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 AALA20090924TUL17Skin · corrodedCORROSION ON NUMBER 7 SLAT ON UPPER SKIN IN AREA OF OUTBOARD AUXILIARY TRACK. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER 57-43-00-1.SDR AALA20090924TUL16Skin · corrodedCORROSION ON NUMBER 7 SLAT IN AREA OF CENTER RIB ON UPPER SKIN. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER 57-43-00-1.SDR AALA20090924TUL15Skin · corrodedCORROSION ON NUMBER 7 SLAT SKIN IN AREA OF INBOARD AUXILIARY TRACK. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER 57-43-00-1.SDR AALA20090923TUL02Skin · corrodedNUMBER 8 SLAT SKIN CORRODED 36 INCHES FROM INBOARD END. INSTALLED DOUBLER.SDR AALA20090923TUL01Skin · corrodedNUMBER EIGHT SLAT SKIN CORRODED APPROXIMATELY 46 INCHES FROM INBOARD END. INSTALLED DOUBLER.SDR AALA20090924TUL13Skin · corrodedTHE LEFT WING NUMBER 2 SLAT TOP SKIN HAS CORROSION AT THE RIVET 16 INCHES FROM THE SLAT BACK END AND 75.5 INCHES FROM THE OUTBOARD END APPROXIMATELY WING STATION 635. REMOVED DAMAGE SKIN AND INSTALLED DOUBLER PER SRM 57-43-01-2R 2.SDR AALA20090923TUL09Slat · corrodedRIGHT WING NUMBER 8 SLAT FASTENER 45 INCHES OUTBOARD FROM INBOARD END HAS CORROSION AROUND HEAD. INSTALLED FLUSH DOUBLER PER SRM 57-43-01-2R.SDR AALA20090923TUL05Skin · corrodedNUMBER 10 SLAT HAS DEEP BLEND AND BLIND FASTENER 28 INCHES FROM OUTBOARD END ON UPPER SKIN. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 57-43-01.SDR AALA20090923TUL04Skin · corrodedCORROSION ON NUMBER 10 SLAT LOWER SKIN FORWARD OF OUTBOARD AUXILIARY TRACK. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 57-43-01.SDR AALA20090923TUL03Skin · corrodedNUMBER 10 SLAT HAS DEEP BLEND WITH BLIND FASTENER ON UPPER SKIN 29.5 INCHES FROM INBOARD END. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 57-34-10.SDR USAA2009092492617Wedge · debondedCLT - C5 - MAJOR REPAIR - NR 3 SLAT WEDGE DISBONDING ON INBOARD END AT UPPER AND LOWER SIDES. REPAIRED NR 3 SLAT WEDGE AT INBOARD END AT UPPER AND LOWER SIDES IAW B737 SRM 51-70-10 REPAIR 4.SDR ASAA0946654Skin · chafedNR 3 SLAT UPPER TRAILING EDGE LOWER SURFACE IS CHAFED FROM CONTACT WITH FIXED LEADING EDGE. REPAIRED NR 3 SLAT TRAILING EDGE PER SRM 57 43 02.SDR ASAA0946653Wedge · chafedNR 4 SLAT T/E WEDGE LOWER SURFACE IS CHAFED. REPAIRED NR 4 SLAT T/E WEDGE PER SRM 57 43 02.SDR IPXA09M57706Structure · misrepairedINSPECTION TYPE:4C REPAIR SURVEY SEQUENCE NR 278-W3-06 NOT CORRELATED TO MD11 SRM FIG 201 57 -40-01 SHT 1 THRU 5 DUE TO 4 EA BLIND FASTENERS INSTALLED INSTEAD OF HL 326-6 PJN. NO ACCESS TO INSTALL FASTENERS. REPAIRED PER EA NR 011-5730-01-A2043 ISSUE A AND ESDR IPXA09657511Slat · damagedINSPECTION TYPE:C RT WING NR 9 SLAT O/B EDGE FOUND DAMAGED. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 202 SHT 8 REV 45.SDR USAA2009092392605Wedge · delaminatedCLT - Q6 - MAJOR REPAIR - DELAMINATION ON NR 2 SLAT WEDGE AT OUTBOARD UPPER EDGES. REPAIRED NR 2 SLAT WEDGE AT OUTBOARD UPPER EDGES IAW B737 SRM 51-70-10/R4.SDR IPXA09657523Panel · delaminatedINSPECTION TYPE:C LT WING NR 6 SLAT LOWER CLOSURE PANEL. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 45.SDR IPXA09657475Skin · crackedINSPECTION TYPE:C LEFT WING NR 3 SLAT I/B NOSE SKIN RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. LEFT WING NR 3 SLAT I/B AREA AT OSS 724.61 NOSE SKIN CUT 9 X 7.125 INCHES REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. THIS REPAIR CLASSIFIED AS MAJORSDR IPXA09657474Skin · crackedINSPECTION TYPE:C RIGHT WING NR 9 SLAT O/B NOSE SKIN RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. RIGHT WING NR 9 SLAT O/B AREA AT OSS 641.49 NOSE SKIN CUT 7.375 X 9 INCHES REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45, THIS REPAIR CLASSIFIED AS MAJOSDR IPXA09657472Skin · crackedINSPECTION TYPE:C RIGHT WING NR 9 SLAT I/B NOSE SKIN RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. RIGHT WING NR 9 SLAT I/B AREA AT OSS 573.25 NOSE SKIN CUT 7.375 X 9 INCHES REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. THIS REPAIR CLASSIFIED AS MAJSDR IPXA09657471Skin · crackedINSPECTION TYPE:N/A RIGHT WING NR 10 SLAT I/B NOSE SKIN RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. RIGHT WING NR 10 SLAT I/B AREA AT OSS 724.6 NOSE SKIN CUT 7.125 X 9 INCH REPAIR AS PER SRM 57-43-01-2R2 FIG 201 REV 45, THIS REPAIR CLASSIFIED AS MAJORSDR SWAA096008Slat · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RT WING NR 5 SLAT O/B AFT UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.SDR IPXA09657516Doubler · delaminatedINSPECTION TYPE:C LT WING NR 3 SLAT LOWER CLOSURE PANEL THE EXISTING REPAIR PATCH DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 45.SDR IPXA09M57729Skin · misrepairedINSPECTION TYPE:4C REPAIR SURVEY SEQUENCE NR 278-W3-03 LT NR 1 SLAT EXISTING REPAIR EXTERNAL DOUBLER DOES NOT CORRELATE TO SRM AND ALSO OVER COUNTER SUNK DOUBLER. REMOVED DOUBLER, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIRS IAW SAA EA 011-5730-01-A2038 ISDR IPXA09557519Wedge · debondedINSPECTION TYPE:C2 LT WING L/E NR 4 SLAT HAS DISBOND ON UPPER SURFACE T/E WEDGE 50.5 FROM O/B END 7 INCHES FROM T/E. REMOVED AND REPLACED NR 4 SLAT ASSY IAW MM 27-81-02-4.SDR ASAA0946747Wedge · delaminatedNR 2 SLAT TRAILING EDGE WEDGE IS DELAMINATED AT THE O/B EDGE. REMOVED DELAMINATED AREA SKIN AND CORE FABBED REPAIR PARTS AND BONDED REPAIR.SDR FDEA200909173319Doubler · gougedRT WING INBD FORE FLAP OTBD L/E HAS DEEP GOUGE FROM LONG SCREW IN WING LWR T/E. STOP DRILLED DEEP GOUGE AT RT WING INBD FORE FLAP OTBD L/E IAW SRM 51-10-1 REV 101. HFEC INSPECTED AREA IAW NDTM 51-00-00, FIG 23 PART 6, NO DEFECTS NOTED. FABRICATED REPAIR PSDR ASAA0996636Structure · chafedWING RIGHT NR 5 SLAT LOWER T/E IS CHAFED IN SEVERAL AREAS. REPLACED NR 5 SLAT LOWER T/E.SDR AALA20090917TUL01Skin · damagedNUMBER 4 SLAT WEDGE DAMAGED AT THE TRAILING EDGE, INBOARD END. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER EXTERNAL REPAIR PER SRM 51-70-10-2R.SDR USAA2009102292849Slat · delaminatedSAL - Q2 - MAJOR REPAIR - DELAMINATION ON NR 6 SLAT UPPER EXTERNAL SKIN SURFACE AT INBOARD SIDE BETWEEN SS 254.4 TO SS 267.15. REPAIRED NR 6 SLAT UPPER EXTERNAL SKIN SURFACE AT INBOARD SIDE BETWEEN SS 254.4 TO SS 267.15 IAW B737 SRM 51-70-10.SDR USAA2009102192824Skin · delaminatedSAL - Q2 - MAJOR REPAIR - DELAMINATION ON NR 5 SLAT SKIN, OUTBOARD UPPER & LOWER SURFACES BETWEEN SLAT STA 241.27 TO SLAT STA 254.27. REPAIRED NR 5 SLAT SKIN, OUTBOARD UPPER & LOWER SURFACES BETWEEN SLAT STA 241.27 TO SLAT STA 254.27 IAW B737 SRM 51-70-10.SDR AALA20090915TUL06Skin · crackedCRACK ON NUMBER 2 SLAT INBOARD DRIVE TRACK COVE SKIN AT FASTENER OUTBOARD SIDE OF TRACK. INSTALLED DOUBLER PER AARD 57-43-00-4.SDR AALA20090914TUL01Bushing · wornNUMBER 5 SLAT IN BOARD KNUCKLE FITTING WORN. REPLACED WORN BUSHINGS IN KNUCKLE FITTING PER ESO-80117.SDR AALA20090911TUL09Rib · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES A CRACK AT 2ND FROM OUTBOARD RIB ON RIGHT WING NUMBER 5 SLAT AT NUMBER 14 SLAT TRACK ATTACHMENT. REMOVED 2ND FROM OUTBOARD ATTACH FITTING AND INSTALLED NEW ATTACH FITTING PER / ESO 80117.SDR AALA20090911TUL08Rib · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES A CRACK AT OUTBOARD RIB ON RIGHT WING NUMBER 5 SLAT AT NUMBER 15 SLAT TRACK ATTACHMENT. INSTALLED NEW ATTACH FITTING PER ESO 80117.SDR AALA20090911TUL07Rib · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES A CRACK AT OUTBOARD RIB ON LEFT WING NUMBER 5 SLAT AT NUMBER 15 SLAT TRACK ATTACHMENT. REPLACED CRACKED OUTBOARD RIB AT NUMBER 15 TRACK ATTACHMENT POSITION PER ESO 80117.SDR USAA2009091692544Skin · crackedCLT - Q4 - MAJOR REPAIR - CRACK IN NR 5 SLAT LOWER SKIN 35 INCHES FROM INBOARD END. REPLACED NR 5 SLAT IAW JOB CARD 03C40227004.SDR SWAA095873Skin · crackedDURING SCHEDULED SPV, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED. REPAIRED SLAT PER SRM.SDR SWAA095864Skin · crackedDURING SCHEDULED 20Y CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED. REPAIRED SLAT SKIN PER SRM.SDR SWAA095854Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND NR 5 L/E SLAT LOWER SKIN CRACKED. REPAIRED SLAT PER SRM.SDR SWAA095829Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND RT WING O/B LEADING EDGE NR 6 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR ASAA0996580Slat · chafedRIGHT WING NR 8 SLAT LWR T/E IS CHAFED. REPAIRED RIGHT WING NR 8 SLAT LWR T/E.SDR SWAA095828Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.SDR SWAA095820Wedge · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE DELAMINATED. REPAIRED SLAT PER MM.SDR ASAA0996582Slat · chafedLEFT WING NR 3 SLAT CHAFED ALONG LWR T/E. REPAIRED LT WING NR 3 SLAT ALONG LWR T/E.SDR SWAA095763Slat · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RT WING NR 6 SLAT DELAMINATED. REPAIRED SLAT PER SRM.SDR USAA2009090992416Slat · debondedPHX - OVERNIGHT - MAJOR REPAIR - NR 5 WING LEADING EDGE SLAT DISBONDED AND BREAKING OFF BETWEEN WS 125 TO WS 180. REPLACED NR 5 WING LEADING EDGE SLAT IAW B737 MM 27-81-01-401.SDR SWAA095762Slat · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RT WING NR 6 SLAT DELAMINATED. REPAIRED SLAT PER MM.SDR SWAA095761Wedge · delaminatedDURING SCHEDULED 18Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER MM.SDR SWAA095750Wedge · delaminatedDURING SCHEDULED 20Y, FOUND RT WING NR 5 SLAT O/B LEADING EDGE I/B UPPER TRAILING EDGE WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.
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