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 DALA1144315656Wedge · damagedNR 5 SLAT T/E WEDGE HAS MULTIPLE HAIL STRIKES. REMOVED AND REPLACED NR 5 SLAT PER B757 AMM 27-81-01.SDR DALA1144305656Wedge · damagedNR 10 SLAT T/E WEDGE HAS MULTIPLE HAIL STRIKES. REMOVED AND REPLACED NR 10 SLAT PER B757 AMM 27-81-02.SDR DALA1144295656Wedge · damagedNR 2 SLAT T/E WEDGE HAS MULTIPLE HAIL STRIKES. REMOVED AND REP NR 2 SLAT PER B757 AMM 27-81-02 SLAT, NR 2 L/E; OFF 56-5754-9-0002 90039 ON 56-5754-9-0002 10748.SDR IPXA1668100Wedge · crackedINSPECTION TYPE:C 1 LT WING NR 4 SLAT T/E WEDGE ASSY LOWER SKIN BROKEN AT OSS 564. CRACK DIMENSION ABOUT 0.4" X 0.3" CUT THE LOWER SKIN 0.5" X 0.375" X 1", AND UPPER SKIN ABOUT 5.375" X 2". REPAIR IAW REV: 49 SRM 57-43-02 REPAIR 1, FIGURE 201 AND SRM 51-70-10 SDR SWAA115156Skin · crackedDURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT L/E LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM AND DWG.SDR FDEA201107172776Slat Track · crackedRT WING L/E NR 8 SLAT TRACK CUTOUT FOUND CRACKED. SKIN REPAIR CARRIED OUT IAW EA 1-5730-150769, TITLE: WINGS - PLATES AND SKIN - RT WING L/E SKIN REPAIR AT NR 8 SLAT TRACK CUTOUT. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112. RT NR 4 SLAT ASSY REMOVESDR DALA1505133244Skin · chafedRT WING NR 2 SLAT INBD T/E LOWER SURFACE IS CHAFED, REPAIRED IAW SRM 51-23-11.SDR AALA20110710TUL02Skin · crackedCRACK IN COVE SKIN 29 INCHES FROM END OF NUMBER 9 SLAT. STOPPED DRILLED END OF CRACK. HFEC SURFACE SCAN CONFIRMS CRACK TERMINATION AT STOP DRILL. FABRICATED AND INSTALLED REPAIR PER AARD 57-43-00-4.SDR AALA20110710TUL01Wedge · debondedDISBOND FOUND ON NUMBER 8 RIGHT OUTBOARD SLAT TRAILING EDGE WEDGE. REPLACED TRAILING EDGE WEDGE.SDR FDEA201107092630Skin · dentedLT WING NR 8 SLAT L/E HAS SEVERAL DENTS. FABRICATED REPAIR PARTS, UPPER AND LOWER DOUBLER, SPLICE PLATE, BAFFLES, UPPER AND LOWER SEAL, AND FILLER. INSTALLED REPAIR PARTS IAW SRM 57-10-00 VOL VI FIG 11. CLASSIFIED AS A MAJOR REPAIR.SDR USAA2011072100023Attach Bolt · corroded2S CHECK - CORROSION ON LEFT WING 12 SLAT TRACK ATTACH BOLT AT WS 14057, RIB 26. REPLACED LEFT WING 12 SLAT TRACK ATTACH BOLT IAW A319 AMM 27-84-67.SDR UIEA2011070200358Web · crackedRT WING NR 15 K/FLAP FOLDING FAIRING MID FTG LWR WEB FOUND CRACK. (LWR WEB REPAIR ACCOMPLISHED IAW RS 57-50-37143, REV A.)SDR USAA2011072200013Attach Bolt · corroded2S CHECK - CORROSION ON ATTACHMENT BOLT OF RIGHT WING 4 SLAT TRACK AT WS 3059, RIB 6. REPLACED ATTACHMENT BOLT OF RIGHT WING 4 SLAT TRACK IAW A319 AMM 27-84-63.SDR SWAA114712Slat · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT DELAMINATED. REMOVED AND REPLACED NR 1 SLAT PER MM.SDR UALA2011062903217Panel · crackedRIGHT WING ROOT-LEADING EDGE SLAT IS CRACKED ABOVE ACCESS PANEL. REFERENCE CF182-UPPER LEADING EDGE IS CRACKED, NOT DELAMINATED. CORRECTION THIS IS A LEADING EDGE CLOSER PANEL AND NOT THE HALF MOON SHAPED PANEL. CRACK IS 3 INCH X 1.25. PICS ON RVI. REPAIREDSDR SWAA114620Slat · delaminatedDURING SCHEDULED CV CHECK FOUND, RT WING NR 5 L/E SLAT DELAMINATED AT O/B TRAILING EDGE. REMOVED AND REPLACED SLAT PER MM.SDR SWAA114605Slat · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED AT I/B AND O/B END. REMOVED AND REPLACED NR 2 SLAT PER MM.SDR FDEA201106262427Angle · crackedLT WING NR 1 SLAT HAS CRACKED LOWER ANGLE AT INBD SIDE OF SLAT, OTBD UPPER STOP PAD. REMOVED NR 1 SLAT ANGLE AND FABRICATED NEW ANGLE AND SPLICE. IAW SRM 57-50-2 FIG 2 AND 51-40-4 FIG 1. INSTALLED NEW ANGLE AND SPLICE IAW SRM 51-30-2SDR IPXA11567609Retainer · crackedINSPECTION TYPE:MOD WHILE WORKING NR 7 L/E SLAT FUNCTIONALS FOUND BULB SEAL RETAINER ON THE SLAT COVE CRACKED, OTBD END, REMOVED RETAINER, FABRICATED REPLACEMENT, AND INSTALLED RETAINER IAW DWG 114N4046, SRM 51-40-05-0G, AND SOPM 20-50-01.SDR FDEA201106232402Skin · dentedRT WING NR 6 SLAT HAS NUMEROUS DENTS ALONG NOSE SKIN.SDR FDEA201106222379Skin · dentedNR 5 SLAT UPPER SKIN INBD OF FENCE HAS A DENT. CUT OUT DAMAGE 5 3/4" X 3 1/2" IAW SRM 57-50-3 FIG1 REV. 103, FABRICATED FILLER IAW SRM 57-50-3. FABRICATED DOUBLER IAW SRM 57-50-3. INSTALLED FILLER & DOUBLER IAW SRM 51-30-2.SDR FDEA201106202349Mount · crackedNR 8 SLAT INBD TRACK MOUNT OTBD CORNER IS CRACKED IN RADIUS. STOP DRILLED CRACK, FABRICATED & INSTALLED REPAIR DOUBLER AT NR 8 SLAT IB TRACK MOUNT IAW SRM 51-10-2, SRM 51-10-1, SRM 51-30-2, & DWG SR27-57-034 & EA 7-5750-136792.SDR UALA2011061702979Skin · damagedLEFT L/E HALF MOON PANEL & SLAT WEDGE PANEL JUST ABOVE ARE DAMAGED WITH HALF MOON PANEL HAVING SECTION MISSING. LEFT NR 6 LEADING EDGE SLAT HAS DAMAGE. ACCOMPLISHED VISUAL INSPECTION OF ADJACENT AREA AND ASSURE NO FURTHER DAMAGE TO SLAT OR WING PANEL. APPLISDR USAA2011071100005Skin · delaminatedQ4 CHECK - DELAMINATION ON NR 5 SLAT SKIN AT LOWER TRAILING EDGE 5 INCHES FROM OUTBOARD END. REPAIRED NR 5 SLAT SKIN AT LOWER TRAILING EDGE 5 INCHES FROM OUTBOARD END IAW EA 103090.SDR SWAA114450Wedge · delaminatedDURING SCHEDULED 26Y CHECK, FOUND RT WING O/B NR 4 SLAT WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR ABXA2011061557Spar Cap · corrodedCORROSION ON UPPER CAP OF FRONT SPAR LES 452 JUST INBOARD OF "T" DUCT. CUT OUT CORRODED SECTIONS OF UPPER SPLICE PLATE AND REPAIRED IAW REA B657-593.SDR SWAA114388Skin · crackedDURING SCHEDULED OTS CHECK, FOUND LT WING NR 2 SLAT O/B SKIN CRACKED. REPAIRED SKIN PER SRM.SDR UALA2011061502940Slat · damagedRT WING NR 8 LEADING EDGE SLAT HAS DAMAGE.SDR FDEA201106142226Skin · dentedRT WING INBD FLAP LOWER SURFACE BETWEEN RIB 1C AND RIB 3 AT APPROX 25 INCH FROM FORWARD EDGE, FOUND WITH A SMOOTH DENT.SDR ABXA2011061462Spar Cap · corrodedCORROSION ON FRONT SPAR UPPER CAP BEHIND NR 9 SLAT INBOARD AUX TRACK. REPAIRED SPAR IAW REA B657-59317.SDR SWAA114328Slat · delaminatedDURING SCHEDULED 26Y CHECK, FOUND RT WING O/B NR 5 SLAT DELAMINATED. REPAIRED SLAT PER SRM.SDR SWAA114305Wedge · delaminatedDURING SCHEDULED 26Y CHECK, FOUND LT WING I/B NR 2 SLAT WEDGE DELAMINATED. REPAIRED WEDGE IAW SRM.SDR ABXA2011061356Skin · corrodedNR 2 SLAT LEADING EDGE UPPER SURFACE HAS AREA OF CORROSION AROUND FASTENER HAD AT APPROX WS 880. REMOVED AND INSTALLED NR 2 I/B AUX TRACK IAW B767 SRM 57-43-01 AND PANEL IAW B767 SRM 51-40-02. BLENDED CORROSION FOUND TO BE OUT OF LIMITS.SDR SWAA114287Skin · crackedDURING SCHEDULED MV2 CHECK, FOUND RT WNG NR 6 L/E SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR DALA1146399880Skin · gougedRT WING NR 1 SLAT PANEL INBOARD LOWER SKIN WITH GOUGE DUE TO CHAFING WITH L/E (MMO89) BLENDED AREA ON LWR SKIN INBD ON RT WING NR 1 SLAT REF DC9 SRM 57-01 FIG 1. BLENDED AREA FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NR 1 RT SLAT IAW AMM DC9-27-80-01SDR IPXA11667254Skin · bulgedINSPECTION TYPE:8C, LT WING NR3 SLAT WEDGE AREA UPPER SURFACE NEAR INBD EDGE FOUND BULGE. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1, REV 50.SDR SWAA114208Skin · crackedDURING SCHEDULED 2HC2 CHECK FOUND, LT WING NR 2 SLAT L/E SKIN CRACKED. REPAIRED SKIN PER SRM.SDR SWAA114202Skin · crackedDURING SCHEDULED HC2 CHECK FOUND, LT WING NR 1 SLAT L/E SKIN CRACKED. REPAIRED SKIN PER SRM.SDR AALA20110608TUL08Skin · dentedLEFT WING AT NUMBER 2 SLAT, UPPER SKIN, 42 INCHES FROM OUTBOARD END 7 INCHES FROM LEADING EDGE DENT IN SKIN. CUT OUT DENT AND CORROSION THEN INSTALLED FLUSH DOUBLER PER AARD 57-43 00-1.SDR AALA20110608TUL07Skin · corrodedCORROSION AROUND FASTENER ON TOP 57 INCHES FROM INBOARD END. REMOVED CORROSION FROM TOP SKIN 57 INCHES FROM END AND INSTALLED DOUBLER PER AARD 57-43-00-1.SDR IPXA11567320Wedge · chafedINSPECTION TYPE:C1 NR7 SLAT T/E WEDGE LOWER SURFACE HAS OUT OF ALLOWABLE DAMAGE CHAFING AT T/E, .75" TO 20" FROM INBD END. REPLACED DUE TO EXCESSIVE DAMAGES.SDR UALA2011060802817Slat Track · damagedRIGHT WING NR 8 SLAT OB AUXILIARY TRACK HARDWARE MISSING. WU 40267. REPLACED NR 8 SLAT OUTBOARD AUX TRACK HARDWARE PER MM.SDR AALA20110607TUL05Skin · corrodedNUMBER 10 SLAT UPPER SKIN 67 INCHES FROM INBOARD END HAS CORRODED FASTENER. FABRICATED DOUBLERS AND FILLER REPAIR PER AARD 57-43-001.SDR AALA20110607TUL02Skin · corrodedLEFT WING, AT NUMBER 3 SLAT, 35 INCHES FROM INBOARD END, TOP SKIN, 8 INCHES FROM LEADING EDGE SKIN CORRODED. INSTALLED FLUSH SKIN REPAIR ON NUMBER 3 SLAT PER AARD 57-43-01.SDR ABXA2011060659Rib · corrodedNR 11 SLAT OUTBOARD AUX TRACK ATTACH FITTING INBOARD RIB HAS CORROSION AROUND NUT PLATE. REMOVED AND REPLACED NR 11 SLAT O/B AUX TRACK I/B RIB ASSY IAW B767 SRM 51-40-02.SDR AALA20110606TUL03Skin · debondedRIGHT WING NUMBER 9 SLAT HAS DENT WITH DISBOND INDICATIONS ON TOP AND BOTTOM SKINS 43 INCHES INBOARD OF OUTBOARD END. REMOVED DAMAGED AREA AND INSTALLED EXTERNAL HOT BOND DOUBLER REPAIR PER SRM 51-70-10-2R.SDR ABXA2011060458Rib · corrodedNR 12 SLAT INBOARD AUX TRACK OUTBOARD FITTING ATTACH RIB CORRODED AT NUT PLATE AND FITTING SHIM PACK CORRODED. REMOVED AND REPLACED NR 12 SLAT I/B AUX TRACK O/B RIB ASSY IAW B767 SRM 51-40-02.SDR AALA20110604TUL05Skin · corrodedNUMBER 8 SLAT CORROSION AROUND FASTENER APPROXIMATELY 2 INCH FROM OUTBOARD END OF SLAT IN UPPER SKIN ALONG TRAILING EDGE. REMOVED CORROSION PER AARD PER 57-43-00-3 ON OUTBOARD AFT UPPER END OF SLAT SKIN. INSTALLED DOUBLER PER AARD 57-43-00-1.SDR AALA20110604TUL01Skin · corrodedRIGHT WING NUMBER 7 SLAT LEADING EDGE HAS SKIN CORROSION, ADJACENT TO A FASTENER LOCATION ON THE LEADING EDGE SKIN SURFACE APPROX 2.5 FEET INBOARD OF THE OUTBOARD EDGE. CORROSION BLENDED TO FINAL SKIN THICKNESS OF .023 INCH. CUT OUT DAMAGE PER AARD. FABRICASDR ABXA2011060364Rib · corrodedNR 12 SLAT INBOARD AUX TRACK OUTBOARD FITTING ATTACH RIB CORRODED AT NUT PLATE. REMOVED AND REPLACED NR 12 SLAT I/B AUX TRACK I/B ATTACH RIB IAW B767 SRM 51-40-02.
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