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.

SDR AALA2009061600010Fseu · inoperativeMIA - AIRCRAFT EXPERIENCED FLAP DISAGREE AND LANDING GEAR ANNUNCIATOR WENT BLANK FLIGHT THEN INITIATED GO AROUND. EMERGENCY DECLARED, LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP SLAT ELECTRONICS UNIT. SYSTEM GROUND CHECK NORMAJun 16, 2009 · N368AA · Boeing 767323SDR CA090617008Selector Valve · inoperative(CAN) PILOT UNABLE TO RETRACT FLAPS THROUGH NORMAL ELECTRIC FLAP CONTROL SWITCH. FLAPS RETRACTED USING MANUAL EMERGENCY FLAP SELECTOR. TROUBLESHOOTING DETERMINED ELECTRIC SOLENOID WAS WORKING BUT UNABLE TO POSITION VALVE INSIDE SELECTOR TO PORT PRESSURE TO FLJun 14, 2009 · Cvac 340CVACSDR ASOA200900665Flap · failedFLAP FAIL AT 20 DEGREES ON APPROACH. EMERGENCY DECLARED, ENROUTE, ACFT DIVERTED DUE TO MX.Jun 14, 2009 · N884AS · Cndair CL6002B19SDR REXA200900066Fcu · failedFLIGHT 2816 ALB/DTW WHEN FLAPS SELECTED DOWN ON APPROACH RECEIVED "FLAPS FAIL" MESSAGE, QRH FOLLOWED WITH UNEVENTFUL LANDING. SYSTEM TROUBLESHOT PER BOMBARDIER FIM FOUND FLAP ELECTRONIC CONTROL UNIT (FECU) FAILED. REMOVED AND REPLACED THE FECU PER BOMBARDIERJun 14, 2009 · N8908D · Cndair CL6002B19SDR AALA2009061000006Transmission · malfunctionedJFK - AIRCRAFT EXPERIENCED TRAILING EDGE FLAP DISAGREE WHEN SELECTING FLAPS. LANDED JFK WITHOUT INCIDENT. FOUND LEFT TORQUE LIMITER POPPED. REPLACED NUMBER 4 FLAP TRANSMISSION. SYSTEM GROUND CHECK NORMAL OPERATION.Jun 10, 2009 · N618AA · Boeing 757223SDR DL76L091013Flap System · malfunctionedON FINAL WITHOUT T/O CONFIG WITH FLAPS MOVED FROM 5 TO 20 AND GEAR EXTENDED THE FLAPS STAYED AT 5 POS WITH LEVER IN 20 POS AND A T/E DISAGREE MESSAGE. CREW DECLARED EMERGENCY INTO VCE. PERFORMED GO-AROUND FIM PROCEDURE 27-51-00 FIG 105. PERFORMED OK. FSEU Jun 9, 2009 · N187DN · Boeing 767332SDR AALA209060800003Transmission · malfunctionedJFK - INFLIGHT MIA-LGA. CREW REPORTED FLAP TRAILING EDGE DISAGREE. EMERGENCY DECLARED, LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT INBOARD NUMBER ONE TRANSMISSION OVERLOAD. FLUSHED AND SERVICED NUMBER ONE TRANSMISSION. SYSTEM GJun 8, 2009 · N618AA · Boeing 757223SDR REXA200900095Ecu · failedJUNE 7, 2009 FLIGHT 2961 SDF/DTW - FLAPS FAILED AT 20 DEGREES WHEN SELECTED DOWN. MAINTENANCE INSPECTED AIRCRAFT PER BOMBARDIER FIM IAW AD 2009-06-12. FOUND FECU FAILED.Jun 7, 2009 · N8721B · Cndair CL6002B19SDR REXA200900094Bpsu · failedJUNE 7, 2009 FLIGHT 2961 SDF/DTW - FLAPS FAILED AT 20 DEGREES WHEN SELECTED DOWN. MAINTENANCE INSPECTED AIRCRAFT PER BOMBARDIER FIM IAW AD 2009-06-12. FOUND RT BPSU FAILED.Jun 7, 2009 · N8721B · Cndair CL6002B19SDR REXA200900093Bpsu · failedJUNE 7, 2009 FLIGHT 2961 SDF/DTW - FLAPS FAILED AT 20 DEGREES WHEN SELECTED DOWN. MAINTENANCE INSPECTED AIRCRAFT PER BOMBARDIER FIM IAW AD 2009-06-12. FOUND LT BPSU FAILED.Jun 7, 2009 · N8721B · Cndair CL6002B19SDR CA090618006Relay · intermittent(CAN) FLAP`S FAILED TO EXTEND INTERMITTENTLY.Jun 7, 2009 · Beech 200BEECHSDR YENA20090610061Computer · faultyFLT 1756 - SJU-FLL - WHEN SELECTING FLAPS 2 RECEIVED F/CTL FAULT ECAM. FLAPS WERE STUCK AT 0. COMPLETED ECAM AND QRH AND LANDED PER QRH/DISPATCH/MTC IN THAT CONFIGURATION. PERFORMED TROUBLESHOOTING AS PER TSM 27-51-00. DURING TROUBLESHOOTING FOUND THAT ALLJun 7, 2009 · N503JB · Airbus A320232SDR COMA2009060850152Control Handle · failedON FINAL RECEIVED FLAPS FAIL CAUTION MSG. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED FLAP CONTROL HANDLE.Jun 6, 2009 · N960CA · Cndair CL6002B19SDR REXA200900060Bpsu · failedON CLIMB GOING THROUGH 19,000 FLAPS FAILED AT ZERO, RETURNED TO DTW WITH UNEVENTFUL LANDING. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM AND WAS DETERMINED TO BE A FAILURE OF THE RIGHT BRAKE POSITION SENSING UNIT (BPSU). UNIT REPLACED AND FLAPS RIGGED PER BJun 3, 2009 · N8891A · Cndair CL6002B19SDR CA090618005Flap System · intermittent(CAN) FLAPS FAIL TO EXTEND INTERMITTENTLY.Jun 2, 2009 · Beech 200BEECHSDR ASOA200900616Flap · failedFLAPS FAIL AFTER T/O WHEN SELECTING FLAPS TO ZERO V2 250 ON LANDING 50000 LBS, EMERGENCY DECLARED. A/C RETURNED TO CVG AFTER T/O. FLT 5570 DEL 215 MINS.Jun 2, 2009 · N922EV · Cndair CL6002B19SDR REXA200900059Fcu · failedFLAP FAIL MESSAGE RECEIVED IN CRUISE. MAINTENANCE TROUBLESHOT SYSTEM PER BOMBARDIER FIM AND DETERMINED FAILURE OF THE FLAP ELECTRONIC CONTROL UNIT (FECU). REMOVED AND REPLACED FECU IAW AMM.Jun 2, 2009 · N8891A · Cndair CL6002B19SDR DL757090935Transmission · malfunctionedUPON SELECTING FLAPS 20, BECAME STUCK BETWEEN 15 AND 20 AND TE FLAP DISAGREE EICAS MSG APPEARED EXECUTED PROC WITH TE FLAP DISAGREE AND FLAPS 26. PERFORMED FSEU BITE NTF INSP FLAP TRANSMISSION, FOUND RT W/W SIDEWAYS TRANSMISSION OVERLOAD INDICATOR POPPED. RESMay 28, 2009 · N645DL · Boeing 757232SDR REXA200900055Flap System · out of rigMAY 25, 2009, CREW RECEIVED "FLAP FAILURE" MESSAGE ON CLIMBOUT WHEN SELECTING FLAPS TO UP. MX INSPECTED THE ACFT AND TROUBLESHOT IAW MFG FAULT ISOLATION MANUAL, FLAPS FOUND TO BE OUT OF RIG. FLAPS RIGGED IAW MM WITH OPS CHECKS PERFORMED WITH NO DEFECTS.May 25, 2009 · N8516C · Cndair CL6002B19SDR AALA2009052200001Warning Switch · activatedJFK - TRAILING EDGE FLAP DISAGREE MESSAGE DISPLAYED AT FLAP 1 DURING APPROACH. CREW EXECUTED GO-AROUND. LANDED JFK WITHOUT INCIDENT. ACCOMPLISHED BITE OF FEEU PER FIM 27-51-00, NO FAULTS NOTED. INSPECTED ALL ROTARY ACTUATORS CHECK NORMAL. CYCLED FLAPS, ALMay 22, 2009 · N323AA · Boeing 767223SDR A6WA200940264Drive Unit · malfunctioned180710/3 -FLAPS FAIL AT 8 DEGREES UPON RETRACTION TO ZERO DEGREES. UPON LANDING BRAKE TEMPS WERE NORMAL (4,4,4,4) LANDED AT 46,100. COMPLIED WITH RESET IAW AWAC SUPP 98-018C. RESET AND PLACED ON MEL. INTEROGATED FECU FOUND PDU DIFF FAULTED. IAW FIM 27-50-May 21, 2009 · N460AW · Cndair CL6002B19SDR UALA2009052101466Fcu · malfunctionedEICAS MSG "FLAP LD RELIEF" DISPLAYED. TRAILING EDGE LIGHT ILLUM. FLAPS 30 SELECTED, 30 UNITS INDICATED, AIRSPEED EXCEEDS 162 KTS (170 KTS WITH -17 AND SUBS FSEU). CREW COMMENTS, T/E DID NOT RETRACT BY 175 KTS AS REQ`D BY TEST PROCEDURE. MAX SPEED 178 KNOTSMay 20, 2009 · N661UA · Boeing 767322SDR SIMA200913901ABpsu · malfunctionedON FLIGHT 3958, CREW REPORTED AT 180KTS THEY SELECTED FLAPS 20 THEN RECEIVED A FLAPS OVER SPEED FOLLOWED BY A FLAPS FAIL THEY DECLARED A EMERGENCY DUE TO THE FLAP FAIL AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT FLAMay 18, 2009 · N512AE · Cndair CL6002C10SDR DL76L090899Flap System · malfunctionedT/E FLAP DISAGREE MSG ILLUMINATED DURING APR REPLACED FLAP SLAT ELECT UNIT ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.May 18, 2009 · N188DN · Boeing 767332SDR SIMA200913902Bpsu · malfunctionedON FLIGHT 3958 CREW REPORTED AT 180KTS THEY SELECTED FLAPS 20 THEN RECEIVED A FLAPS OVER SPEED FOLLOWED BY A FLAPS FAIL THEY DECLARED A EMERGENCY DUE TO THE FLAP FAIL AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED RIGHT FLAPMay 18, 2009 · N512AE · Cndair CL6002C10SDR FDEA200905141663Bypass Valve · failedON DEPARTURE, FLAP RETRACTION NOT NORMAL, SPLIT FLAPS, OUTBOARD FLAPS IN AGREEMENT W/HANDLE AT FLAPS 5 DEG INBOARD FLAPS STAYED AT 15 DEG. RAN QRH, SOME SLATS EXTENDED. ATTEMPTED FLAP MASTER & RAISE INBD FLAPS, ALT FLAP MOTOR INBD C/B POPPED. RTB. INBD FLAMay 14, 2009 · N258FE · Boeing 727200SDR REXA200900050Fcu · failedFLIGHT 2453 ICT/MSP CREW RECEIVED FLAP FAIL CAUTION MESSAGE WHILE BOARDING PASSENGERS. MAINTENANCE PERFORMED FIM TROUBLES SHOOTING PER AD 2009-06-12 FOUND FLAP ELECTRONIC CONTROL UNIT (FECU) SHOWING CODE FOR INTERNAL FAILURE. FECU REMOVED AND REPLACED PER AMMay 14, 2009 · N8698A · Cndair CL6002B19SDR AALA2009051300002Flap System · malfunctionedJFK - CAPTAIN REPORTED WHEN CHANGING FLAPS FROM 20 TO 25 DEGREES , RECEIVED A TRAILING EDGE DISAGREE LIGHT AND FLAPS STUCK MESSAGE ON GAUGE. EMERGENCY DECLARED, LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED FIM 27-51-00 AND FIM 27May 13, 2009 · N332AA · Boeing 767223SDR 2009FA0000449Control Cable · brokenAN INSP OF RT WING FLAP CABLE REVEALED BROKEN STRANDS WHERE THE CABLE THIMBLE AND SHACKLE TO THE FLAP BELLCRANK INSIDE THE WING. THERE IS INSUFFICIENT CLEARANCE BETWEEN THE CABLE AS IT WRAPS AROUND THE THIMBLE AND THE BELLCRANK AND IT WAS GETTING PINCHED WHENMay 12, 2009 · N62045 · Maule M5210CSDR REXA100900049Flap System · malfunctioned5/11/2009 ACFT 8423C FLIGHT NR 2132 MCI/MSP, ON APPROACH WHEN FLAPS SELECTED DOWN FAILED AT 20 DEGREES. FLIGHT CREW REPORTED TO MAINTENANCE THAT THEY MISTAKENLY MOVED THE FLAP SELECTOR A SECOND TIME BEFORE THE FLAPS REACHED THE FIRST SELECTED DEGREE SETTING. May 11, 2009 · N8423C · Cndair CL6002B19SDR UALA2009051101329Fseu · failedFLAPS FAILED TO EXTEND. FOUND MESSAGES 27-21021 AND 27-20431. REPLACED FSEU NR 1 IAW MM 27 -51-01. RAN FLAPS TO FULL EXTEND AND BACK. STILL HAS FLAP-SLAT CONTROL 1 MESSAGE ON ECAM. MESSAGE IS DEFERABLE. SWAPPED FSEU 1 AND 2, PROBLEM FOLLOWED. DISPLAYED CH 2May 10, 2009 · N778UA · Boeing 777222SDR GLBA20090508AControl Unit · malfunctioned(SUP)- PILOTS REPORTED THAT A CONTROL FAULT ILLUMINATED IN FLIGHT. THEY RE-SET ONCE AND IT THEN ILLUMINATED A SECOND TIME. THE OUTBOARD FLAP BAR 10 DEGREE BLINKED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY AND BASED UPON HISTORICAL DATA REMOVED ANMay 8, 2009 · N96ZK · Emb EMB120ERSDR CA090618013Flex Drive · broken(CAN) AFTER LANDING ROLL OUT UPON RETRACTING THE FLAPS, RECEIVED "FLAPS FAIL" (C) MESSAGE. INVESTIGATION REVEALED THE RT NR 4 FLEX SHAFT WAS BROKEN. THE FLEX SHAFT ASSY WAS REMOVED AND REPLACED. AS PRECAUTION OPERATOR REMOVED AND REPLACED ALL 8 ACTUATORS ANDMay 5, 2009 · Cndair CL6002B19SDR CA090506010Fcu · failed(CAN) ON FLAP SELECTION FROM 20 TO 8 RECEIVED FLAP FAIL MESSAGE ON EICAS. CARRIED OUT UNSCHEDULED LANDING WITH 20 FLAP WITH NO FURTHER INCIDENT. FOUND FECU POWER LEDS AND RT PANEL LEDS ILLUMINATED ON SKEW DETECTION UNIT. RESET SDU AND FECU, CARRIED OUT OPS CK May 5, 2009 · Cndair CL6002B19SDR USAA2009050591096Computer · malfunctionedFLT 904 - CLT-ORD - EMERGENCY LANDING - FLIGHT CONTROL SLATS LOCKED - ECAM MESSAGE. PERFORMED RESET OF SLAT FLAP CONTROL COMPUTER (SFCC) 1 AND 2 PER MAINTENANCE MANUAL 27-84-00-05. PERFORMED OPERATIONAL TEST OF THE WING TIP BRAKE PER MAINTENANCE MANUAL 27-51May 3, 2009 · N741UW · Airbus A319112SDR REXA200900044Fcu · malfunctionedFLAP FAIL MESSAGE ON THE GROUND AFTER EXTENSION TO 8 DEGREES. TROUBLESHOT SYSTEM PER BOMBARDIER FIM 27-50-00 FOUND THE FLIGHT ELECTRONIC CONTROL UNIT (FECU)TO SHOW FAILURE CODES. REMOVED AND REPLACED FECU PER BOMBARDIER AMM WITH OPERATIONAL CHECK PERFORMED WMay 3, 2009 · N8903A · Cndair CL6002B19SDR 2009FA0000342Rod Bearing · defectiveDEFECT REPORT GENERATED BASED ON A FAILURE THAT THE MX FOUND BY CHANCE WHILE PERFORMING ANOTHER INSP. FWDING FOR YOUR REVIEW AND SUBMITTAL THROUGH THE QC DEPARTMENT.. MX FOUND ONE OF THESE FLAP CONTROL ROD ENDS TO BE DEFECTIVE WHILE PERFORMING OTHER MX AND UPApr 30, 2009 · N684SA · Cessna 208BSDR RAIA2009050400003Ecu · failedFLT 7933 -IAD- FLAP FAILED AT 2 DEGREES. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. OPERATIONAL CHECK OF THE SYSTEM WAS GOOD.Apr 29, 2009 · N836HK · Emb EMB145LRSDR GLBA200904281Relay · odorBURNING PLASTIC ODOR WHEN MODE CONTROLLER & BLOWERS ON. MAINTENANCE REMOVED FLOORBOARDS OVER THE FORWARD AND AFT VENT BLOWERES. FOUND BLOWERS TO OPERATE. RE-INSTALLED FLOORBOARDS. REMOVED FLOORBOARD COVERING FLAP MOTOR, GEARBOX, AND FLAP RELAY. NOTICED AN Apr 27, 2009 · N153GL · Beech 1900DSDR COMA2009042750122Flap · failedON APPROACH INTO BOS RECEIVED FLAPS FAIL MSG, FLAPS FAILED AT 0 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL GMM 5-2.Apr 26, 2009 · N409CA · Cndair CL6002B19SDR SWIA200921531Flap · out of adjustFLT 6625 - FLAP CAUTION AND FLAP OUT OF ALIGNMENT. REPLACED FLAP AND ACTUATORS.Apr 25, 2009 · N976SW · Cndair CL6002B19SDR MASA2009042400136Bpsu · malfunctionedASH FLT 7303 GSP-IAD. CAPTAIN DECLARED AND EMERGENCY AND RETURNED TO THE FIELD DUE TO A FLAPS FAIL CAUTION AT 8 DEGREES. MX REMOVED AND REPLACED LT BPSU.Apr 24, 2009 · N593ML · Cndair CL6002B19SDR ASAA0945277Bracket · crackedNR 6 FLAP TRANSMISSION O/B TORQUE TUBE DOGHOUSE LOWER I/B BRACKET. REPLACED CRACKED BRACKET.Apr 24, 2009 · N765AS · Boeing 7374Q8SDR AALA2009042300001Control Module · inoperativeORD CREW REPORTED ABNORMAL HEAVYNESS OF ELEVATOR AT ROTATION. EMERGENCY DECLARED RETURNED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP SLAT CONTROL VALVE MODULE AND NUMBER NINE SPEEDBRAKE ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATIApr 23, 2009 · N619AA · Boeing 757223SDR YENA20090424038Flap · malfunctionedFLT 661, SYR-MCO, FLAP FAIL (0) ZERO FLAP, LANDING SLATS WORKED. VERIFIED BOTH OUTBOARD FLAP ACTUATORS WERE NOT TRIPPED. CLEARED SURFACE INHIBITS. PERFORMED PDU BRAKE RELEASE AND RE-ENGAGE. PERFORMED OPS CHECK OF FLAPS/SLATS SYS PER AMM 27-50-00. ALL CHECApr 23, 2009 · N281JB · Emb ERJ190100IGWSDR ASOA200900459Flap · failedFLAPS FAIL AT FL220 AT 0, EMERGENCY DECLARED. FLT 5328 DEL 31 MINS.Apr 18, 2009 · N916EV · Cndair CL6002B19SDR MASA2009041700130Bpsu · malfunctionedASH FLT 7263 ORD-ABE. AIRCRAFT RTF AND CREW DECLARED AN EMERGENCY FOR FLAP FAIL AFTER FLAP WAS RETRACTED TO 0 DEGREES. MX SWAPPED AND R2 BOTH BPSU.Apr 17, 2009 · N592ML · Cndair CL6002B19SDR IPXA09M55574Flap System · vibrationDURING CLIMB TO ALTITUDE NOTICED VIBRATION. SELECTED CONFIG PAGE RIGHT INNER FLAP BOX WAS SHOWING EMPTY BOX OUTER BOX SHOWED 0 DESCEND TO FLIGHT LEVEL 20.000 STOWED AND EXTENDED SLATS AND FLAPS TO 15, THEN GOT A LEVEL TWO FLAP DISAGREE. PERFORMED INSPECTIONApr 16, 2009 · N254UP · Doug MD11FSDR DJFA2009013Control Cable · brokenWHILE INSPECTING FLIGHT CONTROL CABLES FOR A REPORTED VIBRATION DISCREPANCY, MX DISCOVERED THE FWD (EXTENSION) FLAP FOLLOW-UP CABLE BROKEN AT THE CRIMPED FERRULE FOR THE CENTER BELL CRANK. INSP OF THE BREAKAGE REVEALED SEVERE CORROSION CONCENTRATED IN THE AREApr 15, 2009 · N413LX · Beech 400ASDR DXTA2009041403602None · noneON CLIMBOUT AND AT A FLAPS SETTING OF 7 DEGREES, A NEAR MISS CAUSED A FLAP OVERSPEED OF APPROX 40 KNOTS. COMPLIED WITH CESSNA 'OVERSPEED CHECK'. NO DEFECTS NOTED. INSPECTED IAW MM CH 5-50-00. PERFORMED TRAVEL CHECKS ALSO. TRAVELS GOOD. WORK IAW MM TASK 27-57-Apr 13, 2009 · N818QS · Cessna 560CESSNA
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