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 REX2005F00021Warning Light · illuminated(REF NR: 05-082) FLAP FAIL CAUTION MESSAGE. QRH FOLLOWED. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)SDR SWIA200515202Bpsu · out of rigAFTER DEPARTURE FLAPS WOULD NOT RETRACT PAST FLAPS 8. RIGGED BPSU'S IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD.SDR REX2005F00022Fcu · failed(REF NR: 05-081) FLAPS FAIL ON CLIMB-OUT. QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU). (K)SDR 05FDEA01687Warning Light · false indicationON APPROACH, GOING FROM FLAPS 22 TO FLAPS 35, GOT LEVEL 2 ALERT SLATS DISAGREE. AFTER GO AROUND, FOUND SLAT HANDLE SCREW LOOSE. EXTENDED FLAPS AND SLATS. VISUAL INSPECTION OF FLAPS AND SLATS BOTH SIDES. NO DEFECTS FOUND. RAN FLAPS AND SLATS SEVERAL TIMES SDR REX2005F00024Control System · failed(REF NR: 05-079) FLAPS FAIL ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAP SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)SDR REX2005F00023Fcu · failed(REF NR: 05-080) FLAP FAIL ON TAXI, RETURNED TO GATE. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU) IAW AMM, SYSTEM TESTS GOOD. (K)SDR CA050627002Drive Assy · broken(CAN) ON ROUTINE INSPECTION FOUND THAT SECONDARY FLAP DRIVE CORE HAD BROKEN STRANDS AND BLISTERING, CORE REPLACED WITH SERVICEABLE. FUNCTION CARRIED OUT IAW MAINTENANCE MANUAL, AIRCRAFT RETURNED TO SERVICESDR CA050804006Control Cable · frayed(CAN) DURING A 100 HR INSPECTION THE FLAP CONTROL SYSTEM CENTER CABLE WAS DISCOVERED TO BE FRAYED AT THE AREA OF THE PULLEY. THE CABLE WAS REPLACED NEW.SDR CA050804005Control Cable · frayed(CAN) DURING A 100 HR INSPECTION THE FLAP CONTROL SYSTEM CENTER CABLE WAS DISCOVERED TO BE FRAYED AT THE AREA OF THE PULLEY. THE CABLE WAS REPLACED NEW.SDR DJFA2005115Spring · contaminatedON APPROACH, FLAPS WERE SELECTED TO 15 DEGREES WHILE AC WAS SLOWED. NO FLAP EXTENSION WAS INDICATED. CREW DECLARED EMERGENCY DUE TO FAILURE OF FLAPS. AC WAS DIVERTED, WHILE ON APPROACH, FLAPS WERE SUCESSFULLY EXTENDED. AC, MADE AN UNEVENTFUL LANDING. MAINT SDR VTZA200500127Fcu · failedFLAP FAIL AT "0" ON CLIMB-OUT. PERFORMED BITE AND SYSTEM TEST ON FECU. TEST GOOD.SDR REX2005F00026Control System · malfunctioned(REF NR 05-077) FLAPS FAIL ON APPROACH AT 30, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD-98-20-01. (K)SDR REX2005F00025Control System · malfunctioned(REF NR: 05-078) FLAPS FAIL ON APPROACH AT 20 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)SDR 05FDEA01645Control Valve · lack of lubeL/E DEVICES WOULD NOT RETRACT AT FLAPS 2 DEGREES. PERFORMED ADJUSTMENT AND TEST OF FLAP 2 DEG SWITCH AS PER M/M 27-82-021-2, OPS CK GOOD. INSPECTED PULLEYS ROD END GOING TO FLAP CONTROL VALVE AND LUBED AS NEEDED. FLAPS AND LEADING EDGE DEVICES GROUND CKS NOSDR 71405Control System · malfunctionedAFTER TAKEOFF, CREW OBSERVED FLAPS WILL NOT RETRACT TO ZERO. AIRCRAFT RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE CHECKED RIGGING AND CLEAND FLAP SPLIT FLAP SAFETY SWITCHES. THEREFORE NO PARTS WERE USED.SDR REX2005F00027Control System · failed(REF NR: 05-076) FLAP FAIL ON APPROACH WHEN GOING FROM 20 TO 30, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAP SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD-98-20-01. (K)SDR REX2005F00020Control System · failed(REF NR: 05-083) FLAPS FAILED AT 8 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)SDR SWIA200515181Bpsu · malfunctionedON FLAP RETRACTION, FLAPS FAILED AT 8 DEGREES. RIGGED RT BPSU IAW CRJ MM 27-51-10. OPERATIONAL CHECK GOOD.SDR DXTA200500785Converter · malfunctioned"FLAPS FAIL" CAS MESSAGE DISPLAYED IN CRUISE AND RESET PER CHECKLIST WHEN FLAPS WERE DEPLOYED FROM 5-15 DEGREES, A MOMENTARY ROLL OCCURRED. FLAPS EXTENDED NORMALLY BEYOND 15 DEGREES. OPS CHECKED FLAPS WITH FLAP BREAKOUT BOX. TESTED AT DIFFERENT FLAP ANGLES WISDR SWIA200515174Control Handle · malfunctionedON APPROACH, FLAPS FAILED AT 20 DEGREES. REPLACED FLAP CONTROL HANDLE IAW CL 600 MM 27-51-01. OPERATIONAL CHECK GOOD.SDR SWIA200515148Bpsu · malfunctionedCLIMBING THRU FLT LEVEL 280, RECEIVED AMBER FLAPS FAIL CAUTION MSG. REPLACED RT BPSU IAW MM 27-51-10 AND FECU IAW MM 27-51-05. OPS CHECK GOOD, PN: 860D100-18 SN OFF: 1104.SDR COMA0560354Warning Light · illuminatedFLIGHT 5611- EN ROUTE LAN - CVG RECEIVED A FLAP FAIL CAUTION AT ZERO DEGREE FLAP POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. FLAP SYSTEM WAS RESET.SDR DXTA200500779Resolver · faultyFLAP FAIL AMBER CAS MSG CAME ON DURING CRUISE ATTEMPTED ONE RESET PER CHECKLIST LIGHT DID NOT GO OUT PERFORMED NO FLAP LDG PER CHECKLIST SLATS DID EXTEND NORMALLY. PLACED FLAP BREAK OUT BOX ON FLAP SYSTEM & RAN FLAPS FOUND FAULT CODES 1, 6 & 8 POINTING TO FLASDR REX2005F00028Control System · malfunctionedFLAPS FAILED AFTER LANDING WHEN SELECTED UP DURING TAXI. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)SDR VNAA0506008Fcu · failedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH BOTH FLAPS AT 45 DEGRESS ON FINAL APPROACH. MAINTENANCE CYCLED THE CIRCUIT BREAKERS AND OPERATIONALLY TESTED THE FLAP SYSTEM IAW CRJ 200 AMM 27-54-00-710-801. ALL OPS CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RESDR DXTA200500773Controller · malfunctionedFLAPS FAIL CAS ILLUMINATED AT ALTITUDE TRIED ONE RESET PER CHECK LIST BUT FAILED AGAIN CONDUCTED NO FLAP LANDING AND MESSAGE STILL ILLUMINATED ON GROUND. TROUBLESHOT DISCREPANCY TO FLAP CONTROLLER DUE TO MULTIPLE BIT FAULTS 1, 2, 7 & 8 TRIPPED. REMOVED AND RSDR REX2005F00030Control System · failed(REF NR 05-073) FLAPS FAIL MESSAGE WHEN GOING FROM 20 TO 30 DEGREES. EMERGENCY DECLARED QRH FOLLOWED UNEVENTFUL LANDING WITH FLAPS 20. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)SDR REX2005F00029Control System · failed(REF NR: 05-074) FLAPS FAIL MESSAGE AT ZERO WHEN RETRACTED. EMERGENCY DECLARED QRH FOLLOWED UNEVENTFUL LANDING WITH FLAPS 0. RESET FLAPS AND PLAED ON 72 HOUR WATCH IAW AD 98-20-01. (K)SDR VNAA0506005Control Unit · malfunctionedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED AFTER FLAPS REACHED 45 DEGREES ON APPROACH. MAINTENANCE RESET THE FLAP ELECTRONIC CONTROL UNIT IAW RJ-SL-00-001. OPERATIONAL CHECKS WERE NORMAL. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.SDR VNAA0506004Control Unit · malfunctionedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON SHORT FINAL WITH FLAPS AT 45 DEGREES. MAINTENANCE CHECKED THE FLAP ELECTRONIC CONTROL UNIT AND SKEW DETECTION SYSTEM FOR CODES IAW RJ-SL-27-84. SYSTEM FAULTS CLEARED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT SDR MASA200500457Control Unit · malfunctionedASH FLT 2787 CLT RETURNED TO FIELD DUE TO THE FLAPS FAILED AT 8 DEGREES. MAINTENANCE REMOVED AND REPLACED THE RT BPSU AND FECU.SDR SWIA200515137Control Unit · malfunctionedFLAP DISAGREEMENT FROM FLAP 25 DEGREES TO 45 DEGREES. REPLACED FLAP CONTROL UNIT IAW MM 27-50-06. OPERATIONAL CHECK GOOD.SDR COMA056343Warning Light · illuminatedFLIGHT 5217- FLAPS FAIL CAUTION. INSPECTED FLAP SYSTEM PER AS 98-20-01, NO DEFECTS FOUND. RESET SYSTEM, CND.SDR 0500869952Flap System · out of rigACFT BEING CONFIGURED FOR LANDING AND ONCE FLAPS EXTENDED PAST 25 DEGREES ACFT ROLLED TO RIGHT. CREW DID NOT NOTICE ANY UNCOMMANDED AIRCRAFT MOVEMENTS WHEN FLAPS WERE INITIALLY LOWERED, ONLY AFTER THE 25 DEGREE DOWN SETTING. FLIGHT CREW STABILIZED ACFT FOR RESDR DL738050308Bellcrank · brokenCREW VERBAL A/C TOOK 2 DEGREES TRIM WITH FLAPS DOWN ON LANDING. FOUND WITH FLAPS DOWN RIGHT O/B FLAP I/B ATTACH POINT BELLCRANK BROKEN. REPLACED SAME.SDR SWIA200515107Handle · malfunctionedON TAXI OUT, WHEN FLAP SELECTOR PUT AT 15 DEGREE POSITION, GOT FLAP AND ADV SWS ON MAP, CONTROL FAULT AND ALL FLAP BARS FLASHING. REPLACED FLAP SELECTOR HANDLE ASSY. OPERATIONAL CHECK GOOD.SDR SWAA051660Drive Assy · brokenDIVERSION/DECLARED EMERGENCY, FLIGHT ATTENDANT NOTIFIED COCKPIT THAT PIECE OF LT WING WAS FALLING OFF. VISUAL INSPECTION CONFIRMED THAT NR 2 OUTBOARD T/E FLAP TRACK FAIRING CANOE EXTENDED BELOW WING. REMOVED AND REPLACED NR 2 OUTBOARD T/E FLAP TRACK FAIRING SDR 632005N217CARheostat · burnedENROUTE, THE CREW OBSERVED SMOKE FROM CENTER CONSOLE, THE CREW REQUESTED AN EMERGENCY DESCENT AND LANDED. MAINTENANCE FOUND THE RHEOSTAT HAD BURNED INSIDE THE FLAP CONTROL BOX. (K)SDR ASMF200506001Switch · out of adjustAIRCRAFT RETURNED TO PLATFORM, DEPLOYED SPOILER LIGHT DID NOT COME ON DURING FLIGHT CONTROLS TESTS. AIRCRAFT WAS DISPATCHED AND RETURNED TO PLATFORM, TAKE OFF FAILED. AIRCRAFT SENT TO THE HANGAR AND THE SWITCH S1-492 CAM IN FLAPS ADJUSTED IAW MM 27-53-01, TESTSDR RAIA00505025Control Unit · bypassingFLAPS WOULD NOT RETRACT TO 0 DEGREES ON DEPARTURE. MX INSP AND FOUND FLAP CONTROL UNIT BYPASS PIN POPPED. RESET AND OPS CHECKED GOOD.SDR 05FDEA01490Controller · malfunctionedON TAKEOFF FROM FRA, GOT FLAP SYSTEM 2 FAULT. RESELECTED FLAPS TO SLATS/FLAPS 20/20, WHICH DID NOT FIX THE PROBLEM. WENT TO HOLDING AND WORKED THE PROBLEM. RETURNED TO FRA AND LANDED. REMOVED AND REPLACED NR 2 SFCC PER MM 27-51-18-4. SYS OPS CHECK OK. PRSDR REX2005F00034Control System · failed(REF NR: 05-069) FLAPS FAILED AT 20 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED SYSTEM ON 72 HOUR WATCH IAW AD 98-20-01. (K)SDR REX2005F00032Control System · failed(REF NR: 05071) FLAPS FAIL AT 11 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)SDR REX2005F00035Control System · failed(REF NR: 05-068) FLAP FAIL. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD98-20-01. (K)SDR CA050608004Rod End · bent(CAN) ROD END ON FLAP SYNCHRONIZING ROD FOUND BENT FROM CONTACT WITH FLAP BELLCRANK DUE TO RIGGING OF FLAP SYSTEM FROM MANUFACTURE. NEW ROD INSTALLED AND SYSTEM RIGGED SO IT WOULD NOT CONTACT THE BELLCRANK.SDR SWIA200515080Bpsu · malfunctionedFLAPS FAIL IN 20 DEGREE POSITION UPON TAKEOFF. RIGGED LEFT BPSU IAW MM 27-51-10. OPERATIONAL CHECK GOOD.SDR VNAA0505007Flap System · unknownINBOUND TO DCA THE FLAPS FAILED AT 20 DEGREES. THE CREW ELECTED TO DIVERT TO IAD. MAINTENANCE TROUBLESHOT THE SYSTEM IAW CRJ 200 FIM 27-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.SDR SWIA200515030Control Unit · malfunctionedLEFT OUTBOARD FLAP SHOWED DISAGREEMENT AFTER TAKEOFF AFTER SELECTING FLAPS UP. REPLACED FCU IAW MM 27-50-06. OPERATIONAL CHECK GOOD.SDR REX2005F00037Control System · out of rig(REF NR: 05-066) FLAPS FIAL ON TAXI. QRH FOLLOWED, RETURNED TO BLOCKS. FLAP SYSTEM RIGGED IAW AMM. OPS CHECKED GOOD. (K)SDR REX2005F00038Control System · failed(REF NR: 05-065) FLAPS FAILED AT 30 ON APPROACH. RESET SYSTEM, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. (K)
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