JASC 2782
Service difficulty reports · 1,225
Reports filed under 2782 · Leading Edge Slat Actuator, 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 = '2782' 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 = '2782' 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 DHL9974109CAngle · crackedAT C CHECK, LEFT WING LEADING EDGE CAVITY INBD VERTICAL SUPPORT ANGLE FOR NR 2 SLAT ACTUATOR IS CRACKED. REMOVED AND REPLACED VERTICAL SUPPORT ANGLE PER SRM 51-30-2. INSTALLED STAINLESS STEEL DOUBLER ON THE SUPPORT ANGLES PER S/B 57-130, N/R 1356.SDR DL72S990357Actuator · failedSLC- AFTER T/O, LOST -A- SYSTEM HYDRAULIC SYSTEM. FOUND NR 2 L/E FLAP ACTUATOR LEAKING AND ACTUATOR BRACKET BROKEN. REPLACED SAME.SDR UPS99228770Web · crackedINSPECTION TYPE-C, NR 6 K-FLAP ACT MOUNTING STRUCTURE LWR WEB BETWEEN I/B AND O/B MOUNT IS CRACKED. REMOVED OLD WEB AND INSTALLED NEW WEB IAW SRM 51-30-2, SRM 51-20-1, OHM 20-50-01, SRM 51-10-2.SDR DL72W990315Actuator · leakingINFLIGHT 'A' SYS HYD QTY DECREASED TO NEAR ZERO, ACCOMPLISHED PROD IAW POM. REPLACED INBOARD KRUEGER FLAP ACTUATOR.SDR 99UAL900099Actuator · failedRETURNED TO ORD DUE TO A LEADING EDGE SLAT PROBLEM. *S/D* POSITION NR 15 LEADING EDGE SLAT ACTUATOR FAILED WHICH CAUSED SYSTEM BINDING AND SHUTDOWN OF THE SLAT SYSTEM AT THE POWER DRIVE UNIT. ALSO, THE OVERLOAD INDICATOR POPPED. REPLACED THE NR 15 SLAT ACTSDR CA990303011Actuator · jammed(CAN) AFTER LANDING, NR 7 RIGHT SPOILER STAYED UP. ACTUATOR REPLACED.SDR AALA990166Mount · crackedTUL - FOUND NR 1 SLAT ACTUATOR OUTBOARD MOUNT CRACKED (INBOARD PIECE). INSTALLED NEW SLAT ACTUATOR OUTBOARD MOUNT. (M)SDR AU990062Actuator · faulty(AUS) LEFT NR 2 LEADING EDGE SLAT OUTBOARD ACTUATOR FAULTY.SDR 99ZZZM270Actuator · frozenDURING CRUISE AT FL100 ENCOUNTERED FLAP PROBLEM. AIR TURN BACK. MAINTENANCE FOUND THE NR 5 LEADING EDGE ACTUATOR FROZEN. MAINTENANCE REPLACED ACTUATOR AND OPS CHECKED GOOD. (M)SDR 99FDEA00033Actuator · failedTOTAL HYD SYS A FAILURE AT GEAR UP AFT T/O. BOTH FLUID A SWITCH OFF. ENG SHUTDOWN. REMOVED AND REPLACED NR 4 ACTUATOR IAW MM 27-81-22 PG 401.SDR DL72S990172Bracket · crackedREF E - 2 LETTER CHECK TPA, NR 8 SLAT ACT MOUNT BRACKETS CRACKED AT I/B AND O/B SIDES. INSTALLED DOUBLERS PER M/M 57-20-21.SDR AU990146Gear · corroded(AUS) NR 3 OUTBOARD AND NR 4 INBOARD LEADING EDGE SLAT ROTARY ACTUATORS CONTAINED INTERNAL CORROSION ON THE RING GEAR BEARING SURFACES AND THE PLANET GEAR P/N 256T2152. FOUND DURING VISUAL INSPECTION IAW ER B76-27-80-27 (AD/B767/095). PART TC: 51,949.SDR 99UAL900025Actuator · failedUNABLE TO RETRACT NR 5 SLAT, NOTICEABLE YAW. RETURNED TO DTW. *S/D* REPLACED NR 5 LEADING EDGE SLAT ACTUATOR, SYSTEM OPS CHECKS OK.SDR 99UAL900026Actuator · failedON EXTENSION OF FLAPS NR 5 KRUEGER FLAP DID NOT EXTEND. AMBER LIGHT ON FORWARD PANEL REMAINED ON. SECOND OFFICERS PANEL INDICATED NO EXTENSION. YAW WAS PRESENT IN CONTROLS. MISSED APPROACH WAS ACCOMPLISHED. *S/D* REPLACED LEADING EDGE FLAP ACTUATOR, SYSTSDR CALA9900056Bracket · crackedLEFT WING NR 1 L/E KRUEGER FLAP ACTUATOR I/B MOUNT BRACKET IS CRACKED .375 INCH. REMOVED BRACKET, FABRICATED AND INSTALLED NEW BRACKET PER SRM 51-10-1.SDR CALA9900050Mount · crackedLEFT WING NR 2 KRUEGER FLAP ACTUATOR INBOARD MOUNT CRACKED AT TOP (1). REMOVED, FABRICATED AND INSTALLED BRACKET PER SRM 51-10-1.SDR DL72L990034Bracket · crackedTHE ACTUATOR SUPPORT BRACKET DOUBLERS WERE FOUND CRACKED FOR THE NR 7 SLAT. THE CRACKS ARE TYPICAL OF BAC S/B 727-57- 0130. THE BRACKETS WERE MODIFIED PER THE INSTRUCTIONS OF THE S/B AND DOCUMENTED PER ER/A 366431-14.SDR 98FDEA00771Actuator · malfunctionedWITH FLAPS RETRACT AS A/C ACCEL THRU 270 KIAS, AMBER LEAD EDGE LIGHT ILLUM ON 2ND OFFICER AUXILIARY PNL AND A/C ROLL CONTROL WAS AFFECTED. ANTI ICE WAS ON. BELOW 250 KIAS ALL IND WERE NORM, FLAP EXTENSION AND LAND, ALL APPROPRIATE CK LIST WERE COMPLETE. *S/SDR DL72W982652Bolt · missingON APPROACH, LEADING EDGE FLAP NR 3 UNSAFE HAD AMBER LIGHT, ON GO-AROUND FLAPS WENT GREEN. SAFE INDICATION ON LANDING. AFTER LANDING FLAPS TO 25 DEGREES, FLAP INDICATION WENT TO AMBER. FOUND ACTUATOR DISCONNECTED FROM FLAP, BOLT MISSING. DAMAGE TO FLAP COSDR DL72S982614Doubler · crackedWING FIXED LEADING EDGE, NR 8 SLAT ACTUTOR SUPPORT BRACKET REPAIR FOR CRACKED DOUBLER. THE OUTBD SUPPORT BRACKET DOUBLER FOR THE NR 8 SLAT WAS FOUND CRACKED. THE INBD AND OUTBD ACTUATOR BRACKETS FOR THE NR 8 SLAT WERE REPAIRED/MODIFIED PER THE REQUIREMENTS OSDR CA981230036Actuator · cracked(CAN) FLAP ACTUATOR DUST COVER FOUND DAMAGED. NO REPORTED FLAP OPERATION SNAGS. PART TC: 5,015.SDR DL72S982564Actuator · leakingAIRCRAFT LOST 'A SYSTEM HYDRAULICS WHILE TAXING TO THE GATE AFTER LANDING IN CVG. MTC FOUND THAT THE NUMBER 7 LEADING EDGE SLAT ACTUATOR HAD FAILED. REPLACED ACTUATOR AND BOTH HYDRAULIC PUMPS.SDR DL73K982498Actuator · failedLEADING EDGE AMBER LIGHT ON SLAT NR 5. REPLACED NR 5 SLAT AND ACTUATOR.SDR AWXA9800229Actuator · malfunctionedCABIN FLOORBEAM STA 696 LBL 63 FLOORBEAM WEB IS CRACKED, MARKED NR 38. RESEARCHED, NOT A REPAIR IN THE SRM MAPPED AREA AND SENT TO ENGINEERING REF LOG 5082720.SDR CALA9802122Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 LEADING EDGE FLAP ACTUATOR MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-10-2 AND 51-30-7.SDR DL72W982445Actuator · damagedNR 3 L/E SLAT ACTUATOR CASE FAILURE, RESULTING IN LOSS OF A-SYS HYD POWER. REPLACED ACTUATOR.SDR CALA9802111Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN I/B AND O/B BRACKETS AT LT WING NR 2 LE FLAP ACTUATOR MOUNT. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-2, FIGURE 1.SDR SWAA982941Actuator · failedRETURNED TO DAL DUE TO NR 3 SLAT STUCK IN TRANSIT POSITION, VISUALLY CONTINUED PARTIALLY EXTENED IN FLAPS 1/5 POS. WITH T/E FLAPS AT POS 15 ALL LEADING EDGE SLATS WENT FULL EXTEND. REMOVED AND REPLACED NR 3 SLAT ACTUATOR PER M/M. LEAK CK OK. REMOVED AND RESDR 98FDEA00711Actuator · failedWHILE RETRACTING FLAPS AFTER T/O, NR 6 LED FAILED TO RETRACT. TRIED LOWERING FLAPS TO 2 DEG AND THEN RETRACTING BACK TO FULLY UP POSITION AND NR 6 LED STILL FAILED TO RETRACT. REMOVED AND REPLACED NR 6 SLAT ACT IAW MM 27-81-32, OPS CK NORMAL.SDR SWAA982988Actuator · failedAFTER TAKEOFF, NR 4 L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO SDF AND MADE AN UNEVENTFUL LANDING. REPLACED NR 4 L/E SLAT ACTUATOR PER BOEING M/M.SDR DL72S982389Actuator · failedA-SYS HYD FAILURE ON APPROACH. FOUND THE NR 4 L/E SLAT ACT FAILED. REPLACED SAME.SDR CALA9802073Bracket · crackedINSPECTION FOUND TWO .5 INCH CRACKS IN NR 6 LE FLAP O/B ACTUATOR MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-20-1, FIGURE 18.SDR CA981130013Actuator · failed(CAN) UNABLE TO ARM SPOILERS ON APPROACH, QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT. REPLACED AUTO SPOILER ACTUATOR.SDR CALA9802028Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN O/B LOWER END OF SUPPORT BRACKET WHERE LT WING NR 1 L/E FLAP ACTUATOR MOUNTS INSIDE LEADING EDGE. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2 AND 51-20-2 FIGURE 7.SDR CALA9802011Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN INBOARD SUPPORT BRACKET AT LOWER END WHERE LT WING NR 1 L/E FLAP ACTUATOR IS MOUNTED. A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 51-30-2, PAGE 3.SDR DL72K982236Fitting · crackedO/B SUPPORT FOR ACTUATOR FITTING LOBE CRACKED AT NR 7 SLAT. REPAIRED PER MM 57-42-0.SDR DHL9871520CAngle · crackedAT C-CHECK, LEFT WING NR 2 SLAT ACTUATOR COVER DOOR BOTH ATTACH ANGLE I/B AND O/B ARE CRACKED AT FWD END. REMOVED AND REPLACED ATTACH ANGLES PER SRM 51-40-4, 11 INCHES LONG. N/R 1112SDR SWAA982649Actuator · inopRETURNED TO HOU DUE TO THE INABILITY TO RETRACT NR 6 L/E SLAT. REPLACED NR 6 SLAT ACTUATOR PER BOEING M/M.SDR DL72S982225Bracket · crackedREF. SHIP 545 TPA LTR. CHECK C2 10/28/98, NO. 6 L/E FLAP ACTUATOR SUPPORT BOX FOUND CRACKED AT UPPER I/B ANGLE. REPAIRED PER MM 57-20-21 PG. 811SDR DL72W982173Support · crackedNR 1 LE FLAP ACT SUPPORT BOX CRACKED AT UPPER IB CORNER. REPAIRED PER MM 57-21-21.SDR USAABB98108Actuator · stiffLAX - FLT 86 - AFTER TAKEOFF, CREW RECEIVED EICAS MESSAGE 'SLAT DISAGREE' WITH SLATS STUCK HALFWAY UP. FLIGHT DIVERTED TO LAX. MAINTENANCE AT LAX COULD NOT DUPLICATE THE PROBLEM AND REPLACED THE FSEU AS A PRECAUTION. SUBSEQUENTLY, IN PIT ON 10/20/98, EN ROUTESDR ARWA981019Actuator · inopL/E TRANS LIGHT ON, AFTER SLAT/FLAP RETRACTION. FLAPS RECYCLED, LIGHT REMAINED ON, AIRFRAME VIBRATES SLIGHTLY WITH FLAPS RETRACTED. SLAT DEGREE IND SHOWS 1-2 DEGREE EXTENSION WITH SLAT UP. AFTER LANDING L/E TRANS LIGHT EXTINGUISHED WHEN FLAPS RETRACTED. RESDR DL72L982142Support · crackedTHE DOUBLERS FOR THE NR 7 SLAT ACTUATOR SUPPORT STRUCTURE WERE FOUND WITH THE TYPICAL CRACKS PER BAC S/B 727-57-0130, REV 2. THE CRACKED DOUBLERS WERE REPAIRED/MODIFIED PER THE REQUIREMENTS OF THE S/B. THE REPAIR WAS DOCUMENTED PER ER/A 365879-14AD.SDR SWAA982521Fitting · corrodedDURING SCHEDULED D-CHECK, FOUND CORRODED NR 5 SLAT ACTUATOR FITTING, I/B RIB HAS A PITTING CORRODED IN ROD END ATTACH HOLE. REMOVED AND REPLACED PER BOEING SRM.SDR DL72S982129Bracket · crackedTHE O/B ACTUATOR SUPPORT BRACKETS ON THE NR 2 AND NR 7 SLATS WERE FOUND WITH TYPICAL CRACKS IN THE WEB AND DOUBLER ASSY. THE I/B AND O/B ACTUATOR SUPPORT BRACKETS WERE REPAIRED/ MODIFIED PER THE REQUIREMENTS OF BAC S/B 727-57-0130, REV 2. THE REPAIRS WERE DOSDR TWAA9816301Actuator · wornTHE RT WING LE SLATS EXTENDED ONLY HALF WAY. LT WING SLATS EXTENDED NORMALLY. ACFT HAD PRONOUNCED ROLL TENDENCY. LANDED WITH SLATS RETRACTED. REPLACED BOTH RT WING SLAT ACTUATORS. CHECK-C 4-24-98 STL.SDR DL72S982074Bracket · crackedWING NR 1 SLAT ACTUATOR SUPPORT BRACKET, REPAIR FOR CRACKED WEB AND DOUBLER. THE NR 1 SLAT OUTBD ACTUATOR SUPPORT BRACKET WAS FOUND WITH THE WEB AND DOUBLER CRACKED. BOTH THE INBD AND OUTBD BRACKETS WERE MODIFIED PER BAC S/B 727-57-0130. THE REPAIR WAS DOCUSDR 98UAL900484Actuator · failedNUMBER 6 LEADING EDGE FLAP WOULD NOT RETRACT FROM FULL-DOWN POSITION. NO CONTROL PROBLEMS REPORTED. RETURNED TO DEN. *S/D* REPLACED NR 6 LE FLAP ACTUATOR. SYSTEM OPS CHECKS OK.SDR DHL9871526CFitting · crackedAT C-CHECK, RT WING LEADING EDGE THE NR 6 L/E FLAP ACTUATOR HINGE UPPER SUPPORT FITTING IS CRACKED AT O/B FLANGE ATTACH FASTENERS. REMOVED AND REPLACED FITTING PER SRM 51-30-2. N/R 2034SDR DHL9871522CFitting · crackedAT C-CHECK, LEFT FRONT SPAR NR 3 SLAT ACTUATOR I/B SUPPORT FITTING IS CRACKED AT TOOLING HOLE. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-10-1. N/R 1113
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