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 AWXA200701100Slat Track · corrodedMCN - MAJOR REPAIR - C-11 CHECK - NR 5988782, CORROSION ON LEFT WING NR 2 SLAT OUTBOARD TRACK, SS 665.75. REPLACED LEFT WING NR 2 SLAT OUTBOARD TRACK, SS 665.75 IAW B757-200 AMM 27-81-13-4.SDR UIEA200700356Skin · damagedLEFT WING NR 7 VARIABLE CAMBER FLAP OUTER SKIN HAS LOWER EDGE RIVETS LOOSE AND UPPER EDGE FASTENER HEADS BROKEN. REMOVED LT WING NR 7 L/E FLAP TO FACILITATE ACCESS FOR SHEET METAL REPAIR. REPLACED RIVETS AND FASTENERS AS NECESSARY AS PER SRM 51-30-02. REINSSDR DHL2007367510Web · crackedLT SLAT FOLDING NOSE HAS WEB CRACK BY O/B MOUNT. REMOVED L/W SLAT FOLDING NOSE. OPS AND ADJUSTMENT TEST PERFORMED. NO DEFECTS NOTED IAW A300 MM 27-81-34 AN 27-81-33.SDR AWXA200701105Skin · crackedMCN - MAJOR REPAIR - C-11 CHECK - NR 5988280, RIGHT WING NR 10 SLAT COVE SKIN CRACKED, OSS 797.46 - OSS 809.46. REPLACED RIGHT WING NR 10 SLAT COVE SKIN, OSS 797.46 - OSS 809.46 IAW B757-200 SRM 51-40-02.SDR AWXA200701104Skin · crackedMCN - MAJOR REPAIR - C-11 CHECK - NR 5988289, LEFT WING NR 3 SLAT COVE SKIN CRACKED, OSS 542.70 - OSS 573.30. REPLACED LEFT WING NR 3 SLAT COVE SKIN, OSS 542.70 - OSS 573.30 IAW B757-200 SRM 51-40-02.SDR AWXA200701103Skin · crackedMCN - MAJOR REPAIR - C-11 CHECK - NR 5988286, LEFT WING NR 2 SLAT COVE SKIN CRACKED, OSS 691. REPLACED LEFT WING NR 2 SLAT COVE SKIN, OSS 691 IAW B757-200 SRM 51-40-02.SDR AWXA200701102Skin · crackedMCN - MAJOR REPAIR - C-11 CHECK - NR 5988285, LEFT WING NR 2 SLAT COVE SKIN CRACKED, OSS 665.50 - OSS 677.50. REPLACED LEFT WING NR 2 SLAT COVE SKIN, OSS 665.50 - OSS 677.50 IAW B757-200 SRM 51-40-02.SDR SWAA074087Slat · delaminatedDURING SCHEDULED C2 CHECK, FOUND LEFT WING NR 3 L/E SLAT DELAMINATED AT INBOARD END. REMOVED AND REPLACED SLAT PER MM.SDR 07FDEA02960Support Fitting · brokenLEFT WING, NR 3 LEADING EDGE SLAT OUTBOARD SUPPORT FITTING BROKEN. 09-04-07 REMOVED & REPLACED AS PER AMM 27-80-30. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-80-30, FOUND SATISFACTORY.SDR ASAA0741977Skin · crackedRIGHT WING NR 6 SLAT I/B CORNER 2 INCH CRACK FOUND. RIGHT WING NR 6 SLAT I/B CORNER CRACK REPAIRED IAW SRM 57-43-01 FIG 201.SDR ASAA0741968Skin · wornNR 3 SLAT INBOARD T/E LWR SURFACE SKIN WORN. REPAIRED SLAT DAMAGE IAW SRM 51-70-10.SDR SWAA074063Slat · crackedDURING SCHEDULED 20Y CHECK, FOUND RT WING NR 5 L/E SLAT CRACKED AT LOWER INBOARD END. REPAIRED SLAT PER SRM.SDR SWAA074064Slat · crackedDURING SCHEDULED 20Y CHECK, FOUND LT WING NR 1 L/E SLAT CRACKED AT LOWER OUTBOARD END. REPAIRED SLAT PER SRM.SDR 07FDEA02947Skin · dentedSLAT 32 RT DENT IN SKIN, RIB 48 DENT IS ACCEPTABLE AS IT IS, FASTENER CHANGED TO TO NAS1739E5, APPROVED BY EA 6-5740-112472 AND RAS/FOK/183/2007 ISS A.SDR 07FDEA02935Skin · damagedOLD REPAIR ON SLAT NR 1 INBOARD EDGE WITHOUT ANY DOCUMENTATION REPAIR RENEWED IAW EA 6-5742-106524 AND RAS/FOK/148/2007 ISS A.SDR 07FDEA02902Structure · dentedRIGHT WING NR 6 SLAT FOUND WITH DENTS. 08-31-07 MEASURED AND FOUND 4 AREAS EXCEEDED LIMIT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 16 VOLUME I. ALL DENT AREAS REPROTECTED AS PER SRM 51-21-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA02900Structure · crackedLEFT WING FIXED LEADING EDGE SLAT TRACK COVER CUTOUT OUTBOARD CORNER AT STA XOS = 832, FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING FIXED LEADING EDGE STA XOS = 889 SLAT TRACK COVER CUTOUT AREA AS PER SRM 57-100-00 FIGURE 21 VOLUME I. REPAIR CLASSISDR 07FDEA02899Structure · crackedLEFT WING FIXED LEADING EDGE SLAT COVER CUTOUT OUTBOARD CORNER AT STA XOS = 774 FOUND CRACKED. 08-31-07 REPAIR CARRIED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. FABRICATED FILLER AND DOUBLER INSTALLED AS PER SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MISDR K11A2008121272016Stiffener · corrodedRT LEADING EDGE STIFFENER HAS CORROSION.SDR AWXA200701054Skin · crackedMCN - MAJOR REPAIR - C-18 CHECK - NR 5987801, RIGHT WING NR 6 SLAT LOWER SURFACE HAS 3 CRACKS, SS 292 - SS 327. REPAIRED RIGHT WING NR 6 SLAT LOWER SURFACE, SS 292 - SS 327 IAW B737-300 SRM 57-43-01-2R6, FIGURE 201.SDR AWXA200701016Skin · crackedMCN - MAJOR REPAIR - C-18 CHECK - NR 5987798, CRACKS FOUND ON NR 4 SLAT BOTTOM SKIN, SLAT STA 55 - SLAT STA 87. REPAIRED NR 4 SLAT BOTTOM SKIN, SLAT STA 55 - SLAT STA 87 IAW B737-300 SRM 57-43-01-2, REPAIR 6, FIG 201.SDR AWXA200701013Skin · crackedMCN - MAJOR REPAIR - C-18 CHECK - CRACKS FOUND ON NR 5 SLAT BOTTOM SKIN, SLAT STA 213 - SLAT STA 217. REPAIRED NR 5 SLAT BOTTOM SKIN SLAT STA 213 - SLAT STA 217 IAW B737-300 SRM 57-43-01-2, REPAIR 6.SDR UIEA200700317Structure · damagedON WALK AROUND FOUND NR 12 L/E KRUGER FLAP DAMAGED. PERFORMED INTERIM REPAIR IAW XEO 57-081307. PERM REPAIR TO BE ACCOMPLISHED AT NEXT "A' CHECK 20 AUG 07.SDR ASAA0771963Skin · chafedNR 1 SLAT LOWER SIDE T/E IS CHAFED. REPAIRED IAW SRM 51-70-10.SDR ASAA0771962Skin · chafedNR 2 SLAT LOWER SIDE T/E CHAFED. REPAIRED IAW SRM 51-70-10.SDR ASAA0771961Skin · chafedNR 3 SLAT LOWER SIDE T/E IS CHAFED. REPAIRED IAW SRM 51-70-10.SDR ASAA0771960Skin · chafedNR 4 SLAT LOWER SIDE T/E CHAFED. REPAIRED IAW SRM 51-70-10.SDR ASAA0771958Skin · chafedNR 6 SLAT LOWER SIDE T/E IS CHAFED. REPAIRED IAW SRM 51-70-10.SDR ASAA0771957Slat · chafedNR 7 SLAT LOWER SIDE EG IS CHAFED. REPAIRED IAW SRM 51-70-10.SDR ASAA0771956Skin · chafedNR 8 SLAT LOWER SIDE T/E CHAFED. REPAIRED IAW SRM 51-70-10.SDR ASAA0771955Skin · chafedNR 5 SLAT LOWER SIDE CHAFED. REPAIRED IAW SRM 51-70-70.SDR 07FDEA02842Skin · chafedSLAT NR 2 LT WITH CHAFING MARKS ON UPPER SKIN AT NOSE SECTION. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS IAW EA 6-5743-112493 AND RAS/FOK/177/2007 ISS A .SDR 2007UALA03089Skin · delaminatedNR 4 SLAT UPPER TRAILING EDGE SURFACE HAS DELAMINATION APPROX FIVE INCHES LONG AND SIX INCHES WIDE STICKING UP AT FORTY FIVE DEGREE ANGLE. PERFORMED COMPOSITE REPAIR ON NR 2 PYLON FAIRING.SDR SWAA073961Slat · crackedDURING SCHEDULED C1 CHECK, FOUND LT WING NR 2 L/E SLAT CRACKED AT OUTBOARD T/E. REPAIRED SLAT PER SWA EA.SDR 07FDEA02816Skin · crackedRT WING NR 8 SLAT UNDERSIDE SKIN AT OTBD END HAS SEVERAL SHEARED FASTENERS AND A POSSIBLE CRACK AT ONE OF THE FASTENER HOLES. REMOVED AND REPLACED NR 8 SLAT ASSY IAW 27-81-011-4.SDR TAMF20070006SSpar · crackedDURING C-CHECK INSPECTION (MFG TASK CARD 06-099-01-1) WAS FOUND A CRACK ON LOWER CHORD AT FRONT SPAR STA ISS 256-261 RT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-499965004 AND EWO 767-57-021. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 SDR 2007UALA03024Doubler · peelingNR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE, UNDER SIDE HAS OLD HOT BOND METAL PATCH PEELING OFF. PATCH IS 4 X 4 INCH. PATCH IS JUST INBOARD OF SLAT ACT ON UNDER SIDE OF SLAT. DELAM IS LOCATED 59 INCHES FROM INBOARD EDGE OF NR 5 SLAT ON THE TRAILING EDGE WEDSDR TAMF20070004SSpar · corrodedDURING C-CHECK INSPECTION (TASK CARD 06-099-01-2) WAS FOUND A CRACK ON LOWER CHORD AT FRONT SPAR STA ISS 256-261 RT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-495025865 AND EWO 767-57-020. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS SDR TAMF20070003SSkin · corrodedDURING C-CHECK INSPECTION (TASK CARD 57-500-00) WAS FOUND A CORROSION ON SLAT NR 2 LOWER SKIN STA OSS 953.48 LT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-495025537 AND EWO 767-57-022. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUSDR COEA0701901Strip · chafedIN HEAVY CHECK IN COE, FOUND CHAFING ON LOWER SLAT STRIP AT RIB 20 COMMON TO SINGLE POINT REFUEL ACCESS DOOR RT WING. REPAIRED CHAFING ON FWD SPAR, LOWER FLANGE AT FUEL DOOR BY INSTALLATION OF REPAIR DOUBLER IAW ART DWG S572R0093. (K)SDR DALA1134399222Skin · dentedCSTA XIS=12.290 OF RT NR 0 SLAT DENT REPAIR. REPAIRED PER MESSAGE 1-432640761-3.SDR 2007UALA02930Panel · puncturedLEFT LEADING.EDGE SLAT NR 1 CLOSURE PANEL HAS 3 INCHES PUNCTURE, CRACKED, APPROX 20 INCHES FROM INBOARD EDGE. PERFORMED TEMPORARY REPAIR PER ENGINEERING VARIATION AUTHORITY. SLAT TO BE PERMANENTLY REPAIRED WITHIN 300 HOURS. PUNCTURE CAUSED BY GROUND EQUIPMSDR ASAA0781913Vane · chafedLEFTHAND WING OUTBOARD FLAP INBOARD VANE TRAILING EDGE IS CHAFED. REPAIRED DAMAGED AREA WITH BONDED FILLER AND DOUBLER PER SRM 51-70-2.SDR 07FDEA02624Structure · crackedRIGHT WING, NR 1 LEADING EDGE SLAT INBOARD EDGE FILLET ASSEMBLY ALIGNMENT PIN HOLE FOUND CRACK. [08-17-07] REPAIR CARRIED OUT AS PER FEDEX EA 1-5710-114770, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR UPS07M51043Skin · dentedINSPECTION TYPE:C RIGHT NR 5 SLAT L/E 6 DENTS IN A ROW. RIGHT WING NR 5 SLAT L/E DENTS MEASURED FOUND OUT OF LIMIT. DAMAGE AREA TRIM OFF AS PER EN1663-07. HFEC INSP C/OUT ON TRIM OFF AREA FOUND NO CRACK. REPAIR PARTS FAB PER SRM 57-10-00 FIG 5 VOL I REV 38SDR AWXA200700926Wedge · separatedMCN - MAJOR REPAIR - C-12 - CHECK - RIGHT WING NR 6 SLAT TRAILING EDGE WEDGE SEPARATED, SS 133.15 - SS 134.15. REPAIRED RIGHT WING NR 6 SLAT TRAILING EDGE, SS 133.15 - SS 134.15 IAW B757-200 SRM 51-70-10-2R4.SDR 2007UALA02835Structure · damagedNR 1 SLAT DAMAGED ABOVE INBD GUIDE OUT OF LIMITS. REMOVED NR 1 SLAT AND REPAIRED, REINSTALLED.SDR 2007UALA02810Skin · crackedLEFT WING NR 1 L/E SLAT LOWER SKIN CRACK THREE INCHES LONG INBOARD OF ACTUATOR. FABRICATED AND INSTALLED EXTERNAL DOUBLER-FILLER REPAIR PER SRM 57-43-01, REPAIR NR 6.SDR 07FDEA02564Fitting · corrodedCORROSION ON FITTING AND DAMAGED REINFORCING ANGLE IN KRUEGER FLAP AREA RT. REPAIR WAS PERFORMED BY REPLACEMENT OF FITTING IAW SRM 57-45-11 AND REINFORCEMENT ANGLE IAW SRM 57-41-11.SDR 07FDEA02563Structure · corrodedHEAVY CORROSION IN KRUEGER FLAP AREA LT ON FITTING P/N: A535-10217-200 RIBLET (P/N A572-41993-200) IS CRACKED. REPAIR WAS PERFORMED BY REPLACEMENT OF FITTING IAW SRM 57-45-11 AND CHANGE RIBLET IAW SRM 57-41-11/FIG 1.
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