JASC 2780
Service difficulty reports · 2,159
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 CALA2016072800466Flap System · malfunctionedLE FLAP TRANSIT LIGHT ILLUIMATED AND FLAP NEEDLE SPLIT WHEN FLAPS SELECTED TO 5. EMERGENCY DECLARED. RAN FLAPS TRAILING EDGE FLAPS DISAGREE CHECKLIST.SPLIT WENT AWAY WHEN HANDLE WAS POSITIONED UP. RAN BITE CHECK ON FSEU, SHOWED NO EXISTING FAULTS. RAN FLASDR AALA20160718006Warning Message · false activationDURING APPROACH, RECEIVED A LEADING EDGE SLAT DISAGREE EICAS MESSAGE. EMERGENCY DECLARED. LANDING UNEVENTFUL. ACCOMPLISHED FSEU BITE CHECK IAW FIM 27-51-00. FSEU NR 1 SHOWED AUTOSLAT FAIL CODE 309, FSEU NR 2 SHOWED NO DATA CODE 209. ALL THREE FSEU SHOWED NO SDR AALA201607069009Computer · defectiveRETURNED TO DEPARTURE , THE FLIGHT CREW REPORTED DURING CLIMBOUT THAT DURING FLAP RETRACTION THE FLAPS LOCKED OUT BEFORE POSITION 1, WING TIP BRAKE ON. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DEPARTURE WHERE IT SAFELY LANDED WITHOUT FURTHER INCISDR AALA20160705006Flap System · malfunctionedDURING APPROACH, WHILE CONFIGURING FOR FLAPS 1, LEADING EDGE FLAP TRANSIT LIGHT STAYED ILLUMINATED. THE FLIGHT BROKE OFF APPROACH AND RECONFIGURED FOR A FLAPS 15 APPROACH BY THE CHECK LIST. THE FLIGHT DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. SDR P5CA2016063000159Nut · detachedON ARRIVAL, LEFT NR 5 SLAT WING LEADING EDGE SLAT LINKAGE FOUND NUT DETACHED ITEM 3 LEADING EDGE NR 5 SLOT WING PANEL DAMAGE, AND FOUND HARDWARE MISSING REINSTALLED AS REQUIRED IAW AMM 27-80 ITEM 3. TEMPORARY REPAIR COMPLETED IAW SRM 57-41-01-2R-1 NOTED A SDR DALA2016052604149Control Valve · malfunctionedDURING SLAT EXTENSION SLAT DISAGREE MSG ENUNCIATED AND ACFT ROLLED TO THE RT. FLIGHT CREW DECLARED AN EMERGENCY, FOLLOWED QRH PROCEDURES NO SLATS NO FLAP LANDING. MAINTENANCE R & R SLAT CONTROL VALVE.SDR VNAA2016051500010Warning Message · false activationSLATS HALF SPEED ON DEPARTURE WOW, FLAP OVERSPEED, AND STABILIZER TRIM RUNAWAY. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, PERFORMED ELECTRICAL RIGGING OF SLATS, CLEARED INHIBITS, AND PERFORMED CHECKS IAW THE AMM. THE ACFSDR UHLA201604300200Warning Light · false activationSLAT FAIL MESSAGE CLIMBING THROUGH ROUGHLY 13,000 FT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. PERFORMED FIM 27-83-00-810-814-A, MESSAGE CLEARED AND DID NOT RETURN AFTER MULTIPLE OPS CHECKS.SDR ASMF201606005Nut · looseDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE AFT FUSELAGE SKIN. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING HYDRAULIC LEAK AT NUT ON FLAPS, SLATS CONTROL VALVE. THE FLAPS, SLATS CONTROL VALVE NUT WAS TIGHTENED IAW AMM 27-81-81, TESTED COSDR VNAA2016042500024Sensor · damagedBIRD STRIKE LT L/E OTBD FOLLOWED BY FLAPS HALFSPEED AND SLAT STATUS MESSAGES. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R THE LT OTBD SLAT DISCONNECT SENSOR, AND DEFERED THE FLAP SUB SYS IAW MEL. MAINTENANCE CLSDR IPXA2016041202020Pseu · inoperativeON DEPARTURE, AT FLAP RETRACT RECEIVED A STICK SHAKER, MOMENTARY, SAW A MOMENTARY SLAT DISAGREE. AFTER RETRACTING THE SLATS RECEIVED A LEVEL 2 SLAT DISAGREE, SPEED 300 STAYED BELOW 280 KTS AND ACCOMPLISHED SLAT INSP SLAT MECHANICAL SYS, INSP OK SLAT POS IND SSDR FDEA201603291098Computer · inoperativeAT LEVEL OFF FLIGHT 360, EICAS MSG LE SLAT ASYM MSG CAME ON. COMPLIED WITH QRH. ACFT ARRIVED WITH NO LOWER EICAS MSG OR MX MSG. LE LIGHT WAS ON ABOVE POSITION GAUGE. CREW HAD, LE SLAT ASYM, IN ORANGE ON UPPER EICAS. RESETTING FSCUE 1 BREAKER CLEARED LIGHTSDR AALA20160323005Coupling · looseAIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING POST CHECK FUNCTIONAL CHECK FLIGHT THE LE ASYMMETRY LIGHT ILLUMINATED AT FLAPS 30. FOUND BROKEN SAFETY WIRE & BACKED OUT SET SCREWS ON TORQUE TUBE COUPLING INBD NR 5 SLAT OFSDR YENA20160320250Slat System · failedCREW REPORTS SLAT ON APPROACH, FAULT CODE 27811013, ACE PRESENT. INSPECTED AND CHECKED LT OTBD SKEW SENSORS 2-3 +3-4 CK GOOD, INSPECTED AND CHECKED SKEW HARNESSES FROM P0585-P0989+P0991 WITH MULTIMETER. CHECKS GOOD, REMOVED AND REINSTALLED SLAT/FLAP CONTROL SDR DALA2016030801805Bearing · corrodedBEARING RUSTED, NR 2 SLAT OTBD, INBD SUPPORT BEARING HAS RUST COMING OUT OF IT. SUMMARY NR FOR ADDITIONAL INFORMATION 001-0258:2020-2339/008. CLEANED AND LUBED BEARING IAW PS 900-2-1001-0258:2020-2339/008.SDR FDEA201602280701Control Cable · shearedDURING POST FLIGHT INSPECTION, FOUND SHEARED DRIVE CABLE PROTRUDING FROM NR 8 RT OTBD SLAT, AT TRACK 19. NO FLIGHT CONTROL FAULTS WERE INDICATED IN THE FLIGHT DECK. PERFORMED RT SLAT NR 8 RETRACT, 84E & 84F IAW AMM 27-80-00-5, CONTROL CABLE INITIAL RIG LOAD.SDR YENA20160223123Slat System · failedDIVERTED, SLAT FAIL 0, FLAP FAIL 2. PERFORMED FIM 27-81-00-810-805. INSPECTED LT OTBD SLAT ACTUATORS AND SKEW SENSORS, NO DEFECT NOTED. CHECK WIRE HARNESS AND SKEW SENSOR ON LT OTBD S2/3 AND S3/4 FOR CONTINUITY & SHORTAGE. NO DEFECT NOTED. OPS CHECK GOOD RSDR R61A201602220119Slat System · malfunctionedCREW RECEIVED A SLAT FAIL MESSAGE. CREW RAN QRH, DIVERTED AND WITH PASSENGERS BRACING, LANDED WITHOUT INCIDENT. AFTER BEING CHECKED OUT BY THE FIRE DEPARTMENT, CREW TAXIED TO GATE. MAINTENANCE CLEARED INHIBITS, RESET SYS IAW AMM AND OPS CHECKED GOOD.SDR HALA2016021800049Pseu · malfunctionedAIR DIVERSION - DIPSEU FAIL ILLUMINATED IN FLIGHT AFTER SLAT RETRACTION, REMAINED ON, WENT OFF AT SLAT EXTENSION. R & R PSEU CONTROL BOX IAW AMM 32-61-01-400-801. OPS CHECK OK-NO DEFECTS.SDR FDEA201602030435Sensor · failedDUAL SLATS FAULT 1 & 2 ON APPROACH, 3000' MSL 170 KTS, FLAPS STUCK AT 15'. R & R SLAT COMMAND SENSOR UNIT 51CV IAW AMM 27-51-17-04. R & R BOTH SFCC'S IAW AMM 27-51-18-04. FLAP & SLATS OPERATION TESTED GOOD IAW AMM 27-81-00-05. ALSO REF TSM 27-80-07.SDR DALA2016020400945Control Valve · malfunctionedAFTER TAKEOFF, SLATS SELACTED TO UP POSITION. DISAGREE LIGHT ILLUMINATED. PILOTS OBSERVED SLATS IN EXTEND POSITION DURING FLIGHT. MAINTENANCE REMOVED AND INSTALLED SLAT CONTROL VALVE.SDR EBVR201602020664Detector · out of limitsDURING A SCHEDULED INSPECTION EVENT. THE FLAP ASYMMETRY/OVER SPEED DETECTOR AND BRAKE UNIT FUNCTION TEST WAS COMPLIED WITH AS PART OF THE SCHEDULED INSPECTION. DURING THE FUNCTION TEST, THE LT BRAKE UNIT FAILED THE TESTING.SDR YENA20160128090Sensor · failedDIVERTED, FLAP LOW RATE MESSAGE DURING DESCENT, SLAT/FLAP ELECTRICAL SYSTEM. R & R SKEW SENSORS LT WING T3 + T4 CLEARING THIS MDDR. MX-4 UPDATED.SDR YENA20160128089Sensor · failedDIVERTED, FLAP LOW RATE MESSAGE DURING DESCENT, SLAT/FLAP ELECTRICAL SYSTEM. R & R SKEW SENSORS LT WING T3 + T4 CLEARING THIS MDDR. MX-4 UPDATED.SDR CA160114005Bpsu · failed(CAN) SLATS FAIL CAUTION MESSAGE POSTED ON THE EICAS AND SLATS FAILED TO RETRACT DURING CLIMB. MDC SLAT ACT SYS/ASYMMETRY, B1-007771, SFECU 2/SLAT CHANNEL, B1-007813, SFECU 1/SLAT CHANNEL, B1-007802, AND SLAT LT BPSU/LT BRAKE 1, B1-007829, MESSAGES LOGGED IN SDR AALA20160113006Relay · faultyAIRCRAFT WAS GNDED. EMER DECLARED, LANDING UNEVENTFUL, ACFT NOT OVERWEIGHT. DURING APPROACH AFTER FLAPS 1 SELECTED FLPS1 RECEIVED, LE SLAT DISAGREE, ACCOMPANIED BY A SPLIT IN FLAP INDICATOR. MX COULD NOT DUPLICATE SLAT DISAGREE. R & R FSEU IAW AMM 27-51-01SDR SWAA2015113046481Flap · faultyAIR RETURN, NR 1 KRUEGER INDICATOR DOWN IN FLIGHT WITH ASSOCIATED LE FLAP TRANSIT LIGHT. R & R NR 1 KRUEGER FLAP IAW MM.SDR FDEA201511183729Flap · damagedON DIRTY UP FOR APPROACH, KRUEGER FLAP FAILED TO EXTEND. REPLACED DAMAGED LT KRUEGER FLAP INBD CARRIER & SUPPORT WITH KRUEGER FLAP POSITION SWITCHES IAW MM 27-87-14-04. AWAITING INSTALLATION OF KRUEGER FLAP FOR OPERATIONS CHECKS. INSTALLED LT KRUEGER FLAP SDR Q2SA20151117228Flap System · malfunctionedAMBER "L/E FLAPS TRANSIT" LIGHT ILLUMINATED AFTER FLAPS RETRACTED. OVERHEAD PANEL INDICATOR L/E DEVICE FLAPS NR 3 INDICATED DEPLOYED. QRH PROCEDURES FOLLOWED.SDR DALA2015111206904Support · crackedRT SLAT DRIVE, AFT SUPPORT CRACKED AT BEARING ASSY LOWER FASTNER HOLES. REMOVED RT SLAT DRIVE ASSY.SDR VNAA2015102700028Control Unit · intermittentCREW REPORTED SLATS FAIL CAUTION MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R NR 1 SLAT-FLAP ELECTRONIC CONTROL UNIT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.SDR SWIA201541556Roller · wornLEFT WING SLAT TRACK 1-2 FORWARD/OTBD SIDE ROLLER WITH A FLAT SPOT. R & R LT SLAT TRACK 1-2 FWD OTBD SIDE ROLLER IAW AMM.SDR AALA201510279008Computer · defectiveEMERGENCY LANDING, CREW MESSAGED AT 0509Z THAT ACFT SLATS WERE LOCKED, BUT DID NOT STATE SLAT POSITION. THEY HAD CHECKED THE ECAM NON-NORMAL LANDING MANUAL & DECLARED AN EMER FOR LANDING RNWY 8. DISPATCH VERIFIED WITH ECAM MANUAL. CREW REPORTED AFTER LANDINSDR FDEA201510153232Computer · faultedON APPROACH ON SLAT EXTENSION 1 & 2 SLATS & FLAPS FAULT, CYCLED NO HELP. WHILE PERFORMING QRH PROCEDURE SLAT & FLAPS EXTENDED NORMALLY. DURING POST FLIGHT CHECKS FOUND FAULTS ON BOTH SFCC'S. SFCC 1 & SFCC 2, BOTH INDICATED SLAT JAM. RESET BOTH SFCC'S & CYSDR FDEA201510103160Slat System · malfunctionedSLAT SYSTEMS 1 & 2 FAULTED DURING EXTENSION. SPF I SLAT LIGHT WAS NOT ILLUMINATED. CYCLING SLATS, DID NOT CORRECT THE STUCK SLATS. BITE CHECKED SFCC'S, FOUND SLAT JAM FAULT ON BOTH. RESET SFCC'S, OPERATED SLATS NO HELP FAULTS ON SFCC'S RETURNED. SWAPPED SDR FDEA201510013029Jackscrew · malfunctionedSLATS STUCK ZERO, LANDED WITH SLATS AT ZERO, FLAPS FORTY. SLAT SYS NR 1 & 2 FAULTED ON OVERHEAD. SFCC NR 1 & 2 SHOWED FAULT 01111. REMOVED AND REPLACED 3L SLAT JACKSCREW PER AMM 27-84-22-04. OPS CHECKED GOOD OKAY FOR SERVICESDR SIMA20150912003Slat · failedSLATS FAIL IN APPROACH. TROUBLE SHOT IAW FIM TASK 27-81-09-810-802. INSPECTED ACTUATORS IAW ETN CR-27-084. SLAT OPERATIONS CHECKED GOOD IAW AMM 27-52-00.SDR CA150901011Ecu · burned(CAN) DURING REGULAR MAINTENANCE, SMELL OF SMOKE WAS NOTICED IN THE AVIONICS BAY AND SLAT CB ON ACPC FOUND TRIPPED. SFECU NR 1 FOUND TO BE BURNT.SDR N6WA2015082601Torque Tube · disconnectedSLATS FAIL, CAUTION MSG ON APPROACH, ACFT DID A GO AROUND. FOUND LT OTBD TORQUE TUBE AT WS 327.00 - 353.00, DISCONNECTED. RE-CONNECTED LT OTBD TORQUE TUBE IAW AMM 27-81-01. PERFORMED OPERATIONS CHECK IAW AMM 27-81-00. THE SLAT DISCONNECT SENSOR WAS ALSO DASDR CA150824002Electronic Unit · malfunctioned(CAN) ON ARRIVAL THE CREW RECEIVED A FLAP ASYMMETRY MESSAGE. AN UNEVENTFUL LANDING WAS CONDUCTED AFTER COMPLETION OF THE CHECKLIST. 27-81 FAULT TREE 809 FSEU RESET SYS. OPS CHECK OK. NO FAULTS. ACFT SERVICEABLE.SDR FDEA201508212681Control Cable · cutON ARRIVAL, WALK AROUND CHECK FOUND LT NR 8 LE SLAT CABLE CUT IN TWO PLACES, SECOND & THIRD TRACK FROM MOST OTBD. R & R LT NR 8 LE SLAT EXTENSION & RETRACTION CABLES & PULLEYS IAW AMM 20-20-07-2, IPC 27-81-27-01 & 20-00-00-0 SMP. COMPLIED LOCKWIRE & LOCK CLSDR AALA20150817001Pseu · failedAIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, CREW REPORTED LE SLAT ASYMMETRY MSG & LE LIGHT ON WHEN FLAPS RETRACTED FROM 1DG TO UP. R & R PSEU IAW AMM 32-09-04. SYS CHECKED NORMAL.SDR CA150811001Electronic Unit · failed(CAN) ON ARRIVAL INTO ATH THE CREW REPORTED A L/E SLAT ASYMMETRY AND LANDED IN A FLAPS 20 AND SLATS 0 CONFIGURATION. NO DEGREE OF EMERGENCY WAS DECLARED. REPLACED FLAP/SLAT ELEC UNIT IAW 27-51-01 PB 401, CHECKED SERVICEABLE.SDR SIMA20150804001Indicator · trippedSLATS FAIL IN FLIGHT. INTERROGATED MDC, FOUND SLAT ACT JAMMED MECHANICAL MDC MESSAGE. INSPECTED SLAT ACT TRIP INDICATORS. RESET THE TRIPPED INDICATORS & PERFORMED OPERATIONS TEST OF SLATS & FLAP SYSTEM. INSPECTED THE SLAT ACT TRIP INDICATOR & NO TRIP INDICSDR FDEA201507272403Cable · damagedRIGHT WING OUTBOARD NR 18 SLAT TRACK CABLE, RUN 83E IS DAMAGED. R & R IAW AMM 20-20-06-2. PERFORMED ADJUSTMENT & OPERATIONS CHECK RT NR 8 SLAT CABLES, GOOD IAW AMM 27-80-30-5.SDR AALA20150724004Slat System · false indicationDURING APPROACH LE SLAT ASYMMETRY DISPLAYED ON EICAS. LANDING ABORTED, EMERGENCY DECLARED, AND LANDING UNEVENTFUL. ACCOMPLISHED FIM 27-81-00, CHECKED LE SENSORS FROM PSEU RACK PLUG. ALL SENSORS OHMED NORMAL, SENSOR GAPS NORMAL. COULD NOT DUPLICATE ON GND. SDR FDEA201507212287Fseu · inoperativeON DEPARTURE, WHEN SELECTING FLAPS UP, HAD A LE DISAGREE EICAS. FLAP INDICATOR SHOWED STUCK BETWEEN 1 DEGREE & UP. PERFORMED CHECKLIST & RETURNED TO DEPARTURE. R & R FSEU IN NR 1 POSITION. OPS CHECKED IAW AMM 27-51-01-2 PAGE 1-16. FLAPS & SLATS OPERATED NSDR HALA201506130110Cable · brokenLEADING EDGE SLATS ON LT WING, NOT RETRACTING PROPERLY. FOUND NR 5 SLAT CABLE RUNS 194A BROKEN. REPLACED NR 5 SLAT CABLE RUNS IAW DWG 5910451. ADJUSTED CABLES IAW AMM 27-80-380-802. ALSO REPLACED PULLEYS, STA Z0S 530.SDR SWAA2015051539743Proximity Sensor · faultyDIVERTED & DECLARED EMER NR 6 SLAT WOULD NOT FULLY EXTEND. R & R NR 6 SLAT OTBD PROXIMITY SWITCH S1004 SENSOR IAW AMM.SDR AALA20150501008Slat System · malfunctionedDURING FLAP RETRACTION RECEIVED EICAS, LE FLAP DISAGREE, MESSAGE. EMERGENCY DECLARED, LANDING UNEVENTFUL. INTERROGATED FLAP & SLAT ELEC UNIT WITH NO LAST LEG FAULTS SHOWN. FLAPS & SLAT CYCLED FULL RANGE SEVERAL TIMES WITH ALL INDICATIONS NORMAL IAW AMM 27-
Back to JASC 2780