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 QXEA200500970Warning Light · illuminatedFLAP POWER CAUTION LIGHT ILLUMINATED SELECTING FLAPS FROM ZERO TO 5 DEGREES. COMPLIED WITH CHECKLIST AND RESET FLAP CONTROL CIRCUIT BREAKER AND FLAP POWER CAUTION LIGHT EXTINGUISHED. FLAPS OPERATED NORMALLY. NO PARTS REPLACED. ACFT RETURNED TO SERVICE.SDR DHL2005807537Fitting · crackedRT WING T/E RT INBD FLAP WELL FITTING HAS TWO 2.000 CRACKS, STA XRS 59.000 RT WING. REMOVED CRACKED FITTING IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-3-0 PG.1, SRM 51-1-21 PG 1.SDR SWIA200515045Control Unit · malfunctionedRECEIVED FLAPS HALF SPEED. REPLACED FECU IAW 27-57-05. OPERATIONAL CHECK GOOD. P/N 860D100-18ABCD, S/N OFF 741.SDR COMA0560308Bpsu · unreliableFLIGHT 5851 - FLAPS FAIL CAUTION. COULD NOT DUPLICATE, REPLACED THE LT BPSU AND WIRING HARNESS.SDR COMA0560307Bpsu · unreliableFLIGHT 5076 - FLAPS FAIL CAUTION. COULD NOT DUPLICATE. REPLACED THE LT BPSU.SDR 05FDEA01272Power Unit · leakingDURING FLAP RETRACTION INDICATORS SHOWED SPLIT FLAP W/INBOARDS REMAINING AT 2 DEG W/FLAP UP. AFTER RUNNING QRH AND INBOARDS GOING TO FULL UP, HYD A SYSTEM INDICATED 0 QTY. RAN QRH AGAIN W/ALTERNATE FLAPS SYSTEM AND MANUAL GEAR EXTENSION PROCEDURES. WHEN ASDR DXTA200500716Pdu · inoperativeFLAPS FAIL CAS ILLUMINATED ON APPROACH. SLATS EXTENDED AND FLAPS FAILED AT 5 DEGREES. REMOVED AND REPLACED FLAP PDU IAW 750 MM CHAPTER 27-52-00. OPS CHECK GOOD.SDR COMA0560306Control Unit · malfunctionedFLIGHT 5146 - FLAPS FAIL CAUTION. COULD NOT DUPLICATE REPLACED THE FECU.SDR COMA0560305Bpsu · unreliableFLIGHT 5537 - FLAPS FAIL CAUTION. COULD NOT DUPLICATE REPLACED THE LT BPSU.SDR REX2005F00040Control System · failed(REF NR: 05-063) FLAP FAILED AT 20 ON APPROACH. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)SDR COMA0560302Control System · malfunctionedFLIGHT 5144 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.SDR COMA0560297Control Unit · activeFLIGHT 5366 FLAPS FAIL CAUTION. REPLACED THE FECU.SDR COMA0560301Bpsu · out of rigFLIGHT 5349 FLAPS FAIL CAUTION. RERIGGED THE LT AND RT BPSU.SDR COMA0560298Control Unit · activeFLIGHT 5142 FLAPS FAIL CAUTION. REPLACED THE FECU.SDR REX2005F00042Fcu · failed(REF NR: 05-061) FLAPS FAIL AT ZERO ON CLIMB-OUT. QRH FOLLOWED, EMERGENCY DECLARED RETURNED TO DEPARTURE WITH UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT. (FECU) (K)SDR REX2005F00043Bpsu · failed(REF NR: 05-060) FLAP FAIL MESSAGE UPON POWER UP. REMOVED AND REPLACED RT BRAKE POSITION SENSING UNIT (BPSU). (K)SDR SDR2005030Valve · leakingDURING APPROACH TO TORTOLA ISLAND (EIS), THE FLAPS UNLOCK WARNING CAME ON. UNABLE TO LAND. AIRCRAFT RETURNED TO SAN JAUN. REPLACED FLAP BLOCK VALVE. (K)SDR CA050510003Motor · overheated(CAN) FLAP MOTOR OVERHEATNG, BURNING ODOR IN CABIN. FLAP MOTOR/GEARBOX ASSY REPLACED WITH OVERHAULED UNIT. VOLTAGE TO MOTOR CHKD & GROUND WIRE CHKD OKAY. CHKD FLAP SYS FOR BINDING, ACTUATORS, CABLES & FLAPS OPERATED WITHOUT BINDING. SYS CHKD FLAP MOTOR/GEARBOXSDR COMA0560296Control System · malfunctionedFLIGHT 5727 FLAPS FAIL CAUTION. RESET FLAP SYSTEM, FOUND NO DEFECTS, DEFERRED MAINT PER AD 98-20-01.SDR QXEA200500969Control System · malfunctionedWHEN SELECTING FLAPS, FLAP POWER CAUTION LIGHT ILLUMINATED, FOLLOWING EMERGENCY CHECKLIST, UNABLE TO RESTORE POWER TO FLAP SYSTEM. CONDUCTED ZERO FLAP LANDING WITHOUT FURTHER INCIDENT. MX COMPLIED WITH SL DH8-400-SL-27-002A, CAUTION LIGHT EXTINGUISHED. COMPSDR QXEA200500834Control System · malfunctionedGEG - FLIGHT NR 2300 ON APPROACH, WHEN SELECTING FLAPS, THE FLAP POWER CAUTION LIGHT ILLUMINATED. FOLLOWING THE EMERGENCY CHECKLIST, UNABLE TO RESTORE POWER TO THE FLAP SYSTEM. CONDUCTED ZERO FLAP LANDING WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH S/L DH8-SDR 2005FA0000937Bracket · brokenPILOT REPORTED THAT THE FLAPS FELT FUNNY AND THAT THEY MADE A GRINDING NOISE. INSPECTION OF FLAP SYSTEM FOUND PULLEY BRACKET FOR LT FLAP EXTEND CABLE HAD BROKEN AT 2 OF THE 4 MOUNTING SCREW TABS.SDR SWIA200514985Control Unit · malfunctionedFLAP CONTROL FAULT ON OUTBOARD FLAPS. REPLACED FLAP CONTROL LEVER & FCU IAW MM 27-50-06 & 27-50-01. OPERATIONAL CHECKS GOOD. P/N 120-64207-615; S/N OFF 120278.SDR LAT2005F00000Switch · frozen(4-30-05-1) UPON DEPARTURE, THE WING FLAPS WOULD NOT RETRACT. AC RETURNED TO BASE. INSPECTION REVEALED A FROZEN UPLOCK LIMIT SWITCH, FLAP OPERTION NORMAL. (AL03200512861) (K)SDR CA050427013Switch · failedSWITCH CONTROLLING FLAP RETRACTION FAILED DURING FLAP RETRACTION AFTER LANDING. FLAPS WERE STUCK AT APPROX 10 DEGREES. FAILURE INSIDE SWITCH AND APPEARS TO INVOLVE BROKEN INTERNAL MECHANISM.SDR RAIA00504027Control Unit · failedSTL - FLAP FAIL INDICATION. MAINTENANCE REMOVED AND REPLACED FLAP CONTROL UNIT.SDR SWIA200514923Selector · malfunctionedWHILE ENROUTE AT FL240, RECEIVED SEVERAL CONTROL FAULT WARNINGS ACCOMPANIED BY "AWS" AND FLAP WARNINGS ON MAP. REPLACED FLAP SELECTOR LEVER. CLEARED ALL FAULTS FROM FCU. OPERATIONAL CHECK GOOD.SDR MASA200500309Sensor · malfunctionedASH 6588 SAN TO PVR. THE CREW REPORTED FLAPS FAIL IN FLIGHT. MX R2 RIGHT OUTBOARD FLAP OUTBOARD SKEW SENSOR.SDR QXEA200500712Power Unit · failedPDX - FLIGHT 2310 - FLAP POWER CAUTION. CREW ABORTED LANDING DUE TO THE FLAPS REMAINING UP WHEN SELECTED TO 5 DEGREES. THE FLAP CONTROL CIRCUIT BREAKER WAS RESET IAW THE EMERGENCY CHECKLIST. THE FLAP POWER CAUTION CAME BACK AND THE FLIGHT MADE A ZERO FLAP LSDR 05FDEA01118Control Valve · malfunctionedAFTER TAKEOFF, DURING FLAP RETRACTION LEVEL 2 FLAP DISAGREE ALERT. O/B FLAPS SHOWED 5 AND 6 INBOARD FLAPS WERE AT 0. PER QRH ATTEMPTED TO RETURN FLAPS TO LAST POS THAT ALERT WAS NOT DISPLAYED. AT 12 O/B FLAPS STAYED AT 5 AND 6. DURING RETURN TO KMEM O/B FLSDR SWIA200514900Control Unit · malfunctionedRIGHT ELEVATOR DOES NOT PASS FFOD CHECK WITH 3A OR 3B SYSTEMS. REPLACED RIGHT INBOARD ELEVATOR PCU IAW CRJ MM 27-33-0. OPERATIONAL CHECK GOOD.SDR SWIA200514911Control Unit · malfunctionedFLAP CONTROL FAULT WHILE DROPPING THE FLAPS. REPLACED FCU AND RIGHT OUTBOARD FLAP ACTUATOR PER MM 27-50-00. OPERATIONAL CHECK GOOD.SDR O2G2005F00006Shaft · failedFLAPS STUCK AT 8 DEGREES. REPLACED BROKEN FLAP DRIVE SHAFT. (K)SDR SWIA200514909Selector · malfunctionedCREW REPORTED FLAP CONTROL FAULT AND ADVANCED SWS WHEN FLAPS SELECTED. REMOVED AND REPLACED FLAP LEVER IAW MM 27-50-01, OPERATIONAL CHECK GOOD.SDR SWIA200514881Control Unit · malfunctionedFLAPS DEGRADED MSG ON EICAS. REPLACED FLAP ELECTRONIC CONTROL UNIT IAW CRJ 200 MM 27-51-05. OPERATIONAL CHECK GOOD.SDR MALA050325Unknown · oscillatesPITCH OSCILLATIONS, REPO FLIGHT FROM GLH TO MSP CREW ENCOUNTERED LIGHT TO MODERATE TURBULENCE ON CLIMBOUT. THE AIRCRAFT HAD 2 EVENTS OF SEVERE PITCH OSCILLATIONS ABOUT 15 MINUTES INTO THE FLIGHT BETWEEN 24,000 TO 31,000, LIGHT RIME ICE PROTECTION ON. CREW PESDR COMA0560252Warning Light · illuminatedFLIGHT 5811 FLAPS FAIL CAUTION. INSPECTED FLAP SYSTEM IAW AD 98-20-01. NO DEFECTS FOUND. COULD NOT DUPLICATE.SDR CA050411002Flex Drive · failed(CAN) ON APPROACH FLAPS WERE SELECTED TO 17 DEG, FLAPS STARTED TO MOVE THEN STOPPED, AIRCRAFT LANDED SAFELY. INSPECTION OF THE FLAP SYSTEM SHOWED THAT THE RT FLAPS WERE IN A SPLIT FLAP CONDITION BETWEEN 0 DEG AND 17 DEG. FURTHER INVESTIGATION REVEALED THE RTSDR QXEA200500985Power Unit · malfunctionedAFTER PUSHBACK FROM GATE AND SELECTED FLAPS -15 DEGREES, FLAP POWER CAUTION ILLUMINATED. PERFORMED ABNORMAL FLAP POWER CAUTION CHECK LIST. RESET FLAP CONTROL CIRCUIT BREAKER. SET FLAPS TO 15 DEGREES AND FLAP POWER CAUTION CAME ON AGAIN. MX REPLACED FLAP POWSDR SWIA200514858Selector · bindingFLAP SELECTOR BINDS IN 45 DEG NOTCH. REPLACED FLAP SELECTOR LEVER ASSY IAW EMB MM 27-50-01, OPERATIONAL CHECK GOOD.SDR COMA0560254Bpsu · failedFLIGHT 5854 FLAPS FAIL CAUTION MESSAGE AFTER LANDING. C/W RIGGING MAINT OF THE FLAP SYSTEM BPSU'S.SDR QXEA200500984Control Unit · malfunctionedUPON SELECTION OF FLAPS FROM 0 TO 5 DEGREES, FLAP POWER CAUTION LIGHT ILLUMINATED. FLAP CONTROL CIRCUIT BREAKER RESET VIA EMERGENCY PROCEDURE. FLAPS OPERATED NORMALLY FOR LANDING. MX REPLACED FLAP CONTROL UNIT AS A PRECAUTIONARY MEASURE IAW AMM 27-51-01, PASDR SWIA200514851Control Unit · malfunctionedFLAPS HALF SPEED STATUS DURING PREFLIGHT. REPLACED FECU IAW 27-50-00, OPERATIONAL CHECK GOOD.SDR COMA0560246Fcu · faultyFLIGHT 5142 RECEIVED A FLAP FAIL CAUTION WHILE PARKED AT THE GATE. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.SDR COMA0560245Control Panel · failedFLIGHT 5315 DURING CLIMBOUT OF CVG WITH FLAPS RETRACTED THE STAB AND MACH TRIM MASTER CAUTION MESSAGES ACTIVATED, CREW FOLLOWED QRH PROCEDURES, RE-ENGAGED STAB/MACH TRIM AND LANDED AT SAV WITHOUT INCIDENT. CLEANED STAB/MACH TRIM ENGAGE PANEL SWITCHES AND RE-RSDR SWIA200514850Selector · malfunctionedEXTENDING FLAPS FROM 15 DEGREES TO 25 DEGREES GOT A CONTROL FAULT LIGHT. REPLACED FLAP CONTROL HANDLE. OPERATIONAL CHECK GOOD.SDR QXEA200500983Light · false indicationFLAP POWER CAUTION LIGHT IN FLIGHT AFTER SELECTING FLAPS 5 DEGREES. ACCOMPLISHED CHECKLIST, FLAPS RESET. NO CAUTION LIGHT UPON MX ARRIVAL. NO FAULTS IN CDS. FLIGHT CREW INDICATED NO FURTHER FAULTS AFTER RESET. NO PARTS REPLACED. ACFT RETURNED TO SERVICE.SDR QXEA200500982Warning Light · false indicationFLAP POWER CAUTION LIGHT ON APPROACH WHEN FLAPS WERE SELECTED TO 5 DEGREES. FOLLOWED EMERGENCY CHECKLIST. CIRCUIT BREAKER L7-L ESSENTIAL PULLED AND FLAPS OPERATED NORMALLY. MX CONTACTED VIA SELCAL. NO FURTHER MX ACTION REQUIRED. NO PARTS REPLACED. ACFT RESDR COMA0560223Bpsu · faultyFLIGHT 5446 RECEIVED A FLAP FAIL CAUTION AFTER LANDING WHEN FLAPS WERE RETRACTED. REPLACED THE LEFT BPSU.SDR SWIA200514848Detector · malfunctionedAFTER SELECTING FLAPS AT 20 DEGREES, RECEIVED FLAPS DEGRADED STATUS MESSAGE. INSTALLED FLAP SKEW DETECTION UNIT, OPERATIONAL CHECK GOOD IAW CRJ MM 27-51-15. P/N 601R59014-1, S/N ON A734.
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