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 FDEA201007202601Skin · wornRT WING NR1 SLAT ERODED ABOVE NR 2 PYLON. BLEND OUT (2) ERODED AREAS TO SMOOTH CONTOUR AND DAMAGE AREAS MAY DIMENSION ARE 1.1" X 1", PENETRANT TO HONEYCOMB 2. 3" X 0.7", (2) LAYERS DAMAGED, THEN REPAIR WITH FIBERGLASS AND RESIN COMPOUND (CURE AT 180 DEGREE SDR IPXA10561323Wedge · out of limitsINSPECTION TYPE:C2, NR 4 SLAT HAS OUT OF LIMIT DENTS (DUE TO CLOSE PROXIMITY) LOCATED ON T/E WEDGE UPPER SURFACE 45" FROM INBD END 2.25" FROM T/E. REPAIRED NR 4 SLAT T/E WEDGE IAW SRM 51-70-10-2R-4 AND SRM 51-70-10-2R-0.SDR FDEA201007202600Skin · wornLT WING NR1 SLAT ERODED ABOVE NR1 PYLON, BLEND OUT THE EROSION AREA TO SMOOTH CONTOUR AND MEASURED THE AREA MAX DIMENSION IS 4" * 0.9" AND (3) LAYERS DAMAGED, THEN REPAIRED WITH FIBERGLASS AND RESIN COMPOUND. (CURE AT 180 DEGREE F) IAW EA NR 6-5750-141608. RSDR FDEA201007202599Skin · crackedRT WING NR 1 SLAT L/E PREVIOUS REPAIR FILLER CRACKED. CONFIRMED NO SKIN CRACK BUT ONLY LIMITED TO FILLER FROM A "DENT" REPAIR. REMOVED RT NR 1 SLAT ASSY IAW AMM 27-80-11-4 2. CUT-OUT DAMAGED AREA 98MM X 84MM IAW SRM 57-42-11-3. NDI WAS COMPLETED THE CUT-OSDR SWAA104178Slat · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT LOWER T/E CRACKED. REPAIRED SLAT PER SRM.SDR SWAA104211Slat · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING NR 2 SLAT UPPER T/E DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR USAA2010090791932Skin · delaminatedSAL - Q4 - MAJOR REPAIR - DELAMINATION ON NR 3 SLAT INBOARD EDGE UPPER SKIN BETWEEN SLAT STA 12.25 TO 44.25. REPLACED NR 3 SLAT IAW JOB CARD 03C30227005.SDR HALA201007160303Support Bracket · crackedRT AILERON NR 1 SLAT DRIVE DOOR SUPPORT BRACKET CRACKED. DEFERRED AND TRANSCRIBED TO HAL LOG PAGE.SDR HALA201007160302Support Bracket · crackedLEFT NR 1 SLAT DRIVE DOOR SUPPORT BRACKET CRACKED. DEFERRED AND TRANSCRIBED TO HAL LOG PAGE 339060.SDR TAMF20100048SRib · corrodedDURING "SC3" CHECKS, INSPECTION FOUND CORROSION ON RIB, PN 114T2203-13, STA OSS 479.854 LT , REPAIR ACCOMPLISHED IAW EWO 767-57-064R0 AND MFG 1-1635744504.SDR FDEA201007152550Rib · misrepairedRT NR 1 SLAT INBD FACE AREA FOUND 01 EACH EXISTING REPAIR. EXISTING REPAIR AT RT NR 1 SLAT INBD FACE AREA EVALUATED AND FOUND NOT CONFORMING TO SRM. EXISTING REPAIR R & R WITH NEW REPAIR IAW SRM 57-00-01, FIG 4, VOL I, REV 96 AND EA 8-5750-140394 EO 8-5100-7SDR AALA20100714TUL06Rib · crackedRIGHT WING NUMBER 5 SLAT: HIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES A CRACK ON NUMBER 15 SLAT RIB MOST OUTBOARD RIB. REPLACED CRACKED RIB OUTBOARD MOST NUMBER 15 POSITION RIGHT SLAT PER ESO 80117.SDR AALA20100714TUL05Rib · crackedRIGHT WING NUMBER 5 SLAT: HIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES A CRACK ON NUMBER 14 SLAT RIB 2ND FROM OUTBOARD. REPLACED CRACKED RIB 2ND FROM OUTBOARD NUMBER 14 POSITION RIGHT NUMBER 5 SLAT PER ESO 80117.SDR ASAA1048064Slat · delaminatedNR 1 SLAT L/E DELAMINATED I/B AFT CORNER. REMOVED DAMAGE, INSTALLED AND BONDED REPAIR DOUBLER.SDR IPXA10661194Wedge · chafedINSPECTION TYPE:C, RT WING NR 7 SLAT T/E WEDGE FOUND CHAFED. METAL HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 8.SDR FDEA201007122483Skin · unknownEXISTING REPAIR AT RT WING NR 2 SLAT INNER SKIN XIS 260. EXISTING REPAIR AT RT WING NR2 SLAT INNER SKIN XIS 260 R & R WITH NEW REPAIR IAW SRM 57-00-01, FIG 4, VOL I, REV 96, EO 8-5100-7-5001, A7 PT 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR IPXA10561143Wedge · dentedINSPECTION TYPE:C4, NR 1 SLAT HAS 2 OUT OF LIMITS DENTS. REPAIR WAS ACCOMPLISHED IAW SRM 51-70-10.SDR IPXA10561142Wedge · dentedINSP TYPE:C4, NR 1 SLAT T/E WEDGE UPPER SURFACE HAS 2 EA OUT OF LIMIT DENTS (DUE TO PROXIMITY TO EACH OTHER) AT 15" FROM INBD END AND 6.2500" FWD OF T/E REPAIRED NR 1 SLAT IAW SRM 51-70-10.SDR USAA2010071291400Skin · delaminatedCLT - C1 - MAJOR REPAIR - DELAMINATION ON NR 6 SLAT OUTBOARD UPPER TRAILING EDGE SURFACE. REPLACED NR 6 SLAT IAW JOB CARD 03C40227004.SDR ASAA1048094Skin · delaminatedNR 1 SLAT UPPER O/B AFT CORNER DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR.SDR ASAA1048093Skin · delaminatedNR 2 SLAT O/B AFT CORNER DELAMINATED. REMOVED PREVIOUS REPAIR AND INSTALLED NEW.SDR ASAA1048092Skin · chafedNR 4 SLAT LOWER TRAILING EDGE I/B END IS CHAFED. REMOVED DAMAGE, INSTALLED REPAIR.SDR ASAA1048091Skin · delaminatedNR 2 SLAT INBOARD AFT CORNER IS DELAMINATED. REMOVED DAMAGED AREA, BONDED THE REPAIR.SDR UALA2010070902437Slat · separatedL/E SLAT SKIN SEPARATION, FLIGHT DIVERTED. CREW REPORTS FAA INSPECTOR SAW A PIECE OF SHEETMETAL DEPART THE LEFT WING LEADING EDGE INBOARD OF NR 1 ENG. HONEYCOMB MATERIAL IS EXPOSED. REPLACED THE NR 5 LEADING EDGE SLAT. FIXED LEADING EDGE PANEL REPAIRED ALSSDR USAA2010071391410Slat · debondedPHX - B-CHECK - MAJOR REPAIR - NR 8 LEADING EDGE SLAT INBOARD END/TRAILING EDGE CORNER DISBONDED 22 (APPROX) WEDGE. REPLACED NR 8 LEADING EDGE SLAT IAW JOB CARD 19L52027002.SDR USAA2010071391409Slat · debondedPHX - B-CHECK - MAJOR REPAIR - NR 5 LEADING EDGE SLAT- OUTBOARD END 18 INCHES INBOARD X 6 INCHES FROM TRAILING EDGE DISBONDED (APPROX) WEDGE. REPLACED NR 5 LEADING EDGE SLAT IAW JOB CARD 19C51227001.SDR AALA20100708TUL05Skin · corrodedCORROSION ON NUMBER 9 SLAT SKIN LOWER TRAILING EDGE AROUND FASTENER AT OUTBOARD AUXILIARY TRACK. REMOVED CORROSION AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR FDEA201007082432Skin · dentedLT WING - NR 3 SLAT, APPROX STA XOS 390 TO XOS 440 EXTERIOR FWD SKIN FOUND WITH DENTS. R & R IAW AMM 27-80-01, REV 10. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082431Skin · dentedLT WING - NR 6 SLAT, APPROX STA XOS 789 EXTERIOR FWD SKIN FOUND WITH DENT. REPAIRED IAW SRM 57-10-00, FIG 11, VOL I REV 96. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 110.SDR FDEA201007082430Skin · dentedRT WING - NR 7 SLAT ENTIRE FWD EXTERIOR SURFACE SKIN FOUND WITH DENTS. SLAT ASSY R & R IAW AMM 27-80-01, REV 10. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082429Skin · dentedRT WING - NR 6 SLAT, ENTIRE FWD EXTERIOR SURFACE SKIN FOUND WITH DENTS. NR 6 SLAT ASSY R & R IAW AMM 27-80-01, REV 10. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082425Rib · gougedLT WING L/E KRUEGER FLAP LOWER LIP OTBD L/E GOUGED, 2 SQ INCHES FOUND DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-41-11. REMOVED DAMAGED END CAP AND FABRICATED REPLACEMENT PART, END CAP, IAW DWG A57843755 AND INSTALLED ON LT WING KRUEGER FLAP OTBD L/E IAW SDR SWAA103994Skin · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT L/E LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR FDEA201007082421Rib · damagedRT WING KRUEGER FLAP FWD OTBD CORNER HAS IMPACT DAMAGE TO THE EXTERIOR SKIN & CLOSE OUT RIB. FOUND DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 57-41-11. REMOVED DAMAGED END CAP AND FABRICATED REPLACEMENT PART, END CAP, AND INSTALLED ON RT WING KRUEGER FLAP IAW SRSDR AALA20100707TUL02Slat · damagedIMPACT DAMAGE 10IN BY 22IN AT 43 INCHES FROM INBOARD END OF LEFT SLAT. FLUSH REPAIR DOUBLER INSTALLED PER SRM 57-42-01-2R 5.SDR IPXA10560992Wedge · chafedINSPECTION TYPE:C3 NR 3 SLAT LOWER SURFACE TE WEDGE CHAFED ABOVE INBD MAIN TRACK. REPAIRED CHAFE NR 3 SLAT T/E WEDGE LOWER SURFACE IAW SRM51-70-10 REPAIR 4, SRM51-70-10-0G.SDR IPXA10561168Wedge · chafedINSPECTION TYPE:C4, WHILE WORKING CARD NR 879181 FOUND CHAFE ON RT WING NR 8 SLAT T/E WEDGE LOWER SURFACE AT INBD MAIN TRACK OUT OF LIMITS REQUIRING REPAIR. REPAIRED CHAFE ON R/W NR 8 SLAT T/E WEDGE LOWER SURFACE AT INBD MAIN TRACK IAW SRM 51-70-10 AND EO 757SDR CA100714001Skin · debonded(CAN) TOP AND BOTTOM SKINS DISBONDED. 21 INCH BY 6.5 INCH. 21 INCHES INBOARD OF OUTBOARD EDGE DUE TO WATER INGRESS THROUGH THE BOND LINE BETWEEN THE TRAILING EDGE SKINS AND THE SPAR. UNIT REPAIRED WITH STANDARD HOT BOND TECHNIQUES PER MANUFACTURER RECOMMENDASDR USAA2010070691345Wedge · delaminatedCLT - C4 - MAJOR REPAIR - DELAMINATION ON UPPER SURFACE OF NR 4 SLAT TRAILING EDGE WEDGE. REPLACED NR 4 SLAT IAW B737 AMM 27-81-21.SDR FDEA201007022316Slat Track · chafedLT WING NR 6 SLAT TRACK CHAFING WITH OTBD ATTACHED RIB FITTING. R & R IAW SRM 51-31-01 VOLUME I, REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.SDR UALA2010070102348Structure · dentedDENT ON LEADING EDGE NR 2 SLAT APPROX 1 FT OUT FROM INBOARD EDGE MEASURES 6-32 DEEP. TEMPORARY REPAIR INSTALLED. MUST INSTALL STRUCTURAL INSERT REPAIR WITHIN 4500 FC, OR 6000 FH OR 20 MONTHS OR CHECK WHICHEVER OCCURS FIRST. REPLACED SLAT ON WUP K4341F.SDR AALA20100630TUL02Rib · wornSLAT BRACKET ON OUTBOARD SKIN AT RIB NUMBER 15 WORN. REPLACED SLAT BRACKET AND NEW SKIN ON LEADING EDGE OUTBOARD PER ESO 80117SDR FDEA201006302310Attach Bracket · crackedNR 8 SLAT ACTUATOR IB & OB ATTACH BRACKETS INSIDE PLATES ARE CRACKED. REMOVED I/B AND O/B BRACKETS IAW SRM 51-30-2. FABRICATED BRACKETS FROM 7075-0 .063" DIM. 9" X 4.80 " (2 EA) AND I/B PLATE FROM 7075T6 .125" DIM. 3.8" X 7.5" IAW DWG. 65-17255. HEAT TREATED BSDR FDEA201006302309Attach Bracket · crackedNR 8 SLAT ACT. IB & OB ATTACH BRACKETS INSIDE PLATES ARE CRACKED. REMOVED I/B AND O/B BRACKETS FROM NR 8 SLAT IAW SRM 51-30-2. FABRICATED I/B AND O/B BRACKETS FROM 7075-0 .063" DIM. 9" X 4.80 " (2 EA) AND I/B PLATE FROM 7075T6 .125" DIM. 3.8" X 7.5" IAW DWG. 6SDR SWAA103874Skin · crackedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT LOWER SURFACE CRACKED. REPAIRED SKIN PER SRM.SDR SWAA103861Slat · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 4 SLAT I/B END DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER SRM.SDR SWAA103857Wedge · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 3 SLAT I/B END UPPER T/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER SRM.SDR SWAA103856Skin · crackedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT I/B OF O/B AUX TRACK LOWER SKIN CRACKED. REMOVED AND REPLACED NR 2 SLAT PER SRM.SDR SWAA103855Skin · crackedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 1 SLAT LOWER T/E SKIN CRACKED. REPAIRED SKIN PER SRM.SDR SWAA103813Slat · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT I/B END DELAMINATED. REPAIRED SLAT PER SRM.
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