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 FDEA200911184014Skin · damagedRT WING - NR 5 L/E SLAT UPPER SURFACE INBD EDGE FOUND EDGE CUT. REPAIR CARRIED OUT IAW EA 1-5740-132271. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108.SDR FDEA200911184011Skin · crackedRT WING NR 9 SLAT AT OTBD TRACK ATTACHMENT SKIN CRACKED AROUND ATTACH POINTS. REMOVED PANEL 624GB ,OTBD RIB, SEAL RETAINER, SEAL, AND CRACKED COVE PANEL FROM OTBD NR 9 SLAT AT WS 565-WS 681. IAW SRM 51-40-02. FABRICATED NEW COVE PANEL IAW SRM 57-43-05 FIG 1 ASDR FDEA200911184007Skin · crackedNR 5 SLAT UPPER SKIN CRACKED AT INBD SLAT HOOK MOUNT SCREW. REMOVED THE HOOK FOR ACCESS IAW SRM 51-30-2. STOP DRILLED CRACK IAW SRM 51-10-1. C/W HFEC INSP IAW NDTM PT 6, 51-00-00 FIG 23. CRACK END IN STOP DRILL HOLE. FAB REPAIR DOUBLER MAT USED 2024 T3 .125" SDR ASAA0947055Wedge · damagedNR 6 SLAT AFT I/B CORNER DAMAGED. REMOVED DAMAGE FABBED FILLER & DOUBLER, BONDED REPAIR IAW B737 400 SRM 51 70 10 REPAIR 4.SDR SWAA097312Wedge · delaminatedDURING SCHEDULED HC2 CHECK, FOUND NR 2 L/E SLAT T/E WEDGE DELAMINATED. REPAIRED SLAT PER SRM.SDR QXEA2009111800965Skin · chafedLT WING INBD SLAT LWR T/E CHAFED AT WING PICCILLO TUBE CONNECTION AND INBD ELECTRICAL CONNECTOR. BLENDED DAMAGED AREA IAW 51-21-00-001-001-A01. REQUESTED REO REPAIR FROM MFG. PERFORMED LPI, NO CRACKS OR CHAFING FOUND AT THIS TIME IAW LPI NDTM 51-20-006. TRSDR 2009F00113Skin · debondedWHILE PERFORMING ULTRASONIC INSP IAW AD 93-14-19, SKIN TO CORE DISBAND IS DETECTED IN THE UPPER AND LWR SURFACES OF SLAT POSITION 8 T/E WEDGE AT AFT INBD CORNER AREA.SDR 2009F00110Skin · debondedWHILE PERFORMING ULTRASONIC INSP IAW AD 93-14-19, SKIN TO CORE DISBAND IS DETECTED IN THE UPPER AND LWR SURFACES OF SLAT POSITION 8 T/E WEDGE AT AFT INBD CORNER AREA.SDR SWAA097191Skin · crackedDURING SCHEDULED MV2 CHECK, FOUND NR 7 L/E SLAT SKIN CRACKED. REPAIRED SLAT SKIN PER EA.SDR SWAA097187Skin · crackedDURING SCHEDULED 6Y CHECK, FOUND NR 7 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.SDR UALA2009111603562Structure · damagedNUMBER 16 LE KRUEGER FLAP DAMAGED AND MISSING CORNER DUE TO BIRD STRIKE. (INBD OF NR 3 ENGINE). SUPPLEMENTAL DATA UPDATE REMOVED NR 16 KRUEGER FLAP. INSTALLED ROBBED FLAP & TORQUED. COULD NOT RIG DUE TO FLAP OUTBOARD EDGE INTERFERRING WITH PYLON, WILL NEED TRSDR UALA2009111603561Skin · damagedNR 15 L/E KRUEGER FLAP HAS SURFACE DAMAGE, APPROX 4 SQ INCHES DUE TO BIRD STRIKE (2ND I/B OF NR 3 ENG). REMOVED NR 15 KRUEGER FLAP. INSTALLED ROBBED FLAP, BOLTS ARE NOT TORQUED AND BONDING STRAPS ARE NOT CONNECTED. COMPLETED TORQUE OF NR 15 KRUEGER FLAP. RSDR USAA2009111793120Wedge · delaminatedBFM - C1 - MAJOR REPAIR - NR 4 SLAT T/E WEDGE DELAMINATED AT OSS682.74 & OSS628. REPAIRED NR 4 SLAT T/E WEDGE IAW B767 SRM 57-43-43 & 51-70-10.SDR SWAA097197Skin · crackedNR 2 L/E SLAT SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.SDR ASAA0946984Skin · chafedLT NR 3 L/E SLAT INBD LWR SURFACE CHAFED ON AFT CORNER. REPAIRED DAMAGE AT INBD LOWER SURFACE.SDR ASAA0946985Skin · chafedRT NR 4 LE SLAT INBD UPPER AFT LOWER SKIN IS CHAFED. REPAIRED NR 4 SLAT.SDR USAA2009111193084Slat · corrodedBFM - C4 - MAJOR REPAIR - CORROSION AROUND FASTENERS ON NR 8 SLAT AT WS 509.50. REPLACED NR 8 SLAT AT WS 509.50 IAW B757 AMM 27-81-02.SDR NOCA06209Repair · crackedREPAIR ANGLE CRACKED L/E STA 690 AT INBOARD END OF NR 10 SLAT. REPLACED ANGLE AS PER SRM 51-40-02.SDR NOCA06109Repair · crackedRIB STIFFENER REPAIR IS CRACKED L/E STA 690 AT FWD END OF NR 10 SLAT. REPLACED ANGLE AS PER SRM 51-40-02.SDR SWAA097245Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA097244Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR AALA20091108TUL11Skin · damagedRIGHT WING NUMBER 8 SLAT HAS DEEPLY BLENDED AREA. REMOVED DAMAGED SKIN INSTALLED DOUBLER PER AARD 57-43-00-1.SDR AALA20091108TUL10Skin · bulgedRIGHT WING NUMBER 8 SLAT SKIN BULGED TOP UPPER SURFACE SKIN AT STATION 460 FORWARD OF MAIN DRIVE TRACK. REMOVED DAMAGED SKIN, INSTALLED DOUBLER PER AARD 57-43-00-1.SDR AALA20091108TUL09Skin · corrodedNUMBER 8 SLAT HAS CORROSION AROUND FASTENER 18.5 INCHES FROM OUTBOARD END ON NOSE SKIN {TOP}. REMOVED DAMAGED SKIN AND INSTALLED FLUSH REPAIR PER AARD 57-43-00-1.SDR AALA20091108TUL08Skin · damagedNUMBER 8 SLAT TWO {2} SCREWS INSTALLED ON THE LEADING EDGE SKIN AT THE AFT END 32 INCHES FROM THE OUTBOARD END. REMOVED FASTENERS AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20091108TUL07Skin · damagedNUMBER 8 SLAT HAS PREVIOUS BLEND AROUND FASTENER ON NOSE SKIN {TOP}. REMOVED DAMAGED AREA OF SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20091108TUL06Skin · damagedNUMBER 8 SLAT HAS A BLENDED AREA WITH A BLIND FASTENER INSTALLED IN THE LEADING EDGE SKIN 45 .75 INCHES FROM THE INBOARD END. REMOVED DAMAGED AREA AND INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.SDR AALA20091108TUL05Skin · damagedNUMBER 8 SLAT HAS A SCREW IN THE LEADING EDGE SKIN 34 INCHES FROM THE INBOARD END. REMOVED FASTENER AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1.SDR AALA20091108TUL04Wedge · delaminatedNUMBER 4 SLAT INBOARD UPPER TRAINING EDGE WEDGE DELAMINATED. REMOVED DAMAGED TRAILING EDGE INSTALLED NEW WEDGE PER ESO 90248.SDR AALA20091108TUL03Skin · corrodedNUMBER 7 SLAT HAS CORROSION AROUND FASTENER 32 INCHES FROM OUTBOARD END ON NOSE {TOP}. REMOVED AFFECTED AREA AND INSTALLED FLUSH REPAIR AS PER SRM 57-43-01-2R AND AARD 51-43-00-1.SDR AALA20091108TUL02Skin · corrodedNUMBER 7 SLAT HAS CORROSION ON SKIN FROM INBOARD END. REMOVED AFFECTED AREA AND INSTALLED FLUSH REPAIR AS PER SRM 57-43-01-2R AND AARD 51-43-00-1.SDR AALA20091108TUL01Skin · corrodedNUMBER 7 SLAT HAS A CORROSION BLISTER NEXT TO THE FASTENER 63 .75 INCHES FROM THE OUTBOARD END ON THE LEADING EDGE SKIN. REMOVED AFFECTED AREA AND INSTALLED FLUSH REPAIR AS PER SRM 57-43-01-2R AND AARD 57-43-00-1.SDR UALA2009110903492Wedge · missingA SECTION OF RIGHT INBOARD SLAT TRAILING EDGE WEDGE IS MISSING. INSTALLED NEW NR 6 SLAT. ACCOMPLISHED INSPECTION OF NR 6 SLAT INSTALLATION. ACCOMPLISHED TEST OF L/E SLAT INSTALLATION. OP CHECKS GOOD.SDR AALA20091107TUL04Skin · corrodedRIGHT WING NUMBER 7 SLAT SKIN BULGED AT TOP UPPER SURFACE SKIN STATION 350 FORWARD OF MAIN DRIVE TRACK. REMOVED DAMAGE PER SRM 57-43-00-2R PG 1 AND INSTALLED FLUSH DOUBLER REPAIR PER SRM 57-43-00-2R PG 2.SDR AALA20091107TUL02Skin · corrodedCORROSION ON NUMBER 3 SLAT UPPER SKIN AROUND FASTENER APPROXIMATELY 69 INCHES FROM INBOARD END. CUT OUT CORROSION AREA AND INSTALLED FLUSH DOUBLER PER AARD 57-43-00-1 PAGE 1.SDR ASAA0997015Doubler · chafedNR 7 SLAT T/E WEDGE PREVIOUS REPAIR DOUBLER CHAFED OUT OF LIMITS. REMOVED DAMAGED SECTION OF T/E WEDGE, FABRICATED CORE PLUG FILLER AND DOUBLER AND INSTALLED.SDR ASAA0996969Wedge · chafedNR 2 SLAT TE WEDGE PREVIOUS REPAIR DOUBLER CHAFED OUT OF LIMITS, INBD END. REMOVED PREVIOUS REPAIR FROM LOWER SKIN REMOVED HONEYCOMB CORE INSTALLED DOUBLER FILLER HONEYCOMB CORE AND EXTERNAL DOUBLER TO UPPER SKIN.SDR ASAA0996968Wedge · chafedNR 6 SLAT TE WEDGE PREVIOUS REPAIR DOUBLER CHAFFED OUT OF LIMITS, OTBD END. REMOVED PREVIOUS REPAIR FROM LOWER SKIN REMOVED HONEYCOMB CORE INSTALLED DOUBLER FILLER HONEYCOMB CORE AND EXTERNAL DOUBLER TO UPPER SKIN.SDR ASAA0996967Wedge · chafedNR 7 SLAT TE WEDGE PREVIOUS REPAIR DOUBLER CHAFED OUT OF LIMITS, OTBD INBD CENTER AREAS. REMOVED PREVIOUS REPAIR FROM LOWER SKIN REMOVED HONEYCOMB CORE INSTALLED DOUBLER FILLER HONEYCOMB CORE AND EXTERNAL DOUBLER TO UPPER SKIN.SDR ASAA0996970Wedge · chafedNR 8 SLAT TE WEDGE PREVIOUS REPAIR DOUBLER CHAFED OUT OF LIMITS, INBD OTBD CENTER END. REMOVED PREVIOUS REPAIR FROM LOWER SKIN REMOVED HONEYCOMB CORE INSTALLED DOUBLER FILLER HONEYCOMB CORE AND EXTERNAL DOUBLER TO UPPER SKIN.SDR AALA20091106TUL06Skin · damagedLEFT WING NUMBER 3 SLAT LOWER SKIN TRAILING EDGE GOUGED ABOVE INBOARD DRIVE TRACK. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER PER SRM 51-70-10 2R 4 ON TRAILING EDGE ABOVE INBOARD DRIVE TRACK.SDR AALA20091106TUL04Door · crackedRIGHT WING NUMBER 7 SLAT OUTBOARD DRIVE TRACK DOOR CRACKED. INSTALLED NEW DOOR PER AARD 51-20-00-1.SDR AALA20091106TUL03Slat · damagedRIGHT WING NUMBER 7 SLAT LOWER TRAILING EDGE DAMAGED AND DEFORMED FROM INBOARD EDGE TO 4 FEET OUTBOARD. ACCOMPLISHED WET LAYUP REPAIR PER SRM 51-70-06-0G.SDR AALA20091106TUL02Fastener · damagedNUMBER 2 SLAT BLIND FASTENER HEAD DAMAGED. REMOVED DAMAGED AREA AND INSTALLED FLUSH REPAIR PER SRM-57-43-01-2R 2.SDR AALA20091106TUL01Skin · crackedNUMBER 2 SLAT BACK SIDE COVE SKIN IS CRACKED BY A FASTENER AT THE INBOARD DRIVE TRACK. INSTALLED REPAIR DOUBLER ON COVE SKIN PER AARD-57-43-00-4.SDR ASAA0997020Skin · debondedLOWER SURFACE SKIN DISBONDED ON NR 1 SLAT 3 INCHES FROM AFT EDGE ON O/B END. REMOVED DISBONDED SKIN CORE, REPLACED CORE AND INSTALLED DOUBLER.SDR ASAA0996981Wedge · chafedNR 4 SLAT TE WEDGE LOWER SURFACE INBD END IS CHAFED IN 3 AREAS. REMOVED DAMAGED SKIN INSTALLED DOUBLER FILLER AND REPLACEMENT HONEYCOMB CORE AND INSTALLED.SDR DL757100160Skin · dentedLT WING NR 5 SLAT T/E UPPER SKIN SURFACE HAS MULTIPLE DENTS, HAIL DAMAGE, LOWER SURFACE HAS 1 EA DENT/REPAIRED AT SAA SAT ON N/R CARD 140591.SDR AALA20091105TUL02Skin · damagedNUMBER NINE RIGHT OUTBOARD SLAT PLATING SEPARATING ON LEADING EDGE SKIN 26 INCHES OF OUTBOARD EDGE. REMOVED DAMAGED SKIN AND INSTALLED DOUBLER PER AARD 57-43-00-01.SDR AALA20091105TUL01Skin · crackedNUMBER NINE RIGHT OUTBOARD SLAT INNER SKIN CRACKED INBOARD OF INBOARD DRIVE ATTACH. INSTALLED DOUBLER ON SKIN PER AARD 57-43-00-4.
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