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 VNAA202209029925None · corrodedPITTING CORROSION ON SLAT TRACKS 1-1 (SEVERAL LOCATION AT UPPER SURFACE), SLAT #1 RH WING.
SLAT TRACKS 1-1 (SEVERAL LOCATION AT UPPER SURFACE) WAS REPAIRED PER REO 670-57-42-1377 REV.--SDR CALA2022082402153Slat · damagedRH SLAT #3 TRACK #7 LOWER FWD ANTI-ROTATION STOP DAMAGED, FURTHER EVALUATION REQUIRED. AS NOTED ON LTPR NR#5001171165-0010 PERFORMED REPAIR ON RH SLAT #3 TRACK RIB #7 AS PER A319 SRM TASK 57-40-00-300-112 REV 142. THE REPAIR IS CLASSIFIED AS MAJOR CATEGORY "A"SDR CALA2022082402152Slat · damagedRH SLAT #3 TRACK #7 LOWER FWD ANTI-ROTATION STOP DAMAGED, FURTHER EVALUATION REQUIRED. AS NOTED ON LTPR NR#5001171165-0010 PERFORMED REPAIR ON RH SLAT #3 TRACK RIB #7 AS PER A319 SRM TASK 57-40-00-300-112 REV 142. THE REPAIR IS CLASSIFIED AS MAJOR CATEGORY "A"SDR SWAA2022081240613Sensor · intermittentNR 1 SLAT MID POSITION TRANSIT INDICATION INTERMITTANT. OK TO CONTINUE IAW MEL 27-4-05 SP1 SP2. FAULT CODES 27-81201, 27-53279, & 27-53280. REMOVED AND REPLACED NR 1 SLAT SENSOR INBD S995 IAW AMM 27-88-11. OPS CHECK GOOD.SDR YENA2022080800769Slat Track · crackedDURING HEAVY MAINTENANCE: CRACK ON SLAT TRACK #5 CUTOUT AT LH WING FIXED LEADING EDGE UPPER SKIN; REF TOMX WO # 1997 N/R# 00208. SLAT TRACK #5 CUTOUT AT LH WING FIXED LEADING EDGE UPPER SKIN WAS REPAIRED PER.EMB-190 ETI-190-22-600 REV ORIGINAL, EC E22-532-01 ASDR SWAA2022071327805Flap · faultyFLAP DISAGREE SELECTED FLAPS 5; FLAPS DID NOT MOVE. PERFORMED ALT FLAP EXTENTION FLAP DISAGREE SELECTED FLAPS 5 FLAPS DID NOT MOVE. PERFORMED ALT FLAP EXTENTION PER QRH LANDED UNEVENTFULLY. / [01] OPS CHECK LEADING EDGE FLAP AND SLAT REF. AMM 27-81-00. CHECK NSDR SWAA2022071126703Actuator · faultyLEADING EDGE FLAPS WOULD NOT RETRACT ON DEPARTURE. LE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED. ALL LEADING EDGE TRANSIT LIGHTS ON OVERHEAD PANEL REMAINED ILLUMINATED. MAX LANDING WEIGHT NOT EXCEEDED. / [01] REF WOS TTG8Q00DEQFC; TTG8Q00DEQFF; TTG8Q00DEQFH; & SDR SWAA2022071127697Actuator · faultyLEADING EDGE FLAPS WOULD NOT RETRACT ON DEPARTURE. LE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED. ALL LEADING EDGE TRANSIT LIGHTS ON OVERHEAD PANEL REMAINED ILLUMINATED. MAX LANDING WEIGHT NOT EXCEEDED. / [01] REF WOS TTG8Q00DEQFC; TTG8Q00DEQFF; TTG8Q00DEQFH; & SDR SWAA2022071127698Actuator · faultyLEADING EDGE FLAPS WOULD NOT RETRACT ON DEPARTURE. LE FLAPS TRANSIT LIGHT REMAINED ILLUMINATED. ALL LEADING EDGE TRANSIT LIGHTS ON OVERHEAD PANEL REMAINED ILLUMINATED. MAX LANDING WEIGHT NOT EXCEEDED. / [01] REF WOS TTG8Q00DEQFC; TTG8Q00DEQFF; TTG8Q00DEQFH; & SDR FDEA202206211490Bracket · crackedR.WING I/B L/E @ LES 285 SLAT TORQUE TUBE GUIDE BRACKET IS CRACKED. REMOVED CRACKED BRACKET, LOCATED AND DRILLED NEW BRACKET AND REINSTALLED BRACKET PER B767 SRM 51- 40-05, 51-40-02 AND BAC DWG 114T1240 REV -SDR CALA2022062001542Slat System · faultySLATS DRIVE EIDAS DISPLAYED ON CLIMB OUT PILOTS GOT A "SLAT DRIVE" MESSAGE. WHILE RUNNING CONFIGURATION.. UPON ENTERING ORD, THEY WERE LIMITED TO SEE ATTACHED IMAGES. THROUGH THE QRH FOR THAT, THEY GOT A FLAP/SLAT CONTROL TO WHICH DROPPING FLAPS AND SLATS TOSDR DALA2022061504189Actuator · faultedSHIP 3238 - MISC/DE - DUE TO F/CTL SLAT SYS 1 FAULT. CORRECTIVE ACTION: R/R NUMBER 6 SLAT ACTUATOR 6029CM AND NUMBER 12 SLAT ACTUATOR 6045CM. ADJUSTMENT AND TEST OK. OK FOR SERVICE. (2277046)SDR IPXA2022061083009Slat System · malfunctionedEMERGENCY DECLARED, A/C OOS, LE SLAT DISAG WHEN CONFIGURING TO FLAP 1. PROCEDED TO HOLD & WORK CHK LIST. CHK LIST LED US TO LE SLAT ASYM CK LIST. ENDED UP WITH FLAP 20 LANDING WITH LE SLATS IN UP POSITION. DECL'D EMERG. LANDED AT MIN FUEL DUE TO EXTENDED VESDR IPXA2022062283358Slat · crackedINSPECTION TYPE:3CL/H WING #4 SLAT OUTER SKIN DOUBLER REPAIE REQUIRES PERMANENT REPAIR.REMOVED AND REPLACED SLAT IAW AMM 27-80-30-400-802. (MINOR)SDR DALA2022060803993Slat System · faultedSHIP 3229 >>> HIGH ALERT WITH DECLARED EMERGENCY <<< F/CTL SLATS FAULT. CORRECTIVE ACTION: DEFERRED. AIRCRAFT CURRENTLY IN CHECK MTC. REPAIR TBD. (2267080)SDR AALA202206028215Proximity Sensor · inoperativeAIRCRAFT WAS GROUNDED: LEADING EDGE FLAPS TRANSIT LIGHT ILLUMINATED/SLAT DISAGREE WITH SELECTED POSITION.(FOUND NUMBER 7 SLAT TRANSIT LIGHT STAYS ON. MESSAGE 27-81212 FAULTED). INSTALLED PROXIMITY SENSOR S1006 ON NUMBER 7 SLAT PER AMM 27-88-11.SDR MASA2022051900148None · noneSLAT FAIL CTN IN FLT (EMERGENCY DECLARED). PERFORMED CEAR INHIBITS - OP GOOD.SDR IXXA2022053101Door · cracked0. 11 SLAT OB CONTROL ROD COVER DOOR CRACKEDSDR FDEA202205021099None · noneLE SLAT ASYM EICAS ALERT ON FINAL @ 1300 MSL WHEN FLAPS SELECTED TO 25 DEGREES . EXECUTED MISSED APPROACH @ 700 . LEVELED AT 2000 CLEANED AIRCRAFT TO FLAPS 5 AND NOTICED LE SLAT ASYM EICAS EXTINGUISHED WHEN FLAPS RETRACT TO 20. REATTEMPED FLAP EXTENSIOSDR AALA202204281547Proximity Sensor · noneAIRCRAFT WAS GROUNDED: AT FL360 NUMBER 1 SLAT IN TRANSIT LIGHT ILLUMINATED LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED. ACCOMPLISHED QUICK REFERENCE HANDBOOK ITEMS. AFTER APPROXIMATELY 1 HOUR, BOTH LIGHTS EXTINGUISHED. EMERGENCY WAS DECLARED AND RETURNED TO DFSDR IPXA2022042081321Slat · noneINSPECTION TYPE:NA**ATB** **EMERGENCY DECLARED** **LANDED WITHOUT INCIDENT** LE SLAT DISAGREE ON DEPARTURE. RAN APPROPRIATE CHECKLIST AND RETURNED TO MSP. ATB.TROUBLESHOT LE SLAT DISAGREE IN REF TO FIM 27-81-00-815-803. FOUND O/B OVERLOAD INDICATOR TRIPPED ON SDR FDEA202204180987Skin · crackedR/W #10 SLAT COVE SKIN IS CRACKED IN LINE WITH I/B TRACK. REMOVED AND REPLACED SKIN PER BAC DWG # 114N4075 AND 114N4004SDR IPXA2022042781511Retainer · brokenINSPECTION TYPE:CLH KRUGER FLAP UPPER EDGE SEAL RETAINER BROKEN AT O/B END.REMOVD AND REPLACED IAW SRM 51-40-21SDR SWAA2022041694534Proximity Sensor · failedAFTER TAKEOFF #3 LEADING EDGE SLAT WOULD NOT RETRACT. / [01] FLAP/SLAT ELECTRONICS UNIT BITE SHOWS F/C 27-81204 SL3 PROX OUTBOARD; #3 SLAT OUTBD. PROX. SENSOR SHOWS TARGET NEAR WHEN TARGET FAR; PERFORMED FIM 27-88 TASK 803; REPLACED #3 SLAT OUTBD. PROX. SENSORSDR IPXA2022041581182None · noneINSPECTION TYPE:NA**ATB ** NON TAKEOFF WHILE RETRACTING FLAPS, RECEIVED A L.E. SLAT DISAGREE. WHILE RUNNING CHECKLIST TO CONFIGURE RECIEVED A T.E. DISAGREE. LANDED PER CHECKLIST WITH FLAPS 15 DEGREES.TROUBLESHOT PER FIM 27-81-815-803. NO FAULTS FOUND. PERFORMESDR FDEA202204140959Warning Message · false activationDURING APPROACH AND SLAT EXTENSION, RECEIVED ECAM. SLAT SYS 1 FAULT. & FLAPS SYS 1 & 2 FAULT. CYCLE PER ECAM. FAULT DID NOT CLEAR. ALL 3 FAULTS RETURNED INCLUDING AMBER ECAM KRUGER NOT EXTENDED. COMPLIED WITH QRH DECLARED EMERGENCY & LANDED. LT FLAPS SLSDR SCNA20220414031None · noneDEFECT: LE TRANSIT LIGHT ILLUMINATED ON APPROACH. RESOLUTION: R&R #8 IB SLAT PROX SENSOR OPS CHECK GOOD REF AMM 27-88-11 ACCOMPLISHED BITE CHECK OF FSEU NO FAULTS NOTED REF FIM 27-88 TASK 804 OK FOR SVC.SDR UIEA2022040900276Flap · damagedDURING WALK AROUND, FOUND #7 L/E FLAP VARIABLE CAMBER DAMAGED(<P ><SPAN>REPLACED #7 L/E FLAP VARIABLE CAMBER PER AMM 27-81-02/401. PERFORMED FLAP OPS AND FCU GROUND TEST OK PER AMM 27-81-00/801.</SPAN></P> / <P> </P>)SDR AALA202204076818Fseu · faultedAIRCRAFT WAS GROUNDED: AT POWER UP ON TAKEOFF, TAKEOFF WARNING HOLD AND TAKEOFF CONFIGURATION LIGHT ACTIVATED. CONFIRMATION WAS RECHECKED, ALL SETTINGS AS REQUIRED. REAPPLIED POWER AND WARNING CONTINUED TAKEOFF WAS DISCONTINUED. SPEED DID NOT EXCEED 5 KNOTS, FSDR AALA202203291109Actuator · leakingAIRCRAFT WAS GROUNDED: IN FLIGHT SLAT #4 FAILED TO EXTEND. LE FLAPS TRANSIT LIGHT ILLUMINATED. FLAPS - TRAILING EDGE - WERE NORMAL FOLLOWING LE FLAPS TRANSIT LIGHT PROCEDURE AND WHEN A/C CONFIGURED FOR FLAPS 15 LANDING. CONDITION CORRECTED IT SELF. CREW RECONFSDR AALA202203251109None · noneAIRCRAFT WAS GROUNDED: IN FLIGHT SLAT #4 FAILED TO EXTEND. LE FLAPS TRANSIT LIGHT ILLUMINATED. FLAPS - TRAILING EDGE - WERE NORMAL FOLLOWING LE FLAPS TRANSIT LIGHT PROCEDURE AND WHEN A/C CONFIGURED FOR FLAPS 15 LANDING. CONDITION CORRECTED IT SELF. CREW RECONFSDR SWAA2022032485720Sensor · faultyAFTER TAKEOFF; WITH LANDING GEAR LEVER IN UP POSITION; THE RIGHT MAIN GREEN LANDING GEAR INDICATOR LIGHT REMAINED ILLUMINATED. / [01] REMOVED AND REPLACED THE RH FORWARD MLG DOWN-AND-LOCKED SENSOR (S0073) PER AMM 32-61-31. OPS CHECK GOOD; COULD NOT DUPLICATE; SDR FDEA202203120487Sensor · failedPASSING 9000 FEET ON CLIMB OUT, WHILE ACCELERATING, LEVEL 2 SLAT DISAG. ALERT. COMPLIED WITH QRH. ALERT WAS SPURIOUS AND WENT OUT PRIOR TO CRUISE ALTITUDE. ALERT RETURNED ON DESCENT CAUSING SPURIOUS AIRSPEEDS ON APPROACH. COMPLIED WITH QRH, PERFORMED A FLSDR IXXA2022033004Bracket · crackedRW INBD L/E UPPER SLAT TORQUE TUBE SUPPORT BRACKET IS CRACKED LOCATED APPROX AT LES 292SDR UIEA2022021700142Flap · erodedRHW NO.20 V/C FLAP EXT. LSA FOUND EROSION.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1.</P>)SDR UIEA2022021700143Flap · corrodedRHW NO.20 V/C FLAP EXT. LSA FOUND EROSION(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1.</P>)SDR YENA2022022400090None · failedFLT #915, JFK-SFO. (EMERGENCY DECLARED) F/CTL SLATS FAULT NO LAT LANDED WITH FLAP 3 165K; PERFORMED TSM 27-81-00-810-810-A FOUND RH WING SLAT ACTUATOR (6091CM) TORQUE LIMITER TRIPPED. REMOVED & REPLACED 6091CM PER AMM 27-84-49PB401. OPS CK GOOD PER AMM 27-84-0SDR FDEA202202210335Slat · noneR/H WING #8 SLAT T/E WEDGE LOWER SURFACE T/E IS GOUGED APPROX 42" OTBD OF THE INBD EDGE OF THE SLAT. REPAIRED GOUGED AREA ON THE RH WING #8 SLAT TRAILING EDGE WEDGE LOWER SURFACE APPROX 42" OUTBOARD OF THE INBOARD EDGE OF SLAT IAW B767 SRM 57-43-02-2R-1 ANSDR FDEA202202210334Slat · none#4 SLAT INBD AFT LOWER SKIN CHAFFED. REPAIRED CHAFFED AREA OF #4 SLAT INBOARD AFT LOWER T/E IAW B767 SRM 57-43-02-2R FIG 201 AND B767 SRM 51-70-10-2R REPAIR GENERAL AND 51-70-10-2R REPAIR 4SDR FDEA202202070238None · none#6 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED,REPLACED, ADJUSTED AND OPS CHECK IAW B7578 AMM 27-81-01-4 AND FEDEX EA F- 5750-T0366777SDR FDEA202202070239None · none#1 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED, REPLACED, ADJUSTED AND OPS CHECK IAW B757-2 AMM 27-81-01-4SDR FDEA202202070237None · none#5 SLAT FOUND DISBONDED DURING ULTRASONIC INSPECTION REMOVED, REPLACED, ADJUSTED AND OPS CHECK #5 SLAT IAW B757 AMM 27-81-01-4SDR 2022F00210Slat Valve · leakingLOW HYDRAULIC A VOLUME DISPLAYED ON EICAS. REMOVED AND REPLACED LEAKING SLAT CONTROL VALVE.SDR HALA2022020400039Computer · faultedBTB 2 - SELECTING FLAPS 1 ECAM F/CTL FLAPS FAULT // PERFORMED BITE OF SFCC PER AMM 27-54-00. FAULTING SFCC2 22CV. REMOVED AND REPLACED SFCC2 PER AMM 27-51-34, OPS CHECK GOOD. OK FOR SVCSDR AALA202201283414Slat System · intermittentAIRCRAFT WAS NOT GROUNDED: ON FINAL AT FIRST FLAP/SLAT EXTENSION - FLAPS EXTENDED BUT SLATS STAYED UP. SLATS APPEARED JAMMED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. PERFORMED TSM TASK 27-81-00-810-810A. NO FAULTS OR SDR VNAA202201241111Warning Message · false activationCREW RECEIVED A SLATS FAIL CAUTION MESSAGE. THEY DECIDED TO GO AROUND AND CONSULT THE QRH. UPON LANDING THE FLAPS DEPLOYED BUT THE SLATS DID NOT. SLATS FAIL CAUTION MESSAGE WHEN LOWERING FLAPS TO 8 DEGREES MSG DID NOT GO AWAY DURING QRH PROCEDURE HAPPENDED DURSDR IPXA2022012178118Slat System · fault messageEMERG DECL'D* NO EQUIP USED, A/C LANDED UNEVENTFULLY*ON SHORT FINAL WE GOT A SLAT DISAG WENT AROUND ON DOWN WINDW WITH SLATS EXTENDED THE SLAT DISAG LEVELWOULD COME & GO. IT WAS DISPLAYED 4 OR 5 TIMES WE RETRACTED THE SLATS AND IT WENT AWAY SLATS RETRACTEDSLASDR CALA2022011000100Slat · fault message*EMERGENCY DECLARED* F/CTL SLATS FAULT UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PLEASE CALL TOMC AND FOLLOW TSM 27-81-00-810-810A REF TSM TASK 27-81-00-810-094 OPERATING WITH GREEN SYSTEM RECEIVED SLAT SYSTEMSDR AALA202201030323Sdac · fault messageAIRCRAFT WAS GROUNDED: FLIGHT CONTROL SLAT SYSTEM 2 FAULT ECAM DISPLAYED IN ROUTE TO DFW. DECLARED AN EMERGENCY AND LANDED AT DFW SAFELY WITHOUT FURTHER INCIDENT. ACCOMPLISHED TSM 27-81-00-810-832A WITH NO FAULTS NOTED. REPLACED SDAC (SYSTEM DATA ACQUISITION CSDR SIMA20211229002Ecu · faultedREF AML 4604436-1, SLAT FAIL MESSAGE ON EICAS DURING CRUISE AND ON LANDING. DECLARED EMERGENCY. -C/A-SLEIGHTED FLAP/SLAT ELECTRONIC CONTROL UNIT FOR T/S PURPOSES. DID NOT FIX PROBLEM. REINSTALLED FLAP/SLAT ELECTRONIC CONTROL UNIT AS REQUIRED IAW EMB 175 AMM 27
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