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 IPXA11M66463Doubler · crackedINSPECTION TYPE:3C, IN LT WING L/E COMPARTMENT AT XOS 545 APPX, CEILING DOUBLER IS CRACKED AT FASTENER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.SDR SWAA112897Slat · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT CRACKED. REPAIRED SLAT PER MM.SDR USAA2011050291736Panel · crackedMCN - C2 - CRACK IN NR 4 SLAT COVE PANEL AT WS 620. REPAIRED NR 4 SLAT COVE PANEL AT WS 620 IAW B767 SRM 51-40-02.SDR DALA1127669861Seal · crackedMETAL SEAL BETWEEN NR 2 & NR 3 LT WING SLATS CRACKED. NO DAMAGE PROGRESSION FOUND. REPAIRED LT NR 2 SLAT SEGMENT SEAL IAW ER/A491825-14, OK FOR SERVICE.SDR SWAA112872Slat · delaminatedDURING SCHEDULED MV3 CHECK, FOUND RT WING NR 5 SLAT UPPER LT CORNER DELAMINATED. REMOVED AND REPLACED SLAT PER MM.SDR UALA2011041801892Wedge · delaminatedNR 3 SLAT WEDGE DELAM NR 3 SLAT WEDGE DELAM AT OUTBOARD END, RPRD PER MM. ACCOMPLISHED REINSPECTION OF REPAIR FOUND AREA OF DELAM APPROX 2 INCH SQUARE. SMC WU MADE.SDR SWAA112873Slat · crackedDURING SCHEDULED MV2 CHECK, FOUND RT WING NR 6 SLAT CRACKED FROM O/B EDGE I/B. REPAIRED SLAT PER SRM.SDR DALA1126845501Wedge · damagedRT WING SLAT NR 8 LOWER T/E WEDGE PUNCTURED AS MARKED. REMOVED DAMAGE AREA AND FABRICATED DOUBLER REPAIR IAW SRM 51-70-10 PER WORKCARD 5742-01022-02H. DOUBLER FABBED FROM 2024T3-.020. AREA PAINTED IAW MM 51-21-10.SDR FDEA201104151500Channel · corrodedNR 6 SLAT INBD INNER L CHANNEL HAS CORROSION REMOVED CORROSION ON NR 6 SLAT INBD " L "CHANNEL IAW SRM 51-10-02 FOUND TO BE OUT OF LIMITS IAW SRM 57-43-02, FIG 101 DETAIL II. ORIGINAL MATERIAL .080 AFTER REWORK .060 SLAT. R & R ON N00817, MAJOR REPAIR.SDR SWAA112757Slat · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED AT I/B END. REPAIRED SLAT PER SRM.SDR SWAA112756Slat · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING NR 4 SLAT DELAMINATED AT I/B END. REPAIRED SLAT PER SRM.SDR FDEA201104141486Skin · delaminatedLT WING NR 4 SLAT - DELAMINATION FOUND ON WEDGE AFT SIDE 3-4 INCHES FROM INBD SIDE. DAMAGED AREA ON LT WING NR 4 SLAT WEDGE AFT SIDE SKIN, 3 TO 4 INCHES FROM INBD SIDE, REMOVED AND REPAIRED IAW SRM 51-70-10 REV 102, REPAIR 4. REPAIR IS CLASSIFIED AS MAJOR.SDR FDEA201104141485Wedge · delaminatedNR 4 SLAT L/E SURFACE APPROX 30" FROM INBD END - WEDGE HAS DELAMINATION AT PRIOR REPAIR AT EDGE OF REPAIR AT 5.00 POSITION - APROX 1" X 1". NR 4 SLAT L/E SURFACE APPROX 30" FROM INBD END, WEDGE DAMAGED AREA REMOVED AND REPAIRED IAW SRM 51-70-10 REPAIR 4, RESDR SWAA112792Wedge · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE I/B END DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.SDR EE4Y1104005Rib · crackedLT WING LEADING EDGE CAVITY NR 4 SLAT, I/B RIB CRACKED AT XRS 100. ACTION CORRECTIVE, FAA DER REPAIR APPROVAL.SDR SWAA2012052104152Slat · crackedRIGHT WING NR 6 SLAT LOWER AFT TRAILING EDGE CRACKED. REMOVED AND REPLACED NR 6 SLAT PER MM.SDR USAA2011041991545Wedge · debondedCLT - Q2 CHECK - DISBONDED AREA ON LOWER SURFACE OF NR 5 SLAT TRAILING EDGE WEDGE. REPAIRED AREA ON LOWER SURFACE OF NR 5 SLAT TRAILING EDGE WEDGE IAW B737-400 SRM 57-43-02, 51-70-10.SDR SWAA112652Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 4 SLAT SKIN DELAMINATED AT I/B END. REMOVED AND REPLACED SKIN PER MM.SDR SWAA112651Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 2 SLAT SKIN DELAMINATED AT I/B END. REMOVED AND REPLACED SKIN PER MM.SDR SWAA112650Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING N R4 SLAT DELAMINATED ON UPPER SKIN. REMOVED AND REPLACED SLAT PER MM.SDR SWAA112639Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 5 SLAT SKIN I/B END DELAMINATED. REPAIRED SKIN PER SRM.SDR IPXA11166544Skin · gougedINSPECTION TYPE:10YR, LT WING NR 2 SLAT LOWER SKIN BETWEEN RIBS 2 AND 3 IS GOUGED. REPAIRED LT WING NR 2 SLAT LOWER SKIN BETWEEN RIBS 2 AND 3 IAW EO A300-5750-42478-A AND STA-SA EA 300-53750-01-A3077-I/R.SDR FDEA201104111442Skin · corrodedNR 10 SLAT UPPER NOSE SKIN CORRODED AT OSS 736. REMOVED CORROSION ON NR 10 SLAT IAW SRM 51-10-02. BLENDED AREA L=1.5 W=1.5 D.028. ORIG MATERIAL .063 AFTER REWORK .035 FOUND OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DETAIL VI. ACCOMPLISHED EA F-5750-146287. SDR FDEA201104111441Skin · corrodedNR 10 SLAT UPPER NOSE SKIN CORRODED AT OSS 809. REMOVED CORROSION ON 10 SLAT IAW SRM 51-10-02. BLENDED AREA L=1.5 W=1.5 D=.025 ORIG MATERIAL .063 AFTER REWORK .038. FOUND OUT OF LIMITS IAW SRM 57-43-01 FIG 101 DETAIL VI. ACCOMPLISHED EA F-5740-146287. SDR LR7A2011041900178Hinge · wornDURING SCHEDULED C-9 CHECK, FOUND LT OUTTER WING FRONT BEAM LOWER HINGE ASSY LOBE HOLES WORN-OUT AT OWS 201.0 TO OWS 255.0. REPAIR ACCOMPLISHED BY REPLACING HINGE IAW SMP583 CHAP 51-60 & 51-70.SDR AALA20110411TUL01Wedge · dentedNUMBER 6 SLAT HAS DENT ON WEDGE AREA APPROXIMATELY 5 INCHES LONG BY 1 INCH WIDE APPROXIMATELY 48 INCHES FROM OUTBOARD END AND 3 INCHES FROM SLAT SKIN. REMOVED DAMAGED AREA REMOVED CORE. INSTALLED NEW CORE AND EXTERNAL DOUBLER PER SRM 51-70-10-2R.SDR SWAA112687Wedge · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER EA.SDR SWAA112562Skin · crackedDURING SCHEDULED 16Y CHECK, FOUND RT WING NR 6 SLAT L/E LOWER SURFACE CRACKED. REPAIRED NR 6 SLAT PER MM.SDR SWAA112561Skin · corrodedDURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 SLAT SKIN CORRODED. REPAIRED SKIN PER SRM.SDR HNAA2011050600121Shaft · corrodedLEFT NR 5 FLAP CARRIAGE FWD AND AFT OTBD MAIN ROLLER SHAFT WORN AND CORRODED. R & R LT NR 5 FLAP CARRIAGE FWD AND AFT OTBD MAIN ROLLER SHAFT IAW -8300 AMM57-50-53.SDR HNAA2011050600120Bushing · corrodedRT NR 5 FLAP CARRIAGE UPPER DEAD WEIGHT ROLLER SHAFT BUSHING CORRODED. R & R RT NR 5 FLAP CARRIAGE DEAD WEIGHT ROLLER SHAFT BUSHING IAW -8300 AMM57-50-53.SDR HNAA2011050600119Bolt · corrodedRT NR 4 FLAP CARRIAGE HOOK ROLLER GUARD BOLT IS CORRODED. R & R NR 4 RT FLAP CARRIAGE HOOK ROLLER GUARD BOLT IAW -8300 AMM 57-50-43.SDR USAA2011041291484Skin · crackedCLT - Q2 CHECK - LEFT WING NR 2 SLAT LOWER SKIN HAS 2 CRACKS, 31 INCHES TO 42 INCHES FROM THE INBOARD END AND 36 INCHES TO 41 INCHES FROM THE OUTBOARD END. REPAIRED LEFT WING NR 2 SLAT LOWER SKIN, 31 INCHES TO 42 INCHES FROM THE INBOARD END AND 36 INCHES TO 4SDR SWAA112573Slat · delaminatedLT WNG NR 2 SLAT DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM.SDR SWAA112397Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND RT WING NR 4 SLAT LOWER SPAR SKIN CRACKED. REPAIRED SKIN PER SRM.SDR ASAA1149636Skin · delaminatedNR 5 LEADING EDGE SLAT UPPER INBOARD TRAILING EDGE SURFACE DELAMINATED. REPAIRED SLAT UPPER INBOARD TRAILING EDGE SURFACE IAW B737 400 SRM 51 70 10 REPAIR 4.SDR SWAA112349Skin · crackedDURING SCHEDULED OTS CHECK, FOUND LT WING NR 2 SLAT CRACKED AT I/B AUX TRACK LOWER SURFACE. REPAIRED NR 2 SLAT PER SRM.SDR SWAA112343Slat · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT CENTER OF SLAT, BOTTOM SIDE CRACKED. REPAIRED SLAT PER SRM.SDR NOCA03111Rib · crackedAFT END OF L/E RIB CRACKED LES 662 AFT OF NR 9 SLAT. REMOVED ANGLE DRILLED AND INSTALLED RIB ANGLE AS PER SRM 51-10-02.SDR USAA2011041991519Wedge · debondedMCN - C2 CHECK - NR 7 SLAT WEDGE HAS AREA OF DISBOND, ISS 245.88 - ISS 250.88. REPAIRED NR 7 SLAT WEDGE , ISS 245.88 - ISS 250.88 IAW B767 SRM 51-70-10 REPAIR 4.SDR USAA2011050291729Fairing · erodedSAL - S4 - EROSION ON RIGHT WING NR 1 SLAT AERODYNAMIC FAIRING BETWEEN WS 0 TO WS 700 & BETWEEN RIB 1 TO RIB 2. REPAIRED RIGHT WING NR 1 SLAT AERODYNAMIC FAIRING BETWEEN WS 0 TO WS 700 & BETWEEN RIB 1 TO RIB 2 IAW EA 133477 & A319 SRM 51-77-12.SDR ABXA2011032825Rib · crackedNR 9 SLAT INBOARD TRACK CUTOUT INBOARD L/E RIB IS CRACKED. CRACK IS .5 INCH LONG. REMOVED AND REPLACED RIB IAW B767-200 SRM 51-40-02. AIRCRAFT WAS GROUNDED.SDR ABXA2011032822Rib · corrodedNR 11 SLAT OUTBOARD AUX TRACK OUTBOARD RIB IS CORRODED. REPLACED STRUT 114T2224-16 IAW 767-200 SRM 51-40-02.SDR SWAA112268Skin · crackedDURING SCHEDULED 26Y CHECK, FOUND LT WING NR 1 SLAT LOWER SKIN CRACKED AT LOWER CHORD. REPAIRED SKIN PER SRM.SDR USAA2011042991711Fairing · erodedSAL - S4 - EROSION ON LEFT WING NR 1 SLAT AERODYNAMIC FAIRING BETWEEN WS 0 TO WS 700 & BETWEEN RIB 1 TO RIB 2. REPAIRED LEFT WING NR 1 SLAT AERODYNAMIC FAIRING BETWEEN WS 0 TO WS 700 & BETWEEN RIB 1 TO RIB 2 IAW EA 133477 & A319 SRM 51-77-12.SDR USAA2011041291447Slat · debondedMCN - C2 CHECK - LEFT WING NR 3 SLAT HAS 2 AREAS OF DISBOND, OSS682.74 - OSS 684.940 AND OSS 830.74. REPAIRED LEFT WING NR 3 SLAT AT OSS682.74 - OSS 684.940 AND OSS 830.74 IAW B767 SRM 51-70-10 FIGURE 202.SDR KNNA20112492Skin · dentedDURING WALKAROUND NOTICED LT WING NR 2 L/E SLAT BIRD STRIKE. REMOVED LT NR 2 L/E SLAT IAW ACO 052775. CKD OK.SDR SWAA112233Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED ON EXTERNAL SKIN LOWER SUFRACE O/B EDGE. REPAIRED SKIN PER SRM.SDR SWAA112174Skin · crackedDURING SCHEDULED OTS CHECK, FOUND LT WING NR 1 SLAT I/B LOWER SURFACE CRACKED. REPAIRED NR 1 SLAT PER SRM.SDR USAA2011041991520Slat · debondedMCN - C2 CHECK - NR 10 SLAT TRAILING EDGE HAS AREA OF DISBOND, OSS 727.74 - OSS 736.74. REPAIRED NR 10 SLAT TRAILING EDGE, OSS 727.74 - OSS 736.74 IAW B767 SRM 51-70-10 REPAIR 3 AND 4.
Back to JASC 5754