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 SWAA103822Skin · puncturedDURING SCHEDULED 12Y CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED ON I/B LOWER SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA103821Skin · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP I/B UPPER AND LOWER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA103793Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING O/B AFT FLAP T/E DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR QXEA2010062800363Skin · chafedC-CHECK - RT WING INBD FLAP UPPER SURFACE CHAFED APPROX 6 INCHES OTBD OF INBD EDGE AND 18.5 INCHES UP FROM T/E. REPAIRED DAMAGE IAW SRM 57-51-30-02-01. BLEND MEASURED .45" LONG .38" WIDE, MAX DEPTH .004". ORIGINAL THICKNESS IS .057", BLEND WITHIN LIMITS IAW SDR ABXR201006272010Flap Track · corrodedDURING MX, THE LEFT OTBD FLAP, OTBD TRACK WAS BLEEDING RUST. UPON DISASSEMBLY, THE TRACK WAS FOUNDED CORRODED. THE CORROSION WENT BEYOND THE CMM LIMITS. MFG ENGINEERING ISSUED AN REA TO FURTHER CLEAN THE CORROSION WITH ADDITIONAL LIMITS ESTABLISHED. THE CORROSDR FDEA201006262190Vane · delaminatedDELAMINATION - LT WING INBD FLAP VANE LOWER SURFACE. REMOVED AND REPLACED AS PER AMM 27-50-22 REV 66 ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-830-801 REV 66.SDR CA100625003Flap Track · corrodedNR 4 LT FLAP TRACK BEAM ASSEMBLY FOUND WITH ADVANCED CORROSION IN HIDDEN AREA. THIS BEAM WOULD NORMALLY BE A REPEAT INSPECTION AND BLENDING OF WEAR POINTS. IT WAS DECIDED TO CHANGE OUT THIS BEAM TO HAVE IT OVERHAULED INSTEAD OF RE-WORKING ON WING. THE HIDDENSDR IPXA10560901Skin · dentedINSPECTION TYPE:C3, RT WING OTBD FLAP HAS A DENT IN THE UPPER SURFACE 23.5" FROM 013 END AND 4" FWD OF T/E REPAIRED DENT 23.5" FROM OTBD END AND 4" FWD OF T/E ON THE RT WING OTBD FORE FLAP IAW SRM 51-70-07-OG.SDR IPXA10560852Skin · dentedINSPECTION TYPE:C3 R/W OTBD FOREFLAP HAS A DENT IN THE UPPER SURFACE 23.5" FROM OTBD END AND 4" FWD OF T/E. REPAIRED DENT 23.5" FROM OTBD END AND 4" FWD OF T/E ON THE R/W OTBD FOREFLAP IAW SRM 51-70-07-0G.SDR UIEA2010062500048Skin · dentedDURING C-CHECK, A DENT/WRINKLE WAS DETECTED IN SKIN OF RT FLAP NR 18 L/E AT 29 INCHES FROM THE INBD EDGE LOOKING AFT. DAMAGE WAS TRIMMED OUT AND REPAIRED IAW INRC 0386 AND SRM 57-50-03, FIG 3, SHEET 4, DETAIL III FIG 1.SDR SWAA103723Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP I/B SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA103721Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR AALA20100623TUL06Skin · wornRIGHT OUTBOARD MAIN FLAP LEADING SKIN HAS WORN AREA 15 INCHES LONG FROM INBOARD END. REMOVED LEADING EDGE SKIN, CUT OUT WORN AREA, FORMED DOUBLER AND DRILLED, PRIMED AND INSTALLED DOUBLER PER SRM 57-53-01-2R.SDR A6WA201040573Cam · wornRT OTBD FLAP, FLAP VANES CAMS WORN MEASURED RT OTBD FLAP VANE CAMS AND FOUND CAMS TO BE IN SERVICEABLE LIMITS IAW REO 601R-57-53-195.SDR A6WA201040464Cam · wornLT OTBD FLAP CAMS ARE WORN. MEASURED LT OOTBD FLAP CAMS AND FOUND CAMS TO BE IN SERVICEABLE LIMITS IAW REO 601R-57-53-195.SDR FDEA201006232117Skin · dentedRT WING INBD FLAP LOWER SKIN IS DENTED. CHECKED ALL DENTS IAW MD/DC10 SRM 57-10-00, FIG 48, PG 162A, VOL I. ALL DENTS BETWEEN XIFH 192 TO XIFH 199 AND YIFH 39 TO YIFH 51 ARE WITHIN LIMITS. DENT AT XIFH 201 AND YIFH 72 IS CREASED OUT OF LIMITS. BLENDED OUSDR CA100623004Skin · crackedPILOT REPORTED SLIGHT VIBRATION IN FLAPS. UPON INSP, BEFORE THE NEXT FLIGHT, THE RT AILERON WAS FOUND TO HAVE SIGNIFICANT CRACKING IN MULTIPLE AREAS WITH A PORTION OF THE T/E (APROX 18 INCHES LONG AND 1 INCH FWD) BLOWN OUT. THIS AILERON HAD 118.4 HOURS SINCE SDR AALA20100622TUL05Wedge · dentedINBOARD FLAP WEDGE ON INBOARD FLAP HAS 3 DENTS. TWO DENTS REMOVED BY DRILLING AND THIRD DENT REMOVED BY CUTTING 1 INCH HOLE. DYE CHECKED AREA FOR CRACKS, NONE FOUND. PLUGGED THE DRILLED HOLES WITH RIVETS PER SRM 57-01-00, FIGURE 2 SHEET 2. REPAIRED 1 IN HOSDR CA100622024Bolt · shearedA PORTION OF THE BOLT AND A BUSHING (PN NAS72-7E007) WAS DISCOVERED ON A TAXIWAY USED BY ACFT EARLIER IN THE DAY. THE ACFT WAS INSPECTED, AND THE PART WAS FOUND BE MISSING FROM THE LT WING, INBD FLAP, OTBD FLAP CARRIAGE ASSY. THE ACFT WAS TAKEN OUT OF SERVICSDR ASAA1047933Skin · dentedLT INBOARD FORE FLAP LOWER SURFACE HAS MULTIPLE MINOR DENTS BETWEEN INBOARD AND CNT TRACKS. REMOVED DAMAGED AREA AND BONDED REPAIR.SDR IPXA0B60653Skin · dentedLT WING INBD AFT FLAP LWR SKIN DENT REPAIR WBL 208.2 REF EO B747-5750- 37247-A. REPAIRED IAW EO B747-5750-37247-B.SDR WRLA20100620394Angle · crackedCRACK - CRACK WAS FOUND ON ANGLE OF LT SEAL RETAINER SUPPORT BEAM NR 2 FLAP TRACK MOVABLE FAIRING. FABRICATE AND INSTALL NEW STIFFENER PER DWG 314T4210.SDR SWAA103555Flap · corrodedDURING SCHEDULED 16Y CHECK, FOUND LT WING MID FLAP I/B END CORRODED. REMOVED AND REPLACED MID FLAP PER MM.SDR SWAA103542Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING O/B AFT FLAP I/B END DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IXXA10SMN071SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND THE LT WING OTBD FLAP UPPER SKIN DENTED AT STA XF 238.000 - 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FSDR FDEA201006182386Skin · gougedRT WING - FLAP OUTBD UPPER SKIN WITH 2 SCRATCHES BTW RIB 2 AND RIB 3. FLAP UPPERSKIN WAS REPAIRED IAW EA 6-5758-141543.SDR WRLA20100618396Vane · brokenINBOARD FLAP VANE TRAILING EDGE BROKEN OF LT WING. THIS NRC HAS BEEN COVERED BY ERA: DOCUMENT NUMBER 10-57-029 REVISION 1. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR IPXA10B60682Skin · delaminatedINSPECTION TYPE:C, RT WING INBD MID FLAP L/E FAIRING LOWER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PARA 5A (1) FIG 5, REV 56.SDR ASAA1048131Skin · dentedRIGHT O/B AFT FLAP AT APPROX 12 INCHES FROM I/B EDGE DENTED. REMOVED DAMAGED AREA, INSTALLED DOUBLER REPAIR.SDR A6WA201040434Fitting · chafedLT OTBD FLAP GUIDE ROLLER FITTING CHAFED. REPAIRED IAW REO 601R-57-53-809.SDR A6WA201040436Fitting · chafedRT OTBD FLAP, GUIDE ROLLER FITTING CHAFED. REPAIRED IAW REO 601R-57-53-809.SDR FDEA201006162032Attach Fitting · corrodedLT WING INBD FLAP ASSY INBD ACTUATOR LOWER ATTACHMENT FITTING FOUND CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140360, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.SDR FDEA201006162036Bracket · corrodedRIGHT WING - INBOARD FLAP ASSEMBLY INBOARD FLAP TRACK MOUNTED FITTING NR 3 FROM FORWARD, FOUND LOWER FORWARD HOLE "SPOT FACE" CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140359, REPAIR CLASSIFIED MINOR PER GMM 6- 2-100 REVISION 110.SDR FDEA201006162034Attach Bracket · corrodedRT WING - INBD FLAP ASSY INBD FLAP TRACK MOUNTED FITTING NR 3 FROM FWD, FOUND LOWER FWD HOLE "BORE" CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140359, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.SDR FDEA201006162033Bracket · corrodedRT WING - INBD FLAP ASSY INBD FLAP TRACK MOUNTED FITTING NR3 FROM FWD, FOUND UPPER FWD HOLE, BORE CORROSION. REPAIR CARRIED OUT PER E.A. 8-5750-140359, REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISION 110.SDR SWAA103539Flap · delaminatedRIGHT WING I/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER EA.SDR FDEA201006162026Skin · misrepairedLT INBD T/E FLAP LOWER SURFACE FOUND 1 EACH EXISTING REPAIR AT OTBD OF INBD FLAP OTBD HINGE AREA. FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. REPAIR CARRIED OUT PER DRAWING ARC2992 REVISION R AND AMM 20-50-02 REVISION 10. E.O. 8-5100-7-5001SDR USAA2010061791171Flap · crackedBFM - Q5 - MAJOR REPAIR - CRACK ON RIGHT MID FLAP BETWEEN WS 259 TO WS 384. REPAIRED RIGHT MID FLAP BETWEEN WS 259 TO WS 384 IAW B737 SRM 57-53-01 AND 51-70-10.SDR SWAA103533Flap · delaminatedDURING SCHEDULED 10Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED AT I/B TRAILING EDGE. REPAIRED AFT FLAP PER MM.SDR SWAA103479Flap · delaminatedDURING SCHEDULED 10Y CHECK, FOUND RT WING O/B TRAILING EDGE FLAP, TRAILING EDGE FLAP I/B CORNER DELAMINATED. REMOVED AND REPLACED O/B FLAP PER SRM.SDR V0XR201006140002Flap Track · cracked(V0XR) CRACK ON LT NR 2 FLAP TRACK. R & R FLAP TRACK. W/C 5042SDR V0XR201006140001Flap Track · cracked(V0XR) CRACK ON LT NR 1 FLAP TRACK. R & R FLAP TRACK. W/C 5038SDR FDEA201006131974Skin · misrepairedEXISTING REPAIR 01 EACH FOUND AT LT OUTBOARD TRAILING EDGE FLAP LOWER SURFACE, INBOARD AREA, LOCATION 15 INCHES FROM INBOARD EDGE. EXISTING REPAIR 01 EACH AT LT OUTBOARD TRAILING EDGE FLAP LOWER SURFACE, INBOARD AREA, LOCATION 15 INCHES FROM INBOARD EDGE ESDR SWAA103494Flap · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA103430Skin · crackedDURING SCHEDULED 12Y CHECK, FOUND LT WING I/B AFT FLAP LOWER SKIN CRACKED. REPAIRED AFT FLAP PER SRM.SDR IPXA10B60464Skin · damagedLT OTBD AFT FLAP DAMAGED BOTTOM SIDE. REPAIRED IAW EO B747-5750-38156-A.SDR IPXA10B60463Skin · puncturedRT INBD AFT FLAP T/E .7500" PUNCTURE. REPAIR IO EO B747-5750-38155-A.SDR IPXA10B60462Skin · puncturedRT INBD AFT FLAP T/E .7500" PUNCTURE. REPAIRED IAW E0 B747-5750-38155-A.SDR SWAA103415Wedge · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING I/B TRAILING EDGE AFT FLAP O/B END UPPER SURFACE OF AFT WEDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY PER MM.SDR WRLA20100612399Flap Track · corrodedCORROSION - NR 4 FLAP TRACK FORWARD END CLEVIS BUSHING HOLE AND OUTSIDE SURFACE CORROSION. BLEND OUT THE CORROSION. SPOT FACE THE FWD END CLEVIS. OVERSIZE THE BUSHING HOLE. NDT MEASURE NO DAMAGE WAS FOUND. FLAP PEEN EACH CLEVIS LUG. FABRICATE AT INSTALL
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