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 SWAA095764Slat · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED. REPAIRED SLAT PER SRM.SDR IPXA09557375Skin · dentedINSPECTION TYPE:C2 NR 6 SLAT TRAILING EDGE UPPER SURFACE 2 DENTS 7 INCHES FWD TRAILING EDGE 66 INCHES INBOARD OF OUTBOARD EDGE. EVALUATED DAMAGE, REMOVED DAMAGE, FABRICATED CORE PLUG, REPAIR DOUBLER PREPARED SURFACE, INSTALLED REPAIR PARTS, BAGGED AND CURED RSDR AALA20090903TUL01Skin · corrodedCORROSION ON UPPER SURFACE OF SKIN 30 INCHES FROM INBOARD END. INSTALLED DOUBLER ON UPPER SURFACE PER SRM 57-43-01 AND AARD 57-43-00-1 MRT 022536.SDR SWAA095706Wedge · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING NR 1 SLAT I/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR IPXA09657380Skin · misrepairedINSPECTION TYPE:C SURVEY SEQ 311-W3-01 LT WING NR 4 SLAT OUTER SKIN L/E 42 INCHES FROM O/B EDGE EXISTING REPAIR DOES NOT CORRELATED TO A SRM. LEFT WING NR 4 SLAT NOSE SKIN BETWEEN OSS 638 TO OSS 645 REPAIRED AS PER UPS EO B767-5750-34944-A AND HX RS R57-43-36SDR IPXA09657304Skin · crackedINSPECTION TYPE:C LT WING - NR 4 SLAT I/B NOSE SKIN AT I/B SUPPORT WEB RIVET HOLE FOUND CRACK. CRACK LENGTH 0.125 INCH. LT WING - NR 4 SLAT I/B NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 JUST AT OSS 573.25. THIS IS CLASSIFIED A MAJOR REPAIR WSDR IPXA09657303Skin · crackedINSPECTION TYPE:C RT WING - NR 9 SLAT O/B NOSE SKIN AFT O/B SUPPORT WEB RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. RT WING - NR 9 SLAT O/B NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 JUST AT OSS 641.62 INCH. THIS IS CLASSIFIED AS A MAJSDR IPXA09657302Skin · crackedINSPECTION TYPE:C RT WING - NR 9 SLAT I/B NOSE SKIN AT I/B SUPPORT WEB RIVET HOLE FOUND CRACKED (CRACK LENGTH 0.125 INCH). RT WING NR 9 SLAT I/B NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45 JUST AT OSS573.25". THIS IS CLASSIFIED A MAJOR REPAIR WSDR AALA20090902TUL22Wedge · delaminatedSLAT NUMBER 4 DELAMINATED ON TRAILING EDGE WEDGE. REMOVED FOR REPAIR. INSTALLED NEW CORE AND DOUBLER UNDER SRM 51-70-10-2R.SDR SWAA095691Skin · crackedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 1 SLAT SKIN LOWER T/E CRACKED. REMOVED AND REPLACED SKIN PER MM.SDR SWAA095681Wedge · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 SLAT O/B WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA095680Skin · crackedDURING SCHEDULED 20Y CHECK, FOUND LT WING NR 1 SLAT LOWER SURFACE CRACKED. REMOVED AND REPLACED SLAT PER SRM.SDR SWAA095679Wedge · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 SLAT I/B WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER SRM.SDR AALA20090901TUL02Skin · crackedTHE RIGHT WING NR 10 SLAT BACK SKIN IS CRACKED IN TWO PLACES BY THE OUTBOARD GUIDE TRACK. REPAIRED AND INSTALLED INBOARD AND OUTBOARD DOUBLERS PER AARD 57-43-00-4.SDR SWAA095650Wedge · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 SLAT O/B END OF WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR CNMA20090152Skin · damaged5:22 INTO FLIGHT, HEARD A LOUD THUMP WITH AN ASSOCIATED PITCH CHANGE WATER SYS, PRESS LOW LIGHTS ILLUMINATED AND SYS 2 QTY REDUCED TO 0. 7:22 INTO FLIGHT, HEARD 2ND LOUD THUMP WITH ASSOCIATED PITCH CHANGE. NO ADDITIONAL ABNORMAL INDICATIONS WERE NOT. FOUND SDR SWAA095637Wedge · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING NR 1 SLAT WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA095617Wedge · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 L/E SLAT I/B TRAILING EDGE WEDGE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.SDR SWAA095586Slat · delaminatedDURING SCHEDULED 12Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED O/B END. REPAIRED SLAT PER SRM.SDR AALA20090828TUL10Skin · corrodedCORROSION ON NUMBER 10 SLAT, 30 INCHES FROM INBOARD UPPER SURFACE. INSTALLED DOUBLER UNDER SRM 57-43-01.SDR AALA20090828TUL06Skin · corrodedCORROSION ON NUMBER 10 SLAT 30 INCHES FROM INBOARD BOTTOM SURFACE. INSTALLED DOUBLER UNDER SRM 57-43-01.SDR AALA20090828TUL04Skin · corrodedCORROSION ON NUMBER 10 SLAT, 41 INCHES FROM OUTBOARD UPPER SURFACE. INSTALLED DOUBLER UNDER SRM 57-43-01.SDR AALA20090827TUL06Flap · damagedSMMR TUL 9457 - AN INTERIM REPAIR WAS MADE ON A STATIC DISCHARGE HOLE ON THE EXTENDED EDGE LIMIT OF THE LEFT INBOARD FLAP PER SMMR TUL9457. ATBT 15JAN/TUL AT NEXT HEAVY C CHECK MAKE PERMANENT REPAIR OF LEFT INBOARD FLAP. REMOVED AND REPLACED TRAILING EDGE UNSDR ASAA0956456Wedge · chafedLEFT WING NR 3 SLAT TRAILING EDGE WEDGE HAS A SMALL CHAFED AREA ON THE LOWER SKIN I/B CORNER. REPAIRED CHAFE ON NR 3 SLAT LOWER SKIN I/B CORNER.SDR SWAA095580Wedge · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 L/E SLAT OUTBOARD T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR AALA20090827TUL07Skin · corrodedRIGHT WING NUMBER 10 SLAT HAS CORROSION ON UPPER SURFACE/REF E-58 5999524/FMR-63457FFAA. REMOVED CORROSION AND INSTALLED FLUSH-DOUBLER UNDER SRM-57-43-01-2 AT OUTBOARD SLAT-TRACK FITTING AREA.SDR SWAA095569Skin · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 4 SLAT I/B END T/E WEDGE SKIN DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR HALA2009082600386Structure · dentedRT WING INBD SLAT HAS DENT AND HOLE. REPAIRED SLAT IAW M105 FILE NR 589036. OK FOR SERVICE.SDR FDEA200908263093Skin · wornLT WING SLAT FOUND 1EA DEEP WEAR ON EXTERNAL SKIN SLAT DROOPED AT STA XDLE 309 REPAIR IAW SRM 57-21-01 FIG 4, VOL 3 AND SRM 57-00-01 FIG4, SHEET 2, VOL.1SDR FDEA200908263092Skin · wornRT L/E SLAT FOUND 1EA DEEP WEAR ON EXTERNAL SKIN L/E DROOPED AT STA XDLE 309 REPAIR IAW SRM 57-21-01 FIG.4 VOL 3 AND SRM 57-00-01 FIG 4 SHEET 2 VOL 1.SDR IPXA09557218Wedge · delaminatedINSPECTION TYPE:C2 WHILE WORKING CUSTOMER CARD 817194 FOUND NR 6 SLAT UPPER SURFACE T/E WEDGE TO HAVE DELAMINATED AREA 9 - 28 INCHES FROM I/B END 8 INCHES FROM T/E. REPAIRED PER SRM 51-70-10, REPAIR 4.SDR ASAA0946464Wedge · delaminatedNR 5 T/E WEDGE IS DELAMINATED 2 INCHES FROM I/B END UPPER SURFACE ON PREVIOUS REPAIR. REPAIRED NR 5 SLAT T/E WEDGE PER SRM 57-43-02.SDR AALA20090825TUL46Skin · crackedNUMBER 7 SLAT HAS 2 CRACKS ON UPPER SKIN. REMOVED CORROSION INSTALLED DOUBLER UNDER SRM 57-43-01, MRT 022493 DWMS 1215532.SDR AALA20090824TUL01Skin · corrodedRIGHT WING NUMBER 9 SLAT HAS CORROSION ON UPPER SURFACE, REF: E58 5999523. REMOVED CORROSION, INSTALLED DOUBLER UNDER SRM 57-43-01.SDR AALA20090824TUL04Door · crackedNUMBER 9 SLAT INBOARD DRIVE TRACK DOOR IS CRACKED. REMOVED AND REPLACED TRACK DOOR PER ESO 90249. MRT 022468 MRR/SDR ACCOMP DWMS 1213681.SDR AALA20090824TUL03Skin · crackedNUMBER 9 SLAT AT OUTBOARD DRIVE TRACK SKIN IS CRACKED AT FASTENER. INSTALLED DOUBLER PER AARD 57-43-4. MRT 022467 MRR/SDR ACCOMP. DWMS 1213686.SDR AALA20090824TUL02Skin · crackedNUMBER 9 SLAT AT INBOARD DRIVE TRACK SKIN IS CRACKED AT FASTENER. MARKED, BLENDED PRIMED AND PAINTED PER ESO 90249. MRT 022470 AND MRR/SDR ACCOMP. DWMS1213690.SDR USAA2009090192306Skin · crackedCLT - Q3 - MAJOR REPAIR - 3 CRACKS ON NR 6 SLAT LOWER TRAILING EDGE SKIN BELOW ATTACH ACTUATOR POINT. REPAIRED NR 6 SLAT LOWER TRAILING EDGE SKIN IAW B737 SRM 57-43-01 REPAIR 6.SDR IPXA09557217Closeout Panel · corrodedINSPECTION TYPE:C2 NR 2 SLAT LOWER CLOSE OUT PANEL T/E FACE SKIN CORRODED SEVERAL LOCATIONS. REMOVED AND REPLACED IAW AMM 27-81-02-4.SDR AALA20090822LAX01Slat · debondedLAX - INFLIGHT SAN-DFW. CREW REPORTED PASSENGER ADVISED FLIGHT ATTENDANT SOMETHING HAD COME OFF WING DURING TAKEOFF. EMERGENCY DECLARED, LANDED AT LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT INBOARD SLAT TRAILING EDGE DISBONDED. REPLSDR SWAA095424Skin · delaminatedDURING SCHEDULED OTS CHECK, FOUND LT WING NR 2 L/E SLAT TOP SURFACE DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.SDR SWAA095433Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT NR 1 SLAT UPPER WEDGE SKIN DELAMINATED. REMOVED AND REPLACED NR 1 SLAT PER MM.SDR USAA2009082192193Skin · debondedCLT - Q3 - MAJOR REPAIR - RIGHT WING NR 4 SLAT, TAP TEST INDICATES DISBOND AT INBOARD END OF TRAILING EDGE WEDGE LOWER SURFACE. REPAIRED RIGHT WING NR 4 SLAT AT INBOARD END OF TRAILING EDGE WEDGE LOWER SURFACE IAW B737 SRM 51-70-10.SDR UALA2009082102578Web · crackedRIGHT WING FIXED LEADING EDGE, CLOSE-OUT WEB CRACKED AT LOWER RADIUS, NR 9 SLAT, OUTBOARD EDGE AREA. MAJOR REPAIR ACCOMPLISHED. CUT OUT CRACKED AREA, FABRICATED & INSTALLED FILLER, STRAP AND REPAIR ANGLE.SDR IPXA09657250Panel · crackedINSPECTION TYPE:C LT WING NR 6 SLAT LWR CLOSURE PANEL CRACKED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 44. REPAIR PATCH SIZE 12 X 6 INCHES.SDR IPXA09657241Support Fitting · crackedINSPECTION TYPE:7C LT WING - NR 4 SLAT O/B AUX TRACK I/B FAIRING SUPPORT WEB AFT SPAR CLIP FOUND CRACKED. LT WING - NR 4 SLAT O/B AUX TRACK I/B FAIRING SUPPORT WEB AFT SPAR CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 44.SDR IPXA09657151Skin · crackedINSPECTION TYPE:C LT WING NR 4 SLAT I/B LEADING EDGE NOSE AREA RIVET HOLE FOUND CRACKED (CRACK LENGTH 0.125 INCH). LT WING NR 4 SLAT I/B AREA OSS 573 NOSE SKIN REPAIRED AS PER SRM 57-43-01- 2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR, REPSDR IPXA09657150Skin · crackedINSPECTION TYPE:C LT WING - NR 4 SLAT O/B LEADING EDGE NOSE AREA RIVET HOLE FOUND CRACKED (CRACK LENGTH 0.125 INCH). LT WING NR 4 SLAT O/B AREA OSS 641.49 NOSE SKIN REPAIRED AS PER SRM 57-43- 01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAISDR USAA2009082092187Wedge · debondedPHX - B-1 - MAJOR REPAIR - NR 6 LEADING EDGE SLAT DISBONDED ON AFT FACE UPPER WEDGE 24-30 INCHES. REPLACED NR 6 LEADING EDGE SLAT.SDR SWAA095406Slat · delaminatedDURING SCHEDULED MV1 CHECK, FOUND NR 5 SLAT DELAMINATED. REMOVED AND REPLACED NR 5 SLAT PER MM.
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