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 AALA20111102TUL02Skin · corrodedNUMBER 9 SLAT HAS CORROSION ALONG BLEND, UPPER SKIN SURFACE ABOVE INBOARD SLAT TRACK. REPAIRED PER AARD 57-43-00-1.SDR AALA20111102TUL01Skin · damagedNUMBER 5 SLAT SPEED TAPE INTERIM REPAIR PER EA B737-57-009067. FABRICATED AND INSTALLED PERMANENT SKIN SPLICE REPAIR OUTBOARD END NUMBER 5 SLAT PER SRM 57-42-01-2R SHEET.SDR FDEA201111014709Skin · misrepairedLT WING NR6 SLAT OTBD L/E MISREPAIRED. NR 6 SLAT REMOVED AND REPLACED AS PER AMM 27-80-30-4 REV 70.1. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-30-5 REV 70.1. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 113.SDR FDEA201111014714Skin · crackedLT WING NR 8 SLAT, INNER SURFACE FOUND CRACKED AT FASTENER HOLE. CARRIED OUT REPAIR IAW SRM 57-40-01, FIG 201, REPAIR 3, REVISION 47. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 113.SDR AALA20111029TUL01Repair · dentedRIGHT WING NUMBER 4 SLAT HAD A INTERM REPAIR ACCOMPLISHED PER SRM 57-03-00. REPLACED TEMPERATURE REPAIR BY REWORKING THE DENTED AREA TO WITHIN LIMITS GIVEN IN THE SRM 57-03-00 FIGURE 18.SDR AALA20111027TUL02Rib · crackedRIGHT NUMBER 5 LEADING EDGE SLAT OUTBOARD TRACK ATTACH BRACKET IS CRACKED. REPLACED DAMAGED RIB PER ESO 80117 CH 27-80-1.SDR HALA2011102600526Skin · debondedNR 11 SLAT UPPER SKIN ON T/E WEDGE DEBONDED & CORRODED. REPAIRED IAW SRM 57-43-02-01 & 57-43-02-2R-1 FIG 201 & 51-70-2R-0, PARA 6 & 8.SDR HALA2011102600524Skin · corrodedNR 11 SLAT UPPER SKIN ON T/E WEDGE, DEBONDED & CORRODED. REPAIRED IAW SRM 57-43-02-01 & 57-43-02-2R-1, FIG 201 & 51-70-10-2R-0 PARA 6 & 8.SDR COEA2011102622919Rib · chafedHEAVY CK COE / MAJOR REPAIR. RT WING LOWER STRIP SLAT RIB 19-21 IN REFUEL AREA IS CHAFED. REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.SDR AALA20111027TUL01Rib · crackedRIGHT NUMBER 5 LEADING EDGE SLAT OUTBOARD TRACK ATTACH BRACKET IS CRACKED. REPLACED DAMAGED RIB PER ESO 80117 CH 27-80-1.SDR AALA20111024TUL08Skin · corrodedLEFT WING NUMBER 3 SLAT UPPER SKIN AREA CORRODED AT NOSE RIB INBOARD MAIN TRACK AREA. INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20111024TUL07Wedge · damagedAREA WORN TO CORE ON BOTTOM OF TRAILING EDGE WEDGE 33.25 INCHES FROM INBOARD SIDE ON AFT EDGE. INSTALLED DOUBLERS AND HOT BONDED AREA PER SRM 51-70-10.SDR AALA20111024TUL06Wedge · damagedNUMBER 3 SLAT TRAILING EDGE WEDGE UPPER SURFACE HAS TWO AREAS OF DISBOND APPROXIMATELY MID-SPAN. HOT-BONDED BOTH AREAS OF DISBOND PER SRM 51-70-10.SDR AALA20111024TUL05Wedge · damagedNUMBER 3 SLAT TRAILING EDGE WEDGE HAS AREA OF DISBOND ON UPPER OUTBOARD END. INSTALLED AND HOT BONDED DOUBLERS PER SRM 51-70-10.SDR SWAA117272Skin · puncturedDURING SCHEDULED HC2 CHECK, FOUND RT WING L/E UPPER SKIN NR 5 SLAT PUNCTURED. REPAIRED SLAT PER EA.SDR USAA2011102600018Panel · crackedC3 CHECK - CRACK ON NR 1 LEFT WING SLAT COVE PANEL AT INBOARD MAIN TRACK. REPLACED NR 1 LEFT WING SLAT COVE PANEL AT INBOARD MAIN TRACK IAW BOEING DRAWINGS 114N4075 AND 114N4002.SDR SWAA117280Slat · damagedDURING SCHEDULED 2HC1 CHECK, FOUND RT WING NR 6 I/B SLAT CAN DAMAGED AT AFT UPPER WELD SEAM. REMOVED AND REPLACED SLAT CAN PER EA.SDR FDEA201110224619Skin · dentedLT WING SLAT NR 12 FOUND TOP SURFACE NICKED DURING GROUND CREW CHECK NR1 SLAT (LT) NR B6224-509, SN 48476, SRM 57-00-00, FIGURE 202, LT WING NR 1 SLAT XIS 188 NICK BLENDOUT TO 1.0" RADIUS. DEEPEST MEASURED 0.033" AND REPROTECTED IAW SRM 51-21-01, REV 47. ACSDR FDEA201110214616Panel · crackedLT WING NR 1 COVE PANEL INBD SIDE OF INBD TRACK MOUNT FITTING CRACKED. R & R COVE PANEL ON LT WING NR 1 SLAT ON MAE TRAVELER T911/900901 IAW SRM 51-40-02.SDR FDEA201110214615Panel · crackedLT WING NR 1 SLAT COVE PANEL OTBD SIDE OF INBD TRACK MOUNT FITTING CRACKED. R & R COVE PANEL ON LT WING NR 1 SLAT ON MAE TRAVELER NR T11/900902 IAW SRM 51-40-02.SDR IPXA11170014Skin · dentedINSPECTION TYPE:3C, LT WING OTBD FLAP L/E HAS A DENT AT NOSE SKIN BETWEEN RIBS 3 AND 4. ACCOMPLISHED REPAIR ON LT WING OTBD FLAP L/E NOSE SKIN AT RIBS 3 AND 4 IAW EO A300-5750-44826-A, PARA 6A.SDR FDEA201110194591Panel · crackedRIGHT WING NR 8 SLAT COVE PANEL INBD SIDE OF INBD SLAT TRACK MOUNT FITTING CRACKED. REMOVED AND REPLACED COVE PANEL IAW SRM 51-40-02. MAJOR REPAIR.SDR FDEA201110194589Panel · crackedLEFT WING NR 1 COVE PANEL INBD SIDE OF OTBD SLAT TRACK MOUNT FITTING CRACKED. REMOVED SLAT TRACK IAW AMM 27-81-12-4. REMOVED DAMAGED COVE PANEL AND INSTALLED SERVICEABLE FABRICATED PART IAW SRM 51-40-02. TREATED AND PRIMED AREA IAW SRM 51-20-01. REINSTALLESDR SWAA117180Slat · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED ON O/B AFT END. REMOVED AND REPLACED NR 2 SLAT PER MM.SDR SWAA117179Slat · wornDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT O/B SLAT CAN WORN. REMOVED AND REPLACED NR 5 SLAT CAN PER MM.SDR SWAA117178Slat · wornDURING SCHEDULED HC2 CHECK, FOUND RT WING NR 5 L/E SLAT I/B SLAT CAN WORN. REMOVED AND REPLACED NR 5 SLAT CAN PER MM.SDR SWAA117177Slat · wornDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 L/E SLAT O/B SLAT CAN WORN. REMOVED AND REPLACED NR 2 SLAT PER MM.SDR USAA2011101900003Panel · crackedC3 CHECK - CRACK ON NR 9 SLAT COVE PANEL 11.5 INCHES FROM TRAILING EDGE UPPER SURFACE AND 32 INCHES FROM INBOARD END. REPLACED COVE PANEL 11.5 INCHES FROM TRAILING EDGE UPPER SURFACE AND 32 INCHES FROM INBOARD END ON NR 9 SLAT IAW BOEING DRAWING 14N4003.SDR USAA2011101900002Panel · crackedC3 CHECK - CRACK ON NR 9 SLAT COVE PANEL 11 INCHES FROM TRAILING EDGE UPPER SURFACE AND 1 INCH FROM INBOARD END. REPLACED COVE PANEL 11 INCHES FROM TRAILING EDGE UPPER SURFACE AND 1 INCH FROM INBOARD END ON NR 9 SLAT IAW BOEING DRAWING 14N4003.SDR AALA20111015TUL03Skin · damagedLEFT WING WORN AREA ON UPPER TRAILING EDGE OF NUMBER 3 SLAT BOTTOM SIDE FROM CONTACT WITH HIGH SPOT IN FIXED LEADING EDGE. INSTALLED FLUSH DOUBLER PER SRM 51-70-10-2R.SDR SWAA117060Skin · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING NR 3 SLAT LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.SDR HALA2011101100467Wedge · damagedDEBONDED AND CORE DAMAGED TO NR 11 SLAT IN T/E WEDGE. REPAIRED IAW SRM 57-43-02/2RO1 & 51-70-10, PARA'S 10,14 & 15 REV 87.SDR UALA2011101205549Skin · damagedSLAT NR 4 WAS HIT BY BIRD. ACCOMPLISH INSPECTION OR RECHECK REQUIRED BY CF9055. SLAT NR 4 WAS HIT BY BIRD CAUSING DAMAGE MEASURING 10 INCHES LONG X 3 INCHES WIDTH X 3-32 DEEP. VISUAL INSPECTION WAS PERFORMED AND NO OTHER DAMAGES LIKE CRACKS, LOOSE RIVETS ORSDR USAA2011100700016Slat · debondedC3 CHECK - DISBOND ON LEFT WING 3 SLAT BETWEEN WS425.5. TO WS565.5. REPAIRED NR 3 SLAT IAW B757 CMM 57-43-18, B757 SRM 51-70-10 & EA 141753.SDR USAA2011101000022Skin · debondedC1 CHECK - DISBONDING ON UPPER SURFACE OF NR 9 SLAT TRAILING EDGE WEDGE. REPAIRED UPPER SURFACE OF NR 9 SLAT TRAILING EDGE WEDGE IAW B757 SRM 57-43-02 & 51-70-10.SDR ASAA11410466Skin · crackedNR 1 SLAT L/E BULLNOSE SKIN LOWER SURFACE CRACKED AT CENTER AUX TRACK ATTACH AREA 1.5FT FROM AFT EDGE. REPAIRED PER SRM 57-43-01.SDR AALA20111004TUL07Skin · corrodedUPPER SKIN ON NUMBER 8 LEADING EDGE SLAT CORRODED AT OUTBOARD TRACK. CORROSION REMOVED PER SRM 51-10-02-0G. FABRICATED AND INSTALLED FLUSH DOUBLERS PER AARD 57-43-00-1.SDR AALA20111004TUL04Slat · corrodedNUMBER 8 SLAT 44.5 INCHES FROM OUTBOARD END CORRODED. FABRICATED AND INSTALLED FLUSH DOUBLERS PER AARD 57-43-00-1.SDR AALA20111004TUL03Slat · corrodedNUMBER 8 SLAT 58.25 INCHES FROM INBOARD END CORRODED. CORROSION REMOVED PER SRM 51-10-02-0G. FABRICATED AND INSTALLED FLUSH DOUBLERS PER AARD 57-43-00-1.SDR F3LA2011100400681Skin · dentedREF NR 36183, DENT ON THE L/E RT NR 1 SLAT IS BEYOND LIMITS. REPAIRED NR 1 RT SLAT PER SRM 57-40-00 PB201 , PARAGRAPH 5.D.3, FIGURE 204 SHEET 6.SDR ASAA11410438Skin · delaminatedRT WING NR 6 UPPER COMPSITE SURFACE DELAMINATED AT I/B CORNER. REPAIRED THE DAMAGED AREA OF THE NR 6 SLAT UPPER SURFACE I/B CORNER IAW B737 400 SRM 51-70-10 REPAIR 4.SDR ASAA11410437Skin · delaminatedRT WING NR 5 SLAT UPPER COMPOSITE SURFACE DELAMINATED AT I/B CORNER. REPAIRED THE DAMAGED AREA OF THE RT WING NR 5 SLAT UPPER SURFACE I/B CORNER IAW B737 400 SRM 51-70-10 REPAIR 4.SDR ASAA11410436Skin · delaminatedRT WING NR 5 SLAT UPPER COMPSITE SURFACE DELAMINATED AT O/B CORNER. REPAIRED THE DAMAGED AREA OF THE NR 5 SLAT UPPER SURFACE O/B CORNER IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA11410434Skin · chafedRT WING NR 4 SLAT CHAFE AT LOWER SURFACE AFT END IN NUMBEROUS PLACES. REPAIRED CHAFE DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 4 PAGE 201.SDR ASAA11410433Skin · delaminatedRT WING NR 4 SLAT UPPER COMPOSITE SURFACE DELAMINATED AT I/B CORNER. REPAIRED DELAMINATION DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 4 PAGE 201.SDR FDEA201110014260Fitting · corrodedLT WING NR3 SLAT MIDDLE ATTACHMENT FITTING FOUND CORRODED AFTER SLAT REMOVAL. REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 SRM 57-40-02 REV 47, FIGURE 201. ORIGINAL DIAMETER = 0.5015 INCH, REWORKED DIAMETER = 0.5785 INCH, MAXIMUM DIAMETER = 0.625 INCH. REPASDR AALA20111002TUL04Skin · corrodedLEFT WING NUMBER 2 SLAT HAS CORROSION ON LOWER SKIN AT INBOARD MAIN TRACK APPROXIMATELY 31 INCHES OUTBOARD FROM INBOARD END OF SLAT. REMOVED CORROSION FROM SKIN PER SRM 57-43-01-1A AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20111002TUL03Skin · corrodedLEFT WING NUMBER 2 SLAT HAS CORROSION ON LOWER SKIN AT OUTBOARD MAIN TRACK APPROXIMATELY 30 INCHES INBOARD FROM OUTBOARD END OF SLAT. REMOVED CORROSION FROM SKIN PER SRM 57-43-01-1A AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20111001TUL02Skin · corrodedLEFT WING NUMBER 2 SLAT HAS CORROSION ON LOWER SKIN AT INBOARD MAIN TRACK APPROXIMATELY 31 INCHES OUTBOARD FROM INBOARD END OF SLAT. INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20111001TUL01Skin · corrodedLEFT WING NUMBER 2 SLAT HAS CORROSION ON LOWER SKIN AT OUTBOARD MAIN TRACK APPROXIMATELY 30 INCHES INBOARD FROM OUTBOARD END OF SLAT. INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.
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