JASC 2780
Service difficulty reports · 2,160
Reports filed under 2780 · Leading Edge Slat 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 = '2780' 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 = '2780' 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 ABXA010914Slat · malfunctionedFLT 407- THE CREW DECLARED AN EMERGENCY AND PERFORMED A GO-AROUND INBOUND TO ILN. EICAS MSG LE SLAT ASYM DISPLAYED. LEADING EDGE LIGHT ILLUMINATED WITH FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. COMPLETED FIM PROCEDURES IAW B767 FIM 27A-81-00. LIGHTSDR AALA20020900Slat · malfunctionedMIA - FLT 2127 - MIA-CUN - EN ROUTE CUN, AFTER TAKEOFF AND FLAP RETRACTION, LE FLAPS TRANSIT LIGHT REMAINED ON. ACCOMPLISHED LE FLAPS TRANSIT ABNORMAL PROCEDURE. LIGHT WOULD NOTE EXTINGUISH ACCOMPLISHED (ASYMMETRICAL OR NO LEADING EDGE DEVICES) AND MADE UNEVSDR AALA20020899Solenoid Valve · malfunctionedMIA - FLT 1343 - MIA-HOU - EN ROUTE HOU, UPON FLAP RETRACTION FROM 1 TO UP LEADING EDGE FLAPS TRANSIT AND SLED RED LIGHT REMAINED ILLUMINATED. EMERGENCY DECLARED. LANDED MIA WITHOUT INCIDENT. AFTER LANDING UPON FLAP RETRACTION L/E FLAPS TRANSIT AND SLAT LEDSDR AUS20020597Valve · faulty(AUS) OUTBOARD LEADING EDGE SLAT CONTROL VALVE FAULTY.SDR AWXA200200520Actuator · bindingBOI - AIR TURN BACK - FLT 0166 - ON DEPARTURE OUT OF BOI EN ROUTE TO PHX THE NR 4 SLAT REMAINED IN EXTENDED POSITION; FLAPS WERE CYCLED AND NR 4 SLAT STILL REMAINED EXTENDED; TURNED BACK TO BOI AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE INSPECTED THE NR 4 SDR 0201909951Duct · damagedUPON SLAT EXTENSION, THE SLAT DISAGREEMENT ANNUNCIATOR LIGHT ILLUMINATED AND THE AIRCRAFT ROLLED. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED IN MSP WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT -T- DUCT OUTER TOP FORWARD POSITION DAMAGED FRSDR DHL2002802560Torque Tube · crackedLFT WING OUTBOARD SLOT TORQUE TUBE CRACKED (CRANK). REMOVED TORQUE TUBE FROM LEFT WING OUTBOARD SLOT PER M/M 27-80-2 PG 201. REMOVED AND REPLACED CRANK ASSY OF TORQUE TUBE PER SRM 51-1-21 PG 1. INSTALLED TORQUE TUBE ON LEFT WING OUTBOARD SLOT PER M/M 27-80-SDR UPS02238551Rib · crackedINSPECTION TYPE:C RIB CRACKED ON LE SLAT #3, RIB LOCATED I/B OF O/B TRACK #3 SLAT REMOVED TO CARRY OUT REPAIR ON CRACKED RIB IAW MM 27-81-11 CRACKED RIB REPAIRED IAW SRM 57-50-3 FIG 9 #3 SLAT INSTALLED AFTER REPAIR COMPLETED IAW MM 27-81-11SDR 2002UALA00933Skin · cracked#1 SLAT, LOWER TRAILING EDGE SKIN, 1 EA RIVET CRACKED ON INBD SIDE ON SKIN. AT 2ND FROM OUTBOARD AUX TRACK. MAJOR REPAIR ACCOMPLISHED. REPAIR DOUBLER INSTALLED.SDR 2002UALA00931Skin · cracked#3 SLAT OUTER LOWER SKIN IS CRACKED ON AFT ROW RIVETS, 38TH RIVET FROM INBD SIDE. MAJOR REPAIR ACCOMPLISHED. DAMAGE CUT OUT, DOUBLER REPAIR ACCOMPLISHED.SDR MWEA020384Slat · puncturedLEFT WING HIT DELTA BAG CART PUNCTURING LEFT OUTBOARD SLAT PANEL. -- REMOVED AND REPLACED SLAT. OPS CHECK GOOD.SDR 02FDEA00307Flap · failed02-108 RIGHT INBD LEADING EDGE FLAP #5 FAILED TO RETRACT WHEN FLAPS 2 WAS SELECTED. ** S/D ** COMINGSDR SWAA020926Fitting · crackedNR 5 L/E SLAT ACTUATOR MOUNT FITTING CRACKED. REMOVED AND REPLACED FITTING PER MM.SDR 02FDEA00286Link · bindingON TAKEOFF LEAD EDGE W/N RAISE WHEN MOVING FLAP HANDLE FROM 5 DEG TO 2 DEG. REMOVED AND REPLACED LINK ASSY PER MM 27-51-051-4. OPS CHECK NORMAL.SDR 0201199995Duct · ratchetingDURING APPROACH FOR LANDING INTO GRR, THE SLAT DISAGREEMENT LIGHT REMAINED ILLUMINATED AND THE AIRCRAFT ROLLED TO THE LEFT. FLIGHT CREW COMPLIED WITH COM PROCEDURES AND ACCOMPLISHED AN UNEVENTFUL NO SLAT LANDING AT GRR. CONTRACT MAINTENANCE COULD NOT FIND ANSDR UPS02238037Web · crackedINSPECTION TYPE:C SUSPECT CRACK #4 SLAT RIB I/B OF ACTUATOR ROD END CARRIED OUT WEB REPAIR IAW SRM 51-40-2SDR 02FDEA00223Actuator · failed02-83 ON T/O FLAP RETRACTED FROM 5 DEG TO 2 DEG, #4 SLAT IND OUT. R&R #4 SLAT ACTUATOR PER MM 27-81-032-4. OK FOR SERVICE.SDR DL76S020368Duct · damagedL/E SLAT ASYM MESSAGE AND LEADING EDGE LIGHT ON AFTER LANDING WHILE BRINGING FLAPS UP. REPLACED TAI DUCT AND TORQUE TUBE. REPAIRED SLAT PANELS.SDR CA020502012Control Unit · failed(CAN) FLAP DISAGREE MESSAGE ON EICAS WHEN FLAP SELECTED TO RETRACT FROM 5 DEGREE TO 1 DEGREE ON TAKEOFF. ALTERNATE TE FLAP EXTENSION USED FOR LANDING. FOUND TO BE THE FSEU AT FAULT (FLAP SLAT CONTROL UNIT). REPLACED ELECT FLAP SLAT UNIT.SDR UPS02237955Hinge Fitting · corrodedINSPECTION TYPE:C PITTING CORROSION ON I/B UPPER FLANGE OF #5 LE FLAP CENTER HINGE SUP PORT FITTING NEW HINGE FITTING KIT INSTALLED IAW SRM 51-30-02SDR 0201069997Duct · lack of lubeUPON SLAT EXTENSION, THE AIRCRAFT ROLLED TO THE RIGHT AND THE BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE. CREW CYCLED SLATS ONCE MORE WITH SAME RESULTS. FOLLOWED COM PROCEDURES AND LANDED UNEVENTFULLY WITHOUT SLATS AT FSD. MAINTENANCE INSPECTED AND CHECKED THE SDR UPS02237954Hinge Fitting · corrodedINSPECTION TYPE:C PITTING CORROSION ON I/B UPPER FLANGE OF #5 LE FLAP CENTER HINGE SUP PORT FITTING NEW HINGE FITTING KIT INSTALLED IAW SRM 51-30-02SDR AUS20020261Pipe · wrong part(AUS) HYDRAULIC PIPES AND BRACKETS LOCATED IN AREA OF NR 8 LEADING EDGE WERE INCORRECT PARTS. PIPE WORN THROUGH BY STRUCTURE WHEN SLATS RETRACTED. UNAPPROVED PART. MANUFACTURING ERROR.SDR 0200679884Slat · malfunctionedWHILE ON APPROACH FOR LANDING AT MOT, CREW NOTICED THE SLAT DISAGREEMENT LIGHT ON AND THE AIRCRAFT ROLL TO THE RIGHT. FOLLOWED COM PROCEDURES. DUE TO INSUFFICIENT RUNWAY LENGTH FOR A NO SLAT LANDING AT MOT, THE CREW ELECTED TO DIVERT. CAPTAIN DECLARED AN EMSDR 02FDEA00205Switch · failed02-72 #1 L/E FLAP W/N RETRACT ON TAKEOFF. R&R #1 L/E FLAP WARN SWITCH PER 27-82-001-4. R&R LINKAGE & MOUNT BRACKET PER 27-82-001-4.SDR P5CA0200658Screw · missingL/H INBD L/E FLAPS ARE DEPLOYED BUT IND UP AT F/E'S PANEL & FWD IND. ON INSPECTION FOUND PDU DRIVE SHAFT DISCONNECTED, LOCKING SCREW MISSING & LOCKING SLEEVE MIGRATED FROM CONNECTION. RE-RIGGED & RE-ATTACHED DRIVE SHAFT IAW MM 27-81-02. OPS CHECK NORMAL.SDR CA020218002Shaft · broken(CAN) WHILE ON APPROACH, PILOT REPORTED THAT WHEN HE SELECTED 30 DEGS OF FLAP HE GOT FLAP WARNING ON CAWS PANEL. NO EFFECT ON FLT CONTROLS AND HE LANDED WITH OUT INCIDENT. PILOT RESET FLAPS ON GROUND AND TRIED TO RETRACT FLAPS. FLAPS WOULD NOT RETRACT AND FLAPSDR CA020218001Control Unit · malfunctioned(CAN) AT FLAP EXTENSION FOR LANDING, NR 3 LEADING EDGE SLAT SHOWS YELLOW AT FLAP 1 WITH OVERHEAD PANEL CAUTION "LE FLAP INTRASIT" LIGHT STAYING YELLOW UNTIL FLAP 15 IS SELECTED. OCCURS IN FLT BUT SEEMS TO WORK FINE ON GROUND. "MAINT INSPECTION FOUND NR 3 SLAT SDR CA020220008Motor · loose(CAN) THE SUBJECT LT MOTOR WILL MOVE TO ITS EXTREME END TRAVEL AND LOCK THE ARMATURE CAUSING THE C.B. TO POP AND THE FLAP SYSTEM TO STOP. WHEN THE CB WAS RESET THE FLAPS WOULD OPERATE NORMALLY, THIS HAPPENED TWICE DURING FLAP SELECTION AND WAS SNAGGED IN THE LSDR SWAA020345Control Valve · failedAIR TURNBACK, L/E SLATS WOULD NOT RETRACT AFTER T/O. REMOVED AND REPLACED AUTO SLAT CONTROL VALVE PER MM.SDR AUS20020094Coupling · separated(AUS) NR 6 AND NR 7 LEADING EDGE FLAPS DISCONNECTED DUE TO THE OUTBOARD SPLINE COUPLING COMING ADRIFT. THERE WAS NO SIGN OF THE LOCKWIREOR ATTACHMENT SCREWS.SDR 0200239762Coupling · misalignedSLAT DISAGREEMENT LIGHT ILLUMINATED WITH A SLIGHT ROLLING TENDENCY TO THE LEFT ON APPROACH. REINSTALLED THE LEFT WING SLAT ANTI-ICE COUPLING BETWEEN NBR 1 AND NBR 2 SLATS. REPLACED THE LEFT NBR 1 SLAT INBOARD CUTOUT DOOR HINGES, TIGHTENED THE RIGHT 'T' DUCT OUSDR CA020509008Pressure Switch · failed(CAN) WHEN SELECTING FLAP 5 INBOUND ON FINAL APPROX. 3700 FT "FLAP POWER" CAUTION LIGHT CAME ON. RE-SET THE SYSTEM ACCORDING TO CREW BULLETIN 02/01 UNSUCCESSFULLY. CARRIED OUT 0 DEG. FLAP LANDING. DURING TOUBLESHOOTING THE FLAP POWER UNIT WAS FOUND DEFECT ANDSDR 0200209762Guide · wornON SLAT EXTENSION, THE SLAT DISAGREEMENT LIGHT ILLUMINATED ACCOMPANIED WITH A ROLL TO THE RT. CREW RECYCLED THE SLATS AND DISCREPANCY REPEATED INCLUDING ROLL TO THE RT. IN PROCESS OF APPLYING COM PROCEDURES, LIGHT WENT OUT AND LANDING WAS NORMAL. MAINTENANCE FSDR ZW0A0201002CableFOUND FLAP BUS TRAVEL CABLE BROKEN. REPLACED THE CABLE. CHECK-C 8-25-01 STL. --CLOSED--SDR ZW0A0201001CableFOUND FLAP BUS TRAVEL CABLE BROKEN. REPLACED THE CABLE. CHECK-C 8-25-01 STL. ---CLOSED---SDR DHL2002805035Fitting · crackedLEFT WING OUTBOARD SLOT TORQUE TUBE FITTING CRACKED.SDR 02FDEA00054Flap · out of adjON CLIMB NR 5 L/E FLAP POS IND WITHIN SHOW RETRACTED (GREEN) WITH FLAPS 2 DEG SELECTED. ACFT HANDLED AS IF SLAT WAS FULLY AND CORRECTLY RETRACTED. QRH DIRECT RECYCLING TO 5 DEG POS (EXTENDED) POS AND IND CORRECT THEN FLAPS 2 AND FLAPS UP. LIGHTS WERE OUT TISDR 0200059752Seal · damagedAIRCRAFT ROLLS SHARPLY TO THE LEFT WHEN SLAT EXTENDED. A LOUD BANG WAS HEARD AFTER 5 DEGREES OF FLAP SELECTED AND ROLLING MOVEMENT STOPPED. THERE WERE NO ABNORMAL ANNUNCIATOR INDICATIONS. THE FLIGHT LANDED SAFELY AT DTW. MAINTENANCE STATED THAT SLAT EXTENSSDR 0200049876Duct · lack of lubeON SLAT EXTENSION, THE AIRCRAFT ROLLED RIGHT ACCOMPANIED BY THE AMBER SLAT DISAGREEMENT AND BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE. THE CREW ACCOMPLISHED COM PROCEDURES AND LANDED WITHOUT SLATS UNEVENTFULLY. MAINTENANCE LUBRICATED THE RIGHT T-DUCT. OPERASDR 02FDEA00105Slat · crackedN 246 #4 LEAD EDGE SLAT HAS 3 CRACKED RIBS BETWEEN WS 383.5 AND 436.5. R&R SLAT PER MM 27-81-811-4.SDR 02FDEA00005Control Cable · brokenRIGHT WING NR 8 SLAT 2ND SLAT TRACK FROM O/B END CABLE BROKEN. REMOVED AND REPLACED CABLE PER MM 27-89-14-4.SDR DL72S020052Slat · crackedREPAIRED 1.5 INCH CRACK IN #5 L/E SLAT I/B RIB AT ACTUATOR ROD END PER M/M 57-54-000-8 PER ERA 382382-14 REV ORGSDR 0105139995Duct · lack of lubeWHEN CONFIGURING THE AIRCRAFT FOR LANDING, THE AIRCRAFT ROLLED LEFT AND STABILIZED. NO BLUE SLAT EXTEND INDICATION BUT SLAT DISAGREEMENT ANNUNCIATOR LIGHT ILLUMINATED. COMPLIED WITH COM PROCEDURE AND LANDING WAS MADE WITHOUT LEADING EDGE SLAT AT GPT. MAINTESDR CA020118001Control Unit · malfunctioned(CAN) MANY INDICATIONS (DEFECTS REPORTED) OF SLATS / FLAPS SYSTEM NR 1 & 2 FAULTS HAVE BEEN REPORTED ON AIRCRAFT, HAVING SEVERAL MAINTENANCE ACTION C/OUT FROM 2001-11-25 TO 2001-12-20 AND THE FINAL RECTIFICATION BEING THE REPLACEMENT OF THE LAT FLAP CONTROL SDR ARWA20011207Brake · malfunctionedDURING FLAP EXTENSION NO SLAT INDICATION ON FLIGHT ENGINEER PANEL. AIRCRAFT RETURNED TO BLOCKS. RESET L/E SLAT ASYMMETRY BRAKES AND ACCOMPLISHED ALL REQUIRED TEST. L/E SLAT TESTED GOOD PER MM 27-81-00. AIRCRAFT RETURNED TO SERVICE.SDR CA020117018Control Valve · malfunctioned(CAN) ON FERRY FLIGHT TSC 2257 FROM CUN-YMX , DURING TAKE OFF , SLAT SYSTEM LOCKED IN EXTEND POSITION , BUT FLAPS RAISED FULL UP. FLAP RED LIGHT WAS ILLUMINATED ON THE FLAP POSITION INDICATOR (PILOTS CENTER INSTRUMENTS PANEL) AND SLAT MONITOR INDICATED SLATSSDR 01FDEA01022Control Cable · brokenNR 7 RIGHT SLAT RETRACT CABLE HAS BROKEN STRANDS. REMOVED AND REPLACED CABLE AND CONTROL PULLEY PER MM 27-89-13, 27-80-00.SDR DL72S011931Slat · crackedREPAIRED #2 SLAT LOWER COVE SKIN ATTACH ANGLE PER 727 M/M 57-54-000-8 FIG 807A AND ERA 382247-14 REV ORGSDR CA011127014Limiter · failed(CAN) AIRCRAFT LANDED WITH FLAP LOCKED IN THE RETRACT POSITION. AIRCRAFT DID OVERSHOOT, THEN EXECUTED A FLAPLESS LANDING. RT SYSTEM TORQUE LIMITER AND INPUT GEARBOXES 2-5 FOUND EXTENDED.
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