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 USAA2010020390268Flap · corrodedCLT - Q1 - MAJOR REPAIR - CORROSION IN BORE RIGHT INBOARD MID FLAP OUTBOARD ARM (EXCENTRIC BEARING HOLE). REPLACED INBOARD MID FLAP IAW JOB CARD 03C40927012.SDR IPXA10658249Skin · dentedRT WING INBD AFT FLAP LOWER SKIN DENTED. REPAIRED IAW B767-5750-36080-B.SDR ASAA1047444Skin · dentedLEFT I/B MID FLAP TRAILING EDGE WEDGE LOWER SKIN HAS A CLUSTER OF DENTS OUT OF LIMITS. REMOVED CORROSION, FABBED REPAIR PARTS AND INSTALLED.SDR ASAA1047443Skin · dentedLEFT I/B MID FLAP TRAILING EDGE WEDGE LOWER SKIN HAS A CLUSTER OF DENTS OUT OF LIMITS. PREPPED DAMAGED AREA, FABBED DOUBLER AND BONDED.SDR ASAA1047431Skin · dentedRIGHT I/B FOREFLAP UPPER SURFACE DENTED AT WBL 150. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.SDR ASAA1047430Skin · dentedRIGHT I/B FOREFLAP UPPER SURFACE DENTED AT WBL 73 125. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.SDR ASAA1047429Skin · dentedRIGHT I/B FOREFLAP UPPER SURFACE DENTED AT WBL 124. REMOVED DAMAGED AREA FABBED FILLER AND DOUBLER, BONDED.SDR ASAA1047428Skin · dentedRIGHT I/B FOREFLAP UPPER SURFACE DENTED AT WBL 113. REMOVED DAMAGED AREA FABBED FILLER AND DOUBLER, BONDED.SDR ASAA1047427Skin · dentedRIGHT I/B FOREFLAP UPPER SURFACE DENTED AT WBL 121. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.SDR IPXA10558366Skin · damagedINSPECTION TYPE:C3, R/W INBD AFT FLAP PREVIOUS REPAIR OF LIGHTNING DAMAGE 3 FT OUT FROM FUSELAGE WAS ACCOMPLISHED INCORRECTLY. REQUIRES REMOVAL AND REACCOMPLISHED (REF EFN 459LGP1004 EO. NR B757-5100-36085) FLAP WAS REPAIRED IAW SRM 51-70-04 PARA 5E.SDR ASAA1047440Wedge · dentedLEFT I/B MIDFLAP TRAILING EDGE WEDGE HAS A CLUSTER OF DENTS APPROX 43 INCHES 49 INCHES FROM I/B EDGE. PREPPED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.SDR ASAA1047439Wedge · dentedLEFT I/B MIDFLAP TRAILING EDGE WEDGE HAS A CLUSTER OF DENTS APPROX 5 INCHES 9.75 INCHES FROM I/B EDGE. PREPPED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.SDR ASAA1047438Wedge · dentedLEFT I/B MIDFLAP TRAILING EDGE WEDGE HAS A CLUSTER OF DENTS APPROX 31 INCHES 32 INCHES FROM I/B EDGE. PREPPED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.SDR ASAA1047432Skin · dentedRIGHT I/B FOREFLAP UPPER SURFACE DENTED AT WBL 144 154. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.SDR ASAA1047437Skin · dentedRIGHT I/B AFT FLAP TRAILING EDGE WEDGE LOWER SURFACE DENTED 5 INCHES FROM WBL 141. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER, BONDED.SDR ASAA1047277Skin · dentedDENT ON LEFT O/B AFT FLAP LOWER SURFACE I/B OF NUMBER 1 FAIRING. REPAIRED LEFT O/B AFT FLAP LOWER SURFACE.SDR IXXA10SMN025SSkin · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING INBD FLAP T/E PANEL CRACKED AT STA XW 35.000 REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH ADHESIVE. CLEANED, TREATED, PRIMEDSDR ASAA1047261Skin · dentedRIGHT WING I/B FOREFLAP LOWER SKIN HAS A DENT CLUSTER WITH OVERLAPPING DAMAGE WBL 80 TO WBL 95. INSTALLED FILLER AND DOUBLER.SDR ASAA1047260Skin · dentedRIGHT I/B FOREFLAP LOWER SURFACE DENTED NEAR CENTER. INSTALLED FILLER AND DOUBLER.SDR IPXA10158305Skin · gougedINSPECTION TYPE: 4/C REPAIR SURVEY NR 131-W4-01 REPAIR DOUBLER IS GOUGED RT INBD FLAP UPPER OTBD SKIN REPAIR ACCOMPLISHED IAW EA 300-5753-01-A2139, REV. I/R AND UPS EO A30 0-5750-30419-A.SDR SWAA100342Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA100313Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR UIEA20100019Carriage · damagedFOUND DURING MAJOR INSPECTION RIGHT INBD MID FLAP CARRIAGE SIDE (INBOARD POSITION) AFTER REMOVAL OF FAIL SAFE BOLT FOUND DAMAGE IN THE BORE. REPLACED RT INBD MID FLAP ASSY PER ATLAS EO REFERENCE NRC 795 AND 897.SDR IPXA10158299Skin · gougedINSPECTION TYPE:4C REPAIR SURVEY SEQUENCE NR 131-W3-01,REPAIR DOUBLER HAS SEVERAL GOUGES REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW SRM 57-50-00 FIG 205 REF RCD 384317.SDR IPXA10158298Skin · gougedINSPECTION TYPE:4C REPAIR SURVEY SEQUENCE NR 131-W4-02, REPAIR DOUBLER HAS SEVERAL GOUGES REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW SRM 57-50-00 FIG 205 AND EO A300-5750-36420-A.SDR SWAA100248Flap · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LT WING AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR FDEA201001180173Skin · chafedRT WING INBD UPPER FLAP L/E STRUCTURE HAS CHAFINGS. REMOVED CHAFE FROM RT WING INBD FLAP IAW SRM 57-53-01, FIG 101 DETAIL VI. FOUND TO BE OUT OF LIMITS. ORIG MATERIAL 0.055 AFTER REWORK 0.049. CUT OUT DAMAGE AREA IAW SRM 57-53-01 FIG 201 REPAIR 2. REMOVED PASDR FDEA201001170166Tee Fitting · corrodedLT WING OTBD FLAP VANE TEE FITTING (NR 2 FROM INBD) HOLE CORROSION. REPAIR CARRIED OUT IAW EA NR 1-5750-137545. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.SDR UALA2010011800208Skin · chafedLT WING IB FLAP OTBD SIDE CHAFING ON NR 5 SPOILER. MAJOR REPAIR ACCOMPLISHED: REPAIRED FLAP UPPER SKIN. ACP RII INSPECTION ON FLAP SKIN REPAIR.SDR AALA20100224TUL08Skin · damagedONE UPPER SKIN PANEL 666JT FASTENER HOLE ON THE RIGHT OUTBOARD LEADING EDGE FLAP WAS DAMAGED DURING MAINTENANCE. REPAIRED UNDER EA COMP-57-008495.SDR CA100127013Flap Track · out of limits(CAN) DURING AN INSP, 2 FLAP TRACKS FOR OTBD FLAP. INBD TRACK WERE FOUND OUT OF LIMITS AND WERE REPLACED.SDR CA100115004Rib · cracked(CAN) DURING DISASSEMBLY FOR REPAIR TO THE FLAP ATTACH BRACKET, NOSE RIBS PN 62328-00 AND 62328-01 WERE FOUND TO BE CRACKED AT THE FLAP HINGE BRACKET ATTACH POINT. THIS BRACKET ALSO FORMS THE ATTACHING POINT FOR THE FLAP CONTROL ROD. BOTH LT AND RT FLAPS WESDR AALA20100115TUL05Skin · dentedDENT IN UPPER SKIN OF TRAILING EDGE WEDGE 28.5 INCHES FROM INBOARD END. HOT BONDED DOUBLER OVER DAMAGED AREAS PER SRM 51-70-102R 4.SDR AALA20100115TUL04Skin · dentedDENT IN UPPER SKIN OF TRAILING EDGE WEDGE 13 INCHES FROM INBOARD END. HOT BONDED DOUBLER OVER DAMAGED AREAS PER SRM 51-70-102R 4.SDR IPXA10658233Panel · chippedINSPECTION TYPE:7C, LT WING INBD MAIN FLAP OTBD EDGE MID AREA CHIPPED. COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5H REV 45.SDR IPXA10658231Wedge · damagedINSPECTION TYPE: C RT WING OTBD T/E FLAP INBD T/E WEDGE CHIPPED COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5G, FIG 14, REV 45.SDR IPXA10158224Skin · gougedINSPECTION TYPE:4/C, SMALL GOUGE ON UPPER SURFACE OF RT WING MID FLAP AT 40 IN INBD OF OTBD EDGE REPAIRED SA IAW SRM 57-50-00 PARA 4.E, FIG. 205 REF. UPS RCD 385048.SDR USAA2010011990128Skin · debondedDISBOND ON INBOARD END OF RIGHT INBOARD AFT FLAP. REPLACED RIGHT INBOARD AFT FLAP IAW JOB CARD NR R3M27007.SDR FDEA201001140127Structure · crackedLT INBD MID-FLAP T/E LOWER CHORD CRACKED WBL106. REMOVED CRACKED ANGLES AT WBL 106 AND 146, FABRICATED NEW ANGLES AND INSTALLED AT WBL 106 AND 146 IAW SRM 51-30-2, 51-40-4, 51-10-2 AND 51-10-1.SDR FDEA201001130117Hinge Bracket · corrodedCORROSION - PIVOT INBD HOLE AT LT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE). REPAIR CARRIED OUT IAW EA NR 1-5750-137532. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.SDR FDEA201001130116Hinge Bracket · corrodedCORROSION - PIVOT OTBD HOLE AT LT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE). REPAIR CARRIED OUT IAW EA NR 1-5750-137532. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 109.SDR FDEA201001130107Hinge Bracket · damagedSCRATCH MARK - PIVOT INBD HOLE AT RT WING INBD FLAP OTBD AFT HINGE. (FLAP SIDE). REPAIR CARRIED OUT IAW EA NR 1-5750-137533. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.SDR FDEA201001130106Hinge Bracket · corrodedCORROSION - PIVOT OTBD HOLE AT RT WING INBD FLAP OTBD AFT HINGE. (FLAP SIDE) REPAIR CARRIED OUT IAW EA NR 1-5750-137533. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.SDR IXXA10SMN013SSupport Fitting · crackedDURING ROUTINE C CHECK INSP FOUND RT OTBD FLAP OTBD HINGE SUPPORT FITTING CRACKED AT STA XF 339.7332. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA. INSTALLED NEW FITTING IAW SB 27-249 REV 1 DATED 07/15/90, DWG 5894377, SB 27-249, SRM 51-1-21, SRM 51-SDR ASAA1047279Skin · chafedLEFT I/B MID FLAP T/E WEDGE AFT END CHAFED LOWER SURFACE. REPAIRED CHAFED DAMAGE.SDR ASAA1047278Skin · dentedLEFT I/B MID FLAP T/E WEDGE HAS CLUSTER OF SMALL DENTS ON LOWER SURFACE. REPAIRED LEFT I/B MID FLAP T/E WEDGE.SDR IPXA10658219Fitting · crackedINSP TYPE: C LT WING - INBD MAIN FLAP INBD AFT FLAP HINGE FTG FOUND CRACKED LT WING INBD MAIN FLAP INBD HINGE FTG REPAIRED IAW SRM 57-53-02-2R1 FIG201 REV45 ORG MATL IS 7075T73 FORGING, CRACK LENGTH IS 1.5" AT INBD FLANGE & 0.5" AT OTBD FLANGE. DAMAGED CUSDR IPXA10658189Skin · crackedLT WING NR 3 SLAT L/E INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT INBD AREA AT OSS724.4 NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201 REV 45 ORG MATL IS CLAD7075T6-0063" CRACK LENGTH IS 0.125" DAMAGED CUTOUT IS 9" X 7.125" THIS REPAIR IS CLSDR IPXA10658178Fairing · delaminatedINSPECTION TYPE: C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.SDR IPXA10658177Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP INBD L/E FAIRING DELAMINATION COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.
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