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 SWAA095165Flap · delaminatedDURING SCHEDULED 8Y CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA095163Skin · delaminatedDURING SCHEDULED 8Y CHECK, FOUND LT WING O/B AFT FLAP I/B AFT TRAILING EDGE CORNER LOWER SURFACE DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR FDEA200908112970Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND WITH PITTING CORROSION HINGE FITTING. COMPLIED WITH EA 1-5750-132282. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100.SDR FDEA200908112969Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE FOUND WITH PITTING CORROSION. COMPLIED WITH EA 1-5750-132283. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA200908112968Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), INBOARD PIVOT HOLE FOUND WITH PITTING CORROSION HINGE FITTING. COMPLIED WITH EA 1-5750-132283. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100.SDR IPXA09156957Skin · crackedINSPECTION TYPE:N/A LEFT FLAP LOWER SKIN CRACKED. REPAIRED PER EO A300-5750-34534-A.SDR SWAA095103Flap · delaminatedDURING SCHEDULED 24Y CHECK, FOUND RT WING MID FLAP L/E DELAMINATED. REPAIRED MID FLAP PER SRM.SDR A6WA200940499Vane · chafedRT INBD FLAP VANE L/E FOUND CHAFED (3 AREAS) RT INBD FLAP VANE L/E REPAIRED IAW REO 601R-57-52-004, REV C. (K)SDR A6WA200940501Bracket · gougedBRACKET HOLDING LT WING, FLAP STUP FAIRING GOUGED AT W/S 48.00 BRACKET REPLACED IAW SRM 51-42-21. (K)SDR A6WA200940500Bracket · crackedBRACKET HOLDING RT WING, FLAP STUB FAIRING CRACK AT W/S 48.00 CRACK LENGTH .300 INCH BRACKET AT RT WING W/S 48.00 REPLACED IAW SRM 51-42-21. (K)SDR IPXA09157071Doubler · damagedINSPECTION TYPE:3/C LT WING CENTER FLAP UPPER SKIN REPAIR CHAFED REPAIR SURVEY 147-W3-02. FABBED AND INSTALLED REPAIR DOUBLER IAW UPS EO A300-5750-34609-A AND SAA EA 300-5753-01-A1963.SDR FDEA200908082956Stop Fitting · crackedRT WING OTBD FLAP ASSY UP-STOP FITTING FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 51-31-01 REVISION 41 AND SRM 51-33-01 REVISION 41. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 107.SDR DHLA2009873586Vane · damagedRIGHT WING VANE SLOT REPAIR HAS ELONGATED HOLES, STA XOLDO 67.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-23-09, EVA D857-00263 REV IR DATED 07-13-09, DWG REV 01 ED-4968. REMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED HFEC INSPESDR FDEA200908082957Fitting · crackedLEFT HAND WING OUTBAORD FLAP ASSEMBLY UP-STOP FITING FOUND CRACKED ARC4125-501. REMOVED AS PER SRM 51-31-01 REVISION 41 AND REPLACED AS PER SRM 51-33-01 REVISION 41. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR IPXA09M56949Wedge · crackedINSPECTION TYPE:N/A RIGHT I/B AFT FLAP T/E SPLIT FROM IN TO 15 INCHES O/B. REPAIRED PER EO MD11-5750-34526-A.SDR A6WA200940491Skin · dentedSKIN DENTED ON LT INNER FLAP AS REQUIRED. UNDERSIDE SKIN OF LT INNER FLAP REPAIRED IAW REO 601R-57-52-1483. (K)SDR A6WA200940497Vane · chafedL/E LT INBD FLAP VANE CHAFED IN 3 PLACES. L/E OF LT INBD FLAP VANE. REPAIRED IAW REO 601R-57-52-004, REV C. (K)SDR FDEA200908073165Skin · delaminatedLT WING FLAP INBD WITH DEBONDING ON T/E. T/E WAS REPLACED IAW EA 6-5710-131046 AND SRM 51-72-10.SDR FDEA200908072938Skin · dentedRIGHT WING INBOARD FLAP ASSEMBLY LEADING EDGE SURFACE FOUND WITH DENT SKIN. REPAIR CARRIED OUT AS PER E.A. 1-5700-131638, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 107.SDR FDEA200908072932Hinge Bracket · corrodedR/H WING INBD TRAILING EDGE OUTBD AFT HINGE INBD PIVOT BORE HOLE FOUND WITH MINOR SURFACE CORROSION. COMPLIED WITH EA 1-5750-132738. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV. 107.SDR IXXA09SMN076SSkin · brokenDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HAND OUTBOARD FLAP EXTERNAL SKIN UPPER PART BROKEN AT STATION XF 409.000.REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLESDR IXXA09SMN075SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HAND INBOARD FLAP PANEL UPPER SKIN HAS SEVERAL DENTS AT STATION XW 2.000 - STATION XW 84.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. CLEANED, SDR SWIA200922785Vane · wornRIGHT INBOARD FLAP VANE WORN BEYOND LIMITS. (C CHECK) REPAIRED PER SRM.SDR IPXA09M57117Doubler · misrepairedINSPECTION TYPE:C2 REPAIR SURVEY SEQ 258-W4-05 RT INBOARD FLAP UPPER SKIN BETWEEN STA X1FH 147 .300-153.300 REPAIR DOUBLER NOT CORRELATED TO SRM 57-10-00 FIG 38 VOL 1. PERFORMED MAJOR REPAIR, REMOVED AND INSTALLED REPAIR DOUBLER IAW SRM 57-00-01 REPAIR 1 FIG SDR SWAA095026ASkin · delaminatedDURING SCHEDULED MV1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0946369Skin · delaminatedRIGHT O/B FORE FLAP TRAILING EDGE UPPER SURFACE IS DELAMINATED. REPLACED O/B FORE FLAP.SDR AALA20090805TUL01Vane · wornLEFT WING TRAILING EDGE LEADING EDGE OF NUMBER THREE FLAP VANE CONTACTING HYDRAULIC LINE ON INBOARD SIDE OF NUMBER TWO FLAP HINGE. INSTALLED HOT-BOND REPAIR UNDER SRM 51-70-02.SDR IPXA09M57271Skin · dentedINSPECTION TYPE:2C LEFT WING INBD FLAP UPPER SKIN SURFACE HAS 3 EA DENTS. REMOVED EXISTING REPAIRS FROM LEFT WING INBD FLAP UPPER SKIN AT STA X XIFH 159.3 AND XIFH 20.616. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF MD11 SRM 57-00-01 REPAIR 1 FIG 201 SHTSDR FDEA200908042892Vane · delaminatedRIGHT WING - INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. RT WING - INBD FLAP VANE ASSY REMOVED AND REPLACED IAW AMM 27-50-22-4, REV.64. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5 REV. 64.SDR IPXA09157072Skin · chafedINSPECTION TYPE:3/C LT WING CENTER FLAP UPPER SKIN CHAFED IN 2 PLACES ABOVE NR 4 FLAP TRACK. FABBED AND INSTALLED REPAIR DOUBLER IAW UPS EO A300-5750-34610-A AND SAA EA 300-5753-01-A1972.SDR IPXA09157023Doubler · chafedINSPECTION TYPE:3/C LT WING CENTER FLAP UPPER SKIN REPAIR CHAFED REPAIR SURVEY 147-W3-02. FABBED AND INSTALLED REPAIR DOUBLER IAW SAA EA 300-5753-01-A1963.SDR IPXA09656988Wedge · delaminatedINSPECTION TYPE:C RIGHT WING O/B FLAP TRAILING EDGE O/B LWR SURFACE DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-06 PAR 5A (1) FIG 9 REV 44.SDR IPXA09656961Hinge Fitting · crackedINSPECTION TYPE:C RT WING I/B AFT FLAP HINGE FITTING FOUND CRACK. CRACK LENGTH I/B FLANGE 1.2 INCH, O/B FLANGE 1.5 INCH. RT WING I/B AFT FLAP HINGE FITTING REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATERSDR SWAA094957Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING O/B FORE FLAP I/B TRAILING EDGE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR ASAA0956353Skin · delaminatedLEFT WING TRAILING EDGE FLAP LWR SKIN IS DELAMINATED AT PREVIOUS REPAIR 18 INCHES FROM I/B EDGE. REPAIR AFT FLAP LOWER SKIN.SDR ASAA0946346Skin · chafedRIGHT O/B FORE FLAP I/B LEADING EDGE IS CHAFED. REPAIRED IAW SRM.SDR IPXA09M57268Skin · dentedINSPECTION TYPE:2C RT IB FLAP SKIN DENTED LOWER SURFACE OB END NEAR STA XIFH 276. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO MD11-5750-34814-A AND SAA EA 011-5730-01-A2001.SDR ASAA0976320Fitting · wornLEFT WING O/B MAIN FLAP O/B LWR FWD DEFLECTION FITTING IS WORN. REPLACED LWR FWD DEFLECTION FITTING.SDR DLM90091299Flap · dentedRE-INSPECTION OF THE DENT FOUND ANOTHER DENT, ON 08/01/09. NO EMERGENCY PROCEDURE REQUIRE, WILL NEED A SRM/ERA REPAIR. UNKNOWN ON WHAT CAUSE THE DENTS. A PERMANENT REPAIR DONE AT ATL.SDR USAA2009080391988Flap · delaminatedCLT - RON - MAJOR REPAIR - RIGHT OUTBOARD TRAILING EDGE FLAP DELAMINATED BEYOND LIMITS. REPLACED RIGHT OUTBOARD TRAILING EDGE FLAP IAW B737 AMM 27-51-39-4.SDR ASAA0946336Flap Track · corrodedNR 3 FLAP TRACK HAS EVIDENCE OF CORROSION ON ALL ROLLER SURFACES. REMOVED AND REPLACED NR 3 FLAP TRACK.SDR ASAA0946335Flap Track · corrodedNR 7 FLAP TRACK AFT ATTACH POINT RUSTY AT SHIMS. BOLT HOLES WERE FOUND TO BE CORRODED TRACK WAS REMOVED AND REPLACED.SDR C8GA20090244Rub Strip · delaminatedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE RT OTBD FOREFLAP RUB STRIP IS DISBONDED OTBD OF INBD TRACK. REMOVED DAMAGE DIM 21" X 4" FABRICATED FILLER FROM 2024 T3 .016" DOUBLER 2024 T3 .016" DIM 24" X 5.5" INSTALLED HOT BOND REPAIR, NO OTHER DEFSDR C8GA20090243Rub Strip · delaminatedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT OTBD FOREFLAP RUB STRIP IS DISBONDED. REMOVED DAMAGE FROM T/E DIM 13.5" X 5" FABRICATED FILLER FROM 2024 T3 .016" DIM 16.5" X 6.5" INSTALLED HOT BOND REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETSDR C8GA20090242Skin · delaminatedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT INBD AFT FLAP T/E DELAMINATED. REMOVED DELAMINATION DIM 3" X 7" FABRICATED DOUBLER FROM 2024 T3 .020" DIM 4.5" X 10. INSTALLED HOT BOND REPAIR. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVISDR C8GA20090241Doubler · gougedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT INBD FOREFLAP OTBD L/E REPAIR IS GOUGED. REMOVED PREVIOUS REPAIR, FABRICATED DOUBLER FROM2024 T3 .063" DIM 14" X 4.875" FILLER 2024 T3 .050" DIM 14" X 4.5". NO OTHER DEFECTS WERE NOTED. ACFT WAS RETSDR C8GA20090233Skin · delaminatedWHILE IN HEAVY CHECK PERFORMING INSP IT WAS NOTED THAT THE RT INBD MID FLAP T/E HAS DELAMINATION. REMOVED DAMAGED SKIN DIM 5" X 4". FABRICATED FILLER FROM 2024 T3 .016" AND DOUBLER FROM 2024 T3 .020 DIM 8" X 4". INSTALLED HOT BOND REPAIR, NO OTHER DEFECTS WESDR C8GA20090224ASkin · crackedWHILE IN INSP, IT WAS NOTED THAT THE LT INBD AFT FLAP UPPER SKIN AT HINGE IS CRACKED. STOP DRILLED CRACK, HFEC FOR CRACK CONTAINMENT AND FABRICATED DOUBLER. INSTALLED DOUBLER, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR USAA2009091192480Carriage · corrodedSAL - Q6 - MAJOR REPAIR - CORROSION IN FORWARD BEARING BORE OF NR 5 MID FLAP CARRIAGE INBOARD HALF. REPLACED NR 5 MID FLAP CARRIAGE INBOARD HALF IAW B737 AMM 27-51-14.SDR USAA2009091192479Carriage · corrodedSAL - Q6 - MAJOR REPAIR - CORROSION IN FORWARD BEARING BORE OF NR 5 MID FLAP CARRIAGE OUTBOARD HALF. REPLACED NR 5 MID FLAP CARRIAGE OUTBOARD HALF IAW B737 AMM 27-51-14.
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