JASC 5754
Service difficulty reports · 17,348
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 DHL200071708DFence · delaminatedAT D CK, RIGHT WING FENCE AT NR 5 SLAT TEMPORARY REPAIR DETERIORATED, PULLING OFF, FASTENERS ON I/B SIDE PULLING THROUGH. INSTALLED FIBERGLASS OVERLAY REPAIR PER BORING SRM 51-40-8 FIG 1. REF: N/R 2772.SDR DHL200071704DSkin · crackedAT D-CK, RIGHT WING UPPER LEADING EDGE SURFACE HAS CRACK AT WING CUTOUT FOR NR 5 SLAT INBOARD TRACK. STOPPED DRILLED CRACK AS PER SRM 51-10-1, PERFORMED HFEC INSP OF STOP DRILLED HOLE PER NDT MANUAL 51-00-00 PART G. NO CRACK NOTED. FABRICATED DOUBLER 5 BY 7SDR DHL200071703DSkin · dentedAT D-CK, RIGHT WING LEADING EDGE OUTBOARD OF NR 8 SLAT HAS TORN METAL AND DENTED AREA WS 780. STRAIGHTENED OUT DAMAGED AREA PER SRM 51-40-1, BLENDED OUT SMALL DAMAGED AREA PER SRM 57-20-1 FIG 4, MATERIAL LOSS, .003. PERFORMED HFEC INSPECTION OF BLENDED AREA SDR RRXA001037Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, OUTBOARD SLOT VANE BETWEEN XFS 430 TO XFS 440. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM SDR RRXA001032Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RIGHT WING, OUTBOARD SLOT VANE BETWEEN XFS 430 TO XFS 440. CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DSDR CALA9901701Web · crackedINSPECTION FOUND A 2 INCH CRACK IN LEFT WING SLAT NR 1 O/B TRACK TO SLAT WEB. THE SLAT AND TRACK WERE REMOVED IAW MM 27-81-11. A NEW WEB, TRACK FITTING, AND LOWER SKIN WERE INSTALLED IAW SRM 51-30-2. THE SLAT AND TRACK WERE INSTALLED IAW MM 27-81-11.SDR DL757992818Rib · damagedDURING B757 L/E SLAT T/E WEDGE CHANGE PER EO 6-74595-3AD, THE NR 10 L/E SLAT I/B END RIB HAD ONE HOLE OVERSIZED IN THE I/B END RIB AT OSS 707. PER ER/A 387211-14AD THE SUBJECT PART WAS REPAIRED BY OVERSIZING THE DISCREPANT HOLE TO ACCOMODATE A .25 DIA BLIND BSDR DL72W992766Rib · crackedNR 12 RIB CRACKED. REPAIRED RIB PER M/M 57-54-0 FIG 804.SDR DL72W992765Rib · crackedNR 11 RIB CRACKED. REPAIRED PER M/M 57-54-0 FIG 804.SDR SWAA992053Skin · debondedDURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT DISBONDED ON OUTBOARD END. REPAIRED SLAT PER SWA RA NR 1-357-0779.SDR AT9900916Bracket · crackedFOUND CRACKED SUPPORT BRACKET ON RIGHT WING LEADING EDGE. FABRICATED AND REPLACED CRACKED BRACKET.SDR RRXA000299Skin · damagedDURING A MAINTENANCE VISIT FOUND LEFT WING, LEADING EDGE, MOUNT HOLES ENLONGATED AT XFS 520.168. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA DER ENGINEERING SKETSDR DL72E992694Bracket · crackedNR 8 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED ON WEB. REPAIRED PER MM 57-20-21.SDR DL72E992691Angle · crackedDOUBLER CRACKED AT NR 2 L/E SLAT COVE SKIN ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER MM 57-54-0.SDR AWXA9900472Skin · gougedRIGHT WING OTBD FORE FLAP GOUGED AT INBD UPPER SURFACE. REMOVED EXISTING DAMAGED REPAIR. FABRICATED REPAIR DOUBLER PER SRM 57-33-01 FRM .032 301 1/2 HARD R602099--CAD PLATED PER SOPM 20-42-01. INSTALLED REPAIR PER SRM 51-40-02.SDR 99ZZZX4413Bracket · damagedSLAT (OUTBOARD) NR 3 RAIL MOUNT BRACKET ATTACHED TO SLAT RUBBING LEADING EDGE CAUSING DAMAGE TO THE BRACKET. THIS HAS ALSO BEEN NOTICED ON FALCON10, SN 131.SDR 20000511AP012Bracket · crackedOUTBOARD BRACKET CRACKED .375 INCH AT INBOARD TRACK OF LET WING NR 3 SLAT WHERE SKIN ATTACHES. REMOVED DAMAGED BRACKET AND FASTENERS IAW 51-30-2 PAGE 6. FABRICATED BRACKET IAW 51-20-1 PAGE 8. TREATED, PRIMED AND INSTALLED IAW 51-30-2 PAGE, 51-20-1 PAGE 18, SDR 20000510AP007Skin · crackedFOUND .4374 INCH CRACK THROUGH FASTENER HOLE AT RIGHT OUTBOARD FOREFLAP LEADING EDGE ABOVE NR 7 FLAP TRACK AREA. STOP DRILLED CRACK IAW SRM 51-10-1 PAGE 1. FABRICATED COUPLER REPAIR IAW 57-50-4 PAGE 17. HFEC INSPECTION OF CUTOUT CONFIRMED NO CRACKS. FABRICSDR 20000510AP005Skin · crackedFOUND .5 INCH CRACK AT FASTENER HOLE AND TWO RIVETS CRACKED LOWER LEADING EDGE SKIN OF LEFT WING NR 3 SLAT BELOW UPSTOP PAD AREA. ACCOMPLISHED HFEC INSPECTION AND MARKED END OF CRACK IAW 51-00-00 PART 6. STOPPED DRILLED END OF CRACK IAW 51-10-1 PAGE 3. HFEC SDR SWAA992030Skin · delaminatedDURING SCHEDULED D CHECK, FOUND NR 3 L/E SLAT INBOARD END DELAMINATED. REPAIRED SLAT PAR ER NR 99-6418 AND SRM.SDR DL72S992682Skin · crackedA .5 INCH CRACK AT FWD LWR SIDE OF NR 2 MIDFLAP AT I/B AFT FLAP ACTUATING ROD CUTOUT. REPAIRED PER MM 57-52-0 AND ERA 368899-14.SDR DL72S992679Stiffener · crackedVERTICAL SPAR STIFFENER CRACKED NR 7 SLAT O/B SIDE OF I/B TRACK. REPLACED SPAR STIFFENER PER MM 57-20-21.SDR DL72S992678Angle · crackedCOVE SKIN ANGLE CRACKED 15 INCHES O/B OF NR 7 SLAT ACTUATOR ROD. REPAIRED PER MM 57-54-0.SDR DL72W992672Bracket · crackedNR 5 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED TOP AND BOTTOM RADIUS. REPAIRED PER MM 57-20-21.SDR UPS99431172Skin · cracked4 INCH CRACK AFT OF NR 13 KRUGER FLAP.SDR DL72S992632Angle · crackedFOUND ON D1 LETTER CK, NR 6 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT O/B STOP PAD. REPAIRED PER MM 57-54-0.SDR DL72L992782Rib · crackedAT HMV2 FOUND NR 3 SLAT RIBS CRACKED. REPAIR AT RIB MARKED NR 3, RIB MKD NR 10, RIB MKD NR 17. CORROSION - DYE CKD AS PER PS 900-6-3 AND NO CRACKS. FABRICATED DOUBLER PER MM 57-54-0 PG 807. INSTALLED DOUBLER PER SAME, DYE CHECKED RIB NR 17 PER PS 900-6-3 SDR DL72L992727Rib · crackAT HMV2, FOUND NR 4 SLAT RIB (MARKED) CRACKED. FABRICATED DOUBLER PER MM 57-54-0 FIG 804. DYE CHECKED END OF CRACK PER FIG 504. CHEM TESTED PER PS 900-2-4-1 NR 2. REPAIRED RIB PER MM 57-54-0.SDR DL72L992671Rib · crackedAT HMV2, FOUND NR 8 SLAT RIB'S CRACKED, NR 4, 14 (MARKED). REMOVED I/B SLTRK AND STOP DRILLED CRACK PER MM 57-40-0 FIG 809, FABRICATED REPAIR PARTS PER MM 57-54-00 FIG 809.SDR USAA119913Skin · crackedFOUND DURING C-CHECK, RIGHT WING OUTBOARD FLAP, FORE FLAP DOUBLER, ON FORE FLAP HAS LOOSE RIVETS AND CRACKED AREA OUTBOARD FLAP TOGGLE CARRIAGE. INSTALLED DOUBLER REPAIR AT RIGHT WING OUTBOARD FLAP, FORE FLAP IAW SRM 57-50-4 FIG 1. MATERIAL USED, 2024-T3, 0.SDR TWAA0000111Patch · looseDURING CHECK-C MAINT, THE PATCH ON THE LEFT WING NUMBER 6 LE SLAT, TOWARD THE OTBD END, WAS COMING LOOSE AT THE EDGES. INSTALLED A 4 1/2 IN DIAMETER METAL HOT BOND REPAIR PER SRM 51-70-10. ALSO SEALED EDGES.SDR GAIA99204Lug · wornNR 2 L/E FLAP INBOARD BULLNOSE BEARING LUG WORN TOO LARGE FOR BEARING INSTALLATION AND LUG CORRODED AND PITTED. ACCOMPLIHSHED NR 2 LEADING EDGE FLAP BULLNOSE REPAIR IAW BOEING TELEX KHC-MIA-99-00003H, DATED 9-7-99. 8110-3 DATED 9-14-99 ISSUED. REF: N/R 188SDR GAIA99181Rib · crackedNR 2 L/E SLAT INBOARD TRACK OUTBOARD MOUNT RIB IS CRACKED AT UPPER FLANGE BEINDING RADIUS APPROXIMATELY 1.50 INCHES AFT FROM SLAT FRONT SPARE. INSTALLED REPAIR AT THE NR 2 LEADING EDGE SLAT INBOARD TRACK OUTBOARD MOUNT RIB UPPER FLANGE. REPAIR ACCOMPLISHED ISDR DL72W992589Stiffener · crackedL/E SPAR STIFFENER CRACKED AT NR 6 SLAT I/B TRACK I/B STIFFENER. REPLACED PER M/M 57-20-21 PG 813 {NR 6 SLAT}.SDR DL72S992582Angle · crackedLOWER COVE SKIN ATTACH ANGLE CRACKED AT NR 6 SLAT I/B STOP PAD. REPAIRED PER M/M 57-54-0 FIG 812 & ERA 368813-14.SDR DL72S992579Angle · crackedCOVE SKIN ANGLE CRACKED NR 3 SLAT I/B OF ACTUATOR ROD END REPAIR PER MM 57-54-0.SDR DL72S992578Angle · crackedCOVE SKIN ANGLE CRACKED 2 PLACES NR 4 SLAT O/B OF ACTUATOR ROD END. REPAIRED PER MM 57-54-0.SDR TWAA0005807Skin · puncturedDURING OP 16 MAINT CHECK, THE RT WING L/E HAD SMALL PUNCTURE HOLE AT L/E ON O/B END, AFT OF O/B END OF NUMBER 5 L/E SLAT. REMOVED WING TIP SUPPORT EXTENSION L/E PER SRM 51-30 AND 51-10-4. SENT PART TO WELDING SHOP TO BE WELDED PER DRAWING 5923349. CLEANED USDR USAA991256Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT INBOARD LOWER T/E NR 2 SLAT SKIN. INSTALLED DOUBLER PER BOEING DWG 65C30133. (M)SDR CALA9901515Skin · gougedINSPECTION FOUND RT WING NR 3 FLAP LEADING EDGE BULL NOSE GOUGED. REPAIRED IAW ECRA 5750-03318 AND INSTALLED NEW CHAFE STRIP IAW SRM 51-30-2.SDR CALA9901513Slat · dentedINSPECTION FOUND RT WING NR 0 SLAT END LEADING EDGE DENTED AT STA XFS 55. THE DENT WAS BLENDED OUT AND REPAIRED WITH FILLER IAW SRM 57-03, FIGURE 14B.SDR TWAA9916202Skin · disbondedDURING CHECK-C MAINT, FOUND A 1.5 INCH BY 2 INCH DISBONDED AREA ON UPPER SURFACE NEAR THE O/B TRAILING EDGE AREA OF THE NUMBER 11 LEADING EDGE SLAT ON THE RT WING. AN INTERIM REPAIR WAS PREVIOUSLY INSTALLED. REPAIRED PER 767-300 SRM 51-70-10 AND BOEING SERVISDR WXOA99031Slat · dentedAMA - BIRD STRIKE REPORTED TO LEFT WING AT 8500 FT DURING DESCENT FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. BIRD STRIKE INSPECTION ACCOMPLISHED IAW DC-9 MM 05-56. FOUND LEFT WING NR 2 OUTBOARD LEADING EDGE SLAT TO HAVE SUSTAINED BIRD STRIKE DAMAGE. DESDR DL72S992505Rib · crackedOUTBOARD RIB CRACKED. REPAIRED PER M/M 57-54-0 FIG 814.SDR DL72S992504Rib · crackedNR 11 RIB CRACKED. REPAIRED RIB PER M/M 57-54-0.SDR DL72S992503Rib · crackedNR 8 RIB CRACKED IN CORNER OF RADIUS. REPAIRED RIB PER M/M 57-54-0, FIG 814.SDR DL72S992502Skin · crackedSKIN CRACKED AT CORNER OF T DUCT HOLE. REPAIRED SKIN PER M/M 57-54-0, FIG 802A.SDR 20000615AP007Slat Track · crackedDURING C-CHECK, FOUND .375 INCH CRACK AT LT WING FIXED L/E CUTOUT ABOVE NR 4 SLAT OUTBOARD TRACK. TRIMMED OUT DAMAGED SKIN AND FABRICATED DOUBLER AND FILLER, INSTALLED REPAIR PER SRM 57-30-4, PAGE 6. (M)SDR DL72E992496Web · crackedFWD WEB CRACKED INSIDE NR 3 L/E SLAT AT ANTI-ICE DUCT. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS PER M/M 57-40-0 FIG 802 A. OK TO INSTALL. INSTALLED DOUBLER PER M/M 57-40-0 FIG 802 A.SDR TWAA9915806Skin · delaminatedDURING CHECK-C MAINT, FOUND AT LOWER O/B SURFACE OF NUMBER 8 SLAT, THE T/E WEDGE HAD DELAMINATION 6 INCHES FROM THE T/E. INSTALLED HOT BOND REPAIR PER SRM 51-70-10, A 3 INCH BY 5 INCH PATCH.
Back to JASC 5754