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 TWAA9915303Skin · delaminatedDURING CHECK-C MAINT, THE NUMBER 11 LE SLAT HAD DELAMINATION AT LOWER INBD SURFACE, 6 INCHES FROM THE TE. INSTALLED METAL HOT BOND REPAIR PER SRM 51-70-10, PER BOEING SERVICE BULLETIN 767-57A0057 REV 2.SDR TSAA0057012Skin · corrodedREPAIRED NR 4 SLAT TRAILING EDGE EXTRUSION IAW ECO 3057. AIRCRAFT RETURNED TO SERVICE. (M)SDR SWAA991886Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 5 L/E SLAT SKIN CRACKED. REPAIRED SLAT PER SWA RA NR A57-0691 AND BOEING DRAWING.SDR P2EA99330Skin · corrodedSJO - DURING C-CHECK, SPOILER NR 8, P/N 65-46451-51 DELAMINATED AND FITTING IN SPOILER CORRODED. FABRICATED FITTING IAW COOPESA EO COO-3-57-657-99, DATED 11/16/99 AND REPAIRED SPOILER IAW COOPESA EO COO-CMP-3-57-649-99, DATED 11/13/99 SPOILER REMOVED AND REPLSDR TWAA9915304Skin · misrepairedDURING CHECK-C MAINT, THE LEFT WING NUMBER 3 LE SLAT, TOP SIDE AT OTBD END, FOUND THE PATCH COVER HAD COME OFF OF THE METAL SURFACE. INSTALLED A 3.5 INCH IN BY 5.5 IN HOT BOND REPAIR PER BOEING SERVICE BULLETIN 767-57A0057 REV 2, AND SRM 51-70-10.SDR DL72E992521Attach Bolt · cracksAT HMV2, FOUND NR 5 L/E SLAT 2 CRACKS AT FENCE ATTACH BOLT HOLES AT L/E. MFR REPAIR DOUBLER PER MM 57-54-0 FIG 813, REPAIRED PER SAME.SDR AALA991668Rib · crackedTUL - FORMER RIB CRACKED BETWEEN RIVETS TOP FLANGE OUTBOARD OF L/E KRUEGER FLAP ACTUATOR. STOP DRILLED AND INSTALLED REPAIR DOUBLER FITTING PER ESO 30595, DATED 11/05/99. (M)SDR EISA99233Skin · gougedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED LEFT OUTBOARD FOREFLAP WS 417 GOUGED UNDER LEADING EDGE. REMOVED DAMAGED AREA PER SRM 51-10-1, FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-4. TT: 65,345:17 HOURS. TC: 43,816. (X)SDR EISA99232Skin · delaminatedACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED AREA OF DELAMINATION ON RIGHT WING OUTBOARD FOREFLAP, INBOARD TRAILING EDGE. REPAIRED TRAILING EDGE WITH FIBERGLASS REPAIR PER SRM 51-40-6. TT: 65,345:17 HOURS. TC: 43,816. (X)SDR TWAA9915807Spar · crackedDURING OP 16 MAINT CHECK, FOUND A CRACK ON RT WING INSIDE THE I/B TOP HOLE FOR THE I/B FLAP HINGE CASTING UPPER SPAR AREA AT 11 O'CLOCK POSITION. REAMED OUT HOLE AND INSTALLED BUSHING AND DOUBLER REPAIR PER J060271 AND ARA 16217.SDR P2EA99313Fasteners · wrong partSJO - DURING C-CHECK, NR 6 SLAT REPAIRED WITH TEMPORARY FASTENERS. REPAIRED IAW SRM 57-50-3 FIG 4. (M)SDR DL72E992837Skin · wornDURING SHOP INSPECTION, THE LOWER L/E SKIN WAS FOUND WORN APPROX 1 INCH LENGTH AT THE O/B END OF THE FLAP. THE L/E WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0 FIG 803.SDR SWAA991842Skin · delaminatedDURING SCHEDULED D CHECK, FOUND NR 2 L/E SLAT DELAMINATED ON OUTBOARD END. REPAIRED SLAT PER SRM.SDR DL72E992524Rib · crackedAT HMV2, FOUND DOUBLER CRACKED ON RIB LOC I/B SIDE OF ACTUATOR FITTING ON NR 3 L/E SLAT. STOP DRILLED CRACK PER MM 57-54-0. FABRICATED DOUBLER, FOUND SECOND RIB CRACK, DRILLED SECOND RIB, FABRICATED ANOTHER DOUBLER, CUT AND REMOVED RIBS. INSTALLED DOUBLERS SDR DL72E992485Rib · crackedAT HMV2 FOUND NR 3 L/E SLAT, RIB CRACKED I/B SIDE OF I/B TRACK. REMOVED FASTENERS, STOPPED DRILLED CRACK. FABRICATED DOUBLER PER MM 54-57-0 FIG 811. INSTALLED DOUBLER PER SAME.SDR DL72E992484Rib · crackedAT HMV2, FOUND RIB CRACKED INSIDE NR 3 L/E SLAT ON O/B SIDE OF I/B TRACK. TRIMMED OUT DAMAGE, AND REPAIR ANGLE PER MM 57-54-0 FIG 811. INSTALLED DOUBLER PER SAME.SDR DL72E992483Rib · crackedAT HMV2, FOUND RIB CRACKED ON O/B SIDE OF ACT FITTING ON NR 2 L/E SLAT. STOP DRILLED CRACK PER MM 57-54-0 FIG 804. FABRICATED DOUBLER PER SAME, INSTALLED.SDR DL72E992482Rib · crackedAT HMV2, FOUND NR 2 L/E SLAT, RIB TEMP REPAIR STOP DRILLED CRACK, I/B SIDE OF ACT FITTING. STOP DRILLED CRACK PER MM 57-54-0 FIG 804, FAB'D DOUBLER PER SAME, INSTALLED.SDR DL72E992481Rib · crackedAT HMV2, FOUND NR 2 L/E SLAT, RIB CRACKED I/B SIDE OF ACT FITTING. STOPPED DRILLED CRACK PER MM 57-54-0 FIG 804. FAB'D DOUBLER PER SAME, AND INSTALLED.SDR SWAA991805Skin · damagedUPPER AFT SECTION OF NR 1 L/E SLAT TORN AND DELAMINATED. REMOVED AND REPLACED NR 1 L/E SLAT PER MM.SDR CALA9901444Strip · crackedINSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 SLAT O/B STRIP. PERFORMED REPAIR IAW SRM 57-10-00.SDR 20000505AP024Skin · crackedNR 6 SLAT INNER SKIN CRACKED AT FASTENER. INSTALLED REPAIR PER SRM 57-50-3 FIG 1. (M)SDR 20000505AP023Skin · crackedNR 6 SLAT OUTBOARD, HOOK CUTOUT CRACKED. INSTALLED REPAIR PER SRM 57-30-4 FIG 9. (M)SDR 20000505AP019Skin · crackedFOUND .375 INCH CRACK IN LOWER SURFACE OF RIGHT OUTBOARD FORE FLAP AT THE OUTBOARD ATTACHMENT AREA. INSTALLED REPAIR PER SRM 57-50-4 FIGURE 7. (M)SDR 20000505AP018Skin · crackedFOUND .5 INCH CRACK AT LEADING EDGE OF RIGHT OUTBOARD FORE FLAP ADJACENT TO NR 7 FLAP TRACK. STOP DRILLED CRACK, FABRICATED DOUBLER AND INSTALLED PER SRM 57-50-4 FIG 7. (M)SDR UPS99230988Skin · delaminatedINSPECTION TYPE:N/A, LEFT O/B FOREFLAP DELAMINATED REMOVED L/H FOREFLAP PER MM 27-51-11. INSTALLED TEMPORARY REPAIR PER EO B727-5750-3081-C. INSTALLED LT FOREFLAP PER MM 27-51-11, OP CHECKS NORMAL.SDR SWAA991804Skin · crackedDURING SCHEDULED C2 CHECK, FOUND NR 2 L/E SLAT SKIN CRACKED BELOW OUTBOARD TRACK CUT OUT. REPAIRED SKIN PER SWA RA NR1-A57-0691.SDR DL72S992306Rib · crackedAT HMV FOUND NR 5 SLAT ACT MOUNT O/B RIB CRACKED. REF N/R 1140 - RIB NR 11 FROM O/B FWD. STOP DRILLED CRACK AND FABBED REPAIR PER MM 57-54-0 PG 805 AND INSTALLED PER SAME.SDR RRXA000306Angle · crackedDURING A MAINTENANCE VISIT FOUND RIGHT WING LEADING EDGE INTERNAL ANGLE CRACKED AT XW 230. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-4.SDR CALA9901384Skin · dentedINSPECTION FOUND RT WING NR 2 SLAT DENTED. A REPAIR WAS INSTALLED IAW SRM 57-06, FIGURE 1.SDR CALA9901376Rib · crackedSLAT END FITTING DAMAGED (3 CRACK). REMOVED DAMAGED SLAT END FITTING AND REPLACED WITH NEW PART PER SRM 51-30-8.SDR SWAA991697Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND NR 4 L/E SLAT DELAMINATED ON OUTBOARD UPPER CORNER. REPAIRED SLAT PER SRM.SDR DL72S992388Rib · crackedAT HMV, FOUND O/B RIB CRACKED ON NR 7 L/E SLAT AT ACTUATOR FITTING. REMOVED FASTENER AND DOUBLER, FABBED NEW DOUBLER PER MM 57-54-0 FIG 804, AND INSTALLED.SDR DL72S992285Rib · crackedRIB CRACKED NR 8 L/E SLAT O/B RIB. FABRICATED DOUBLER, REPAIRED PER M/M 57-54-0 FIG 814.SDR DL72S992284Rib · crackedRIB CRACKED 2ND FROM I/B END ON NR 5 L/E SLAT. STOP DRILLED CRACK 2ND FROM I/B RIB ON NR 5 L/E SLAT. DRILLED VP DOUBLER FOR RIB 2ND FROM I/B NR 5 L/E SLAT. TREAT AND PAINT PER P/S 900-2-5. OK INSTALLED REPAIR. INSTALLED REPAIR DOUBLER PER M/M 57-40-0 FIG SDR CALA9901360Skin · crackedLEFT WING NUMBER 0 SLAT LOWER SURFACE IN CENTER AREA HAS A 3 CRACK IN SKIN NEAR TRAILING EDGE OF SLAT. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-01 AND MM 51-00-00.SDR DL72S992219Rib · crackedFOUND ON D1 LETTER CK, NR 1 SLAT L/E NOSE RIB CRACKED 1.5 INCH AT I/B SIDE OF ACTUATOR. REPAIRED PER MM 57-54-0.SDR DHL9974218CBracket · crackedAT C-CHECK, NR 4 TRAILING EDGE FLAP INBD BEARING BRACKET TO BULL NOSE CRACKED. REMOVED AND REPLACED NR 4 LE FLAP PER MM 27-81-4. N/R 2366.SDR MZZA99148Fitting · crackedTNN - DURNG S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACK WAS FOUND ON NR 4 L/E FLAP CENTER HINGE MOUNT FITTING OUTBOARD LUG. THE DAMAGED FLAP WAS REMOVED AND REPLACED WITH A NEW ONE PER B727 MM CHAPTER 27-81-0 AND OPERATIONAL CHECK FOUND TO BE SATISFACTOSDR CALA9901291Skin · corrodedINSPECTION FOUND NR 5 L/E FLAP BULL NOSE CORRODED. THE FLAP BULL NOSE WAS REMOVED AND REPLACED IAW MM 27-81-1, PAGE 401.SDR 99T64R429EWAShim · brokenNR 3 STUB WING L/E INBOARD LOWER SPAR CAP SHIM BROKEN OFF XILD .7095. (EO). SMOOTHED REMAINING EDGE OF SHIM. NDT TO ASSURE THAT NO CRACKS EXIST. (NONE FOUND). TREATED AND PRIMED, INSTALLED INBOARD PIECE AS A SHIM USE FACTORY FASTENERS PER EO 99-174 WITH ASDR DHL9974205CAngle · damagedAT C CHECK, RIGHT WING L/E SLAT CRACKED JUST BELOW FWD END OF ANTI-ICE DUCT. CUT OUT DAMAGED SECTION OF ATTACH ANGLE. INSTALLED FORMED SECTION REPAIR PER SRM 51-40-3. 18 BY 1 BY 1, N/R 2271.SDR DL72S992125Stiffener · crackedI/B SPAR STIFFENER CRACKED NR 7 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21 P 813.SDR CALA9901277Skin · dentedINSPECTION FOUND LT SLAT 0 DENTED. THE DENTED AREA WAS CUT OUT IAW SRM 57-6, FIGURE 1. A REPAIR WAS INSTALLED IAW ECRA 5720-01170.SDR RRXA991775Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, LEADING EDGE, TOP SKIN AT XFS=793. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED SDR USAA990920Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 3 EACH, .50 INCH CRACKS, NR 1 SLAT INBOARD EDGE OF LOWER SKIN AFT FASTENER ROW. INSTALLED DOUBLER PER BOEING DWG 65C30133 AND TR 57-50-01 REV H. (X)SDR RRXA991777Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LEFT WING, INBOARD FLAP, TOP SKIN AT XW=5. DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-7-0. CORROSISDR DL72S992081Stiffener · cracked2 INCH CRACK IN VERTICAL SPAR STIFFENER NR 7 SLAT O/B TRACK I/B SIDE. REPLACED SPAR STIFFENER PER MM 57-20-21.SDR SWAA991540Skin · crackedDURING SCHEDULED C1 CHECK, FOUND RT WING NR 5 L/E SLAT LOWER SKIN CRACKED AT 3 EACH PLACES. REMOVED AND REPLACED L/E SLAT ASSY PER MM.SDR DL72L992055Rib · crackedFOUND ON MV2 CK, .375 INCH CRACK ON NR 2 L/E SLAT RIB O/B OF ACTUATOR ATTACH BOLT. REPAIRED PER MM 57-54-0.
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