEU BITE PROCEDURE FOUND FAULT T/E FLAP INDICATION 27-56400. PERFORMED TASK 27-51 -00-810-826, TEST PASSED. PERFORMED OP TEST OF FLAPS WITH PRIMASDR VNAA2011111000004Shaft · lack of lubeCREW REPORTED FLAPS FAIL CAUTION MESSAGE ON APPROACH TO CLT. FLAPS FAILED AT 20 DEGREES AND WOULD NOT EXTEND ANY FURTHER IN FLIGHT. AIRCRAFT LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, CLEANED AND LUBED LEFT AND RIGHT FLAP FLEX SHAFTS ANDSDR TRBA2011110531101Flap System · malfunctionedDURING APP WHEN SELECTING FLAPS TO 30, FLAP UNLOCK LIGHT CAME ON . VERIFIED FLAPS AND DID NOT LOCK AT 30 DEGREES. FLAPS REMAINED BETWEEN 15 AND 30 DEGREES. FOLLOWED PROCEDURES IAW AOM 1 AND PERFORMED A FLAP 0 LANDING. PERFORMED OPS CHECK ON FLAP CONTROL SYSDR BKEA2012F00005Drive Unit · inoperativeFLAPS WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT DIVERTED FOR MAINTENANCE. FOUND DRIVE UNIT INOPERATIVE.SDR CA111103007Sensor · failed(CAN) CREW ADVISED FLIGHT DISPATCH OF A FLAP FAIL MSG, CREW ELECTED TO DIVERT. TROUBLESHOT IAW FIM 27-51-00-810-805-A. REPLACED BOTH RT WING FLAP OTBD SKEW SENSORS T3 AND T4 IAW AMM 27-53-06. ELECTRONICALLY RIGGED AND OPS TEST SERVICABLE. SKEW SENSOR PN: 5SDR UALA2011103105886Fseu · malfunctionedFLAPS FAILED TO MOVE. TRAILING EDGE LIGHT ILLUMINATE. EICAS MESSAGE 'T/E FLAP DISAGREE' & 'FLAP ISLN VAL' DISPLAYED. REPLACED FSEU 3 PER MM. 201 DUE TO BITE ON FSEU 1 (-40 TYPE BOX) FAULTED FSEU 3 ON LEG 0. PERFORMED TESTS. NORMAL OPERATION NOTED.SDR VNAA2011110300032Control Unit · failedCREW REPORTED FLAPS FAIL AT 20 DEGREES DURING APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AISDR SIMA201130403Ecu · inoperativeON FLIGHT 4142 ON APPROACH THE CREW REPORTED THEY RECEIVED A CAPTAINS PITCH TRIM FAIL MESSAGE AND FLAP FAIL MESSAGE. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S CONTROSDR REXA201100790Flap · malfunctionedFLAPS FAIL COMPLIED WITH PA AD27-052G AND DEFERRED PER MEL 27-50-00. RETURNED TO SERVICE.SDR CA111028002Flap System · failed(CAN) CREW ADVISED FLIGHT DISPATCH VIA THE ACARS OF A FLAP FAIL EICAS MESSAGE. DURING APPROACH, WHEN FLAPS WERE SELECTED THEY CONFIRMED A FLAP FAIL AND DECLARED AN EMERGENCY WITH ATC. QRH PROCEDURES CARRIED OUT. SF ACE 1 REPLACED IAW MM 27-53-02 FLAP OPERASDR SIMA201129704Shroud · looseON FLIGHT 4099 THE CREW REPORTED THAT ON APPROACH, SELECTED FLAPS 9 DEGREES. FLAPS STOPPED AT 1 DEGREE WITH FLAP FAIL MESSAGE ON EICAS. THE CREW DECLARED AN EMERGECNY. THE CREW DID ZERO FLAP LANDING AS PER AOM VOL 1. THE AIRCRAFT LANDED WITHOUT INCIDENT. SDR MASA2011102163886Bpsu · malfunctionedFLAPS FAIL ON LANDING AND SLATS FAIL ON LANDING. R2 RT BPSU.SDR CALA2011102000678Unknown · malfunctionedON APPROACH GOING TO FLAP POS 25 GOT THE T/E FLAP DISAGREE ICAS. RAN CHECK LIST AND LANDED FLAPS 20 T-S IAW FIM 27-51-00-815-809 PERFORMED A BITE OF THE FSEU NO FAULTS NOTED AT THIS TIME. RAN FLAPS DOWN AND UP. NO FAULTS NOTED. OK TO CONTINUE.SDR REXA201100733Computer · looseSLATS HALFSPEED (STATUS INFLIGHT) FLAPS HALFSPEED (STATUS INFLIGHT) SPLR/STAB (STATUS INFLIGHT)- HIGHSPEED CLACKER ABOVE 230 KIAS WITH SLATS/FLAPS RETRACTED. MTC ENTRY- FOUND NR 2 SFECU LOOSE IN RACK. RESECURED NR 2 SFECU COMPUTER, CLEAR INHIBITS, RAN FLAP + SDR HALA2011101800470Flap System · malfunctionedAFTER TAKEOFF: WHEN RETRACTING FLAPS FROM 18 OR 13 DEGREES TO SLATS/0 DEGREES THERE IS A SHUDDER. THROUGH THE ACFT THAT FEELS LIKE A HYD PROBLEM NOT A FLAP POSITION AERODYNAMIC ISSUE. ONLY OCCURS WHEN RETRACTING 18/13 DEGREES AIRBORNE. INSPECTED FLAP/SLAT SSDR ASOA201101943Fcu · failedFLAPS FAIL MESSAGE IN FLIGHT GOING FROM 0 TO 8 DEGREES. EMERGENCY DECLARED AS A PRECAUTION. R & R FECU IAW AMM 27-51-05. OPS CHECKED GOOD.SDR REXA201100702Bpsu · defectiveFLAPS FAIL CAUTION MSG INFLIGHT. EMERGENCY DECLARED. SECURED FLAPS AT FLAP 20 BY PULLING & COLLARING CB 1F4, B5 2F4, B5 IAW SERVICE LETTER RJ-CL27-077. A/C FLAP SYSTEM INSPECTED AND DETERMINED TO BE INOPERATIVE AND NOT AIRWORTHY FOR REVENUE FLIGHT, BUT THE SDR AALA20111009MIA01Relay · inoperativeMIA - CREW REPORTED TRAILING EDGE FLAP DISAGREE EICAS MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RELAY K10104. SYSTEM GROUND CHECK NORMAL OPERATION.SDR REXA201100696Bpsu · defectiveON APPROACH AT 200 KNOTS HAD A FLAPS FAIL AT 0 DEGREES. AC LANDED SAFELY AND DID NOT DECLARE AN EMERGENCY. DEFERRED FLAP SYSTEM PER MEL 27-50-00 AND DOWNGRADED CAT II PER 34-00-10. RECORD FLAP CODES PER PA AD027-52G. FOUND FLAP CODES TO BE: RIGHT BPSU, FECSDR ANCF2011108900097Flap · malfunctionedDURING APPROACH WHEN SETTING FLAPS AT POSITION 2 F/CTL: FLAPS LOCKED - AUGMENT FAULT ON ECAM.SDR ASOA201101891Flap System · failedFLAPS FAIL AT 20 DEGREES PRIOR TO LANDING. COMPLIED WITH QRH. LANDED WITHOUT INCIDENT (EMERGENCY DECLARED AS A PRECAUTION) R & R BRAKE POSITION SENSOR IAW AMM 27-51-10, AIC REF 27-51-00 ITEM 10G. R & R SKEW DETECTION UNIT IAW AMM 27-51-15, REF 27-51-15 ITEM 5SDR REXA201100645Control Unit · failedFLAPS FAIL DURING CRUISE. TROUBLE SHOT FLAP FAIL IAW 27-052G AND FIM 27-50-00 FECU CODES SHOWED LEFT BPSU, ADC SIGNALS FECU PER FIM 27-50-00 MEGAOHMED LEFT BPSU AND WIRING HARNESS WITH NO DEFECTS NOTED. R & R FECU IAW 27-51-05. OPS CHECKED GOOD. SSDR REXA201100644Control Unit · defectiveFLAPS FAIL CAUTION MESSAGE ON DEPARTURE AT 0 DEG FLAP POSITION, INITIATED RETRACTION AT 165 KTS, FULLY RETRACTED AT 185 KTS. VSI AT LANDING LESS THAN 100 FPM. PERFORMED TROUBLE SHOOTING PER FIM REV 39 AD2009-06-12 PARAGRAPH (H)(6)(I). REPLACED BPSU IAW AMM 27-SDR REXA201100642Control Unit · defectiveACFT DIVERTED DUE TO FLAPS FAIL AT ZERO ON EXTENSION 190 KTS. PERFORMED TROUBLESHOOTING PER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AND PA AD 27-052G, COMPLETED STEPS IN PARAGRAPH 4.A. (12) OF FIM 27-50. NO DEFECTS NOTED. REMOVED AND REPLACED FECU ISDR AALA20110928TUL04Transmission · inoperativeTUL - CREW REPORTED FLAP DISAGREE ON DESCENT. EMERGENCY DECLARED FLIGHT LANDED TUL WITHOUT INCIDENT. ON TAXI INTO GATE, FLAPS/SLATS WOULD NOT STOW. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT OUTBOARD TRAILING EDGE FLAP TRANSMISSION. SYSTEM GROUND CHECK SDR MASA2011092963772Unknown · malfunctionedFLAP FAIL CAUTION STUCK AT 35 DEG. RESET PER THE FIM.SDR UALA2011092705216Flap System · malfunctionedRECEIVED A TRAILING EDGE FLAP DISAGREE EICAS MESSAGE. MESSAGE CAME ON BETWEEN FLAPS 20 & 25. BITE CHECKED FSEU NR1 SHOWED INTERMITTENT FLAP FAULT. CLEARED FAULT, OPERATED FLAPS SEVERAL TIMES ALL CHECKED NORMAL.SDR VNAA2011092900023Bpsu · failedCREW REPORTED FLAPS FAIL AMBER CAS MESSAGE IN FLIGHT EN ROUTE FROM CAK TO CLT. CREW DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING ASDR VNAA2011092800022Ecu · failedCREW REPORTED FLAPS FAIL CAUTION MESSAGE AT ZERO DEGREES ON DESCENT INTO SDF. AIRCRAFT LANDED IN SDF WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANSDR MASA2011091963711Bpsu · failedFLAP FAIL IN FLT. R2 LEFT BPSU.SDR DXTA2011091904729Switch · out of adjustAFTER TAKEOFF FLAPS WOULD NOT RETRACT OUT OF 15 DEGREES. ADJUSTED FLAP UP SWITCH IN PEDESTAL SC012. CYCLED SEVERAL TIMES AND CHECKED FLAP DEFLECTION ANGLES. FOUND ALL OPS CHECKED NORMAL.SDR MASA2011091963705Ecu · malfunctionedFLAPS FAIL CAUTION MESSAGE IN FLIGHT. R2 FECU AND C/W FLAP EO WORK ORDER.SDR MASA2011091963704Flap · failedFLAP FAIL AT 30 DEG ON LANDING APPROACH. COMPLIED WITH EO.SDR UALA2011091605018Control Valve · faultyPRIMARY FLAPS FAIL EICAS THIRD FLIGHT IN A ROW SYSTEM GOES ALTN FLAP. SAMC TEXT: PLZ ACP MT27-001R1. T/S PER 777MT 27-011 R1. FOUND FLAP PCV CONNECTOR DV27004B PIN 5-12 LOOP IS OPEN. REPLACED FLAP PCV, LEAK CHECK OK & FLAP OPS CHECK NORMAL PER MM.SDR PNBA2011F00006Push-Pull Cable · failedON 3 DIFFERENT FOLLOW-UP CABLES, THE STROKE OR THROW OF THE INSIDE CABLE WAS .7500" ON 1, 1" ON ANOTHER AND 1.1250" ON THE 3RD. UNABLE TO GET THE BLUE PRINT SPECS OF 2.37 ON ANY OF THE CABLES. CABLES WILL BIND-UP WHEN ATTEMPTING TO EXTEND THE FLAPS.SDR MASA2011091663695Flap · unwanted deployINADV FLAP DEPLOY TO 1 DEGREE AT 260. INSPECTED FLAPS/SLATS NO DEFECTS NOTED.SDR VNAA2011091900019Bpsu · failedCREW REPORTED FLAPS FAIL CAUTION MESSAGE IN FLIGHT ON DESCENT INTO CLT. CREW COMPLETED QRH AND AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED RIGHT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKSSDR VNAA2011091600015Bpsu · failedCREW REPORTED FLAPS FAIL CAS MESSAGE IN FLIGHT ON RETRACTION UPON DEPARTURE FROM FAY EN ROUTE TO CLT. FLAPS FAILED AT ZERO DEGREES. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED RIGHT FLAP BPSU (BRAKE ANDSDR ASOA201101692Flap System · failedRECEIVED FLAP FAIL MESSAGE ON FINAL, WHEN SELECTING FLAPS FROM 30-45. FLAPS WILL NOT RETRACT, EMERGENCY DECLARED. RESET SKEW DETECTOR. PERFORMED SKEW DETECTOR TEST. OPS CHECKED GOOD. OPERATED FLAPS UP & DOWN SEVERAL TIMES. CHECKED GOOD IAW AMM 27-51-15.SDR C41R20110907101Switch · out of adjustOWNER REPORTED FLAPS INTERMITTENTLY WOULD NOT GO FROM 10 TO 20 DEGREES UNLESS SELECTOR HANDLE WAS MANIPULATED. FOUND FLAP SWITCHES ON SELECTOR CAM TO BE OUT OF ADJUSTMENT. SLIGHT PRESSURE ON SELECTOR HANDLE ROD WOULD ACTUATE FLAPS AS NORMAL. ADJUSTED FLAP SSDR VNAA2011090900005Control Unit · failedCREW REPORTED FLAPS FAIL CAS MESSAGE UPON SELECTING FLAPS EIGHT (8) DEGREES DURING APPROACH TO HSV. FLAPS EXTENDED TO EIGHT (8) DEGREES, THEN FAILED. AIRCRAFT LANDED IN HSV WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FL
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