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 ASOA02460Flap · malfunctionedFLT 4450 - ON DESCENT INTO VPS, CAPTAIN RECEIVED A FLAP FAIL MESSAGE. AN EMERGENCY WAS DECLARED AND A 0 FLAP LANDING WAS MADE. AIRCRAFT LANDED SAFELY IN VPS. REVIEWED HISTORY AND NO FLAP FAILURE HISTORY WAS FOUND. INTERROGATED FECU. SYSTEM TEST PASSED. RAug 22, 2002 · N871AS · Cndair CL6002B19SDR AUS20020926Cable · frayed(AUS) TRAILING EDGE FLAP CABLES (14OFF) FRAYED. FLAP CABLE PART NUMBERS ARE:- PNO 6565007-102-1CR, PNO 6565007-100-1CR, PNO 6565007-114CR, PNO 6565007-112CR, PNO 6565007-401, PNO6565007-90CR, PNO 5565150-16CR (2OFF), PNO 5565150-3CR(2OFF), PNO 5565150-2CR, PNOAug 21, 2002 · Cessna 550SDR AALA20021198Ecu · failedMIA - FLT 1736 - EN ROUTE SJU-MIA - INBOUND TO MIA, TRAILING EDGE FLAPS STUCK AT 20 DEGREES. LANDED AT MIA WITHOUT INCIDENT. REPLACED NR 1 FLAT/SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Aug 20, 2002 · N675AN · Boeing 757223SDR SWIA200211152Control Unit · malfunctionedON APPROACH THE NACELLE FLAPS ARE INOP. REPAIRED WIRE W628-0007-22 BETWEEN P1869 & P0828. REMOVED AND REPLACED FLAP CONTROL UNIT. OPS CHECKS GOOD.Aug 20, 2002 · N199SW · Emb EMB120ERSDR ASOA02456Control Unit · faultyAFTER TAKEOFF, THE FLAPS DID NOT COME UP ABOVE SIX DEGREES. CAPTAIN PERFORMED APPROPRIATED CHECKLIST AND THE DECISION WAS MADE TO DIVERT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED OVERWEIGHT. MAINTENANCE COMPLIED WITH THE OVERWEIGHT LANDING INSPECTIAug 18, 2002 · N885AS · Cndair CL6002B19SDR COMA0260490FlapFLIGHT 6008 FLAPS FAILED AT 8 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANE PER AD 98-20-01.Aug 18, 2002 · N954CA · Cndair CL6002B19SDR CX7A194J17Potentiometer · out of adjustDURING INITIAL CLIMBOUT FLAPS BEGAN UNCOMMANDED DEPLOYMENT TO LESS THAN 7 DEGREES, THEN RETRACTED. CYCLE REPEATED APPROX EVERY 20 SEC W/PITCH UP MOVEMENT. NO AUTOPILOT ENGAGED, YAW DAMPER ENGAGED. FLAPS NOT SPLIT AND HANDLE AT FLAPS 0 DEG. FOUND LT FLAP POAug 16, 2002 · N308CE · Saab 340BSDR 2002UALA01314Indicator · looseRIGHT TRAILING EDGE FLAP WILL NOT EXTEND BEYOND 15 DEGREES. THE FLAP POSITION INDICATOR WAS IMPROPERLY TORQUED DURING INSTALLATION. INDICATOR WAS RETORQUED AND OPS CHECKED GOOD.Aug 14, 2002 · N504UA · Boeing 757222SDR COMA0260486Bpsu · malfunctionedFLAPS FAILED WHEN SELECTED TO 8 DEGREES AT GATE.REPLACED THE R/H BPSU.Aug 14, 2002 · N473CA · Cndair CL6002B19SDR CA030312010Control Quadrant · failed(CAN) AFTER TAKEOFF THE PILOT SELECTED FLAPS UP. A FLAP WARNING LIGHT ILLUMINATED AND THE FLAPS DID NOT MOVE. (FLAPS REMAINED AT 15 DEGREES). THE PILOT RETURNED TO LAND AT THE AIRPORT WITHOUT INCIDENT. A FLAP RESET WAS CARRIED OUT ON THE GROUND SERVICEABLE.Aug 13, 2002 · Pilats PC1245SDR COMA0260477Bpsu · malfunctionedFLIGHT 5761 FLAPS FAIL MESSAGE.REPLACED THE R/H BPSU.Aug 12, 2002 · N473CA · Cndair CL6002B19SDR ZW0A0208601Control Handle · dirtyTHE FLAP/SLAT SELECTOR HANDLE WAS DIFFICULT TO MOVE. FLIGHT RETURNED TO STL. FOUND THE HANDLE MECHANISM WAS DIRTY. CLEANED AND LUBRICATED THE FLAP/SLAT HANDLE MECHANISM.Aug 12, 2002 · N978TW · Doug DC983SDR COMA0260481FlapFLIGHT 5968 FLAPS FAILED AT 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Aug 11, 2002 · N420CA · Cndair CL6002B19SDR COMA0260480FlapFLIGHT 5961 FLAPS FAIL MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Aug 11, 2002 · N473CA · Cndair CL6002B19SDR YENA200222Proximity Sensor · defectiveUpon configuration for landing, slats operated normally. Flaps locked at 1. Landed at flap 1 configured slats 3 per FCOMMaintenance removed and replaced interconnecting struct Prox Sensor 39CV IAW MM 27-51-44-400-002 and Ops Tested IAW MM 27-51-00-710-002, OpsAug 11, 2002 · N531JB · Airbus A320232SDR AUS20020936Transmission · faulty(AUS) NR 7 FLAP TRANSMISSION ASSEMBLY FAULTY WITH A LOUD CLICKING NOISE BEING HEARD. EXCESSIVE AXIAL PLAY ALSO FOUND IN OUTPUT SHAFT.Aug 10, 2002 · Boeing 747438SDR SWIA200211111Control Unit · malfunctionedON TAXI IN WITH FLAPS TO 20 DEGREES, FLAPS FAIL CAUTION. REMOVED & REPLACED FCU WITH SERVICEABLE UNIT. ALSO COMPLIED WITH AD 98-20-01.Aug 8, 2002 · N594SW · Cndair CL6002B19SDR COMA0260473FlapFLIGHT 6044 FLAPS FAIL MESSAGE DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Aug 6, 2002 · N868CA · Cndair CL6002B19SDR UPS02439008Terminal · looseINSPECTION TYPE:N/A OUTBOARD FLAPS WOULD NOT EXTEND. SECURED TERMINALS 6 & 7 OF TB 258 AND TERMINAL 11 OF TB 259 IN J42, REPLACED S1404 GL 51752, S329, S339, PER MM 27-51-07. CYCLED FLAPS, NO MALFUNCTIONS FOUND.Aug 6, 2002 · N527UP · Boeing 747259BSDR CA020806006Bpsu · failed(CAN) FLAP FAILED AT 8 DEGREES. LT AND RT BPSU REPLACED AND ADJUSTED AS PER AMM 27-51-10Aug 5, 2002 · Cndair CL6002B19SDR VNAA0208004Fcu · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A FLAP CONTROL FAILURE CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND RESET THE FLAP CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELAug 5, 2002 · N439JS · Dorner DO328100SDR C2XA02IA155Brake · failedCREW REPORTED THAT ON DESCENT THE FLAPS WOULD NOT EXTEND. THE AIRCRAFT ACCOMPLISHED AN EMERGENCY DESCENT AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT FLAP TRANSMISSION BRAKE TO HAVE FAILED. THE AFFECTED FLAP BRAKE WAS REMOVED AND REPLACED,Aug 3, 2002 · N11565 · Emb EMB145LRSDR COMA0260464Actuator · bindingFLIGHT 5332 FLAPS FAIL CAUTION MESSAGE.REPLACED THE R/H #3 FLAP ACTUATOR.Jul 31, 2002 · N810CA · Cndair CL6002B19SDR 02FDEA00534Gearbox · lack of lubeLEFT WING FLAP SYS RT ANGLE GEARBOX FOUND NO OIL IN GEARBOX. R & R LT WING FLAP SYS RT ANGLE GEARBOX PER MM 27-54-13. REF N00509 FOR FLAP SYS ADJ.Jul 30, 2002 · N420FE · Airbus A310222SDR GLBA2002113Switch · malfunctionedFLAP STUCK AT 35 PERCENT, CHANGED FLAP SWITCH OPS CHECK GOODJul 29, 2002 · N261GL · Beech 1900DSDR AUS20020775Fitting · separated(AUS) SECONDARY DRIVE FLEXIBLE SHAFT ALUMINIUM END FITTING SEPARATEDFROM THE OUTER WIRE BRAID. THE INNER FLEX DRIVE WAS FOUND TO BE SLIGHTLY BENT AT ONE END. DURING REMOVAL OF THE DRIVE SHAFT, IT WAS FOUND THAT THE OTHER ALUMINIUM END FITTING HAD COME FREE FROJul 29, 2002 · Dhav DHC8102SDR VNAA0207042Fcu · malfunctionedDURING TAKEOFF, THE CREW RECEIVED A FLAP CONTROL FAIL CAS MESSAGE. MAINTENANCE INSPECTED AND RESET THE FLAP CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.Jul 29, 2002 · N439JS · Dorner DO328100SDR SWIA200211094Fcu · malfunctionedFLAP DISAGREEMENT ON INBOARD PAIR. CYCLED 3 TIMES AFTER TAKEOFF. RETURNED TO DENVER. INSTALLED SERVICEABLE FLAP CONTROL UNIT. REMOVED AND REPLACED FLAP ANNUNCIATOR. CLEANED CANNON PLUGS & TRACKS. OPS CHECK GOOD.Jul 29, 2002 · N581SW · Emb EMB120ERSDR COMA0260459FlapFLIGHT 5273 FLAPS FAILED AT 45 DEGREES AFTER LANDING.RESET THE FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Jul 29, 2002 · N957CA · Cndair CL6002B19SDR ASOA02421Flap · malfunctionedFLT 4463 - ON APPROACH INTO SHV, THE FLAPS FAILED AT 20 DEGREES. THE CAPTAIN FOLLOWED THE APPROPRIATE QRH PROCEDURES. AN EMERGENCY WAS DECLARED AS A PRECAUTION. AIRCRAFT LANDED SAFELY IN SHV. MAINTENANCE RESET THE FLAP SYSTEM AND FOUND IT TO OPERATE NORMALJul 24, 2002 · N871AS · Cndair CL6002B19SDR COMA0260456FlapFLIGHT 5160 FLAPS FAILED AT 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Jul 24, 2002 · N821CA · Cndair CL6002B19SDR COMA0260455Actuator · bindingFLIGHT 5037 FLAPS FAIL CAUTION MESSAGE.REPLACED THE R/H #3 FLAP ACTUATOR.Jul 23, 2002 · N868CA · Cndair CL6002B19SDR SWIA200211066Bpsu · failedFLAP FAIL MESSAGE APPEARED DURING TAXI IN. REMOVED AND REPLACED RIGHT FLAP BPSU IAW CRJ MM 27-51-10. OPS CHECK GOOD.Jul 23, 2002 · N920SW · Cndair CL6002B19SDR COMA0260451Bpsu · malfunctionedFLIGHT 5085 FLAPS FAILED AT 45 DEGREES.REPLACED THE L/H BPSU.Jul 23, 2002 · N962CA · Cndair CL6002B19SDR COMA0260447FlapFLIGHT 5020 FLAPS FAIL CAUTION MESSAGE AT 26 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Jul 22, 2002 · N868CA · Cndair CL6002B19SDR COMA0260445Potentiometer · malfunctionedFLIGHT 6085 LEFT FLAP INDICATION FLUCTUATED BETWEEN 4 AND 0 DEGREES DURING FLIGHT.FECU AND DFDR VERIFIED THERE WAS NO FLAP MOVEMENT. REPLACED L/H FLAP POSITION POT.Jul 21, 2002 · N962CA · Cndair CL6002B19SDR COMA0260437Actuator · bindingFLIGHT 5306 RECEIVED A FLAP FAIL CAUTION MESSAGE AT 30 DEGREES.REPLACED THE RIGHT WING #3 FLAP ACTUATOR.Jul 18, 2002 · N868CA · Cndair CL6002B19SDR COMA0260435Actuator · bindingFLIGHT 5306 RECEIVED A FLAP FAIL CAUTION MESSAGE AT 30 DEGREES. REPLACED THE RIGHT WING #4 FLAP ACTUATORJul 18, 2002 · N868CA · Cndair CL6002B19SDR COMA0260434Actuator · bindingFLIGHT 5306 FLAPS FAIL MESSAGE AT 30 DEGREES.REPLACED R/H #3 AND #4 FLAP ACTUATORS.Jul 18, 2002 · N868CA · Cndair CL6002B19SDR WC72002F00002Bearing · seizedTHE FLAPS WERE STUCK AT 20 DEGREES. ANY ATTEMPT TO RAISE OR LOWER THEM CAUSED THE 40 AMP FUSE TO BLOW. SUBSEQUENT INVESTIGATION REVEALED THAT THE FLAP MOTOR HAD A SEIZED BEARING AT THE TELEFLEX DRIVE ON ONE END. IT WAS NOTED THAT A FUSELAGE DRAIN WAS LOCATEJul 15, 2002 · N398CW · Cessna 650SDR COMA0260428Computer · malfunctionedFLIGHT 5806 - FLAPS FAIL CAUTION MESSAGE.REPLACED THE FECUJul 15, 2002 · N932CA · Cndair CL6002B19SDR SWIA200211053Ecu · failedFLAPS FAIL MSG DURING CLIMB. CONTINUED TO SLC. ZERO DEGREE FLAP LANDING AT 43,000 LBS. RERIGGED FLAPS AND INSTALLED NEW FECU C/W AD 98-20-01/02. OPS CHECK GOOD.Jul 14, 2002 · N442SW · Cndair CL6002B19SDR COMA0260430Computer · malfunctionedFLAPS FAILED CAUTION AT 30 DEGREES.REPLACED THE FECU.Jul 13, 2002 · N965CA · Cndair CL6002B19SDR COMA0260429Lever · malfunctionedFLIGHT 5694 FLAPS FAIL CAUTION MESSAGE.REPLACED THE FLAP CONTROL LEVER ASSY.Jul 13, 2002 · N938CA · Cndair CL6002B19SDR GLBA2002107Control Unit · inoperativeFLAP DISAGREEMENT. REPLACED FLAP CONTROL UNIT OPS CHECKED SATISFACTORY.Jul 13, 2002 · N96ZK · Emb EMB120ERSDR COMA0260424Bpsu · malfunctionedFLIGHT 5507 FLAPS FAILED CAUTION MESSAGE.REPLACED THE R/H BPSU.Jul 11, 2002 · N467CA · Cndair CL6002B19SDR CA020731013Control Cable · failed(CAN) NR 5 FLAP ACTUATOR ROLLER TRACK DISENGAGED AND WENT THROUGH THE INBOARD SIDE OF NR 5 FLAP FAIRING. NR 5 FLAP TRACK FITTING FOUND DAMAGED (SNAPPED) DUE BOOM CABLE BROKEN. CABLE, TRACK FITTING, PULLEYS, BOOM ASSY, AND CAM FOLLOWER GUARD ADJUSTED AS PERJul 9, 2002 · Boeing 7372T7SDR COMA0260418Computer · malfunctionedFLIGHT 5322 FLAPS FAIL CAUTION MESSAGE DURING LANDING.REPLACED THE FECUJul 6, 2002 · N940CA · Cndair CL6002B19SDR SWIA200211027Flap · malfunctionedON APPROACH RECEIVED A FLAPS FAIL MESSAGE. LANDED WITH FLAPS AT ZERO. COMPLIED WITH AD 98-20-01/03. NO DISCREPANCIES NOTED ON FLAP INSPECTION. RESET FLAP COMPUTER WITH NO FURTHER INSTANCES OF FLAP FAILURE. FLAP SYSTEM IS OPERATING NORMALLY.Jul 6, 2002 · N442SW · Cndair CL6002B19SDR COMA0260414FlapFLAPS FAILED MESSAGE AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.Jul 5, 2002 · N960CA · Cndair CL6002B19
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