JASC 5753
Service difficulty reports · 31,521
Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753' 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 = '5753' 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 05FDEA01889Hinge · corrodedLT WING, O/B FLAP O/B HINGE (WING SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87592A.SDR 05FDEA01886Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.SDR 05FDEA01885Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REMOVED IAW CMM 20-11-02. FABRICATED BUSHING AND INSTALLED IAW EA1-5750-87591.SDR 05FDEA01884Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT ASPER EA1-5750-87591.SDR 05FDEA01883Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.SDR 05FDEA01882Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.SDR 05FDEA01881Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.SDR 05FDEA01880Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.SDR 05FDEA01879Hinge · corrodedRT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87591.SDR 05FDEA01878Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.SDR 05FDEA01877Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.SDR 05FDEA01876Hinge · corrodedRT WIN, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.SDR 05FDEA01875Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590. SDR 05FDEA01874Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87590.SDR 05FDEA01873Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED IAW CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA1-5750-87590.SDR 05FDEA01872Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA1-5750-87590.SDR 05FDEA01871Hinge · corrodedRT WING, O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B BORE FOUND CORRODED.SDR AWXA200500855Skin · debondedDURING C16 CHECK DISCOVERED DISBOND AREA ON THE BOTTOM SURFACE OF THE RT OUTBOARD FORE FLAP, 87 INCHES FROM OUTBOARD END. MAINTENANCE REMOVED AND CLEANED THE DISBOND AREA ON THE BOTTOM OF THE RT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-0. FABRICATESDR 05FDEA01840Hinge · corrodedLT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87588.SDR 05FDEA01839Hinge · corrodedLT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87588.SDR 05FDEA01838Hinge · corrodedLT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIRED AS PER CMM 20-11-02 AND EA 1-5750- 87588.SDR 05FDEA01837Hinge · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87588.SDR 05FDEA01836Structure · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED.SDR 05FDEA01835Structure · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87588.SDR 05FDEA01834Structure · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED.SDR 05FDEA01833Structure · corrodedLT WING, O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED A PER EA 1-5750-87588.SDR 05FDEA01831Structure · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIRED AS PER EA1-5750-87587.SDR 05FDEA01829Structure · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. REPAIRED AS PER EA1-5750-87587.SDR 05FDEA01827Structure · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. SUPPORT BRACKET REPAIRED AS PER EA1-5750-87587 LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR 05FDEA01825Structure · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. SUPPORT BRACKET REPAIRED AS PER EA1-5750-87587 LT OUTBD FLAP INBD SUPPORT BRACKET CORROSION REMOVAL AND REPAIR.SDR 05FDEA01823Structure · corrodedLT WING, O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA1-5750-87587.SDR 05FDEA01821Structure · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA1-5750-87587.SDR 05FDEA01820Structure · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA1-5750-87587.SDR 05FDEA01819Structure · corrodedLT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA1-5750-87587.SDR AWXA200500987Wedge · debondedDURING C15 CHECK DISCOVERED DISBOND AREA ON THE LT OUTBOARD FORE FLAP FROM WBL 310 TO WBL 313.5. MAINTENANCE REMOVED DISBOND SKIN AND CORE ON THE LOWER SKIN OF LT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-0 REPAIR 7, FIG 16. FABRICATED CORE AND EXTESDR ASAA0540353Skin · dentedYXX - FOUND LEFT OUTBOARD FORE FLAP HAS A DENT FROM CHAFING OUTBOARD OF FORE FLAP TRACK. DENT ON OUTBOARD LEFT FORE FLAP OUTBOARD OF NR 1 FORE FLAP TRACK REPAIRED IAW B737-400 SRM 57-53-01 FIGURE 201. (M)SDR ASAA0540346Skin · dentedYXX - FOUND RIGHT INBOARD FORE FLAP LOWER SIDE DENTED MID-SPAN. RIGHT INBOARD FORE FLAP LOWER SIDE REPAIRED IAW B737-400 SRM 51-70-10 REPAIR NR 7. (M)SDR ASAA0540345Skin · delaminatedYXX - FOUND RIGHT OUTBOARD AFT FLAP HAS DELAMINATION ON THE UPPER AND LOWER SURFACES. REMOVED AND REPLACED RIGHT OUTBOARD FLAP IAW B737-400 AMM 27-51-39. (M)SDR CA050706010Attach Fitting · corrodedDURING ROUTINE C2 INSPECTION OF AIRCRAFT, BOTH LOWER FLAP MECHANISM ATTACH FITTINGS WERE FOUND TO BE CORRODED. DATA WAS PASSED TO COMPANY ENGINEERING DEPARTMENT WHO CONTACTED BOEING ENGINEERING. BOEING SENT AN APPROVED TIME LIMITED REPAIR WHICH WAS CARRIED OSDR 05FDEA01802Fitting · crackedLT WING INBOARD FLAP OUTBOARD LEADING EDGE MOUNT FITTING CRACKED. (OPEN)SDR 05FDEA01797Support · corrodedLT WING OUTBOARD FLAP INBOARD HINGE SUPPORT FOUND COROSSION EXCEEDED LIMITS. LT WING OUTBOARD FLAP ASSY R & R PER AMM 27-50-30-4. REMOVED AND REPLACED PER AMM 27-50-30-4. (CLOSED)SDR 05FDEA01795Hinge Fitting · corrodedDURING ACCOMPLISHEMENT OF EA 1-5750-87541, LT WING OUTBOARD FLAP INBOARD HINGE FITTING (FLAP SIDE) INBOARD FORWARD BOLT HOLE FOUND CORRODED. LT WING OUTBOARD FLAP ASSY R & R PER AMM 27-50-30-4.SDR ASAA0540343Skin · dentedOKC - FOUND RIGHT INBOARD FORE HAS A DENT ON THE LOWER SIDE ABOVE INBOARD TRACK. PREPARED DAMAGED AREA, FABRICATED AND INSTALLED A REPAIR DOUBLER AND BONDED, IAW 737-400 SRM 51-70-30 REPAIR 2. (M)SDR ASAA0540338Skin · dentedOKC - FOUND LEFT INBOARD FORE FLAP HAS 2 EACH GROUPS OF DENTS ON LOWER SURFACE. FILLED DENTS, FABRICATED AND INSTALLED SKIN DOUBLERS IAW 737-400 SRM 51-70-10 REPAIR 2. (M)SDR ASAA0540337Skin · debondedOKC - FOUND RIGHT WING INBOARD AFT FLAP LOWER SKIN AT PREVIOUS REPAIR IS DISBONDED ON FORWARD END AT SECOND TRACK. REMOVED DISBONDED AREA, REPAIRED AREA WITH FIBERGLASS OVERLAY VIA HOTBOND IAW 737-400 SRM 51-70-06 PARAGRAPH 3A. (M)SDR ASAA0540336Skin · delaminatedOKC - FOUND RIGHT INBOARD FORE FLAP UPPER SKIN IS DELAMINATED 60 INCHES FROM INBOARD END AND 8 INCHES FROM T/E. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLERS AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10 REPAIR 21. (M)SDR ASAA0540335Skin · delaminatedOKC - FOUND RIGHT INBOARD FORE FLAP UPPER IS DELAMINATED 34 INCHES FROM OUTBOARD END AND 8 INCHES FROM T/E. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10 REPAIR 21. (M)SDR ASAA0540334Skin · dentedOKC - FOUND RIGHT INBOARD FLAP LOWER SKIN IS DENTED AND DELAMINATED JUST OUTBOARD OF CENTER TRACK. REMOVED DAMAGED AREA, FABRICATED SKIN FILLER AND DOUBLER AND INSTALLED REPAIR PIECES IAW 737-400 SRM 51-70-10 REPAIR 21. (M)SDR AWXA200500856Skin · delaminatedDURING C16 CHECK DISCOVERED DELAMINATED AREA ON THE BOTTOM SURFACE OF THE LEFT OUTBOARD AFT FLAP, APPROXIMATELY 20 INCHES FROM INBOARD END AND 6 INCHES FROM THE TRAILING EDGE. MAINTENANCE REMOVED AND CLEANED DELAMINATED AREA FROM THE BOTTOM SURFACE OF THE LEFSDR DU4R0507143Skin · delaminatedRIGHT WING INBOARD MID FLAP WEDGE LOWER T/E SKIN SURFACE DELAMINATED AND DENTED.
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