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 RAIA00211305Fcu · false indication5305-PIT- FLAP LOW SPEED WARNING INDICATION. MAINTENANCE DEFERRED PER MEL; SUBSEQUENTLY REMOVED AND REPLACED FLAP CONTROL UNIT, OPS CK OK.SDR AUS20021197Torque Tube · corroded(AUS) RH INBOARD FLAP TORQUE TUBE AND COLLAR FITTING CORRODED BEYONDLIMITS. FOUND DURING INSPECTION IAW AD/B767/108.SDR COMA0260579Fcu · malfunctionedFLAPS FAILED AT 13 DEGREES. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.SDR COMA0260577FlapFLAPS FAIL MESSAGE AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0260571Actuator · malfunctionedFLAPS FAILED AT 36 DEGREES.REPLACED ALL FOUR INBOARD FLAP ACTUATORS.SDR COMA0260576Bpsu · malfunctionedFLAPS FAILED AT 40 DEGREES. REPLACED THE RIGHT BRAKE AND POSITION SENSOR UNIT.SDR CX7A194J21Flap · out of rigIN FLIGHT MULTIPLE UNCOMMANDED PITCH CHANGES WITH NO OTHER NOTICEABLE ANOMALIES. FLIGHT DIVERTED TO IND. RIGGED FLAPS IAW SAAB AMM.SDR COMA0260565Bpsu · failedFLAPS FAILED AT 30 DEGREES. REPLACED THE RIGHT BRAKE POSITION UNIT.SDR COMA0260564Bpsu · failedFLAPS FAILED AT 30 DEGREES. REPLACED THE RIGHT BRAKE AND POSITION SENSOR UNIT.SDR COMA0260561Bpsu · failedFLIGHT 5237 FLAPS FIALED AT 41 DEGREES.REPLACED THE L/H BPSU.SDR COMA0260558FlapFLIGHT 5962 - FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.SDR CA021003009B-Nut · cracked(CAN) DURING INSPECTION THE B-NUT ON THE FLAP DRIVE CABLE WAS LOOSE, AN ATTEMPT TO TIGHTEN THE CAUSED THE NUT TO BRAKE INTO TWO PIECES, THE NUT WAS CORRODED AT THE SEPARATION POINT. DO NOT KNOW IF IT WAS OVER TORQUE ON INSTALLATION OR IF THE NUT WAS DEFECTIVE.SDR KZ52002F00003Gear · strippedGEAR ON END OF ARMATURE STRIPPED CAUSING FLAPS TO BE INOPERATIVE, ALSO CAUSED CONTAMINATION TO FLAP GEARBOX.SDR COMA0260554FlapFLIGHT 5706 FLAPS FAIL CAUTION.RESET FLAP SYSTEM AND DEFERRED MAINT.PER AD 98-20-01.SDR QXEA0201588Skin · chafedPDX - RIGHT HAND TOP OUTBOARD FLAP HAS A 16 INCH LONG CHAFE THROUGH THE PAINT 67 1/2 INCHES FROM THE NACELLE AND A 2 INCH CHAFE 34 1/2 INCHES FROM NACELLE. MAINTENANCE BLENDED AND REPAIRED THE DAMAGED AREAS IAW E.A. 6-57-65 AND RD8/4-57-016.SDR QXEA0201569Flap · wornGEG - UPON PUSHBACK, THE FLAP DRIVE CAUTION LIGHT ILLUMINATED WITH THE FLAPS SET TO 5 DEGREES. MAINTENANCE RESET THE FLAP CONTROL UNIT. THE FLAPS OPERATED NORMALLY FORM 5 DEG TO 35 BUT THE FLAP DRIVE CAUTION REMAINED ILLUMINATED. MAINTENANCE INSPECTED THE AIRCSDR QTVA901UControl Cable · brokenON SHORT FINAL, HEARD A THUD IN FLOORBOARDS. JUST AFTER PUTTING GEAR DOWN. AIRCRAFT HAD A SLIGHT YAW AND ROLL AND LANDED UNEVENTFULLY. TAXIED IN, SELECTED FLAPS UP AND SHUTDOWN AIRCRAFT. DURING POSTFLIGHT NOTICED FLAPS WERE STILL FULLDOWN. MAINTENANCE INSSDR COMA0260548Bpsu · malfunctionedFLIGHT 5506 - FLAPS FAIL CAUTION MESSAGE.REPLACED THE L/H BPSU.SDR COMA0260543Bpsu · malfunctionedFLIGHT 5507 FLAPS FAILED WHEN SELECTED TO 30 DEGREES.REPLACED THE L/H BPSU.SDR CA020926003Control Cable · broken(CAN) FLAP SELECTOR CONTROL CABLE WAS FOUND BROKEN AT THE POINT WHERE THE CABLE EXITS THE FUSELAGE AND CONTINUES ON TO THE FLAP SELECTOR. A SECOND SPOT ON THE CABLE WAS ALSO ALMOST BROKEN THROUGH WHERE THE CABLE RETURNS FROM THE FLAP SELECTOR AND REENTERS THESDR SWIA200211260Bpsu · failedFLAPS FAIL MESSAGE DURING CLIMBOUT. RETURNED TO FIELD. RIGHT BPSU REMOVED DUE TO FLAPS FAIL MSG. INSTALLED A SERVICEABLE BPSU IAW CRJ MM 27-51-10.SDR C2XA02BT057Control Handle · faultyCREW REPORTED, "LANDING GEAR WARNING HORN WARNING CONSTANT WITH GEAR IN UP POSITION, SYSTEM CUTOUT INOPERATIVE." MAINTENANCE REMOVED AND REPLACED FLAP SELECTOR HANDLES IAW EMB135 AMM 27-53-03. OPS CHECKED SYSTEM GOOD. TEST FLIGHT OF AIRCRAFT SATISFACTORY. SDR DL76G021129Fseu · failedAFTER T/O LEADING EDGE SLAT ASSYM LIGHT ON. FLAP GAUGE WOULD NOT COME FULL UP. INDICATOR STUCK BETWEEN 1 AND UP. PERFORMED BITE TEST OF FLAP/SLAT ELEC UNIT. REPLACED FSEU.SDR COMA0260544FlapFLIGHT 5258 FLAPS FAILED WHEN SELECTED UP AFTER T/O.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.SDR CA020925004Relay · intermittent(CAN) AIRCRAFT DEPARTED AND FLAPS WOULD NOT RETRACT FROM TAKE OFF POSITION. CREW ELECTED TO RETURN AND AN UNEVENTFULL LANDING WAS COMPLETED. DURING TAXI FLAPS RETRACTED. FLAPS WHERE DEEMED TO BE INTERMITTENT AND WHERE DEFERRED AND CB PULLED. AT ARRIVAL TO MAISDR CA020923003Control Unit · failed(CAN) 'FLAP FAIL ' MESSAGE ON EICAS IN CRUISE FECU CHANGED AND TESTED AS PER AMMSDR 2002FA0001086Control Cable · frayedPILOT REPORTED AN 'UNUSUAL FEEL TO THE FLAP CONTROL. INVESTIGATION REVEALED THAT THE FLAP EXTENSION CABLE WAS SEVERELY FRAYED. IT WAS REPLACED..SDR 02FDEA00664Flap · looseAIRFRAME BUFFET OCCURRED DURING CLIMB OUT AT .65 MACH, SLOWING THE AIRCRAFT DECREASED THE BUFFET. NO BUFFET AT .58 MACH. INSPECTED FLAPS AND AILERONS FOR SECURITY. FOUND THE RT OUTBD AFT FLAP HAD EXCESSIVE PLAY. DROPPED FLAPS AND CHECKED THE AFT FLAP AFTSDR CA020920002Actuator · malfunctioned(CAN) WHEN FLAPS 450 SELECTED A/C ROLLS LT HALFWAY OF RT, AILERON TRIM NEEDED TO LEVEL WINGS, LT FLAPINDICATION JUMPS 400 TO 450 REPLACED RT NR 1 ACTUATOR , FLEXSHAFT ON INBD FLAP AND LT POS TRANSMITTER, PERFORMED RIGGING OF AILERON SYS AND FLAP SYSTEM, OPS NOSDR FMAA2002002Switch · inoperativeFLAP SWITCH IS HELD TO THE ARM ASSEMBLY WITH SMALL NR 40 MACHINE SCREWS. IF SCREWS ARE OVER TIGHTENED, THE PLASTIC SWITCH CRACKS, IF IT IS NOT TIGHTENED ENOUGH, IT LOOSENS WHICH CHANGES THE ADJUSTMENT OF THE FLAPS. THE SWITCH WIRES OBVIOUSLY LOOSENED ENOUGH SDR EIA2002100Relay · failedKJFK - GROUND SAFE RELAY ON LIGHT STAYED ILLUMINATED AFTER TAKEOFF, INBOARD FLAPS WOULD NOT RETRACT NORMALLY AFTER LANDING. REPLACED RELAYS, R952 AND R226 IN P14 EPR MM 32-09-02. (M)SDR COMA0260533FlapFLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.SDR COMA0260532Pcu · malfunctionedFLAPS FAIL, WOULD NOT EXTEND.REPLACED THE POWER DRIVE UNIT.SDR MALA020560Control Valve · failedDURING FLIGHT 3264, CREW REPORTED THE FLAPS WILL NOT EXTEND ON LANDING. MAINTENANCE REPLACED FLAP CONTROL VALVE IAW SAAB AMM 27-51-15-2. OPS CHECK AND LEAK CHECK GOOD.SDR C2XA02IA193Control Unit · failedIAH- DURING FLIGHT 3642, AT CRUISE ALTITUDE THE CREW NOTED A FLAP FAIL MESSAGE AND RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT, PERFORMED A OPERATIONAL CHECK OF THE FLAP SYSTEM AND NO DEFECTSSDR COMA0260522FlapFLIGHT 5922 DURING LANDING AT CVG RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREE FLAP POSITION.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3, (A,B,C AND E). FLAP SYSTEM WAS RESET WITH NO FURHTER FLAP CASDR DLM88021054Cable · brokenDURING APPROACH THE LEFT FLAP INDICATION STUCK AT 0 DEGREES DURING FLAP EXTENSION. A/C ROLLED AND AUTO PILOT DISC A/C FLAP HANDLE RECYCLED AND FLAPS CAME DOWN NORMALLY HOWEVER A/C REQUIRED 2 UNITS OF RIGHT AILERON TRIM FOR REMAINDER OF APPROACH. SDR COMA0260514FlapFLIGHT 5084 - DURING CRUISE FLIGHT TO MCO RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY, AIRCRAFT LANDED SAFELY AT MCO.COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1,2,3, (A,B,C AND E). FLAP SDR AUS20021085Solenoid Valve · failed(AUS) FLAP SOLENOID VALVE FAULTY. VALVE COIL HAD SHORT CIRCUITED. VALVE IS LOCATED IN HYDRAULIC POWER PACK.SDR C2XA02CL177Flap · malfunctionedCLT FLT 3061 CREW REPORTED THAT THE FLAPS FAILED TO EXTEND. GOT SPS ADVANCED AND FLAP FAIL ON EICAS. CREW DECLARED EMERGENCY, AND LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM, PULLED AND RESET THE FLAP CIRCUIT BREAKER. ALL OPERATIONAL CHECKSSDR COMA0260509FlapFLAPS FAIL MESSAGE DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.SDR COMA0260508FlapFLIGHT 5789 FLAPS FAIL MESSAGE WHEN SELECTED 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.SDR COMA0260504FlapFLIGHT 5789 FLAS FAIL MESSAGE WHEN SELECTED TO 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.SDR 2003F00174Connector · looseFLAP FAIL MESSAGE INBOUND. THE CREW DECLARED AN EMERGENCY. MAINTENANCE FOUND A LOOSE CONNECTOR AT THE FECU AND RESECURED. OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR CA030106017Cotter Pin · broken(CAN) DURING A SCHEDULED INSPECTION THE FLAP HANDLE RELEASE ASSEMBLY WAS NOT ENGAGING THE FLAPS IN THE CORRECT DEGREES SETTING. UPON INVESTIGATING THE FLAP HANDLE ASSEMBLY, WE FOUND A BROKEN COTTER PIN PN 38022 LOCATED IN THE RELEASE ASSEMBLY. THE FLAP HANDLESDR SWIA200211187Bpsu · failedFLAP FAIL MESSAGE DURING PREFLIGHT. REMOVED AND REPLACED LEFT BPSU IAW 27-51-10. OPS CHECK GOOD.SDR MALA020518Control Valve · failedDURING FLIGHT 3697, FLAPS WOULD NOT EXTEND. MAINTENANCE CONNECTED BREAKOUT BOX AND FOUND FLAP VALVE INOP. REPLACED VALVE IAW SAAB AMM 27-51-15-2. ALL CHECKS GOOD, OPS CHECK GOOD IAW SAAB AMM 27-51-00.SDR MALA020509Control Valve · faultyINBOUND ON FLIGHT 3089, FLAPS WOULD NOT EXTEND. OVERFLEW MCW DIVERTED TO MSP. A/C LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FLAP CONTROL VALVE, OPS CHECKS GOOD.SDR COMA0260497FlapFLIGHT 5270 FLAPS FAIL CAUTION MESSAGE.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR 02FDEA00606Flap · failedOUTBOARD FLAPS DID NOT EXTEND PAST 23 ALTERNATE FLAP MOTOR USED TO EXTEND FLAPS.
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