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 CA010119003Fitting · broken(CAN) DURING INSPECTION THE LEFT OUTBOARD FORE FLAP ATTACHMENT BRACKET WAS FOUND CRACKED.SDR AWXA0001068Skin · chafedLT WING O/B FORE FLAP LE CHAFED AT PREVIOUS REPAIR DOUBLERS 58 INCHES FROM I/B OF LE. REMOVED PREVIOUS REPAIR IAW SRM 51-40-02; FABED DOUBLER IAW 57-53-01 FIG 201; TREATED AND PRIMED REPAIR DOUBLER IAW 51-20-01; INSTALLED CONICAL WASHERS IAW 51-40-8 FIG 3; INSSDR AWXA0001067Skin · gougedRT O/B FORE FLAP LE 4E CHAFED & GOUGED ON PREVIOUS SKIN REPAIR DOUBLER. REMOVED DAMAGED REPAIR DOUBLER, FABED REPLACEMENT DOUBLER, INSTALLED REPLACEMENT DOUBLER IAW SRM 57-53-01 & 51-40-02SDR AWXA001065Skin · chafedRT I/B FORE FLAP LOWER SKIN SURFACE T/E CHAFED AT WBL 123. REMOVED DAMAGED SKIN, CLEANED AREA, FABED REPAIR PARTS HF/ALODINED AND APPLIED BONDING PRIMER TO BOND SURFACES AND INSTALLED REPAIR PARTS WITH METAL TO METAL HOT BOND; CURED AT 225-250 DEGREES FOR 90 MSDR AWXA0001064Skin · chafedLT WING OUTBOARD FORE FLAP, INBOARD LEADING EDGE CHAFFED AT PREVIOUS REPAIR ON FLAP INBOARD EDGE. REMOVED SEAL, SEAL RETAINER AND EXISTING REPAIR DOUBLER IAW B737 SRM 51-40-02; FABED TREATED AND PRIMED REPAIR DOUBLER IAW 57-53-01 FIG 201; TREATED, PRIMED & INSSDR AWXA0001055Flap Track · chafedRT O/B FOREFLAP O/B TRACK CHAFFED ON BOTTOM SIDE. REMOVED AND REPLACED IAW M/M 57-53-18.SDR SWAA002623Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT LOWER AFT SURFACE CRACKED. REPAIRED SLAT PER SRM.SDR SWAA002608Flap · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING INBD & OTBD FORE FLAPS DELAMINATED. R&R FORE FLAPS PER MM.SDR SWAA002607Wedge · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 2, NR 5 & NR 6 L/E SLAT T/E WEDGES DELAMINATED. R&R SLATS PER MM.SDR ASAA0040147Panel · crackedPAE - DURING C-CHECK INSPECTION, FOUND SLAT ACCESS PANEL NR 6516 CORNER CRACKED. REPAIRED IAW ASA EA 5740-01231. (M)SDR SWAA002567Skin · crackedDURING SCHEDULED D CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED BETWEEN ROD END FITTINGS. REPAIRED SLAT PER DWG 65C30133, ER 00-1246 & SRM.SDR SWAA002543Skin · crackedDURING SCHEDULED C1 CHECK, FOUND NR 2 L/E SLAT LOWER SKIN CRACKED NEAR OUTBD MID TRACK CUT OUT. REPAIRED SKIN PER SRM.SDR AWXA000109Flap Track · chafedRT OB FOREFLAP OB TRACK CHAFED ON BOTTOM SIDE. GENERATED NEW N/R FOR R/R; MATERIAL LOSS RANGE .941 TO .978 OUT OF LIMITS IAW CMM 57-53-18; REPLACED FLIGHT RECORDER MODULE PART NUMBER 69-37325-52 WITH 69-37325-168 OP CHECK WILL BE COMPLIED WITH ON EO 31-31-73 ASDR TWAA0018903Skin · delaminatedDURING CHECK-C MAINT FOUND NUMBER 8 L/E SLAT INBD EDGE WAS DELAMINATED ON PREVIOUS REPAIR IN TWO PLACES, ONE EA INSIDE (BACK) AND OUTER SKIN. INSTALLED A 11 IN BY 5 IN METAL BOND REPAIR PER SRM 51-70-10.SDR SWAA002517Skin · crackedDURING SCHEDULED C1 CHECK, FOUND NR 5 L/E SLAT SKIN CRACKED AT LOWER SURFACE, AFT RIVET ROW, OTBD DETENT CUTOUT. REPAIRED SLAT PER SRM.SDR TWAA0018905Doubler · delaminatedDURING CHECK-C MAINT THE LT WING NUMBER 3 L.E. SLAT REPAIR, INBD EDGE WAS NOT ADHEARING TO SKIN. REMOVED OLD REPAIR AND INSTALLED NEW 6 IN BY 6 IN METAL TO METAL REPAIR PER SRM 51-70-00.SDR SWAA002525Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING INBD FORE FLAP DELAMINATED ON TOP SURFACE. R&R FORE FLAP PER MM.SDR TWAA0018904Doubler · delaminatedDURING CHECK-C MAINT THE NUMBER 7 L/E SLAT HAD 4 BY 5 PREVIOUS REPAIR THAT HAD DELAMINATION IN CENTER OF REPAIR. INSTALLED A 4 1/2 BY 7 IN METAL BOND REPAIR PER SRM 51-70-10.SDR 00FDEA00809Rib · crackedN 684 DURING ROUTINE INSP, THE NR 6 SLAT INTERNAL RIB AT WING BS 548.5 FND CRACKED. R&R & FAB PER IAW BAC 727 SRM 51-40-3.SDR SWAA002473Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT .5 CRACK, PAST STOP DRILL, 6 OTBD OF ACTUATOR, ON LOWER SKIN. REPAIRED SLAT PER RA 1-257-0555.SDR CA010103020Panel · missing(CAN) ACFT ARRIVED TO WITH L/H LE SLAT ACCESS PANEL MISSING. AREA INSPECTED, NEW PANEL INSTALLED.FEW SCREWS FOUND LOOSE ON THIS PANEL, WHICH MADE THE PANEL TO DROP ENOUGH FOR THE PIN TO COME OUT. DUE TO VIBRATION THE LE PANEL CAME LOOSE DURING FLIGHT AND DETACSDR TWAA0019007Skin · dentedDURING CHECK-C MAINT ON LT WING A DENT TO NUMBER 2 SLAT WAS FILLED WITH BONDO. INSTALLED DOUBLER PER SRM 57-43-02 AND SRM 51-70-10. PRIMED AND PAINTED AS REQUIRED.SDR SWAA002462Skin · crackedDURING SCHEDULED D CHECK, FOUND NR 6 L/E SLAT LOWER CHORD CRACKED AT ACTUATOR ROD END CUTOUT. R&R SLAT LOWER CHORD PER SRM.SDR SWAA002460Skin · crackedDURING SCHEDULED D CHECK, FOUND NR 3 L/E SLAT FIXED INNER SKINS (4 EA.) CRACKED AT UPPER ATTACH HOLES. REPAIRED SLAT PER ER 00-1279 & SRM.SDR SWAA002474Slat · delaminatedDURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT DELAMINATED ON UPPER TRAILING EDGE. R&R SLAT PER MM.SDR UPS00234515Skin · crackedINSPECTION TYPE:C FOUND R/H OUTBRD FOREFLAP WITH A 3/8 INCH CRACK AT HINGE CUTOUT. REPLACED R/H OUTBRD FOREFLAP IAW M/M 27-51-11. OK PER SAMESDR SWAA002457Skin · crackedDURING SCHEDULED C1 CHECK, FOUND NR 6 L/E SLAT SKIN CRACKED AT TWO LOCATIONS; ONE EXTENDS ACROSS THREE FASTENERS AT OTBD AUX TRACK, THE SECOND EXTENDS ACROSS TWO FASTENERS AT OTBD END OF SLAT. REPAIRED SLAT PER SRM.SDR DHL200180244CSkin · dentedDURING C CHECK FOUND LT WING L/E DENTED 2 INCH AT STA XFS 277. CUT OUT DAMAGED AREA PER SRM 57-2-1.FABRICATED FILLER AND DOUBLER PER SRM 57-2-1.CLEANED ,TREATED AND PRIMED PER SRM 51-1-8B.INSTALLED FILLER AND DOUBLER PER SRM 57-2-1.SDR UPS00234506Structure · crackedINSPECTION TYPE:PRE NR 4 LEADING EDGE SLAT CRACKED. AWAITING LOG PAGE ENTRY.SDR CALA0001814Fitting · dentedINSPECTION FOUND LT WING NR 5 SLAT END FITTING DENTED. THE SLAT END FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-10-4 AND 51-10-3.SDR CA001212007Structure · missing(CAN) AIRCRAFT IN CLIMB PHASE OF TAKEOFF. CREW REPORTED THAT WHEN THEY MOVED THE FLAP/SLAT HANDLE FROM POSITION 1 TO FULLY RETRACTED THAT A NOISE WAS HEARD. UPON CARRYING OUT A VISUAL INSPECTION, IT WAS OBSERVED THAT A PORTION APPROXIMATELY 800 SQUARE INCHES SDR CA010115008Access Door · damaged(CAN) ON WALK AROUND LEFT HAND WING NR1 SLAT ACTUATING ROD FAIRING PEELED BACK.NEW BRACKET AND DOOR INSTALLED.SDR USAA001962Skin · crackedCRACKS NR 5 SLAT INBD TRACK IN SLAT LWR SKIN AT SPAR. INSTALLED DOUBLER PER EA 68377SDR DL72S002236Skin · crackedFOUND AT F-1 LTR CK, .75 INCH CRACK IN NR 4 L/E FLAP OUTER SKIN AT O/B LIP HINGE CUTOUT. REPAIRED PER M/M 57-53-00.SDR MWEA001147Rib · damagedLEFT WING FLAP INTERNAL RIB HAS DRILL MARK AND FASTENER HITTING RADIUS OF RIB STATION XRS 71. BLENDED DAMAGE, REMOVED FASTENERS, FABRICATED REPAIR ANGLES AND INSTALLED.SDR CALA0001774Skin · dentedINSPECTION FOUND LT WING 0 SLAT DENTED. THE DENTED AREA WAS CUT OUT IAW SRM 57-06, FIGURE 1. A REPAIR WAS INSTALLED IAW SRM 57-06, FIGURE 1, 51-10-4, 51-10-3, AND 51-30-7.SDR DL72W002227Web · crackedNR 2 SLAT ACT O/B MOUNT WEB BROKEN. REPAIR PER MM 57-42-0.SDR P2EA00393Slat Track · crackedSJO - DURING Q-CHECK, FOUND THE LT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER WITH CRACK LENGTH .50 INCH, WIDTH .50 INCH. REWORKED THE LEFT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER AND WAS FOUND TO BE WITHIN LIMITS IAW BOEING SRM 57-20-1 FSDR P2EA00378Slat Track · crackedSJO - DURING Q-CHECK, FOUND THE LEFT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER WITH CRACK. (X)SDR SWAA002312Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND NR 1 L/E SLAT HAS 2 CRACKS ON LOWER SURFACE. REPAIRED SLAT PER RA 1-257-0555.SDR SWAA002305Frame · crackedDURING SCHEDULED D-CHECK, FOUND NR 1 SLAT LOWER CHORD CRACKED BELOW I/B AUX CUTOUT. REMOVED AND REPLACED CHORD PER SRM.SDR P2EA00359Skin · crackedSJO - DURING Q-CHECK, FOUND THE LEFT WING LEADING EDGE SKIN AT FSS 282 WITH CRACK. (M)SDR TWAA0017617Skin · dentedDURING CHECK-C MAINT, THE LT WING O L/E SLAT HAD DENT IN L/E APPROX CENTER OF SLAT. ACCOMP NDT AND NO CRACK FOUND PER PART 6-51-08-03 HFEC OF AREA IN SHOP PER TWA NDT SPM NUMBER 3 REPAIR PART NUMBER 6, NO CRACK. FOUND OK TO CLOSE LOWER SKIN. REPAIRED L/E PESDR AT0100018Skin · chafedFOUND CHAFE AT LEFT WING NR 5 LEADING EDGE SLAT. BLENDED CHAFED AREA IAW REO-L00322.SDR 20010112SG007Structure · bird strikeSAL-TGU-SAP-MIA- FLT 390 - DURING THE APPROACH, A BIRD IMPACTED THE SLAT NR 4 ON THE LEFT WING. MAINTENANCE TECHS REMOVED AND REPLACED SLAT NR 4 DUE TO DAMAGE TO THE LIMITS. OPERATIONAL TESTED AS PER AMM 27-84-66. THE AIRCRAFT RETURNED TO NORMAL OPERATION. SDR SWAA002259Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED ON UPPER SURFACE. REPAIRED FOREFLAP PER SRM.SDR 2000UALA00655Bellcrank · brokenON ARRIVAL FOUND RETRACT LINK FOR NR 3 (RT INBOARD KRUEGER FLAP) LEADING EDGE DEVICE BROKEN. UNABLE TO RETRACT FLAP. *S/D* BELLCRANK 65C26766-1 WAS REPLACED WITH BELLCRANK 65C26766-4.SDR SWAA002202Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND NR 2 L/E SLAT DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR UPS00234479Skin · crackedINSPECTION TYPE:C, NR 5 KRUEGER FLAP INNER SKIN CRACKED JUST I/B OF ACTUATOR X2. CRACK STOP DRILLED IAW SRM 51-10-1. HFEC C/O IAW B727 NDTM PT.6 51-0 0-00 FIG 4. CRACK FOUND TO BE CONTAINED WITHIN STOP DRILL HOLE. REPAIR C/O IAW EO B727-5750-3082.SDR USAA001830Skin · crackedCLT - FOUND SLAT SKIN CRACKED 6 INCHES, NR 5 SLAT LOWER LEADING EDGE SKIN INBOARD TRACK. REPAIRED DOUBLER PER EA 68377. (M)
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