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 DALA1169441704Pan · damagedLEFT WING NR 6 SLAT O/B PAN FOUND PUNCH HOLE DAMAGE. REF ERA 497633-14, COMPOSITE WET LAYUP REPAIR CARRIED OUT PER B767-300 SRM 51-70-17 FIG 19.SDR DALA1169431704Pan · damagedRT WING NR 7 SLAT O/B PAN FOUND PUNCH HOLE DAMAGE. REF ERA 497660-14. COMPOSITE WET LAYUP REPAIR CARRIED OUT PER B767-300 SRM 51-70-17 FIG 19.SDR ASMF201112005Skin · damagedDURING TRANSIT CHECK, MX DETECTED A ONE INCH HOLE IN FLEX SKIN OF SLAT NR 8, IT WAS CONFIRMED THAT HOLE WAS WITHIN LIMITS IAW SRM 57-42-01, AND WAS TEMPORARY COVERED WITH ALUMINUM FOIL TAPE IAW SRM 57-42-01 PAGES 103 AND 110. SLAT NR 8 WAS REPLACED IAW MM 27-SDR DALA1168611610Skin · looseNR 4 SLAT T/E WEDGE CORNER SKIN IS LOOSE AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 AND SRM 51-70-10 REPAIR 4 FIG 202 SHT 1.SDR DALA1168601610Wedge · chafedNR 12 SLAT T/E WEDGE LWR SURFACE IS CHAFED NEAR I/B AUX TRACK AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 AND SRM 51-70-10 REPAIR 4 FIG 202 SHT 8.SDR USAA2012010900017Wedge · delaminatedC2 CHECK - DELAMINATION ON SLAT 11 TRAILING EDGE WEDGE BETWEEN OSS982 TO OSS984. REPAIRED SLAT 11 IAW B767-200 SRM 51-70-10-2R4, REPAIR 4, FIGURE 202.SDR SWAA20111208481Slat · crackedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED. REMOVED AND REPLACED SLAT PER MM.SDR USAA2011122300023Wedge · debondedQ6 CHECK - DISBONDING ON NR 5 SLAT TRAILING EDGE WEDGE UPPER SURFACE AT SS124.53. REPAIRED NR 5 SLAT TRAILING EDGE WEDGE UPPER SURFACE AT SS124.53 IAW B737 SRM 57-43-02 & 51-70-10 REPAIR 4.SDR FDEA201112075189Skin · damagedLEFT WING NR 5 SLAT, FOUND SMALL DRILLED HOLE AT 22" FROM INBD. REPAIRED IAW EA F-5750-157114. REPAIR IS CLASSIFIED AS MAJOR.SDR AALA20120113TUL09Skin · scratchedRIGHT WING NUMBER 8 SLAT HAS 6 INCH SCRATCH ON UNDERSIDE. INTERNAL FLUSH DOUBLERS INSTALLED PER 57-42-01.SDR SWAA118738Slat · delaminatedDURING SCHEDULED 20Y CHECK, FOUND DELAMINATION ON I/B EDGE OF LT SLAT. REMOVED AND REPLACED SLAT PER MM.SDR SWAA118337Skin · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING NR 2 SLAT SKIN DELAMINATED AT STA 193.40. REPAIRED SKIN IAW SRM.SDR USAA2012011800012Wedge · debondedC2 CHECK - DISBONDED ON THE NR 11 SLAT TRAILING EDGE WEDGE 28 INCHES FROM INBOARD EDGE BETWEEN OSS857.74 TO OSS865.74. REPAIRED NR 11 SLAT IAW B767 SRM 51-70-10-2R, REPAIR 4, FIG 201.SDR USAA2011122800026Wedge · debondedC2 CHECK - AREA OF DISBOND ON NR 12 SLAT TRAILING EDGE WEDGE BETWEEN OSS984.73 TO OSS989.73. REPAIRED NR 12 SLAT TRAILING EDGE WEDGE BETWEEN OSS984.73 TO OSS989.73 IAW B767 SRM 51-70-2R-4 REPAIR 4 FIG 202.SDR AALA20111205DWH02Skin · corrodedLEFT WING NUMBER 4 LEADING EDGE SLAT HAS INDICATIONS OF LIGHT CORROSION ON UPPER SURFACE. REPAIRED IAW AARD 57-43-00-01.SDR AALA20111205DWH01Skin · corrodedLEFT WING NUMBER 3 LEADING EDGE SLAT HAS INDICATIONS OF LIGHT CORROSION ON UPPER SURFACE. REPAIRED IAW AARD 57-43-00-01.SDR AALA20111205AFW01Wedge · damagedSEVERAL SHARP DENTS/GOUGES ON UPPER SURFACE OF THE NUMBER 6 SLAT WEDGE APROXIMATELY 8 INCHES FROM INBOARD EDGE AND APROXIMATELY 8 INCHES FROM TRAILING EDGE. ACCOMPLISHED SLAT REPAIR PER SRM 51-70-10.SDR AALA20111202DWH01Skin · crackedLEFT WING OUTBOARD SLAT NUMBER 1 UPPER SKIN CRACKED AND DENTED OVERWING STATION 711. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, AND INSTALLED PERMANENT REPAIR PER SRM 57-43-01-2R.SDR DALA1166421607Wedge · bulgedLT WING NR 2 SLAT T/E WEDGE UPPER SURFACE HAS A BULGE AND IS REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.SDR USAA2012012000008Wedge · debondedC21 CHECK - RIGHT WING NR 4 SLAT TRAILING EDGE WEDGE DISBONDED BETWEEN SS116 TO SS124, 6 INCHES INBOARD OF OUTBOARD END 2.5 INCHES FROM TRAILING EDGE. REPAIRED NR 4 SLAT IAW B737-300 SRM 51-70-10-2R-4, REPAIR 4 FIGURE 202.SDR R61A20110397Screw · corroded*** WHILE AIRCRAFT WAS IN FOR HEAVY CHECK *** LEVEL 2 CORROSION WAS FOUND ON THE LT WING NR 1 SLAT SEAL HARDWARE. MAINTENANCE REMOVED AND REPLACED THE NR 1 SLAT SEAL HARDWARE IAW EMB 170/175 AMM 57-41-09. REF: SCREW P/N NAS1102-06-5 AND NUT P/N MS21042-06. SDR HALA2011112800592Wedge · debondedNR 8 SLAT OTBD END HAS A T/E WEDGE AREA OF DISBOND. REPAIRED IAW SRM 57-43-02-2R-1, REV 87 AND 51-70-10, REV 87.SDR DALA1164720179Wedge · delaminatedLT WING NR 5 SLAT T/E WEDGE IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 202.SDR DALA1164710179Wedge · delaminatedLT WING NR 6 SLAT T/E WEDGE IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 202.SDR DALA1164700179Wedge · delaminatedRT WING NR 11 SLAT T/E WEDGE IS DELAMINATED AND A HOT BOND REPAIR WAS INSTALLED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 202.SDR DALA1164620179Rib · crackedRT WING NR 12 SLAT I/B RIB FOUND CRACKED.SDR DALA1164601602Slat · crackedRT WING NR 7 SLAT FROM I/B 61 INCHES AND FROM T/E 4 INCHES FOUND A 0.375 INCH CRACK. METAL HOT BOND REPAIR PERFORMED AS PER B767-300 SRM 51-70-10 REPAIR 2 FIG 203.SDR DALA1164581602Skin · chafedLT WING NR 4 SLAT O/B EDGE RIB O/B SURFACE WAS FOUND CHAFED.SDR MASA2011121364213Structure · dentedFIVE DENTS LOCATED ON RT WING L/E SLAT BETWEEN SS58-75-SS92.00 OUT OF LIMITS. C/W RO CRJ9-57-0344.SDR UALA2011112106396Skin · delaminatedCREW REPORT: SKIN DELAMINATION ON RT INBD SLAT. ABOUT 12 INCH PIECE CAME OFF DURING CLMB. NO ADVRS CNTR. SAMC TEXT: CREW REPORTS NO VIBRATION FELT AND NO AIRCRAFT TRIM NEEDED. MAINT TEXT: RT INBOARD LEADING EDGE SLAT HAS A LARGE AREA AT THE TRAILING EDGESDR AALA20111121TUL07Slat · corrodedLEFT WING NUMBER 3 SLAT CORRODED AROUND FASTENER 33 INCHES FROM OUTBOARD END. INSTALLED REPAIR DOUBLER PER AARD 57-43-00-1.SDR SWAA118104Skin · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING NR 2 SLAT LOWER L/E SKIN CRACKED. REPAIRED SKIN IAW SRM.SDR SWAA118103Skin · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING NR 6 SLAT LOWER L/E SKIN CRACKED. REPAIRED SKIN IAW SRM.SDR FDEA201111194979Skin · corrodedPREVIOUS FLUSH REPAIR LOCATED ON LT WING NR 2 SLAT NOSE SKIN BETWEEN RIBS 25 AND 27 HAS 43 EA BLIND BOLTS WITH RUST STARTING FROM COATING LOSS. PREVIOUSLY INSTALLED REPAIR LOCATED ON LT WING NR 2 SLAT NOSE SKIN BETWEEN RIB 25 AND RIB 27 WAS DETERMINED NOT TSDR ABXA20111119142Rib · gougedRIGHT WING L/E SLAT 405 CANTED RIB GOUGED SEVERAL AREAS. BLENDED GOUGED ORIG THICKNESS 0.100. REMAINING THICKNESS .083" BLENDOUT ACCEPTABLE IAW REA B657-59566, AWG.SDR AALA20111120TUL02Skin · corrodedLEFT WING, NUMBER 3 SLAT CORRODED AROUND FASTENER ON TOP SKIN APPROXIMATELY 33 INCHES FROM OUTBOARD END. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS PER AARD 57-43-00-1.SDR AALA20111120TUL01Skin · corrodedCORROSION ON NUMBER 9 SLAT SKIN AROUND FASTENER OUTBOARD DRIVE TRACK AREA. REMOVED CORROSION AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20111122TUL01Wedge · damagedLEFT WING NUMBER 1 SLAT HAS AREA OF DELAMINATION ON UPPER TRAILING EDGE WEDGE. INSTALLED DOUBLER PER SRM 51-70-10-2R.SDR MASA2011121364202Slat · dentedONE OUT OF LIMIT DENT ON NR 1 LHS. PERMANENT REPAIR FOR 1 OFF DENT ON NR 1 LHS SLAT BETWEEN SS82.00 & SS92.20. C/W RO CRJ9-57-0328, TASK MRO 18142.SDR MASA2011121364204Slat · dentedONE OUT OF LIMIT DENT ON NR 2 RHS. PERMANENT REPAIR FOR 1 OFF DENT ON NR 2 RHS BETWEEN SS315.75 &TRACK 2-3. C/W RO CRJ9-57-0330, TASK MRO 18134.SDR MASA2011121364203Slat · dentedONE OUT OF LIMIT DENT ON NR 3 LHS. PERMANENT REPAIR FOR 1 OFF DENT ON NR 3 LHS SLAT BETWEEN SS339.00 &TRACK 3-2. C/W RO CRJ9-57-0329, TASK MRO 18140.SDR AALA20111115TUL02Skin · damagedDAMAGE ON NUMBER 4 SLAT LEADING EDGE SKIN AT OSS 331. INSTALLED FLUSH DOUBLER REPAIR PER SRM 57-43-01-2R.SDR SWAA117913Structure · damagedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 6 I/B SLAT CAN DAMAGED. REPAIRED SLAT CAN IAW EA.SDR AALA20111110TUL10Support · gougedRIGHT WING NUMBER 15 SLAT TRACK OUTBOARD SUPPORT GOUGED AT FORWARD END. REMOVED AND REPLACED DAMAGED NUMBER 15 SLAT TRACK SUPPORTS PER AARD 51-00-00-1.SDR FDEA201111094834Rib · cutON REMOVAL OF NR 2 SLAT INNER SKIN, FOUND RIB HAS DEEP CUT. DAMAGED RIB REMOVED IAW SRM 51-31-01 REV 47. DRILLED NEW RIB AND INSTALLED IAW SRM 51-31-01 REV 47 AND SRM 51-33-01 REV 47 .REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.SDR SWAA117614Skin · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR AALA20111104TUL02Slat · puncturedNUMBER 4 SLAT HAS A .5 INCH PUNCTURE MID SPAN UNDERSIDE OF TRAILING EDGE. INSTALLED HOT BOND DOUBLER REPAIR PER SRM 51-70-10-2.SDR FDEA201111044747Skin · misrepairedRT WING L/E NR 2 SLAT, OTBD INNER SKIN MISREPAIRED. CARRIED OUT REPAIR IAW EA EI-5750-150400. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.SDR FDEA201111044746Skin · misrepairedRT WING L/E NR 2 SLAT SKIN MISREPAIRED. CARRIED OUT REPAIR IAW EA EI-5750-150400. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.SDR SWAA117576Slat · damagedDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 6 SLAT I/B CAN DAMAGED. REMOVED AND REPLACED SLAT CAN PER EA.
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