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 SWAA103228Slat · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 3 SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR SWAA103227Slat · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED. REPAIRED SLAT PER MM.SDR FDEA201006021777Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 617.30. REMOVED CORROSION FROM COVE PANEL IAW 51-10-02. BLENDED AREA L= 39", W=1.0", D=.011, MAT .050 REMAINING .039 OUT OF LIMITS IAW SRM 57-43-01, FIG 101, DET VI. FABRICATED COVE PANEL ON TRAVELER NR T10/83SDR FDEA201006021776Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 605.3. REMOVED CORROSION FROM COVE PANEL IAW SRM 51-10-02. BLENDED AREA L=3.5" W=1.0" D=.011, ORIG. MAT .050 REMAINING .039" OUT OF LIMITS IAW 57-43-01 DET VI. FABRICATED COVE PANEL ON TRAVELER NR T10/837838. MINOSDR FDEA201006021775Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 574.80. REMOVED CORROSION FROM COVE PANEL IAW SRM 51-10-02. BLENDED AREA L=24" W= 1.0" D=.010". ORIG. MAT. .050 REMAINING .040 OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DET VII. FABRICATED COVE PANEL ON TRAVELER NR SDR FDEA201006021774Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 677.5. REMOVED CORROSION FROM COVE PANEL IAW SRM 51-10-02. BLENDED AREA L=24.0" W=1.0" D=.009. ORIGINAL MAT. .050 REMAINING .O41 OUT OF LIMITS IAW SRM 57-43-01 FIG. DET VI. FABRICATED COVE PANEL ON TRAVELER NR TSDR FDEA201006021773Panel · corrodedLT WING NR 2 SLAT COVE PANEL CORRODED AT OSS 665.5. REMOVED CORROSION FROM COVE PNL IAW SRM 51-10-02. BLEND OUTDIM=3.0" LX 1,0"W X .010" D, ORIGINAL MAT'L. THICK .050, MAT'L AFTER REWORK .04" FOUND OUT OF LIMITS IAW. SRM 57-43-01 FIG. 101 DET. VI. FABRICSDR FDEA201006021770Angle · corrodedLT WING SLAT NR 2 LOWER EDGE HAS CORROSION UNDER THE SEALANT AND INTERNAL FROM OTBD EDGE TO INBD END. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=130" W=.75" D=.012" ORIG, MAT. .063 REMAINING .051 OUT OF LIMITS IAW SRM 57-43-02 FIG 101 DET II. R & R NSDR FDEA201006021763Rib · crackedLT WING - NR 2 SLAT OTBD RIB FOUND CRACKED. R & R IAW SRM 51-31-01 VOLUME II. NEW RIB FABRICATED IAW DWG ARB1647, REV C. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.SDR AALA20100601TUL03Skin · crackedCRACK IN THE NUMBER 10 SLAT COVE SKIN OUTBOARD DRIVE TRACK. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER AARD 57-43-00-4.SDR IPXA10B60337Skin · dentedINSPECTION TYPE:C, DMI D411229 - LT INBD MID FLAP BOTTOM SKIN DENT. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10, REPAIR 4, FIG 201, SHEET 3, REV 56.SDR SWAA103162Skin · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING NR 6 SLAT SKIN CRACKED. REPAIRED SKIN PER AAR EA.SDR AALA20100531TUL04Skin · corrodedCORROSION ON NUMBER NINE SLAT UPPER SKIN 30 INCHES FROM INBOARD END AT REAR SPAR. INSTALLED DOUBLER.SDR AALA20100531TUL01Slat · corrodedNUMBER NINE SLAT CORRODED. ACCOMPLISHED DOUBLER REPAIR.SDR ABXA201006010083Slat Track · corrodedNR 11 SLAT I/B AND O/B MAIN TRACKS HAVE SURFACE CORROSION ON UPPER AND LOWER SURFACES. REMOVED AND REPLACED NR 11 SLAT MAIN TRACKS IAW B767 AMM 27-81-54-4. REMOVED AND REPLACED NR 11 SLAT IAW B767 AMM 27-81-02-4, OPS CHECK GOOD.SDR AALA20100528TUL02Skin · corrodedRIGHT WING CORROSION ON NUMBER 9 SLAT UPPER SKIN 30 INCHES FROM INBOARD END. RIGHT WING NUMBER 9 SLAT REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.SDR AALA20100528TUL01Skin · corrodedRIGHT WING NUMBER 9 SLAT CORRODED ON LOWER TRAILING EDGE SKIN AT INBOARD DRIVE. RIGHT WING NUMBER 9 SLAT REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.SDR AALA20100527TUL21Skin · corrodedCORROSION ON NUMBER 8 SLAT UPPER SKIN 67 INCHES FROM OUTBOARD END. INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20100527TUL20Skin · corrodedCORROSION ON NUMBER 8 SLAT UPPER SKIN 33 INCHES FROM INBOARD END. INSTALLED REPAIR DOUBLER PER SRM 57-43-01-2 AND AARD 57-43-00-1.SDR AALA20100527TUL11Rib · crackedRIGHT WING NUMBER 4 KRUEGER FLAP RIB CRACKED AT NUMBER 2 HINGE. RIGHT WING NUMBER 4 KRUEGER FLAP FABRICATED AND INSTALLED DOUBLERS AND FILLERS FOR PERMANENT REPAIR PER SRM 57-43-02-2R 2.SDR AALA20100527TUL09Skin · corrodedRIGHT WING NUMBER 7 SLAT CORRODED AT FASTENER ON UPPER SKIN AT INBOARD DRIVE TRACK. RIGHT WING NUMBER 7 SLAT REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.SDR AALA20100527TUL08Skin · corrodedRIGHT WING NUMBER 7 SLAT CORROSION ON UPPER SKIN 27 INCHES INBOARD OF FLUSH REPAIR. RIGHT WING NUMBER 7 SLAT REMOVED CORROSION AND INSTALLED DOUBLER PER AARD 57-43-00-1.SDR AALA20100527TUL07Skin · corrodedRIGHT WING NUMBER 8 SLAT CORROSION ON UPPER SKIN 33 INCHES FROM INBOARD END. RIGHT WING NUMBER 8 SLAT INSTALLED REPAIR DOUBLER PER SRM 57-43-01-2 AND AARD 57-43-00-1.SDR AALA20100527TUL06Skin · corrodedRIGHT WING NUMBER 8 SLAT CORROSION ON UPPER SKIN 67 INCHES FROM OUTBOARD END. RIGHT WING NUMBER 8 SLAT INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR SWAA103122Skin · crackedDURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 SLAT LOWER SKIN CRACKED. REPAIRED SLAT PER AAR EA.SDR FDEA201005271685Skin · corrodedNR 7 SLAT NOSE SKIN HAS DEEP PITTED AREAS AND IS CORRODED AT WS 369.50 TO 425.50. BLENDED CORROSION IAW SRM 51-10-02, REWORKED AREA DIMENSIONS = 35.0"L X 1.0"W X .019"D, ORIGINAL MAT'L THICKNESS .063", MAT'L AFTER REWORK .044", FOUND OUT OF LIMITS IAW SRMSDR FDEA201005271684Angle · corrodedRT WING SLAT NR 7 T/E HAS SEALANT CRACKED. REMOVED CRACKED SEALANT & FOUND CORROSION, REMOVED CORROSION, IAW SRM 51-10-02. REWORKED AREA = 12.0"L X 1.0"W X .023"D, ORIGINAL MAT'L .063" MAT'L AFTER REWORK .04", FOUND OUT OF LIMITS IAW SRM 57-43-02, FIG 101SDR FDEA201005271682Support Fitting · crackedLT WING - NR 1 L/E SLAT INBD EDGE FWD LOWER FASTENER SUPPORT FITTING FOUND CRACKED AFTER REMOVAL. LW NR1 L/E SLAT INBD EDGE FWD FASTENER SUPPORT FITTING R & R IAW SRM 51-33-01, REV 43. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201005271681Rib · crackedLT WING - NR 1 L/E SLAT INBD EDGE RIB FOUND CRACKED. LT WING NR1 L/E SLAT INBD EDGE RIB FABRICATED IAW DWG ARB 7128 REV L. RIB R & R IAW SRM 51-53-01, REV 43, LT NR1 SLAT ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-80-20-5, REV 66. FOUND SATISFACTORY. REPAISDR SWAA103105Slat · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT I/B T/E DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.SDR FDEA201005261659Angle · corrodedNR 3 SLAT HAS CORROSION BETWEEN UPPER SKIN ASSY & LOWER SKIN IN SEAM AREA. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREA L=1.5,W=1.0,D=.01 ORIG. MAT.063. REMAINING .053 OUT OF LIMITS IAW SRM 57-43-01 FIG.101 DET III. ACCOMPLISHED EA 5740-139134,WINGS L/E SDR FDEA201005251643Skin · misrepairedRT NR 1 L/E SLAT HAS A FLUSH DOUBLER REPAIR ON THE INBD L/E EXTERIOR, NR 1 TRACK VICINITY. EXISTING REPAIR AT RT NR1 L/E SLAT FLUSH DOUBLER REPAIR ON THE INBD L/E EXTERIOR, NR 1 TRACK VICINITY EVALUATED AND FOUND NOT IAW SRM REPAIR SCHEME. RT NR 1 SLAT R SDR VGQY201005250015Panel · crackedRIGHT WING L/E UPPER FIXED PANEL ADJ TO NR 15 KRUEGER FLAP FOUND PANEL CRACKED. REPAIR CARRIED OUT IAW SRM-51-40-15, REV 116.SDR IPXA10660207Skin · crackedINSPECTION TYPE:C, RT WIING NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT L/E OTBD AT OSS792.5 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRACK LENGTH IS 0.1440, DAMAGED CUTOUT IS 0.500" SDR IPXA10660206Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT L/E INBD AT OSS723.9 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRACK LENGTH IS 0.1625", DAMAGED CUTOUT IS 0.500" SDR IPXA10660205Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT L/E OTBD AT OSS641.9 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1460", DAMAGED CUTOUT IS 0.500" DIA,SDR IPXA10660204Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT L/E INBD AT OSS572.5 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1845", DAMAGED CUTOUT IS 0.500" DIASDR IPXA10660203Skin · crackedINSP TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT L/E OTBD AT OSS641.9 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRACK LENGTH IS 0.1530", DAMAGED CUTOUT IS 0.500" DIA. THISDR IPXA10660202Skin · crackedINSPECTION TYPE:C, LT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR4 SLAT L/E INBD AT OSS572.5 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1455", DAMAGED CUTOUT IS 0.500" DIA. SDR IPXA10660201Skin · crackedINSPECTION TYPE:C, LT WING NR3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT L/E OTBD AT OSS792.5 NOSE SKIN REPAIRED IAW RS R57-00-36739, EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1255", DAMAGED CUTOUT IS 0.468" DIA, THSDR IPXA10560090Wedge · chafedINSPECTION TYPE:C2, NR 3 SLAT T/E WEDGE LOWER SURFACE IS CHAFED AT 34 INCHES FROM INBD ABOVE INBD MAIN TRACK. (FOUND OUT OF LIMITS ON CARD 862188) REPAIRED NR 3 SLAT T/E WEDGE IAW SRM 51-70-10-2R-4 REPAIR 4 AND SRM 51-70-10-2R REPAIR GENERAL.SDR AALA20100520TUL08Slat · dentedRIGHT WING LEADING EDGE NUMBER 1 SLAT HAS A DENT. REWORKED DENTED AREA TO BE WITHIN LIMITS. DYE CHECKED AREA AND NO CRACKS FOUND PER ESO 80117. CLEARANCE TO INSTALL PANEL PER ESO 80117.SDR IPXA10560734Skin · gougedINSPECTION TYPE:C3, RT WING OTBD L/E BELL NOSE SKIN IS GOUGED AT OTBD SIDE OF OTBD TRACK CARRIDGE, APROX 5 INCHES LONG. REMOVED L/E PANEL. RECEIVED NEW L/E PANEL ALODINED AND PRIMED INSTALLED IAW 57-53-0-1A1, SRM51-40-08-0G, SRM 51-40-05-0G.SDR FDEA201005201595Angle · crackedNR 6 SLAT LOWER AFT T/E ANGLE IS CRACKED AT OTBD UPSTOP PAD. REMOVED ACCESS PANELS NR 6 SLAT IAW SRM 51-30-2, FABRICATED NEW T/E ANGLE. MATERIAL USED BAC1514-1559 2024T3511 PO 20035137 DIM 9' 6" LONG IAW SRM 57-50-2 FIG 2, 51-30-5 TREATED AND PRIMED IAWSDR FDEA201005201594Angle · crackedNR 8 SLAT LOWER T/E ANGLE IS CRACKED AT OTBD UPSTOP PAD. REMOVED NR 8 SLAT LOWER T/E ANGLE IAW SRM REV 102, 51-30-2. FABRICATED NEW ANGLE USING BAC1514-1559, 2024 T3511 86 1/4" LONG IAW SRM 51-30-5 AND 57-50-2 FIG 2. INSTALLED NEW ANGLE IAW 51-30-2.SDR AALA20100520TUL01Rib · crackedRIGHT NUMBER 5 SLAT OUTBOARD RIB IS CRACKED. REPLACED OUTBOARD DAMAGED RIB UNDER ESO 80117.SDR SWAA103018Slat · crackedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT CRACKED AT O/B EDGE. REPAIRED NR 6 SLAT PER SRM.SDR SWAA102990Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 4 SLAT UPPER WEDGE SKIN DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM.SDR AALA20100519TUL04Rib · wornEXCESSIVE PLAY IN OUTBOARD SLAT MOUNT KNUCKLE OF NUMBER 4 SLAT LEFT WING. REPLACED WORN OUTBOARD SLAT MOUNT RIB PER ESO 80117.SDR DALA1011530646Skin · dentedNR4 SLAT LOWER SURFACE HAS 2 EA DENTS. REMOVED DAMAGE, FABRICATED DOUBLER AND BONDED AT ST AEROSPACE SAT REF NON ROUTINE CARD 175296. (DL757101334).
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