JASC 5754
Service difficulty reports · 17,344
Reports filed under 5754 · Leading Edge Devices, 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 = '5754' 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 = '5754' 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 DALA2015102206322Rib · corrodedCORROSION ON RIB HOLE XIS 83, XIS 136 AND XIS 186 AT LT SLAT PANEL NR 1. RIB HOLES WERE REPAIRED IAW SRM 57-02, PAR 9.SDR SWAA2015111145985Skin · crackedLEFT WING NR 1 SLAT NOSE SKIN CRACKED AT ACTUATOR ATTACH FITTING, INBD ROW, 3RD FASTENER FROM LE. REPAIRED SKIN IAW SRM.SDR SWAA2015111145984Skin · crackedRIGHT WING NR 8 SLAT NOSE SKIN CRACKED AT ACTUATOR ATTACH FITTING, INBD ROW, 3RD FASTENER FROM LE. REPAIRED SKIN IAW SRM.SDR SWAA2015102245254Skin · crackedRIGHT WING NR 8 SLAT, LOWER LE SLAT NOSE SKIN CRACKED AT THE ACTUATOR RIB, OTBD TWO FASTENERS. REPAIRED SLAT SKIN IAW SRM.SDR DALA2015102006263Rib · damagedWEAR ON HOLE OF RIB XOS 530 AT LT SLAT PANEL NR 5 ON REF CARD 2700-4224-LH-05. CARD 18, ZONE 11. HOLES RIB BS XOS 530 AT LT SLAT PANEL NR 5 WERE REPAIRED IAW SRM 57-02 PAR 9.SDR DALA2015102006262Rib · corrodedCORROSION ON RIB HOLES XOS 288 AT LT SLAT PANEL NR 2. HOLES BS XOS 288 AT LT SLAT PANEL NR 2 WERE REPAIRED IAW SRM 57-02 PAR 9.SDR DALA2015102106289Rib · corrodedCORROSION ON RIB HOLES XOS 198 AND XOS 288 AT RT SLAT PANEL NR 2. RIB XOS=198 AND XOS=288 AT RT SLAT PANEL NR 2 WERE REPAIRED IAW SRM 57-02, PAR. 9.SDR DALA2015102006266Slat Track · wornWEAR ON SLAT TRACK NR 13 AT LT WING. LT SLAT TRACK NR 13 WAS REPLACED IAW AMM MD-88 27-80-01. RII COMPLETED.SDR ASAA2015101713867Skin · delaminatedRT WING NR 4 L/E SLAT INBD T/E WEDGE HAS POSSIBLE AREA OF DELAMINATION AT EDGE, MARKED. ACFT GROUNDED. REPAIRED RT WING NR 4 SLAT L/E IB T/E WEDGE AT EDGE IAW SRM 51-70-10-2R-4 REPAIR 4.SDR SWAA2015111145961Slat Track · crackedRIGHT WING FIXED LE OTBD SIDE OF NR 8 SLAT TRACK CRACKED. R & R NR 8 SLAT TRACK IAW SRM.SDR SWAA2015102045080Wedge · delaminatedRIGHT WING, NR 5 SLAT WEDGE DELAMINATED ON INBD END. REPAIRED WEDGE IAW DWG.SDR AALA20151016002Wedge · dentedRIGHT WING NR 13 SLAT, UPPER WEDGE SURFACE FOUND DENTED. REPAIR CARRIED OUT IAW SRM 57-43-02-2R PROCEDURE 2 REPAIR 2 & SRM 51-70-10 REPAIR 4 FIG 201.SDR AALA20151016001Wedge · dentedRIGHT WING NR 12 SLAT, UPPER WEDGE SURFACE FOUND DENTED. REPAIR CARRIED OUT IAW SRM 57-43-02-2R PROCEDURE 2 REPAIR 2 & SRM 51-70-10 REPAIR 4 FIG 201.SDR SWAA2015102745384Support Angle · crackedLEFT WING NR 1 SLAT ON NR 2 AUXILIARY TRACK, OTBD SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.SDR AALA201510159009Slat · delaminatedLEFT WING NR 4 SLAT HAS DELAMINATION AT INBD TE BOTTOM SIDE. REPLACED SLAT IAW 19L52027002.SDR AALA201510159008Slat · delaminatedRIGHT WING NR 8 SLAT HAS DELAMINATION AT PREVIOUS REPAIRS, 3 EACH, AREA 1. APPROX 70" FROM INBD EDGE. AREA 2, 19" FROM INBD EDGE. AREA 3, 13" FROM OTBD END & 2" FROM TE. R & R NR 8 SLAT IAW 19L52027002.SDR DALA2015101406202Skin · dentedRT INBD MAIN FLAP AFT OF NR 6 FLAP TRACK, FLAP LWR T/E WEDGE SKIN HAS DENTS. ACCOMPLSHED REPAIR OF THE DISCREPANT DENTS ON RT INBD MAIN FLAP AFT OF NR 6 FLAP LOWER T/E WEDGE SKIN IAW SRM 51-70-10, PN 113N2603.SDR DALA2015100906029Panel · damagedNR 6 L/E SLAT LOWER AFT CLOSURE PANEL HAS 2 HOLES/DAMAGED NEAR INBD EDGE. REMOVED NR 6 SLAT LOWER INBD CLOSURE PANEL AND ROUTED TO SHOP FOR REPAIR PN 114N3012-16. INSTALLED PERMENENT REPAIR TO CLOSURE PANEL IAW ERA 510361-14MA, REV ORIGINAL INSTALLED CLOSURE SDR SWAA2015102345283Slat · delaminatedRIGHT WING NR 5 SLAT DELAMINATED AT AFT EDGE OTBD END. REPAIRED NR 5 SLAT IAW AMM.SDR AALA20151007019Slat · delaminatedLEFT WING NR 7 SLAT FOUND DELAMINATED. LT WING NR 7 SLAT REPAIRED IAW SRM 57-43-02. SLAT REINSTALLED & AMM OPERATIONAL TEST ACCOMPLISHED IAW AMM 27-81-00, 27-81-10.SDR DALA2015100806027Clevis · corrodedLEFT WING NR 3 SLAT OTBD AUXILIARY TRACK AFT CLEVIS HARDWARE IS RUSTED 77-07. R & R HARDWARE AT NR 3 SLAT OTBD AUXILIARY TRACK AFT CLEVIS IAW AMM 27-81-13-024-006, AND AMM 27-81-13-424-008 AND AMM 27-81-12-424-021.SDR DALA2015100806026Clevis · corrodedRIGHT WING NR 8 SLAT INBD AUXILIARY TRACK AFT CLEVIS HARDWARE IS RUSTED 77-17. R & R HARDWARE AT RT WING NR 8 SLAT INBD AUXILIARY TRACK AFT CLEVIS IAW AMM 27-81-13-024-006, AMM 27-81-13-424-008 AND AMM 27-81-02-424-021.SDR DALA2015100806025Track · corrodedLEFT WING NR 4 SLAT OTBD AUXILIARY TRACK AFT CLEVIS HARDWARE IS RUSTED 77-08. R & R HARDWARE AT LT WING NR 4 SLAT OTBD AUXILIARY TRACK AFT CLEVIS IAW AMM 27-81-02-424-021 AND AMM 27-81-13-024-006.SDR DALA2015100705986Skin · damagedMISSING MATERIAL ON SLAT 3 INBD EDGE AT T/E AREA ON RT WING. PERFORMED REPAIR ON SLAT 3 INBD EDGE AT T/E AREA ON RT WING IAW PRI ER/A 539117-14, REV 0 AND ER/A 539117-14.SDR DALA2015100906036Skin · dentedWHILE PERFORMING INSPECTION , FOUND A DENT ON LT WING NR 2 SLAT T/E WEDGE UPPER SURFACE. REPAIRED IAW SRM 51- 70-10, REPAIR 2.SDR DALA2015101106052Skin · crackedCRACKS ON LT SLAT NR 2 INNER SKIN AT MID RIB. CRACKS ON SLAT PANEL NR 2 LT WERE REPAIRED IAW SRM 57-01, FIG 3.SDR DALA2015101106051Skin · crackedCRACKED LOWER SKIN OF RT SLAT NR 2 AT MID RIB. CRACK ON SLAT PANEL NR 2 RT WAS REPAIRED IAW SRM 57-01, FIG 3, SHEET 2.SDR SWAA2015101544958Skin · crackedRIGHT WING LOWER SURFACE OF THE LE, NR 7 SLAT NOSE SKIN, CRACKED AT SLAT BS 322.71. REPAIRED SKIN IAW SRM.SDR U5QA201510020071Skin · damagedBIRD STRIKE PRIOR TO LANDING. DAMAGE TO RT LE & FLAP, BEING INSPECTED & MAPPED FOR DAMAGE AT THIS TIME.SDR DALA2015100105897Structure · crackedWHILE PERFORMING WC 5750-01176-1201, SLAT INSPECTION, FOUND A CRACK IN THE FIXED L/E UNDER SLAT NR 4. PERFORMED OPTION A TIME LIMITED REPAIR.SDR SWAA2015112346333Angle · crackedLEFT WING INBD SIDE OF NR 12 SLAT TRACK ON SLAT SIDE, ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.SDR DALA2015100205906Skin · dentedLT WING NR 2 SLAT T/E WEDGE UPPER SURFACE 33" FROM INBD EDGE, 1.5" FWD OF AFT EDGE, SKIN HAS DENT. FOUND AND MEASURED 1 EA DENT ON LT WING NR 2 SLAT T/E WEDGE UPPER SURFACE 33" FROM INBD EDGE 1.5" FWD OF AFT EDGE, MEASURED 1 EA DENT A=1.130, WIDE Y=.014, DESDR DALA2015093005884Skin · dentedLEFT WING NR 4 SLAT T/E WEDGE UPPER SURFACE 9" FROM INBD EDGE , 4" FWD OF AFT EDGE, SKIN HAS DENT. ACCOMPLISHED PERMANENT REPAIR ON LT WING NR 4 SLAT T/E WEDGE UPPER SURFACE 9" FROM INBD EDGE, 4" FWD OF AFT EDGE IAW SRM 51-70-10, PN 114N4005-229, SN 000071, TSDR DALA2015093005880Skin · dentedLT WING NR 3 SLAT T/E WEDGE UPPER SURFACE 8" FROM OTBD EDGE, 8.5" FWD OF AFT EDGE, SKIN HAS DENT. ACCOMPLISHED PERMANENT REPAIR ON LT WING NR 3 SLAT T/E WEDGE UPPER SURFACE 8" FROM OTBD EDGE 8.5" FWD OF AFT EDGE IAW SRM 51-70-10, PN 114N4004-215, SN 000071. SDR WX0A2015100172909Slat · damagedRIGHT NR 5 SLAT DAMAGED. R & R NR 5 RT SLAT IAW AMM 27-80=-01-4-0.SDR AALA201510209013Attach Fitting · worn3S CHECK, RT WING NR 4 SLAT ATTACH FITTING BOLT ANTI-ROTATION STOP WORN. REPAIRED FITTING IAW SRM 57-40-00-201-3.SDR SWAA2015100944733Skin · crackedRIGHT WING LE NR 8 SLAT SKIN CRACKED AT ACTUATOR RIB STATION 451.97. REPAIRED SKIN IAW SRM.SDR SWAA2015100144444Skin · crackedRIGHT WING NR 6 LE SLAT, LOWER SURFACE SKIN AT ACTUATOR ATTACH FITTING, CRACKED AT INBD CTR FASTENER HOLE. REPAIRED SKIN IAW ACO.SDR AALA201509299017Skin · delaminatedNUMBER 3 SLAT LOWER SURFACE OTBD SIDE, 4" FROM OTBD EDGE HAS AREA OF DELAMINATION, APPROX 3" X 4" AGAINST EXTERIOR DOUBLER. R & R NR 3 SLAT IAW AMM 27-81-04-024-001. OPERATIONAL & FUNCTIONAL CHECKED GOOD.SDR AALA201509299015Skin · delaminatedNUMBER 2 SLAT UPPER SURFACE INBD EDGE HAS AREA OF DELAMINATION, APPROX .5" IN DEPTH BY 2" LONG. R & R NR 2 SLAT IAW AMM 27-81-04-024-001. OPERATIONAL & FUNCTIONAL CHECKED GOOD.SDR SWAA2015112546462Angle · crackedRIGHT WING INBD SIDE OF NR 12 SLAT TRACK ANGLE CRACKED. R & R ANGLE BUMPER IAW SRM & DWG.SDR SWAA2015101645018Skin · delaminatedLEFT WING OTBD LE NR 2 SLAT, AFT WEDGE UPPER SURFACE SKIN DELAMINATED AT INBD END. REPAIRED SKIN IAW SRM.SDR IPXA2015092593937Skin · puncturedRIGHT WING, NR 4, SLAT LOWER EXTERIOR SKIN PUNCTURED OTBD OF MID TRACK. REPAIRED NR 4 SLAT EXTERIOR SKIN IAW EA 011-5754-01-A5988, REV I/R AND EO MD11-5750-58844-A.SDR SWAA2015092944397Skin · crackedRIGHT WING NR 8 SLAT LOWER SKIN, CRACKED AT THE ACTUATOR ATTACH RIB. REPAIRED SKIN IAW SRM.SDR SWAA2015110245590Flap · crackedRIGHT WING LE KRUEGER FLAP AREA, CRACKED ON BS 208. REPAIRED KRUEGER FLAP IAW SRM.SDR SWAA2015091844041Slat · delaminatedRIGHT WING NR 5 LE SLAT DELAMINATED ON INBD & OTBD CORNERS. R & R NR 5 SLAT IAW MM.SDR SWAA2015091844040Slat · delaminatedLEFT WING NR 2 LE SLAT DELAMINATED ON OTBD CORNER. R & R NR 2 SLAT IAW AMM.SDR AALA20150914014Slat · wornNUMBER 8 SLAT INBD AFT CORNER OF THE TE WEDGE HAS WORN AN APPROX 0.3 INCH GROOVE INTO LE OF THE WING. CHECK OUT X-RAY INSPECTION IAW NTM PT2 51-00-01, RESULT NO WATER FOUND. DAMAGED AREA TRIMMED OFF IAW SRM 51-70-10 REPAIR GENERAL PARA 7. HFEC INSPECTION CHSDR SWAA2015091543891Roller · damagedDIVERSION & DECLARED EMER, LE FLAPS TRANSIT LIGHT ILLUMINATED ON TAKEOFF. FOUND NR 4 SLAT, INBD AUXILIARY TRACK ROLLER DAMAGED, CAUSING RESTRICTED MOVEMENT OF NR 4 SLAT. R & R ROLLER IAW MM.SDR SWAA2015101344869Skin · crackedRIGHT WING NR 6 SLAT, LOWER SKIN CRACKED AT FASTENER AT ACTUATOR ROD END ATTACH POINT. REPAIRED SKIN IAW SRM.
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