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 03FDEA00534Pulley · brokenRT WING T/E INBOARD FLAP INNER TRACK ROLLER AREA FOLLOW UP CABLE INNER PULLEY BROKEN. R/R PULLEY BRACKET & PULLEY.Apr 18, 2003 · N320FE · Doug DC1030SDR SWIA200312023Flex Drive · bentLEFT OUTBOARD FLAP FLEX DRIVE (NR 5) IS BENT AT ENDS. FOUND DURING C-CHECK INSPECTION. LEFT OUTBOARD FLEX DRIVE NR 5 HAS BEEN REPLACED IAW AMM 27-53-10.Apr 17, 2003 · N909SW · Cndair CL6002B19SDR C2XA03BT053Connector · dirtyEWR---CO2546, CREW REPORTED FLAP FAILED, DECLARED EMERGENCY AND LANDED UNEVENTFULLY. MAINTENANCE INSPECTED FLAPS AND CHECKED ELECTRICAL CONTINUITY IN ALL CONNECTOR PINS FOR LEFTHAND AND RIGHTHAND FLAP TRANSMISSION BRAKES AND FLAP VELOCITY SENSORS. INCLUDING Apr 17, 2003 · N13956 · Emb EMB145SDR 03FDEA00467Motor · failedAFTER T/O FLAP RETRACTION - OUTBOARD T/E FLAPS STAYED AT 5 DEG WHEN FLAPS WERE RETRACTED TO 2 DEGREES. USED ALT FLAP MASTER SWITCH TO RETRACT FLAPS PER QRH PROCEDURE. PERF T/S AND FOUND OUTBOARD FLAP STUCK FROM 5 TO 2, RESET USING ALTERNATE. COULD NOT GET IApr 17, 2003 · N220FE · Boeing 727200SDR S2YA03015Switch · inoperativeDURING TAKEOFF OF FLIGHT 1076, THE CREW HEARD A LOAD POP FROM WHAT THEY REPORTED WAS THE LEFT ENGINE. THEY NOTED STRONG FUMES IN THE COCKPIT AND DONNED THEIR OXYGEN MASKS. THE CREW TURNED OFF THE ENVIRONMENTAL AIR, IAW THE QRH AND MADE AN AIR-TURN-BACK. MECApr 16, 2003 · N881SK · Beech 1900DSDR GLBA2003048Switch · lack of lubeFLAPS WILL NOT RETRACT, CLEANED LUBED & OPS CHK FLAP SAFETY SWITCHES OPS CHECKS GOOD.Apr 16, 2003 · N249GL · Beech 1900DSDR SWIA200311881Fcu · malfunctionedFLAP FAIL MESSAGE IN FLIGHT. PERFORMED A NO FLAP LANDING. PULLED AND RESET FLAP CIRCUIT BREAKERS. OPS CHECK OF FLAPS GOOD. UPDATE 3/18/2003: FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH WHEN SELECTING FLAPS 8 DEGREES, FLAPS FAILED AT 0 DEGREES. FLAApr 14, 2003 · N924SW · Cndair CL6002B19SDR SWIA200311886Annunciator · malfunctionedBOTH OUTBOARD FLAPS FLUTTER UP TO 5 DEGREES WHEN IN THE 15 DEGREE AND 25 DEGREE POSITIONS. NO FAILURE INDICATED ON THE FLAP CONTROL PANEL. REPLACED FCU AND ANNUNCIATOR WITH VERSION II. OPS CHECK GOOD.Apr 12, 2003 · N196SW · Emb EMB120ERSDR SWIA200311871Control Unit · malfunctionedFLAP CONTROL FAULT IN CRUISE. ONE SEGMENT NAC FLASHING, REST OK. FLAP CONTROL FAULT WHEN 25 DEGREES OF FLAPS SELECTED AT APPROXIMATELY 15 DEGREES OF FLAPS, REMAINDER OK. REMOVED AND REPLACED FLAP CONTROL UNIT IAW EMB120 MM 27-50-06. OPS CHECK GOOD.Apr 10, 2003 · N268UE · Emb EMB120ERSDR SWAA030778Motor · failedAFTER PUSHBACK T/E FLAPS WOULD NOT FULLY EXTEND, CABIN CREW REPORTED NOISE RT OVERWING. REMOVED AND REPLACED FLAP DRIVE MOTOR AND FLAP DRIVE UNIT PER MM.Apr 7, 2003 · N301SW · Boeing 7373H4SDR SWAA030776Sensor · faultyDECLARED EMERGENCY, DURING APPROACH T/E FLAPS STOPPED AT POSITION 2. REMOVED AND REPLACED NR 6 T/E FLAP SKEW SENSOR PER MM.Apr 7, 2003 · N738CB · Boeing 7377H4SDR SWIA200311872Control Unit · malfunctionedRECEIVED FLAP FAIL CAUTION MESSAGE AT 11,000 FT. ON DOWNWIND, FLAPS FAILED AT 0 DEGREES. INTERROGATED FECU UPON ARRIVAL AT GATE. NO FAILURES LISTED. PERFORMED VISUAL INSPECTION OF FLAPS AND BPSU RIG CHECK AND SYSTEM CHECKS IAW CL600 MM 27-51-00 & 27-51-05.Apr 6, 2003 · N418SW · Cndair CL6002B19SDR U30A200300012Computer · faultyDURING MAINTENANCE AFTER FLT 247 IN EWR, THE NR 1 SLAT FLAP SYSTEM FAULTED. REMOVED AND REPLACED THE NR 1 SLAT FLAP CONTROL COMPUTER (SFCC) IAW 27-51-34-000-001, TESTED OK IAW 27-54-00-710-002. AIRCRAFT RETURNED TO SERVICE.Apr 4, 2003 · N261AV · Airbus A320214SDR SWIA200311895Switch · malfunctionedWITH FLAPS SELSECTED TO 15 DEGREES FLAP CONTROL FAULT. REMOVED AND REPLACED FLAP SELECTOR HANDLE WITH SERVICEABLE UNIT. RAN FLAPS FULL SCALE MULTIPLE TIMES. OPS CHECKS GOOD.Apr 3, 2003 · N593SW · Emb EMB120RTSDR SWIA200311868Controller · malfunctionedDURING APPROACH TO FAT, ATTEMPTED TO EXTEND FLAPS. FLAPS FAIL CAUTION MESSAGE ILLUMINATED AND FLAPS REMAINED AT ZERO DEGREES. FOLLOWED QHR PROCEDURE. LANDED WITH FLAPS AT ZERO DEGREES. RESET CIRCUIT BREAKERS FOR FLAPS CONTROLLER CHANNELS 1 & 2 (CB1 & 2F4).Apr 3, 2003 · N906SW · Cndair CL6002B19SDR SWAA030777Drive Gear · wornDURING APPROACH T/E FLAPS INDICATED SPLIT, WOULD NOT DEPLOY OR RETRACT. REMOVED AND REPLACED SHAFT DRIVE ASSY FOR LT WING T/E FLAPS PER MM.Apr 2, 2003 · N301SW · Boeing 7373H4SDR 2003F00257Motor · shortedAFTER LANDING, DURING POST FLIGHT, BURNING ELECTRICAL ODOR COMING FROM CARGO AREA. REMOVED AND REPLACED FLAP MOTOR. OPERATIONAL CHECK NORMAL. (M)Apr 1, 2003 · N87557 · Beech 1900DSDR SWIA200311865Bpsu · malfunctionedFLAPS FAIL CAUTION MESSAGE AFTER TAKEOFF WHILE RETRACTING FLAPS FROM 20 DEGREES TO 8 DEGREES. PERFORMED QRH AND RETURNED TO MEM FOR 8 DEGREE LANDING. REMOVED AND REPLACED RIGHT FLAP BPSU IAW MM 27-51-10. OPS CHECK GOOD.Mar 31, 2003 · N454SW · Cndair CL6002B19SDR COMA0360175Computer · malfunctionedFLIGHT 5928 FLAPS FAIL CAUTION DURING LANDING. REPLACED THE FECU.Mar 30, 2003 · N868CA · Cndair CL6002B19SDR CA030328003Transmission · seized(CAN) CAPTAIN COULD NOT RETRACT FLAPS AFTER TOUCHDOWN . ASYMMETRIC FLAP CONDITION WOULD NOT ALLOW FLAPS TOMOVE FROM 25 UNITS TO UP POSITION ON GROUND. AFTER APPROXIMATELY 30 SECONDS A LOUD BANG WAS HEARD FROM NR 2 FLAP TRANSMISSION. FLAP THEN MOVED FROM 25 UNIMar 27, 2003 · Boeing 737201SDR SWIA200311863Computer · malfunctionedFLAPS FAILED DURING APPROACH FOR LANDING AT DEN. LANDED WITHOUT INCIDENT. INSPECTED FLAPS FOR KINKS. NO DEFECTS NOTED. CYCLED POWER. RESET COMPUTER. OPS CHECK GOOD.Mar 27, 2003 · N924SW · Cndair CL6002B19SDR DL738030280Warning Light · illuminatedAT CRUISE - FL 390 - YAW DAMPER DISENGAGED AND WAS RESET. LEADING EDGE IN TRANSIT LIGHTS WERE OBSERVED ON OVERHEAD. FOLLOWED BY L/E LIGHTS ON FWD PANEL WITH T/E. FLAPS INDICATING 1/2 DEG. DESCENT INITIATED AND FLAPS RETRACTED FULLY ON THEIR OWN. CHECKED SMar 26, 2003 · N380DA · Boeing 737832SDR VNAA0303030Actuator · failedDURING CRUISE FLIGHT THE FLIGHT CREW REPORTED THAT THE PUSHER FAIL AND FLAP CONTROL FAIL MESSAGES APPEARED ON EICAS. THE FLIGHT CREW DIVERTED TO CAK. MAINTENANCE INSPECTED AND REPLACED THE RT FLAP ACUTATOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-51-Mar 25, 2003 · N431JS · Dorner DO328100SDR ASOA03124Controller · malfunctionedDURING APPROACH INTO ATL FROM SWF,WITH THE FLAPS SELECTED TO 8 DEGREES, THE CREW RECEIVED A FLAPS FAILED MESSAGE. EMERGENCY EQUIPMENT WAS REQUESTED AND THE AIRCRAFT LANDED SAFELY IN ATL WITH THE FLAPS TO ZERO. MAINTENANCE COMPLIED WITH AD 98-20-01 AND RESET Mar 23, 2003 · N861AS · Cndair CL6002B19SDR SWAA030669Fseu · faultyDURING FLAP EXTENSION AN ASYMMETRY DEVELOPED, LOWERED FLAPS WITH ALTERNATE SYSTEM & LANDED UNEVENTFULLY. REMOVED AND REPLACED FLAP/SLAT ELECT. UNIT, OPS CK'D GOOD PER MM.Mar 23, 2003 · N416WN · Boeing 7377H4SDR COMA0360161Computer · malfunctionedFLIGHT 5002 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.Mar 23, 2003 · N431CA · Cndair CL6002B19SDR SWIA200311849Bpsu · malfunctionedDURING APPROACH INTO SLC RECEIVED A FLAPS FAIL MESSAGE WITH FLAPS AT 20 DEGREES. RAN QRH PROCEDURE AND LANDED WITHOUT INCIDENT. FOUND LEFT BPSU TO BE JUMPY (TURNED SEVERAL TIMES WITH NO CHANGE IN POSITION). REMOVED AND REPLACED LEFT BPSU IAW 27-51-10 AND CHMar 22, 2003 · N595SW · Cndair CL6002B19SDR SWIA200311840Control Unit · failedFLAP FAIL MESSAGE - PERFORMED NO FLAP LANDING. COMPLIED WITH OPS CHECK OF FLAP SYSTEM. CHECKED FECU, NO FAULTS FOUND. OPERATED FLAPS, ALL OPS CHECKS GOOD IAW CRJ MM 27-51-00.Mar 20, 2003 · N915SW · Cndair CL6002B19SDR COMA0360160Bpsu · malfunctionedFLIGHT 5242 FLAPS FAIL CAUTION MESSAGE.COULD NOT DUPLICATE - REPLACED THE R/H BPSU FOR TROUBLE SHOOTING.Mar 20, 2003 · N920CA · Cndair CL6002B19SDR 03FDEA00340Solenoid Valve · failedAFTER TAKE OFF AT SIN, RECEIVED FLAPS SYS 1 FAULT. ALSO LOST AIRSPEED HOOK ON CAPT SIDE WITH RED SPEED LIMIT SHOWING. SFCC NR 1 BITE SHOWS FLAP RT WTB. R & R RT WTB SOLENOID VALVE PER MM 27-56-13-4 AND PERFORMED SFCC BITE TEST PER MM 27-51-00 TEST OK. Mar 20, 2003 · N422FE · Airbus A310SDR COMA0360157FlapFLIGHT 5873 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.Mar 18, 2003 · N920CA · Cndair CL6002B19SDR SWIA200311835Fcu · malfunctionedFLAP CONTROL FAULT FOR INBOARD FLAPS UPON RETRACTING FLAPS AFTER LANDING. REMOVED AND REPLACED FLAP ANNUNCIATOR PANEL AND FCU FOR TROUBLESHOOTING. RAN FLAPS UP AND DOWN SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME.Mar 17, 2003 · N190SW · Emb EMB120ERSDR WRLA200304Transmitter · failedAIRLERON DEFLECT DISAGREE IN FLIGHT. RETURNED TO DEPARTING STATION YOKOTA JAPAN. REPLACED FLAP HANDLE POSITION TRANSMITTER. (M)Mar 15, 2003 · N271WA · Doug MD11SDR COMA0360150FlapFLIGHT 5711 FLAPS FAIL MESSAGE AFTER T/O.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.Mar 13, 2003 · N488CA · Cndair CL6002B19SDR COMA0360149FlapFLIGHT 5885 FLAPS FAIL CAUTION DURING TAXI.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.Mar 13, 2003 · N918CA · Cndair CL6002B19SDR COMA0360144FlapFLIGHT 5103 FLAPS FAILED AT 20 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.Mar 11, 2003 · N956CA · Cndair CL6002B19SDR DL76G030231Control Module · malfunctionedTRAILING EDGE FLAP DISAGREE JUST AS FLAPS APPROACHED ONE DEGREE ON FLAP RETRACTION. REPLACED FSEU PER M/M 480771. ADJUSTED FLAP TRANSMITTER 4 AND 5. REMOVED AND REPLACED T/E FLAP PDU CONTROL VALVE MODULE. PERFORMED T/E FLAP PDU TEST AND FLAP/SLAT SHUTOFF VMar 10, 2003 · N1611B · Boeing 767332SDR AUS20030479Control Cable · frayed(AUS) LH TRAILING EDGE FLAP CONTROL CABLE CONTAINED BROKEN STRANDS IN AREA APPROXIMATELY 25.4MM (1IN) FROM SWAGE AT BELLCRANK END.Mar 9, 2003 · Cessna M337BSDR COMA0360138Control Handle · malfunctionedFLIGHT 5532 FLAPS FAILED AT 20 DEGREES DURING LANDING.REPLACED THE FLAP SELECTOR LEVER.Mar 9, 2003 · N934CA · Cndair CL6002B19SDR ASOA03091Seal · crackedDURING HANGAR MAINTENANCE, THE LT FLAP VANE SPOILER, MIDDLE SEAL PLATE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE LT FLAP VANE SPOILER, MIDDLE SEAL PLATE IAW SRM.Mar 8, 2003 · N874AS · Cndair CL6002B19SDR HALA0300105Control Valve · damagedFLT 20 - SMF - FLAPS APPEAR TO BE BINDING/CHATTERING BETWEEN FLAP SETTING 20 AND 30. BINDING OCCURS AT THE END OF TRAVEL FOR EACH SETTING AT 20/25/30. EVALUATION FLIGHT REQUIRED. REMOVED AND REPLACED TRAILING EDGE FLAP POWER DRIVE UNIT HYDRAULIC MOTOR CONDIMar 6, 2003 · N592HA · Boeing 767300SDR MAS2003F00000Flap · malfunctionedFLT 6231. GDL-PHX. MECH CONTROL NR 189906. PIC DECLARED AN EMERGENCY FOR LANDING. FLAP FAIL AT 30 DEGREES. CW FLAPS FAIL MAINTENANCE PROCEDURE PART A (MTC-27-50-001). FLAPS RESET OK. PART B (MTC 27-50-002) DUE NLT 1100MST 03/08/03. 03/07/03. MECHANIC Mar 5, 2003 · N27314 · Cndair CL6002B19SDR MWEA030123Vane · delaminatedLEFT WING FIXED VANE LOCATED BETWEEN #2 FLAP BRACKET AND #3 FLAP BRACKET HAS AN AREA APPROXIMATELY 4" SQAURE OF DELAMINATION ON UNDERSIDE. -- HOT BOND REPAIRED VANE.Mar 5, 2003 · N803ME · Doug DC981SDR AUS20030264Control Cable · corroded(AUS) FLAP CONTROL CABLES PN 14601007 AND PNO 14601008 CORRODED AND FRAYED.Mar 3, 2003 · Cessna 337ASDR SWIA200311820Fcu · malfunctionedON TAXI OUT, UPON SELECTING FLAPS 15 RECEIVED A CONTROL FAULT. INSTALLED SERVICEABLE FLAP SELECTOR AND FLAP CONTROL UNIT. GROUND OPS CHECK GOOD. P/N: 120-64207-615, S/N OFF: 148978-304, S/N ON: 120237.Mar 1, 2003 · N271YV · Emb EMB120ERSDR AUS20030355Control Cable · frayed(AUS) RT INBOARD FLAP CABLE CONTAINED BROKEN STRANDS LOCATED IN AREA APPROXIMATELY 25.4MM TO 38.1MM (1IN TO 1.5IN) FROM THE INBOARD BELLCRANK TURNBUCKLE.Feb 27, 2003 · Cessna 337BSDR CA030227005Control Cable · frayed(CAN) DURING 100 HR INSPECTION THE INBOARD RIGHT HAND FLAP CABLE WAS INSPECTED FOR WEAR IN THE AREA OF THE INBOARD FLAP BELLCRANK. CABLE WAS FOUND FRAYED APPROX. 1 INCH FROM CABLE END ATTACH FITTING.CABLE R EPLACED.Feb 27, 2003 · Cessna 337GSDR COMA0360124FlapFLIGHT 5715 FLAPS FAIL CAUTON MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.Feb 26, 2003 · N403CA · Cndair CL6002B19SDR C2XA03CL051Shaft · brokenCLE FLIGHT 2221 THE CREW REPORTED A FLAP FAIL MESSAGE IN FLIGHT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FLEXIBLE SHAFT NR 2 SECTION ON THE RIGHT INBOARD FLAP. OPERATIONAL CHECKS WERFeb 26, 2003 · N22909 · Emb EMB145LRSDR CA030227004Control Cable · failed(CAN) OPERATOR EXPERIENCED A ASYMMETRIC FLAP CONDITION DURING LANDING CAUSED BY THE FAILURE OF A FLAP CABLE. THE INBOARD RIGHT HAND FLAP CABLE FAILED AT A POINT WHERE THE CABLE STARTS TO BEND AROUND THE INBOARD RIGHT HAND FLAP BELLCRANK. THIS AREA OF THE CABLEFeb 25, 2003 · Cessna 336
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