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 AALA20091015TUL02Slat · corrodedNUMBER 1 LEADING EDGE SLAT HAS CORROSION AROUND FASTENER HEAD AT 30 INCHES FROM INBOARD EDGE. REMOVED CORROSION PER MM 51-00-53 AND INSTALLED DOUBLER PER AARD 57-43-00-1.SDR AALA20091015TUL01Skin · corrodedPREVIOUSLY BLENDED CORROSION AREA ON NUMBER 1 LEADING EDGE SLAT 30 INCHES FROM INBOARD EDGE IS BEYOND LIMITS PER SRM 57-43-01 DETAIL V. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR FDEA200910143601Angle · crackedNR 8 SLAT LWR AFT CHORD ANGLE IS CRACKED AT INBD UP STOP PAD. FABRICATED ANGLE REPAIR FROM EXTRUSION BAC 1514-1559 2024T3-511, PO NR 29111160, DIM: 11" AND OTHER 6" (2 ANGLES) IAW SRM 51-40-4 FIG 1. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED REPAIR ANGLESSDR FDEA200910143576Angle · crackedNR 1 SLAT LWR AFT CHORD ANGLE IS CRACKED BELOW ACTUATOR. REMOVED ACCESS PANEL IAW SRM 51-30-2, CUT OUT DAMAGED AREA IAW SRM 51-10-1 REV 101, FABRICATED NEW LOWER CHORD, AND 1 EACH SPLICER IAW SRM 57-50-2 FIG 2 AND 51-40-4 FIG 1 REV 101, TREATED AND PRIMED SDR ASAA0976801Skin · crackedRIGHT WING NR 5 SLAT EXTERNAL SKIN CRACKED AT ACTUATOR MOUNT LOCATION APPROX .25. REPAIRED RIGHT WING NR 5 SLAT.SDR ASAA0976800Skin · crackedRIGHT WING NR 6 SLAT EXTERNAL SKIN CRACKED AT ACTUATOR MOUNT LOCATION APPROX .25. REPAIRED RIGHT WING NR 6 SLAT.SDR ASAA0976799Skin · crackedNR 2 SLAT EXTERIOR SKIN AT ACTUATOR HAS CRACK COMING OUT OF RIVET. REPAIRED NR 2 SLAT EXTERIOR SKIN AT ACTUATOR FITTING.SDR IPXA09657654Skin · crackedRHW NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS792.24 RHW NR 10 SLAT AT OSS792.24 OTBD NOSE SKIN REPAIR AS SRM 57-43-01-2R2 FIG 201 REV45. ORG MAT'L CLAD 7075T6-0063IN, ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7.25 INCH BY 9 INCH SDR IPXA09657653Skin · crackedRT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS724.24 RHW NR 10 SLAT AT OSS724.24 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01 -2R2 FIG 201 REV 45. ORG MAT'L CLAD 7075T6-0063IN, ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7.125 INSDR IPXA09657652Skin · crackedLT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS572.9. LHW NR 4 SLAT AT OSS572.9 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 SIG 201 REV 45. ORG MAT'L CLAD 7075T6-0063IN, ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7.5 I NCH BY 8.SDR IPXA09657651Skin · crackedLHW NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS792.24 LHW NR 3 SLAT AT OSS792.24 OTBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. ORG MAT'L CLAD 7075T-600631N ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7 INCH BY 9 INCHSDR IPXA09657650Skin · crackedLHW NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACK JUST AT OSS724.24. LHW NR 3 SLAT AT OSS 724.24 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. ORG MAT'L CLAD 7075T6-00631N ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 7 INCH BY 9 INCH TSDR IPXA09657649Skin · crackedLHW NR 2 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACK AT OSS872, LHW NR 2 SLAT OSS872 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. ORG MAT'L 7075T6-00631N CRACK LENGTH .125 INCH DAMAGED SKIN CUTOUT 6.875 INCH BY 9.125 INCH THIS REPAIR IS CLASSDR AALA20091013TUL07Slat · crackedNUMBER 7 SLAT HAS A CRACK AROUND A FASTENER MID-SPAN. REMOVED DAMAGED AREA AND INSTALLED FLUSH-DOUBLER PER SRM-57-43-01.SDR SWAA096594Wedge · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.SDR SWAA096593Wedge · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 1 SLAT T/E WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.SDR ASAA0946916Skin · crackedNR 3 SLAT SKIN CRACKED AT INBOARD AFT RIVET ON THE INBOARD END OF THE SLAT. REMOVED DAMAGED AREA, FABBED FILLER & DOUBLER & INSTALLED REPAIR PARTS IAW B737 400 SRM 57 43 01 FIG 207 REP 6.SDR USAA2009102892913Skin · delaminatedSAL - Q2 - MAJOR REPAIR - DELAMINATION ON NR 5 SLAT UPPER SKIN SURFACE BETWEEN SLAT STA SS124.40 TO SS134.40. REPAIRED NR 5 SLAT UPPER SKIN SURFACE BETWEEN SLAT STA SS124.40 TO SS134.40 IAW B737 SRM 51-70-10 REPAIR 4.SDR DXTA2009101203810Skin · damagedON LANDING ROLL OUT AT APPROXIMATELY 80 KTS, ACFT STRUCK DEER. DAMAGE TO WING LEADING EDGE (RT). DRILLED & REMOVED FLAP ISLAND TOP SKIN & LOWER AFT SKIN DRILLED & REMOVED FLAP ISLAND OUTBD FLAP TRACK AND AF R1B SECTION REMOVED RT OUTBD FLAP INBD BELCRANK FOR SDR IPXA09557741Skin · delaminatedINSPECTION TYPE:C2 WHILE WORKING REPAIR ASSESSMENT FOUND PREVIOUS REPAIR (SEG NR 470-W3-02) ON NR 3 SLAT T/E WEDGE UPPER SURFACE AT OSS 467 TO OSS 475.5 DISBONDED AT UPPER EDGE. REPAIRED PER SRM 51-70-10.SDR AALA20091009TUL02Skin · corrodedRIGHT WING NUMBER 8 SLAT SKIN CORRODED AT OUTBOARD MAIN TRACK ATTACH FITTING. REMOVED CORROSION AND INSTALLED DOUBLER UNDER AARD 57-43-00-1.SDR AALA20091009TUL01Skin · crackedNUMBER 9 SLAT LOWER SKIN CRACKED AT INBOARD MAIN TRACK ATTACH FITTING. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 57-43-00-1.SDR SWAA096442Slat · crackedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 8 SLAT CRACKED. REPAIRED SLAT PER SRM.SDR SWAA096411Wedge · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING NR 3 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA096385AWedge · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING NR 3 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR FDEA200910063493Angle · crackedNR 7 SLAT AFT LWR CHORD ANGLE IS CRACKED 2 PLACES BELOW T-DUCT. REMOVED ACCESS PANEL IAW B 727 SRM 51-30-2. REMOVED LOWER CHORD ANGLE IAW SRM 51-30-2. FABRICATED A NEW LOWER CHORD AND 1 EA SPLICE IAW SRM 57-50-2 FIG 2, AND 51-40-4 FIG 1. TREATED AND PRIMED IASDR FDEA200910063492Skin · crackedNR 7 SLAT INBD HOOK AFT MOUNTING FASTENER IS LOOSE AND EDGE OF COUNTERSINK HAS CRACK INDICATION. HFEC INSPECTED AREA IAW NDTM 51-00-00 PART 6 FIG 23 VERIFIED CRACK ENDS AT EXISTING FASTENER HOLE. FABRICATED DOUBLER FOR NR 7 SLAT INBD AREA IAW SRM 57-50-3 FIGSDR FDEA200910063488Panel · crackedLT WING NR 1 SLAT, INBD NOSE COVE PANEL HAS A 1" CRACK DIRECTLY FWD OF THE INBD DRIVE TRACK. REMOVED NR 1 SLAT SEAL RETAINER FOR REPAIR ACCESS. REMOVED CRACKED COVE PANEL IAW SRM 51-40-02. FABRICATED NEW COVE PANEL IAW MAT ID SHT7075-T6, .050" THICK, BATCH NSDR FDEA200910063486Skin · delaminatedDELAMINATION ON SLAT NR 6, TRAILING WEDGE, ABOUT 30" FROM INBD EDGE. ACCOMPLISHED REPAIR OF RT WING, NR 6 L/E SLAT, T/E WEDGE, ABOUT 30" FROM INBD END IAW EA F5750-133518, SRM 51-70-10, REPAIR NR 4, AND SRM 57-43-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOSDR IPXA09657680Panel · delaminatedINSPECTION TYPE:C RT WING NR 7 SLAT LOWER CLOSURE PANEL THE EXISTING REPAIR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 45.SDR IPXA09657668Skin · crackedNR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS 572.77 CRACK LENGTH 0.125 INCH. RHW NR 9 SLAT AT OSS572.77 INBD NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV45 ORG MATERIAL CLAD 7075T6-0.063 IN ORG CRACK LENGTH .125 INCH DAMAGED SKIN CUSDR IPXA09657667Skin · crackedNR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED JUST AT OSS641.62 CRACK LENGTH 0.125 INCH. RHW NR 9 SLAT AT OSS641.62 OTBD NOSE SKIN REPAIRED AS PER SRM 57-43 -01-2R2 FIG 201 REV45. ORG MATERIAL CLAD 7075T6-0.063 IN ORG, CRACK LENGTH .125 INCH DAMAGED SKIN SDR ABXR200910050032Skin · crackedDURING A HEAVY MX INSP EVENT THE NR6 KRUGER LE FLAP WAS FOUND WITH 2 (EA) CRACKS MID AND OUT BOARD. THE FLAP WAS REMOVED AND REPLACED. ITEM RETURNED TO SERVICE.SDR SWAA096350Wedge · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 3 SLAT I/B END T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR USAA2009100892738Wedge · delaminatedCLT - Q6 - MAJOR REPAIR - NR 2 SLAT DELAMINATED AT INBOARD END OF TRAILING EDGE WEDGE SKIN. REPAIRED NR 2 SLAT AT INBOARD END OF TRAILING EDGE WEDGE SKIN IAW B737 SRM 51-70-10.SDR IPXA09M57574Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ 283-W3-02 LT NR 3 SLAT L/E BETWEEN STA W344-XDS408 EXISTING REPAIR NOT CORRELATED TO SRM 57-40-01 FIG 201 REPAIR 11. FASTENERS C/O BLINDS INSTALLED SOLIDS. REMOVED SKIN INSERT FOR INSPECTION REF MD11 SRM 51-35-01. FOUND SDR USAA2009100292691Slat · delaminatedCLT - Q5 - MAJOR REPAIR - DELAMINATION ON NR 5 SLAT AT LEADING EDGE UPPER INBOARD END OF SLAT. REPAIRED NR 5 SLAT AT LEADING EDGE UPPER INBOARD END OF SLAT IAW B737-400 SRM 51-70-10 REPAIR 4.SDR USAA2009100692714Wedge · debondedCLT - Q5 - MAJOR REPAIR - NR 2 SLAT TRAILING EDGE WEDGE DISBONDED AT OUTBOARD END OF UPPER SURFACE. REPAIRED NR 2 SLAT TRAILING EDGE WEDGE AT OUTBOARD END OF UPPER SURFACE IAW SRM 51-70-10.SDR SWAA096148Slat · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RT WING NR 6 SLAT I/B AFT UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.SDR SWAA096143Slat · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RT WING L/E NR 4 SLAT O/B LOWER SURFACE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR SWAA096129Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 SLAT LOWER SURFACE CRACKED. REPAIRED SLAT PER SRM.SDR SWAA096128Wedge · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING NR 1 SLAT O/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA096123Slat · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RT WING NR 4 SLAT O/B CORNER DELAMINATED. REPAIRED SLAT PER SRM.SDR SWAA096120Wedge · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING NR 3 SLAT O/B TRAILING EDGE WEDGE DELAMINATED. REPAIRED WEDGE PER MM.SDR SWAA096115Slat · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 SLAT CRACKED. REPAIRED SLAT PER ER.SDR SWAA096065Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND RT WING NR 8 SLAT LOWER SKIN CRACKED AT ACTUATOR. REPAIRED PER EA.SDR AALA20090925TUL03Skin · corrodedNUMBER 1 SLAT HAS CORROSION 30 INCHES FROM INBOARD END ON SLAT SKIN. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER PER SRM 57-43-01-2R.SDR AALA20090925TUL02Skin · crackedLEFT WING NUMBER 1 SLAT SKIN IS CRACKED OUT FROM FASTENERS 2 FEET FROM OUTBOARD EDGE. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER PER SRM 57-43-01-2R.SDR AALA20090924TUL18Skin · corrodedCORROSION ON RIGHT NUMBER 7 SLAT ON UPPER SKIN IN AREA OF OUTBOARD MAIN TRACK. INSTALLED FLUSH DOUBLER REPAIR UNDER AARD 57-43-00-1.SDR AALA20090924TUL19Skin · crackedNUMBER 7 SLAT HAD CORROSION AT LEADING EDGE SKIN SURFACE APPROXIMATELY 24 INCHES IN FROM OUTBOARD END AT FASTENER. CUT AWAY CORROSION AND CRACK DAMAGE AT APPROXIMATELY 24 INCHES FROM OUTBOARD END AND INSTALLED A FLUSH REPAIR PER SRM 57-43-01-2R.
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