JASC 5753
Service difficulty reports · 31,515
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 05FDEA02778Attach Fitting · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632.SDR 05FDEA02777Attach Fitting · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87632.SDR 05FDEA02776Attach Fitting · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87632.SDR 05FDEA02775Attach Fitting · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87632.SDR 05FDEA02774Attach Fitting · corrodedRT WING O/B FLAP I/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87632.SDR 05FDEA02773Attach Fitting · corrodedRT 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 1-5750-87630 AND CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 05FDEA02772Attach Fitting · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. REPAIR CARRIED OUT AS PER EA 1-5750-87630.SDR 05FDEA02771Attach Fitting · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. FABRICATED BUSHING AND INSTALLED AS PER EA 1-5750-87630.SDR 05FDEA02770Attach Fitting · corrodedRT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87630.SDR 05FDEA02769Attach Fitting · corrodedRIGHT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AND CARRIED OUT AS PER EA 1-5750-87630.SDR 05FDEA02768Attach Fitting · corrodedRIGHT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87630.SDR 05FDEA02767Attach Fitting · corrodedRIGHT 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. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87630.SDR 05FDEA02766Attach Fitting · corrodedRIGHT WING - O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02. BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-87630.SDR 05FDEA02765Attach Fitting · corrodedLEFT WING - O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87629.SDR 05FDEA02764Attach Fitting · corrodedLEFT WING - O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT O/B BORE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629.SDR 05FDEA02763Attach Fitting · corrodedLEFT WING - O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629.SDR 05FDEA02762Attach Fitting · corrodedLT WING O/B FLAP O/B HINGE (FLAP SIDE), PIVOT PIN ATTACHMENT I/B BORE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629.SDR 05FDEA02761Attach Fitting · corrodedLEFT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629.SDR 05FDEA02760Attach Fitting · corrodedLEFT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT O/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87629.SDR 05FDEA02759Attach Fitting · corrodedLEFT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B HOLE SPOT FACE FOUND CORRODED. CORROSION REPAIR CARRIED OUT AS PER EA 1-5750-87629.SDR 05FDEA02758Attach Fitting · corrodedLEFT WING O/B FLAP O/B HINGE (FLAP SIDE), ACTUATOR ATTACHMENT I/B BORE FOUND CORRODED. REPAIR CARRIED OUT AS PER EA 1-5750-87629.SDR S2YA05054Mount · loosePREVIOUS SDR, SHORTLY AFTER TAKEOFF OF FLIGHT, CREW REPORTED FLAPS WILL NOT RETRACT. AFTER CONSULTING WITH DISPATCH AND MAINT CREW PERFORMED AND AIR-TURN-BACK. MAINT REPLACED RT SAFELY SWITCH LINK AND CAM, OPS CHECKED SYSTEM AND WITH NO FURTHER DEFECTS RETURSDR 05FDEA02755Skin · damagedEXISTNG REPAIR DOUBLER FOUND AT RT WING IB FLAP IB T/E SECTION UPPER SKIN BETWEEN XIFH 195.300 AND XIFH 201.300. EXISTING REPAIR DOUBLER AT RT WING IB FLAP IB T/E SECTION UPPER SKIN BETWEEN XIFH 195.300 AND XIFH 201.300 REPAIRED IAW SRM 57-10-00 FIG.34 VOL.I.SDR 05FDEA02754Skin · damagedEXISTING REPAIR DOUBLER FOUND AT RT WING IB FLAP, IB T/E SECTION UPPER SKIN, BETWEEN XIFH 165.300 AND XIFH 171.300. REPAIRED IAW SRM 57-10-00 FIG.34 VOL.I. THIS REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR MALA050701Tab · chafedWHILE ACCOMPLISHING C3.IG1 INSPECTION FOUND LEFT INBOARD FLAP TAB HAS SEVERAL CHAFING MARKS AT INBOARD ATTACH POINT.SDR 05FDEA02736Skin · tornLEFT WING OUTBORD FORE FLAP UPPER SKIN SECTION MISSING (HONEYCOMB EXPOSED). REMOVED AND REPLACED LEFT WING OUTBORD FORE FLAP ASSEMBLY ON FEDEX SNRM N00079. REFERENCE NON ROUTINE N00007.SDR AWXA200501060Skin · debondedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED AREA OF DISBOND LOCATED ON THE UPPER AND LOWER SURFACE OF THE LEFT HAND OUTBOARD FLAP FROM WS 230.68L TO WS 237.68L. MAINTENANCE REMOVED AREA OF DISBOND FROM LT OUTBOARD FLAP IAW BOEING 737-300 SRM 51-70-10-2R4SDR SWAA052650Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA052637Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR UPS05245470Flap Track · corrodedINSPECTION TYPE:C-CORROSION ON NR 4 FLAP TRACK AFT MOUNT PAD CORROSION REMOVED IAW SOPM 20-10-01 P1 AND EO B727-5742-0651K & TEMPER ETCHED 2B (3) IAW SOPM 20-10-01. CAD PLATED IAW OHM 20-42-10.SDR UPS05245469Flap Track · corrodedINSPECTION TYPE:C-CORROSION FOUND ON FWD MOUNTING PAD OF NR 4 FLAP TRACK. CORROSION REMOVED IAW SOPM 20-10-01 P1 AND EO B727-5742-0651K. SURFACE TEMPER ETCHED 2B (3) IAW SOPM 20-10-01. CAD PLATED IAW OHM 20-42-10.SDR UPS05245468Flap Track · corrodedINSPECTION TYPE:C-CORROSION ON NR 4 FLAP TRACK FWD MOUNTING UPPER AND LWR, ALSO INNER RADIUS OF HOLES. CORROSION REMOVED IAW SOPM 20-10-01 P1 AND EO B727-5742-0651K AND TEMPER ETCHED IAW SOPM 20-10-01.SDR AWXA200501049Skin · debondedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP FROM WBL 301.69 TO WBL 305.69. MAINTENANCE REMOVED DAMAGED AREA ON THE RT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-2R 4. FABRICATED CORESDR 05FDEA02693Fitting · crackedO/B FLAP FOUND CRACK AT UPSTOP BOLT LE STRUCTURE. REMOVED AND REPLACED UP STOP FITTING AS PER SRM 51-33-01 AND 51-31-01 VOL.II.SDR USAA051055Skin · delaminatedRT O/B FLAP TRAILING EDGE, OUT FLAP SKIN. INSTALLED DOUBLER PER SRM 57-53-00 FIG 213 VERSION 3, DEFECT SIZE: 22" LENGTH OF DELAMINATION.SDR 05FDEA02682Skin · dentedRT WING I/B FLAP STRUCTURE AT XIFH 195.300 TO XIFH 189.300 FOUND DENT IN THE LWR EXTERNAL SKIN DIAMETER 2.36 INCH BY .275 INCH DEEP AND FOUND DEFORMATION ON STRUCTURE. CUT DAMAGE SECTION OF SKIN; CHECKED AND REPAIR IAW SRM 57-00-01 FIG 4 SHEET 2 VOL I.SDR SWAA052597Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR USAA051053Wedge · dentedCLT - FOUND WEDGE WITH DENT 4 INCH BY 5 INCH, BOTTOM OF THE WEDGE AT THE OUTBOARD TRAILING EDGE. REMOVED DAMAGE, INSTALLED A NEW CORE AND DOUBLER IAW EA 96745. (M)SDR AWXA200501051Wedge · debondedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE LT INBOARD FORE FLAP FROM WBL 103.0L TO WBL 111.0L. MAINTENANCE REMOVED DAMAGED AREA ON THE LT INBOARD FORE FLAP FROM WBL 103.0L TO WBL 111.0L IAW BOEING 737-300 SRM 51-SDR AWXA200501048Skin · debondedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP FROM WBL 197.5 TO WBL 200.5. MAINTENANCE REMOVED DAMAGED AREA ON THE RT OUTBOARD FORE FLAP IAW BOEING 737-300 SRM 51-70-10-2R 4. FABRICATED CORE, SDR 08232005BAttach Bolt · wornEXCESSIVE PLAY IN ATTACHMENT POINTS OF RT OUTBOARD FLAP. REMOVED AND REPLACED FWD ROLLER BOLT. ADJUSTED FLAP BUMPERS ON NR 4 FLAP. OPS CHECK GOOD.SDR SWAA052554Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA052546Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR ASAA0540428Skin · puncturedRT IB FORE FLAP LWR SKIN PUNCTURED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM. (K)SDR ASAA0540427Wedge · dentedRT IB MID FLAP T/E WEDGE 7420R HAS SEVERAL DINGS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS IAW SRM. (K)SDR ASAA0540426Skin · dentedLT IB FORE FLAP DENTED, DELAMINATED ON LOWER SKIN AT CENTER TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED SKIN SECTION AND DOUBLER IAW SRM. (K)SDR ABXA050214Stud · brokenRIGHT WING OUTBOARD FLAP HINGE, STA 333, INBOARD LOWER STUD BROKEN OFF. REMOVED AND REPLACED ALL 4 STUDS IAW JOB CARD 92410004 AND DC-9 SRM.SDR CA050823001Support · cracked(CAN) DURING A ROUTINE INSPECTION, MAINTENANCE FOUND A CRACK IN THE RT FLAP ASYMMETRY TELEFLEX CABLE SUPPORT. THIS SUPPORT IS LOCATED ON THE RT FLAP IB SUPPORT AND IS ATTACHING POINT FOR ASYMMETRY DETECTOR TELEFLEX ROD END. FURTHER INVESTIGATION, A SECOND CRACSDR 2005UALA00870Skin · puncturedLEFT WING INBOARD FLAP, INBOARD SECTION ON LOWER SURFACE, SKIN IS PUNCTURED ON FOREFLAP. DAMAGE FOUND ON THE LOWER SKIN ON THE FLAP WAS AN ISOLATED INCIDENT BUT WILL BE FILED FOR FUTURE REFERENCE OF SIMILIAR FINDINGS. A 200 DEGREE FAHRENHEIT, WET LAY-UP REPASDR SWIA200515477Structure · damagedLEFT INBOARD FLAP DAMAGE ON UNDERSIDE OF FLAP AFTER NR 1 MAIN BLEW OUT ON LANDING. REPLACED LEFT INBOARD FLAP IAW MM 27-54-01. OPERATIONAL CHECK GOOD.
Back to JASC 5753