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 04FDEA02590Vane · corrodedBFM CLOSE R COMPLY WITH EA NR 8-5750-80607 WINGS-ARC1497 FLAP VANE SUPPORT CORROSION REWORK ENT BY: 527637 RPT BY: 527637 FACT 01 SEP04 04:30 BFM U COMPLIED WITH EA 8-5750-80607 WINGS-ARC1497 FLAP VANE SUPPORT CORROSION REWORK RII:497214, ENT BY: 527637 SDR 2004UALA00810Hinge · crackedRT INBD AFT FLAP EXTERNAL HINGE IS CRACKED AT THE MID FLAP AFT SPAR. REPAIRED FITTING WITH ANGLE REPAIR.SDR ASAA0470016Carriage · unknownMODIFICATION OF FLAP CARRIAGE REQUIRED. ACCOMPLISHED EA 5750-01976.SDR ASAA0440158Skin · dentedOAK - FOUND RIGHT WING FORE FLAP DENTED ON LOWER SURFACE. CUT OUT DAMAGED AREA, INNER CORE REPLACEMENT AND BONDED EXTERNAL DOUBLER. (M)SDR CA040831010Attach Bracket · missing(CAN) DURING DELIVERY FLIGHT FROM THE AIRCRAFT MANUFACTURER, TECHNICAL LOG ENTRY FOR THIS AIRCRAFT STATED (FLAP POWER CAUTION LIGHT ON) DURING TAXI IN WHEN FLAPS SELECTED ZERO. FLAPS STOPPED AT ABOUT 8 DEGREES. ON FURTHER INVESTIGATION OUTER RT FLAP SEEN TO SDR UPS04243032Support Bracket · crackedINSPECTION TYPE: C, SUPPORT BRACKET FOR NR 5 FWD FLAP TRACK FAIRING FOUND CRACKED ON O/B SIDE OF NR 5 FLAP TRACK. SUPPORT BRACKET REMOVED IAW SRM 51-30-02, NEW ANGLE FABRICATED IAW SRM 51-20-01, ANGLE PROTECTED IAW SRM 51-10-01, ANGLE INSTALLED ON FLAP TRACK SDR USAA040817Structure · wornPIT, Q5, MIDFLAP 1 INCH X 1 INCH, WORN. LT OB MIDFLAP LOWER SIDE AFT OF OB JACKSCREW ATTACH BRACKET. INSTALLED DOUBLER IAW TR 57-50-17.SDR IXXA060435SAngle · wornDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING ANGLE WORN AT STATION XF218. REPAIRED PER ALL APPLICABLE DATA.SDR ANCF200400028Fairing · damagedDURING WALK AROUND FOUND DAMAGE TO THE RT EXTERIOR FAIRING FLAP. FAIRING WAS REMOVED IAW CDL 57-51-2 AND TRANS ITEM TO DMI 567.SDR SWAA042454Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.SDR SWAA042453Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RIGHT WING INBOARD T/E AFT FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.SDR COOSDR040037Skin · delaminatedLT WING, OB FORE FLAP LOWER AND UPPER SKIN DELAMINATED AT WBL 300 AND AT WBL 210.SDR UPS04243079Casting · crackedINSPECTION TYPE: C, CRACK ON NR 7 FLAP TRACK CASTING ON VERTICAL FLANGE SECOND FROM I/B. HFEC CARRIED OUT - CRACKS CONFIRMED AND ENDS MARKED. STOP DRILLED CRACKS IAW SRM 51-10-1. OUTSIDE LIMITS PER SRM 51-10-6. CASTING REPLACED AND INSTALLED IAW DRG 65-162SDR DL733040796Wedge · debondedNR 4 FORE FLAP TE WEDGE WAS FOUND WITH A 42 INCH SECTION OF SKIN DISBONDED. REPAIRED PER ER/A 092865-14.SDR 04FDEA02553Support · corrodedCOMPLY WITH EA 8-5750-80595 WINGS RT OUTBOARD FLAP, FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-80595, WINGS RT OUTBOARD FLAP, FLAP VANE SUPPORT CORROSION REWORK.SDR MALA040543Skin · chafedDURING C CHECK INSPECTION PERFORMED, CHAFF MARKS FOUND ON RT FLAP TAB LOWER SKIN AT NR 1 HINGE POINT. MAINTENANCE REPAIRED ON 409 NR 186861.SDR MALA040544Skin · chafedDURING C-CHECK INSPECTION PERFORMED, CHAF MARKS FOUND ON RT FLAP TAB LOWER SKIN AT NR 2 HINGE POINT. MAINTENANCE REPAIRED ON 409 NR 186860.SDR IXXA060418SFitting · crackedDURING ROUTINE C CHECK, FOUND LEFT WING IN BOARD FLAP FITTING CRACKED AT STATION XW97. REPLACED FITTING PER ALL APPLICABLE DATA.SDR IXXA0500077SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION FOUND LT INBOARD FLAP WITH TEMP REPAIR ON UPPER SURFACE STA XW 90.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF PLATING WITH THE TEMP REPAIR ON IT. FABRICATED NEW PLATING. CLEANED, TREATED AND PRIMED AREA AND THE INNER FACE OSDR USAA040581Skin · delaminatedCLT - FOUND TRAILING EDGE FLAPS DELAMINATED 6 INCHES, INBOARD MAIN FLAP AT OUTBOARD TRAILING EDGE. REPLACED TRAILING EDGE WEDGE PER BOEING DWG 113N2600. (M)SDR SWAA042399Skin · crackedDURING SCHEDULED HC1 CHECK, FOUND LT WING INBOARD AFT T/E FLAP CRACKED. REPAIRED T/E FLAP PER EA.SDR SWAA042390Skin · delaminatedDURING SPINDLE INSPECTION, FOUND AREA OF DELAMINATION ON OUTBOARD T/E FLAPS. REPAIRED OUTBOARD T/E FLAPS PER SRM.SDR IXXA0500008SSkin · damagedDURING A ROUTINE C-CHECK MAINTENANCE FOUND RT OUTBOARD FLAP L/E HAS INTERIM REPAIR ON UPPER SKIN, STA XF 418.000. PERFORMED MAJOR REPAIR IAW DCI SRM 57-1-0 PG 1 DC8, SRM 57-7-1 FIG 4 (TR 5794). REMOVED PLATING WITH INTERIM REPAIR ON IT, IAW DC8 SRM 51-1-21 PSDR UPS04843120Fitting · crackedINSPECTION TYPE: C1, RT FLAP HINGE 3 FITTING HAS APPROX 6-8 IN LONG CRACK BETWEEN TRACK LANDS. REMOVED FLAP HINGE 3 FITTING. IAW SRM 51-1-20D, 51-1-21 AND 51-3-0. FABED IAW SAA SK 708-840-2 FITTING SAME MFG P/N 5642342-2, FLAP LINK SUPPORT FITTING FROM 70SDR UPS04243062Skin · debondedINSPECTION TYPE:C LT OB MIDFLAP T-EDGE WEDGE UPPER SKIN DISBOND 45 INCHES IB OF OB EDGE. DAMAGE REPAIRED IAW SRM 51-40-5SDR SWAA042372Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OUTBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED RT WING OUTBOARD AFT T/E FLAP PER MM.SDR SWAA042371Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LEFT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED LT WING INBOARD FOREFLAP PER MM.SDR USAA040454Bracket · gougedPIT - FOUND BRACKET GOUGED 1.75 INCH BY .125 INCH WIDE BY .020 INCH DEEP, LEFT OUTBOARD AFT FLAP BRACKET NR 2. BLENDED PER EA 78975. (M)SDR SWAA042324Spindle · wornWHEN FLAPS LOWERED TO 5, THE AIRCRAFT SHUTTERED. NO ROLL, FELT IN CONTROLS. REMOVED AND REPLACED LT WING OUTBOARD AFT FLAP NR 1 AND NR 2 TOGGLES, SEQ CARRIAGE, SPINDLE. RT WING OUTBOARD AFT FLAP NR 7 AND NR 8 TOGGLES, SEQ CARRIAGE, SPINDLE PER MM.SDR 04FDEA02464Hinge Bracket · damagedC/W WITH EA 8-5740-78234 WING LT OTBD FLAP OUTBD HINGE BRACKET, ACT MOUNT HOLES REPAIR P/N ARC0503. COMPLIED WITH EA 8-5740-78234 TO INCLUDE REV A WINGS LT OUTBD FLAP, OUTBD HINGE BRACKET ACTUATOR MOUNT HOLES REPAIR, P/N ARC0503 AT MAE.SDR USAA040476Skin · debondedCLT - FOUND AFT FLAP RIGHT WING DISBONDED 12 SQUARE INCHES, APPROXIMATELY 3 FEET FROM .125 END. REMOVED AND REPLACED FLAP IAW AMM 27-51-12. (M)SDR USAA040458Wedge · delaminatedCLT - FOUND TRAILING EDGE WEDGE DELAMINATED .5 SQUARE FT AREA, LT WING, INBOARD MAIN FLAP, 48 INCHES IN FROM OUTBOARD END. REMOVED AND REPLACED T/E WEDGE PER SRM 51-72-11 AND BOEING DWG 113N2600. (M)SDR P5CA0401138Flap Track · delaminatedDELAMINATION SEVERAL AREA, I/B FORE FLAP L/E RIGHT WING B/W FLAP TRACK. CLEANED AREA & REPAIRED PER SRM 51-40-15.SDR SWAA042295Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING INBOARD AFT T/E FLAP DELAMINATED AT OUTBOARD END. REMOVED AND REPLACED T/E FLAP ASSY PER MM.SDR 2005FA0000288Rib · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUCSDR 2005FA0000287Carriage · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR METAL CARRIAGE ASSY (PN TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUSDR 2005FA0000286Rib · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUSDR 2005FA0000285Rib · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUSDR 2005FA0000284Rib · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUSDR 2005FA0000283Rib · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUSDR 2005FA0000282Rib · failedBONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS INTRODUSDR 2005FA0000281Rib · failedTHE BONDED INSERTS WHICH PROVIDE THE ATTACH POINTS FOR THE METAL CARRIAGE ASSEMBLY TO THE HONEYCOMB FLAP END-RIB HAVE FAILED. INSPECTION OF THE INSERTS REVEALS THAT THE SEAL BETWEEN THE BONDED INSERT AND THE HONEYCOMB STRUCTURE BECOMES COMPROMISED. WATER IS SDR CA041118003Washer · missing(CAN) RT IB AFT MID FLAP (TWO) OB TRACK CARRIAGE ROLLER BOLT TAB WASHERS AND NUTS MISSING. CORRECT HARDWARE INSTALLED, INDEPENDENT CHECK CARRIED OUT. CONTRACTED AMO ADVISED.SDR USAA040417Skin · delaminatedPIT - FOUND FLAP SKIN DELAMINATED WITH 6 INCH SPLIT IN T/E SKIN, 6 INCHES FROM INBOARD END OF RIGHT AFT FLAP, OUTBOARD AFT FLAP. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR 04FDEA02395Hinge Bracket · corrodedRT WING, OB FLAP, OB AFT HINGE OB PIVOT HOLE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE OUTBOARD PIVOT HOLECORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.097. COMPLIED WITH FEDEX EA 1-5750-76808, SDR 04FDEA02400Hinge Bracket · corrodedRT WING, OB FLAP, OB AFT HINGE IB ACTUATOR ROD END ATTACHING HOLE IB FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.408, MATERIAL REMOVED = 0.002, REMAINING THICKNESS = 0.406. COMPLIED WITH FEDEX EA 1-5750-76808, LEFSDR 04FDEA02399Hinge Bracket · corrodedRT WING, OB FLAP, OB AFT HINGE IB ACTUATOR ROD END ATTACHING HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.090. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGESDR 04FDEA02398Hinge Bracket · corrodedRT WING, OB FLAP, OB AFT HINGE PIVOT HOLE IB FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.504, MATERIAL REMOVED = 0.010, REMAINING THICKNESS = 0.494. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLSDR 04FDEA02397Hinge Bracket · corrodedRT WING, OB FLAP, OB AFT HINGE IB PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMETER=1.082, FINAL DIAMETER=1.097. COMPLIED WITH FEDEX EA 1-5750-76808, LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HINGE BRACKET BORE CORRODED.SDR 04FDEA02396Hinge Bracket · corrodedRT WING, OB FLAP, OB AFT HINGE PIVOT HOLE OB FLANGE CORRODED. RT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE PIVOT HOLE OUTBOARD FLANGE CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.503, MATERIAL REMOVED = 0.004, REMAINING THICKNESS =
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