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 FDEA201011184420Skin · damagedLT WING NR 2 SLAT HAS NUMEROUS CHAFED MARKS ALONG BOTTOM SKIN AFT EDGE REPAIRED LT WING NR 2 SLAT IAW SRM 51-70-10 IAW SRM 57-43-02 DAMAGE LOCATED AT STA 652.50 APPROX 1" FWD OF T/E SLAT REPAIR DIAM. 1"X1.5". REF EA F-5750-142276. CLASSIFIED CAT "A" MAJOR REPASDR USAA2010120792908Bolt · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON RIGHT WING UPPER BOLT OF NR 6 SLAT TRACK BETWEEN WS 6132 TO WS 7316 & BETWEEN RIB 11 TO RIB 13. REPLACED RIGHT WING UPPER BOLT OF NR 6 SLAT TRACK BETWEEN WS 6132 TO WS 7316 & BETWEEN RIB 11 TO RIB 13 IAW A320 AMM 27-84-6SDR USAA2010120792907Bolt · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON RIGHT WING LOWER BOLT OF NR 2 SLAT TRACK BETWEEN WS 1406 TO WS 2580 & BETWEEN RIB 3 TO RIB 5. REPLACED RIGHT WING LOWER BOLT OF NR 2 SLAT TRACK BETWEEN WS 1406 TO WS 2580 & BETWEEN RIB 3 TO RIB 5 IAW A320 AMM 27-84-63.SDR SWAA107060Skin · delaminatedDURING SCHEDULED 10Y CHECK, FOUND RT WING NR 4 SLAT SKIN DELAMINATED. REPAIRED SKIN PER SRM.SDR USAA2010120792906Bolt · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON RIGHT WING UPPER BOLT OF NR 2 SLAT TRACK BETWEEN WS 1406 TO WS 2580 & BETWEEN RIB 3 TO RIB 5. REPLACED RIGHT WING UPPER BOLT OF NR 2 SLAT TRACK BETWEEN WS 1406 TO WS 2580 & BETWEEN RIB 3 TO RIB 5 IAW A320 AMM 27-84-63.SDR DALA1032735637Wedge · delaminatedDURING L-CHECK FOUND RT WING NR6 SLAT UPPER WEDGE AREA INBD SIDE DELAMINATED. FOUND DURING TAP TEST. SANDED & CLEANED AREA, BONDED REPAIR, SANDED EXCESS SMOOTH & PRIMED IAW SRM 51-70-10 REP IAW 4 FIG 202 IAW WC 5742-01022-02F. PAINTED AREA IAW MM 51-21-10. SDR SWAA107090Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED UPPER SURFACE CORNER. REMOVED AND REPLACED SLAT PER MM.SDR ASAA1048530Slat · delaminatedNR 2 SLAT INBOARD AFT UPPER CORNER PREVIOUS REPAIR DELAMINATED. REMOVED DAMAGED AREA. FABRICATED TREATED PRIMED AND BONDED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REPAIR 4.SDR SWAA106944Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 4 SLAT SKIN O/B EDGE DELAMINATED. REPAIRED SKIN PER MM.SDR SWAA106943Skin · delaminatedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 SLAT SKIN O/B EDGE DELAMINATED. REPAIRED SKIN PER MM.SDR SWAA106940Slat · crackedDURING SCHEDULED 20Y CHECK, FOUND LT WING L/E NR 1 SLAT CRACKED. REPAIRED SLAT PER SRM.SDR FDEA201011104298Shim · migratedRT WING T/E NR4 FLAP FRONT CARRIAGE UPPER BRIDGE BOTH SIDE SHIM EXTRUDED IAW EA6-2750-141649, REPAIR ACCOMPLISHED IAW GMM 6-2-100. REPAIR CLASSIFIED AS MINOR.SDR SWAA106921Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT UPPER SURFACE I/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.SDR SWAA106917Slat · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING NR 4 SLAT I/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.SDR DALA1031043210Slat · gougedDURING L-CHECK FOUND GOUGE IN NR 2 SLAT INBOARD TRAILING EDGE IN 4 LOCATIONS. REPAIRED PER SRM 51-21-11, SRM 57-43-21 FIGURE 204 SHEET 2.SDR SWAA106902Skin · crackedDURING SCHEDULED 16Y CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.SDR SWAA106834Slat · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING NR 3 SLAT I/B EDGE DELAMINATED. REPAIRED SLAT PER SRM.SDR FDEA201011084282Skin · damagedEXISTING DOUBLER REPAIR ON NR 9 SLAT INBD AND OTBD END UPPER SURFACE. COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5001 PT 1 EVALUATED REPAIR IAW EO F-5100-7-5001 ATTCHEMENT "B". REPAIR FOUND TO BE IAW SRM 51-70-10, REPAIR 2, FIG 201. REPAIR IS CLASSIFIED AS ASDR SWAA106804Wedge · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING NR 2 SLAT T/E EDGE WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR DALA1030675523Skin · crackedDURING L-CHECK FOUND CRACK IN LEFT WING NR 2 LEADING EDGE SLATE LOWER SKIN JUST FORWARD ON OUTBOARD MAIN SLAT TRACK. REPAIRED PER SRM 57-70-13 PAGES 1 & 2.SDR DALA1030665523Skin · crackedDURING L CHECK FOUND CRACK IN LEFT WING NR 3 LEADING EDGE SLAT LOWER SKIN JUST FORWARD OF OUTBOARD MAIN SLAT TRACK. REPAIRED PER SRM 57-70-13 PAGES 1 & 2.SDR FDEA201011034235Skin · chafedLT WING SLAT NR 4 UPPER SURFACE FOUND CHAFED. REMOVED AND CLEANED AS PER SRM 57-00-01 FIGURE 1A, VOLUME I, REVISION 96. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, REVISION 111.SDR ABXA201011120150Rib · corrodedCORROSION AROUND PANEL ATTACH NUT PLATES ON NR 3 SLAT I/B AUX TRACK I/B AND O/B RIBS. REMOVED AND REPLACED RIB IAW 767-200 SRM 51-40-02.SDR ABXA201011120149Rib · corrodedNR 2 SLAT I/B AUX TRACK FITTING O/B RIB CORRODED AROUND PANEL ATTACH NUT PLATES AND SHIM PACK FOR FITTING. REMOVED NR 2 SLAT I/B AUX TRACK I/B AND O/B LOWER RIBS. INSTALLED NEW RIBS IAW 767 SRM 51-40-02.SDR ABXA201011120148Rib · corrodedNR 2 SLAT O/B AUX TRACK FITTING I/B AND O/B ATTACHE RIBS HAVE CORROSION UNDER PANEL ATTACH NUT PLATES AND AROUND FITTING SHIM PACKS. REMOVED AND REPLACED RIBS IAW B767-200 SRM 51-40-02.SDR ABXA201011120146Rib · corrodedWING L/E PANEL ATTACH NUT PLATE HAS CORROSION UNDER IT AT NR 10 SLAT BETWEEN O/B AUX AND MAIN TRACK. REMOVED AND REPLACED DAMAGED RIB AND CLOSE OUT NOSE BEAM WEB ON LT WING SLAT O/B AUX TRACK O/RIB IAW B767-200 SRM 51-40-02.SDR AALA20101102AFW01Wedge · debondedNR 10 SLAT T/E WEDGE IS DISBONDED ON THE AFT I/B CORNER. CUT OUT IS 7 X 3 INCHES, DATA CONCERNING THIS REPAIR HAS BEEN ENTERED INTO THE MAJOR REPAIR TRACKING REPORT, DO NOT RE-ENTER THIS REPAIR.SDR UALA2010110204067Skin · dentedRIGHT NR 2 SLAT HAS DENT. BEGAN REMOVING SLAT PER MM. DURING SLAT OPS CHECK, HAD NR 2 SFCC FAULT ONE CAM, COULD NOT RESET, SWAPPED MSG FOLLOWED, BACK TO ORIGINAL POS. REPLACED NR 2 SFCC REF AMM, GDN TEST PASSED, CAT III TEST WILL BE ON SMC13. LARGE DENT IN LE SDR DALA1029055523Skin · crackedDURING L-CHECK FOUND CRACK IN RIGHT WING NR 8 SLAT LOWER SKIN. REPAIRED PER SRM 51-40-02 PAGE 7, SRM 51-70-13 PAGES 1 & 2 FIGURE 1.SDR DALA1030755523Skin · crackedDURING L-CHECK FOUND RIGHT WING NR 10 SLAT LOWER SKIN CRACKED JUST FORWARD OF INBOARD MAIN SLAT TRACK. REPAIRED PER SRM 51-70-13 PAGE 2 FIGURE 1 & SRM 51-40-02 PAGE 3, PAGE 7.SDR DALA1031375523Skin · puncturedDURING L-CHECK FOUND PUNCTURE IN RIGHT WING NR 8 LEADING EDGE SLAT LOWER SKIN JUST ABOVE ACCESS PANEL 623. REPAIRED PER SRM 57-42-02 PAGE 201 FIGURE 201, SRM 57-40-10 & ERA 486847-14 REV 0.SDR CA101122001Hinge · sheared(CAN) ON ARRIVAL OF THE MAINTENANCE PERSONNEL THEY FOUND THE INBOARD HINGE BROKEN AND THE CRACK ON THE KRUGER FLAP INBD SKIN WHICH COULD HAVE BEEN CAUSED WHEN THE KRUGER FLAP WAS EXTENDED CATCHING THE WING (WHICH WAS NOT DAMAGED) BENDING THE UPPER INBD SKIN OFSDR USAA2010111592609Wedge · delaminatedCLT - MAJOR REPAIR - C2 CHECK - LEFT WING LEADING EDGE SLAT NR 4 TRAILING EDGE WEDGE LOWER SURFACE HAS DELAMINATION. REPAIRED LEFT WING LEADING EDGE SLAT NR 4 TRAILING EDGE WEDGE LOWER SURFACE IAW B757 SRM 51-70-10.SDR AALA20101028TUL09Skin · corrodedLEFT WING NUMBER 4 SLAT HAS CORROSION 40 INCHES OUTBOARD FROM INBOARD END, 9 INCHES FORWARD OF UPPER TRAILING EDGE OF NOSE SKIN. LEFT WING NUMBER 4 SLAT REMOVED DAMAGED AREA OF SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR SWAA106769Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 4 SLAT O/B LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR SWAA106701Slat · delaminatedDURING SCHEDULED 26Y CHECK, FOUND LT WING NR 1 SLAT T/E DELAMINATED. REMOVED AND REPLACED NR 1 SLAT PER MM.SDR AALA20101027TUL01Slat · damagedMFE - CREW REPORTED BIRD STRIKE TO LEFT WING ROOT, ENGINE VIBRATION EGT SEEMED NORMAL. REDUCED VIBRATION WITH REDUCED THRUST. EMERGENCY DECLARED RETURNED MFE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. ACCOMPLISHED BIRD STRIKE INSPECTION. FOUNSDR AALA20101026TUL05Skin · corrodedLEFT WING NUMBER 1 SLAT HAS CORROSION ON LEADING EDGE 41.5 INCHES INBOARD FROM OUTBOARD END, 5 INCHES FORWARD FROM UPPER AFT TRAILING EDGE OF NOSE SKIN. LEFT WING NUMBER 1 SLAT REMOVED CORROSION AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20101026TUL04Skin · corrodedLEFT WING NUMBER 1 SLAT HAS CORROSION LEADING EDGE 29.5 INCHES OUTBOARD END 7.5 INCHES FORWARD FROM UPPER AFT TRAILING EDGE OF NOSE SKIN. LEFT WING NUMBER 1 SLAT REMOVED CORROSION AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20101026TUL01Skin · corrodedNUMBER 2 SLAT HAS CORROSION 29 INCHES INBOARD FROM OUTBOARD END, 8 TO 9 INCHES FORWARD OF UPPER TRAILING EDGE OF NOSE SKIN. REMOVED CORRODED AREA AND INSTALLED FLUSH DOUBLER PER SRM 57-43-01-2R.SDR SWAA106583Slat · delaminatedDURING SCHEDULED 26Y CHECK, FOUND LT WING NR 2 SLAT I/B TRAILING EDGE CORNER DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER SRM.SDR DALA1029085636Skin · delaminatedDURING L-CHECK FOUND DELAMINATION ON NR 5 SLAT SKIN TRAILING EDGE LOWER SKIN. REPAIRED PER SRM 57-42-02 & SRM 51-70-10 REPAIR 4.SDR AALA20101023TUL02Slat · corrodedNUMBER 7 SLAT CORROSION FOUND AROUND FASTENER HEAD APPROXIMATELY 50 INCHES FROM THE OUTBOARD END AND 7 INCHES FROM INBOARD END (MARKED). INSTALLED REPAIR PER AARD 57-43-01.SDR AALA20101023TUL01Skin · damagedDEEP BLEND IN BLIND FASTENER ON NUMBER 9 SLAT (MARKED) RIGHT WING. REMOVED COVE SKIN CUTOUT DAMAGED AND FABRICATED DOUBLERS. ALODINED AND PRIMED DOUBLERS AND FILLER PER AARD 57-43-00-1 AND SRM 51-20-01.SDR AALA20101021TUL09Skin · corrodedCORROSION AT NUMBER 10 SLAT LEADING EDGE SKIN AT RIVET ROW APPROXIMATELY 2.5 FEET OUTBOARD LEADING EDGE. CORROSION REMOVED AND DOUBLERS INSTALLED PER AARD 57-43-00-1.SDR AALA20101021TUL06Slat · corrodedLEFT WING NUMBER 4 SLAT UPPER CORROSION AT TRAILING EDGE WEDGE 24 INCH INBOARD OF OUTBOARD END. LEFT WING NUMBER 4 SLAT BLENDED AREA OUT OF LIMITS. INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20101020TUL01Rib · crackedNUMBER 5 RIGHT SLAT NUMBER 14 TRACK RIB CRACK INDICATION. REPLACED CRACKED NUMBER 14 TRACK RIB NUMBER 5 RIGHT SLAT PER ESO 80117.SDR SWAA106514Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND RT WING NR 7 SLAT CRACKED. REPAIRED SLAT SKIN PER EA.SDR SWAA106381Skin · crackedDURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 SLAT CRACKED AT LOWER L/E SKIN. REPAIRED SKIN PER EA.SDR USAA2010102592401Bolt · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON NR 2 SLAT ATTACHMENT BOLT ON SLAT TRACK NR 5 RIGHT WING. REPLACED NR 2 SLAT ATTACHMENT BOLT ON SLAT TRACK NR 5 RIGHT WING IAW A320 AMM 27-84-64.
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