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 SWIA200516004Pdu · malfunctionedON APPROACH "FLAPS HALFSPEED" STATUS MESSAGE CAME ON. REPLACED FLAP PDU PER CRJ MM 27-51-00. OPERATIONAL CHECK GOOD.SDR COMA0560724Bpsu · unreliableFLIGHT 5492 - FLAPS FAIL CAUTION. REPLACED THE RT BPSU AND ALL LT FLAP ACTUATORS.SDR DJFA2005177Cable · frayedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A PHASE 16 INSPECTION, THE FLAP POSITION TRANSMITTER CONTROL CABLE WAS FOUND TO BE FRAYED APART. MAINTENANCE REPLACED THE AFT FLAP POSITION INDICATOR CONTROL CABLES AND RIGGED THE CABLES. THE AIRCRAFT WASDR COMA0560720Flex Coupling · wornFLIGHT 5354 - FLAPS FAIL CAUTION. REPLACED THE LT NR 4 FLEX SHAFT.SDR AU510002191Fseu · faultyTRAILING EDGE FLAP ASYMMETRY MESSAGE. FLAP/SLAT ELECTRONIC UNIT (FSEU) RERACKED AND MESSAGE CLEARED.SDR AU510001945Lead · broken(AUS) FLAP SELECTOR MICROSWITCH POWER WIRE OPEN CIRCUIT. (CASA NR 510001945)SDR AU510001915Control Cable · misrigged(AUS) CONTROL CABLES FOR FLAPS ( F1 AND F2) WERE FOUND TO BE 43LB LOW IN TENSION. THE LT AILERON WING CABLE WAS 30LB LOW. THE LT AND RT AILERON UPFLOAT CABLES WERE 45LB LOW. (CASA NR 510001915)SDR AU510001638Flap System · sticking(AUS) LT FLAP STOPPED. FLAP ASSYMETRY. INVESTIGATION CONTINUING. (CASA NR 510001638)SDR AU510001565Rod End · corroded(AUS) IB AFT FLAP DEFLECTION CONTROL ROD PULLED OUT OF IB RODEND. INSPECTION FOUND RODEND BADLY CORRODED AND THREAD STRIPPED.SDR COMA0560715Flap System · warning lightFLIGHT 5151 - DURING JFK APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES. 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 FURTHER FLAP CAUTION MESDR REXA200500154Flap · malfunctionedFLAPS FAIL AT 20 ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01SDR COMA0560685Flap System · malfunctionedFLIGHT 5130- DURING LANDING AT MSG RECEIVED A FLAP FAIL MESSAGE AT 45 DEGREES. 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 FURTHER FLAP CAUTION MESSAGESSDR COMA0560717Flap System · warning lightFLIGHT 5009 - FLAPS FAIL CAUTION. INSPECTED FLAP SYSTEM PER AD 98-20-01. NO DEFECTS FOUND.SDR SWIA200516001Lever · failedFLAPS WOULD NOT EXTEND TO TAKE OFF POSITION. REPLACED FLAP SELECTOR LEVER. OPERATIONAL CHECK GOOD.SDR COMA0560713Control Handle · malfunctionedFLIGHT 5076 - FLAPS FAIL CAUTION. REPLACED THE FLAP CONTROL LEVER.SDR AU510002042Control Rod · separatedRT INBOARD FLAP OUTBOARD FAIRING ATTACHMENT ROD SEPARATED. INVESTIGATION FOUND THE CONTROL ROD FROM FLAP LOWER SURFACE TO THE AFT LINKAGE OF THE FAIRING HAD BECOME DETACHED AND THE LOWER BEARING HAD PULLED OUT OF THE ROD.SDR A6WA200540352Flap System · failedFLAPS FAILED AT 20 DEGREES ON APPROACH. NO DEFECTS NOTED. (K)SDR COMA0560709Bpsu · malfunctionedFLIGHT 5557 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU.SDR REXA200500153Pdu · inoperativeFLAPS FAILED AT 20 ON APPROACH, QRH FOLLOWED WITH UNEVENTFUL LANDING. REMOVED AND REPLACED POWER DRIVE UNIT IAW AMM SYSTEM OPERATIONALLY CHECKED GOOD.SDR COMA0560683Flap System · malfunctionedFLIGHT 5392- INBOUND CVG RECEIVED A FLAP FAIL MESSAGE AT 30 DEGREES. 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 FURTHER FLAP CAUTION MESSAGES.SDR COMA0560681Flap System · warning lightFLIGHT 5854 - INBOUND CVG RECEIVED A FLAP FAIL MESSAGE WHEN HANDLE WAS MOVED FROM 30 TO 45 DEGREES. 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 FURTHER FLSDR MASA200501016Sensor · malfunctionedASH 6152 DSM - FLAPS FAIL CAUTION MESSAGE. THE AIRCRAFT WAS FERRIED TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED LT AND RT BPSU'S OPS CK GOOD.SDR SWIA200516023Control Unit · malfunctioned"FLAPS HALFSPEED" STATUS MSG. REPLACED NR 1 SFECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD.SDR COMA0560702Coupling · unreliableFLIGHT 5106 - FLAPS FAIL CAUTION. REPLACED FLAP FLEX DRIVE SHAFTS.SDR MASA200501008Flap System · malfunctionedASH 2639 CHS - FLAP CONFIG WARNING. CONTRACT MAINTENANCE RESET THE SYSTEM. NO FURTHER DEFECTS NOTED.SDR SWIA200515983Control Unit · malfunctionedON SETTING FLAPS TO 8 DEG, FLAPS HALFSPEED STATUS MSG. INSTALLED A SERVICEABLE FECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD. PN ON 860D100-18ABCD OFF 725SDR COMA0560698Coupling · damagedFLIGHT 4989 - FLAPS FAIL CAUTION. REPLACED THE NR 5 FLEX SHAFT.SDR VNAA0512008Warning Light · illuminatedDURING APPROACH WHEN FLAPS WERE SELECTED FROM 20 TO 30 DEGREES THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM. ALL CHECKS WERE GOOD. THE AIRCRAFSDR COMA0560695Control Switch · malfunctionedFLIGHT 5910 - FLAPS FAIL CAUTION. REPLACED THE FLAP CONTROL LEVER.SDR COMA0560694Coupling · unreliableFLIGHT 5461 - FLAPS FAIL CAUTION. REPLACED FLAP FLEX DRIVE SHAFT.SDR COMA0560693Pdu · malfunctionedFLIGHT 5541 - FLAPS FAIL CAUTION. REPLACED THE PDU.SDR COMA0560679Flap System · warning lightFLIGHT 5006 - RECEIVED A FLAP FAIL CAUTION MESSAGE INBOUND TO YUL, FLIGHT LANDED WITHOUT INCIDENT. 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 FURTHER FLASDR COMA0560677Flap System · warning lightFLIGHT 5616 - RECEIVED A FLAP FAIL CAUTION MESSAGE INBOUND TO YYZ, FLIGHT LANDED WITHOUT INCIDENT. 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 FURTHER FLASDR COMA0560676Flap System · warning lightFLIGHT 5456 - RECEIVED A FLAP FAIL CAUTION MESSAGE INBOUND TO LGA, FLIGHT LANDED WITHOUT INCIDENT. 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 FURTHER FSDR COMA0560674Flap System · warning lightFLIGHT 5667 - EN ROUTE CVG-FSD RECEIVED A FLAP FAIL CAUTION MESSAGE, FLIGHT LANDED AT FSD WITHOUT INCIDENT. 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 FUSDR COMA0560673Flap System · malfunctionedFLIGHT 5305 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING CVG APPROACH. CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A,B,C AND E). FLAPSDR REXA200500152Flap System · malfunctionedFLAPS FAIL AT 20 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01SDR REXA200500151Flap System · malfunctionedFLAP FAIL MESSAGE DURING DEICING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.SDR ASOA051068Bpsu · inoperativeDURING CLIMB-OUT FROM ATL-ALB, THE CREW ATTEMPTED TO RETURN FLAPS FROM EIGHT DEGREES TO ZERO DEGREES, WHEN AN AMBER FLAPS FAIL CAUTION MESSAGE, WITH THE FLAPS REMAINING AT 8 DEGREES WAS RECEIVED. THE CREW COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY. THE SDR COMA0560704Pdu · faultyFLIGHT 5675 - DURING CLIMB-OUT OF CVG RECEIVED A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE POWER DRIVE UNIT.SDR COMA0560690Flap System · warning lightFLIGHT 5253 - FLAPS FAIL CAUTION. INSPECTED FLAPS PER AD 98-20-01 AND DEFERRED MAINTENANCE.SDR COMA0560689Flap System · warning lightFLIGHT 5130 - FLAPS FAIL CAUTION. INSPECTED FLAP SYSTEM PER AD 98-20-01, NO DEFECTS FOUND.SDR COMA0560687Bpsu · unreliableFLIGHT 5399 - FLAPS FAIL CAUTION. REPLACED THE LT BPSU.SDR COMA0560686Pdu · malfunctionedFLIGHT 2750 - FLAPS FAIL CAUTION. REPLACED THE FLAP PDU.SDR REXA200500149Flap System · malfunctionedFLAPS FAIL CAUTION AT FLAPS 2 DEGREES. LANDING UNEVENTFUL. SYSTEM REST AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.SDR REXA200500148Flap System · malfunctionedFLAPS FAILED AT 0 DEGREES ON APPROACH. LANDING UNEVENTFUL. INSPECTED, RESET AND PERFORMED OPERATIONAL CHECK. PLACED ON 72 HOUR WATCH PER AD 98-20-01.SDR REXA200500147Bpsu · out of rigFLAPS FAILED AT 0 DEGREES WHILE ON APPROACH. PERFORMED QUICK REFERENCE HANDBOOK(QRH). LANDING UNEVENTFUL. FOUND LEFT AND RIGHT BRAKE AND POSITION SENSOR UNIT (BPSU) OUT OF RIG. RIGGED BOTH BPSU IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL. OPERATIONALLYSDR REXA200500150Flap System · malfunctionedFLAPS FAILED AT 8 DEGREES WHEN SELECTED TO 20 DEGREES. LANDING UNEVENTFUL. REMOVED AND REPLACED FLAP ELECTRICAL CONTROL UNIT (FECU) IN ACCORDANCE WITH AIRCRAFT MAINTENANCE MANUAL(AMM). OPERATIONALLY TEST AND CHECK RIGGING OF BRAKE POSITON SENSOR UNIT (BPSU)SDR MASA200500997Flap System · malfunctionedASH 7268 ORD - FLAPS FAILED AT 0 DEGREES. MAINTENANCE C/W PART A AND COULD NOT DUPLICATE THE DISCREPANCYSDR DXTA200501132Resolver · malfunctionedFLAPS FAIL CAS MESSAGE / SLATS DEPLOYED. FLAPS FAILED APPROX 1 DEGRESS 14,000 FT MSL 230 KIAS. SLOWED TO 180 KIAS STILL FAIL. PERFORMED FLAP SYSTEM OPS CHECK & COULD NOT FIND ANY FAULTS. REMOVED & REPLACED LT & RT FLAP RESOLVERS IAW CE-750 MM CH 27-52-00.
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