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 DL757100162Skin · wornNR 8 SLAT T/E WEDGE LOWER SURFACE HAS WEAR MARKS. REPAIRED AT SAA SAT ON N/R CARD 140657.SDR NOCA06309Structure · crackedNR 7 L/E SLAT, INTERIOR (AFT SIDE) T/E STRUCTURE HAS TWO ANGLE CLIPS CRACKED, HAS APPROX 42 INCHES AND 52.5 INCHES I/B OF SLAT EDGE. MANUFACTURED ANGLES PER DRAWING 114T3166 AND INSTALLED ON SLAT.SDR USAA2009110993067Slat · delaminatedCLT - MAJOR REPAIR - Q3 CHECK - DELAMINATION ON NR 2 SLAT AT THE OUTBOARD TRAILING EDGE AREA. REPAIRED NR 2 SLAT AT THE OUTBOARD TRAILING EDGE AREA IAW B737 SRM 51-70-10 REPAIR 4.SDR SWAA097067Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND NR 7 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.SDR SWAA096970Skin · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING NR 4 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.SDR FDEA200911043849Skin · delaminatedLT WING, NR5 L/E SLAT, T/E WEDGE, OTBD END, IS DELAMINATED. REPAIRED LT WING, NR 5 L/E SLAT, IAW SRM 57-43-02; BONDED DOUBLER REPAIR. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.SDR HNAA2010022400037Flap Track · corrodedLT WING FLAP TRACK NR 1 IS CORRODED. LT FLAP TRACK NR 1 IS R & R IAW AMM 57-50-11.SDR HNAA2010022400036Flap Track · corrodedRT WING FLAP TRACK NR 2 IS CORRODED. R & R FLAP TRACK WITH NEW, ON RT HANDWING IAW AMM 57-50-26.SDR AALA20091108TUL12Skin · crackedUPPER SKIN CRACKED AT HI-LOC HOLE AT OUTBOARD MAIN TRACK DRIVE RIB. INSTALLED DOUBLER PER SRM 57-43-01-2R 2 AND AARD 57-43-00-1.SDR AALA20091103TUL08Skin · corrodedLEFT WING NUMBER 2 SLAT HAS CORROSION ON INBOARD TRAINING EDGE LOWER SURFACE 2 INCHES FROM AFT EDGE. INSTALLED 350 DEGREE HOT BOND REPAIR PER SRM 51-70-10-2R 4.SDR FDEA200911033805Skin · dentedRT WING NR 1 SLAT LWR SKIN FOUND DENT. RT WING NR1 SLAT LWR SKIN DENT REPAIR SCHEME CARRIED OUT IAW SRM 57-40-01, REV 41. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 108. RT WING NR1 SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-20-5 REV 64 FOUND SASDR SWAA097065Slat · delaminatedDURING SCHEDULED 12Y CHECK, FOUND NR 7 L/E SLAT WEDGE DELAMINATED. REPAIRED SLAT PER SRM.SDR CALA2009110400667Skin · crackedB767-57-3-0130 RT WING NR 9 SLAT EXT SURFACE 2 EA RIVET HOLES SURROUNDING FOUND CRACK. RT WING NR 9 SLAT OUTER SKIN SURFACE 2 RIVET HOLES CRACKED. REPAIRED AS PER SRM 57-43-01 REPAIR 2 FIG 201 AT 0SS572.549 AND OSS568.14 9 AND FORM 44.0008 ATT ITEM 1-18 ACCOSDR CALA2009110400666Skin · crackedLT WING NR 3 SLAT OUTER SURFACE LOWER AREA 3EA RIVET HOLES SURROUNDING AREA FOUND CRACK. LT WING NR 3 SLAT OUTER SKIN SURFACE LOWER AREA 3 RIVET HOLES CRACKED AREA REPAIRED AS PER SRM57-43-01 FIG 201 REPAIR 2 AT OSS723.941 AND OSS722.441 AND FORM 44.0008 ATT SDR ASAA0946937Skin · delaminatedNR 3 SLAT DELAMINATED ON I/B UPPER SURFACE. BONDED DOUBLER AND FILLER.SDR ASAA0946933Skin · crackedRIGHT WING NR 6 SLAT LOWER AFT EXTERNAL SKIN CRACKED AT RIVET FSS 603. REPAIRED SKIN.SDR WRLA20091101277Rib · crackedCRACK - RIB, STA XOS 1003 NR 16 SLAT TRACK IN LT WING FIXED L/E COMPARTMENT L=0.375 INCH, QTY=1EA. REPLACED THE RIB IAW MD11 SRM 51-33-01 REV 41.SDR IPXA09657853Skin · crackedINSPECTION TYPE:ETOP RHW NR 9 SLAT OTBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED RHW NR 9 SLAT OTBD AREA AT OSS641.62 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV45 ORG MAT'L IS CLAD7075T6-0063IN CRACK LENGTH IS 0.090 INCH DAMAGED CUTOUT IS 7.7SDR IPXA09657852Skin · crackedINSPECTION TYPE:ETOP RHW NR 9 SLAT INBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED RHW NR 9 SLAT INBD AREA AT OSS572.9 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV45 ORG MAT'L IS CLAD7075T6-0063 IN CRACK LENGTH IS 0.125IN DAMAGED CUTOUT IS 7.25 ISDR IPXA09657850Skin · crackedINSPECTION TYPE:ETOP LHW NR 4 SLAT INBD NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED LHW NR 4 SLAT INBD AREA AT OSS572.9 NOSE SKIN REPAIRED AS PER SRM 57-43-01 2R2 FIG 201 REV45 ORG MAT'L IS CLAD 7075T6-0063 IN, CRACK LENGTH IS 0.090IN. DAMAGED CUTOUT IS 7.SDR FDEA200910303726Rib · crackedRT WING - NR 3 L/E SLAT RIB AT XOS 495 FOUND CRACKS. REPLACED AS PER AMM 27-80-30-4 REVISION 64. OPERATIONAL CHECK AND ADJUSTMENT CHECK CARRIED OUT AS PER AMM 27-80-30-5 REVISION 64. REFER TO SNRM N01125 FOR DETAILS.SDR FDEA200910303724Rib · damagedRT WING - NR 3 L/E SLAT RIB AT XOS 489 FASTENER HOLES ELONGATED. REPLACED AS PER AMM 27-80-30-4 REVISION 64. OPERATION AND ADJUSTMENT TEST CARRIED OUT AS PER AMM 27-80-30-5 REVISION 64. REFER TO SNRM N01125 FOR DETAILS.SDR SWAA096808Wedge · delaminatedDURING SCHEDULED 18Y CHECK, FOUND LT WING NR 2 SLAT, I/B TRAILING EDGE WEDGE UPPER SURFACE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA096783Skin · crackedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 6 SLAT SKIN LOWER SURFACE CRACKED. REPAIRED SKIN PER SRM.SDR AALA20091028TUL01Slat · damagedRIGHT WING NUMBER 2 SLAT RUBSTRIP LOOSE ON DE-ICE TUBE ACCESS. BLENDED SMOOTH WORN AREA, ALODINED AREA AND FILLED AREAS WITH DEVCON F. RE-ATTACHED RUB STRIP PER ESO 80559 DATED 10/28/09.SDR ASAA0946947Slat · delaminatedNR 5 SLAT UPPER O/B TRAILING EDGE IS DELAMINATED. REPAIRED SLAT.SDR USAA2009110993063Slat · delaminatedBFM - MAJOR REPAIR - C1 CHECK - DELAMINATION ON NR 1 SLAT AT WS 990.2. REPAIRED NR 1 SLAT AT WS 990.2. IAW B767 SRM 57-43-02.SDR ASAA0946928Wedge · chafedLEFT WING L/E SLAT NR 3 T/E WEDGE I/B AFT CORNER CHAFED. REPAIRED CHAFE DAMAGE AT I/B AFT CORNER OF SLAT NR 3 T/E WEDGE.SDR FDEA200910273686Skin · misrepairedPREVIUSLY INSTALLED FLASH REPAIR AT NR 7 L/E SLAT, EXTERNAL SKIN, NOT INSTALLED PER SRM. CUT AND REMOVED EXISTING REPAIR ON NR 7 L/E SLAT EXTERNAL SKIN IAW SRM 57-43-01 FIG 201 REPAIR 1 , FABRICATED REPAIR PLATE ON TRAV. T9/ 806985AND DOUBLER IN TRAV T9/ 8SDR CA091029004Seal · deteriorated(CAN) ON COMPLETION OF A REGULAR SLAT TRACK LUBE, A SLIGHT `CLICKING` SOUND WAS NOTED DURING THE FINAL STEP OF A SLAT OPS CHECK. UPON INSPECTION IT WAS NOTED THAT THE SOUND WAS BEING CAUSED BY: 1- RT WING OTBD SEAL ON NR 4 SLAT IS WORN AND CRACKED. 2- RT WINGSDR FDEA200910263662Skin · damagedNR 3 LEADING EDGE SLAT LOWER SURFACE 4 EACH FASTENER HOLES AT XOS 488 ELONGATED. SLAT ASSEMBLY REPLACED AS PER AMM 27-80-30-4 REVISION 64. OPERATION AND ADJUSTMENT CHECK CARRIED OUT AS PER AMM 27-80-30-5 REVISION 64. REFER TO SNRM N01125 FOR DETAILSSDR IPXA09657865Slat · chafedINSPECTION TYPE:C RHW - NR 9 SLAT OTBD UPPER EDGE FOUND CHAFE. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REV 45, REPAIR 4, FIG 202 SHEET 8.SDR IPXA09657837Slat · chafedINSPECTION TYPE:C LEFT WING NR 4 SLAT I/B UPPER EDGE FOUND CHAFE. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10, REV 45 REPAIR 4 FIG 202 SHEET 8 AND SHEET 9 NOTES.SDR SWAA096770Structure · puncturedFUEL LEAK FOUND, PRIOR TO PUSH, IN LEFT WING COMING FROM WEEP HOLE, (APPROX. 5 FT INBOARD FROM FUEL VENT). FOUND NR 1 SLAT INBOARD SLAT CAN PUNCTURED. REMOVED AND REPLACED SLAT CAN.SDR IPXA09657836Web · crackedINSPECTION TYPE:C LEFT WING NR 3 SLAT O/B NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED (CRACK 0.090 INCH). LEFT WING NR 3 SLAT O/B AREA AT OSS792.3 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45, ORG MATERIAL IS CLAD 7075T6-0.063IN, CRACK LENGTH SDR IPXA09657835Web · crackedINSPECTION TYPE:C LEFT WING NR 3 SLAT I/B NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED (CRACK .0625 INCH). LEFT WING NR 3 SLAT I/B AREA AT OSS724.24 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 ORG MATERIAL IS CLAD 7075T6-0.063IN, CRACK LENGTH SDR IPXA09657834Web · crackedINSPECTION TYPE:C RIGHT WING NR 10 SLAT I/B NOSE SUPPORT WEB SKIN RIVET HOLE FOUND CRACKED (CRACK 0.090 INCH). RIGHT WING NR 10 SLAT I/B AREA AT OSS724.24 NOSE SKIN REPAIRED AS PER SRM 57- 43-01-2R2 FIG 201 REV 45 ORG. MATERIAL IS CLAD 7075T6-0.063IN, CRACK LSDR UALA2009102203297Slat · damagedRIGHT L/E INBOARD, NEXT TO PYLON HAS BIRD STRIKE. DENT DAMAGE NOTED. MEASURED AT 5 INCHES BY 2.5 INCHES, 3-8 INCHES DEEP. REMOVED SLAT AND ROUTED TO SHOP. REPLACED NR 1 SLAT.SDR SWAA096839Slat · crackedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 4 SLAT CRACKED. REMOVED AND REPLACED SLAT PER MM.SDR ASAA0996848Wedge · chafedNR 8 SLAT I/B END UPPER T/E WEDGE LOWER SURFACE IS CHAFED. REMOVED, REPAIRED AND RE-INSTALLED NR 8 SLAT.SDR ASAA0996847Skin · chafedNR 8 SLAT IS CHAFED ON UPPER T/E LOWER SURFACE O/B END. REPAIRED NR 8 SLAT LOWER SURFACE.SDR DL757100281Skin · separatedTAP TEST INDICATES SKIN SEPARATION ON LT WING SLAT T/E WEDGES, OTBD END , T/E DIRECTLY IN LINE WITH THE MAIN TRACK. REMOVED DAMAGED SECTION AND REPAIRED AT SAA SAT REF NON ROUTINE CARD 143409.SDR AALA20091020TUL02Panel · crackedNUMBER 10 SLAT AT FORWARD END OF INBOARD DRIVE TRACK, ADJACENT TO PREVIOUS REPAIR SLAT SKIN, SHOWS CRACK INDICATION. STOP-DRILLED CRACK AND INSTALLED EXTERNAL DOUBLER PER AARD-57-43-00-4.SDR ASAA0996806Wedge · chafedLEFT WING NR 4 SLAT LWR SIDE OF T/E WEDGE HAS AREAS THAT ARE CHAFED. REPAIRED PER EA.SDR FDEA200910163595Rib · crackedNR 3 SLAT HAS 2 CRACKED RIBS, INBD AND OTBD OF ACTUATOR FWD ATTACHMENT. REMOVED CRACKED RIBS, FABRICATED NEW RIBS, HEAT TREATED RIBS TO T4 CONDITION IAW FASI FORM 2-37153-801 REV A AND INSTALLED IAW SRM 51-30-2 AND 51-20-1.SDR AALA20091015TUL08Slat · corrodedNUMBER 10 SLAT INBOARD SIDE CORRODED AROUND RIVET. REMOVED CORRODED AREA AND INSTALLED FLUSH-DOUBLER PER AARD-57-43-00-1.SDR AALA20091015TUL07Slat · corrodedCORROSION FOUND ON NUMBER 10 SLAT 102 INCHES FROM THE INBOARD END. INSTALLED FLUSH-DOUBLER PER SRM 57-43-01-2R.SDR AALA20091015TUL06Slat · delaminatedINBOARD AFT EDGE OF NUMBER 4 SLAT IS DELAMINATED, SLAT WEDGE. REPLACED AND INSTALLED NEW TRAILING EDGE PER ESO 90248. INSTALLED COVE COVERS PER ESO 90248.SDR AALA20091015TUL04Slat · corrodedNUMBER 1 LEADING EDGE SLAT HAS CORROSION AT FASTENER HEAD 65 INCHES FROM OUTBOARD EDGE. REMOVED CORROSION PER MM 51-00-53 AND INSTALLED DOUBLER PER AARD 57-43-00-1.SDR AALA20091015TUL03Access Panel · crackedNUMBER 1 SLAT AFT SIDE ACCESS PANEL IS CRACKED AT FASTENER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER AARD 57-43-00-4.
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