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 USAA2009091192478Carriage · corrodedSAL - Q6 - MAJOR REPAIR - CORROSION ON FORWARD BEARING BORE OF NR 6 MID FLAP CARRIAGE INBOARD HALF. REPLACED NR 6 MID FLAP CARRIAGE INBOARD HALF IAW B737 AMM 27-51-14.SDR USAA2009091192477Carriage · corrodedSAL - Q6 - MAJOR REPAIR - CORROSION ON FORWARD BEARING BORE OF NR 6 MID FLAP CARRIAGE OUTBOARD HALF. REPLACED NR 6 MID FLAP CARRIAGE OUTBOARD HALF IAW B737 AMM 27-51-14.SDR FDEA200907312857Hinge Bracket · corrodedLT WING - FLAP SIDE INBD FLAP OTBD HINGE OTBD PIVOT HOLE FOUND CORROSIONS. HINGE REWORKED AS PER EA 1-5750-132166. BUSHING FABRICATED AS PER MD-11 CMM 57-52-03 REV. 64. AND INSTALLED AS PER EA 1-5750-132166. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 RESDR UIEA200900046Skin · puncturedRT WING INBD FLAP HAS 0.500 INCH DIAMETER PUNCTURED HOLE AT LWR SURFACE, WBL 188.30 AND 4.0 INCHES FROM L/E. PERMANENT REPAIR ACCOMPLISHED IAW SRM 51-40-09 FIG. 5, SHEETS 4 AND 8, 250* F CURE IAW SRM 51-40-12. REF: EO 4757A485.SDR ASAA0976314Skin · delaminatedLEFT O/B FORE FLAP TRAILING EDGE UPPER SKIN IS DELAMINATED AT 60.5 INCHES FROM I/B AND 3 FROM AFT. REPAIRED SKIN.SDR ASAA0976313Skin · delaminatedLEFT O/B FORE FLAP TRAILING EDGE UPPER SKIN IS DELAMINATED AT 97 INCHES FROM I/B AND 4.5 FROM AFT. REPAIRED SKIN.SDR FDEA200907312848Skin · dentedRIGHT WING INBD FLAP LWR SURFACE FOUND DENT LOCATED 8 INCHES FROM OTBD EDGE AND 22 INCHES FROM L/E. REPAIRED AS PER SRM 57-10-00 REV. 41. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.SDR SWAA094911Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA094881Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0946307Wedge · chafedRIGHT I/B MID FLAP TRAILING EDGE WEDGE I/B CONTROL ROD CUTOUT IS CHAFED. REPAIRED IAW EA.SDR ASAA0946306Wedge · chafedRIGHT I/B MID FLAP TRAILING EDGE WEDGE O/B CONTROL ROD CUTOUT IS CHAFED. REPAIRED IAW SRM.SDR SWAA094866Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR IPXA09M57063Doubler · gougedINSPECTION TYPE:1C REPAIR SURVEY SEQ 296-W4-13 RT WING INBOARD FLAP UPPER L/E BETWEEN STA X IFH217.399-225.140 EXISTING PREVIOUS DOUBLER GOUGED. REMOVED EXISTING REPAIR (REPAIR SURVEY SEQ 296-W4-13) AT RT WING INBOARD FLAP UPPER L/E BETWEEN XIFH 216.3-XIFH 21SDR IPXA09557022Skin · gougedINSPECTION TYPE:C1 LEFT WING O/B MAIN FLAP GOUGED IN PREVIOUS REPAIR, UPPER SKIN. REPAIRED MAIN FLAP IAW ER 09-3931.SDR UALA2009072802248Flap Track · damagedRT WING INBD FLAP OTBD FLAP TRACK ASSY STRUT ASSY HAS DEEP CUTS. REMOVED AND REPLACED THE RT I/B FLAP, O/B FLAP TRACK SUPPORT ASSY STRUT.SDR ASAA0946268Skin · chafedRIGHT OB AFT FLAP LEADING EDGE SKIN IS CHAFED JUST IB OF NR 1 RT OB AFT FLAP REPLACED WITH SERVICEABLE UNIT.SDR FDEA200907282812Skin · canningLEFT WING - INBD FLAP UPPER SURFACE FWD INBD SECTION FOUND OIL CANNING.SDR SWAA094898Skin · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING O/B AFT FLAP LOWER SURFACE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA094856Flap · puncturedDURING SCHEDULED MV2 CHECK, FOUND LT WING O/B FORE FLAP PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.SDR FDEA200907272762Vane · corrodedLT WING OTBD FLAP VANE NR 4 FROM INBD TRACK TEE FITTING ATTACH HOUSING FOUND CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-32-4 REVISION 64. ADJUSTMENT AND TEST OF THE LT OUTBOARD FLAP VANE REFER TO WORK CARD E1-5750-7-5002 E2 PART 1.SDR FDEA200907272761Vane · corrodedRT WING OTBD FLAP VANE NR 4 FROM INBD TRACK TEE FITTING ATTACH HOUSING, FOUND CORROSION. REMOVED AND REPLACED AS PER AMM 27-50-32-4 REVISION 64. ADJUSTMENT AND TEST OF THE RT OUTBOARD FLAP VANE REFER TO WORK CARD E1-5750-7-5002 E2 PART 2.SDR ASAA0946328Skin · dentedRIGHT INBOARD AFT FLAP OUTBOARD CORNER DAMAGED. REMOVED DAMAGED AREA, FABBED REPLACEMENT PARTS AND BONDED THE REPAIR.SDR SWAA094819Flap · delaminatedDURING SCHEDULED 6Y CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA094793Wedge · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RT WING O/B AFT FLAP T/E WEDGE DELAMINATED. REPAIRED WEDGE EPR SRM.SDR SWAA094792Flap · delaminatedDURING SCHEDULED 18Y CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWIA200922684Rod · corrodedLEFT INBOARD FLAP LOWER INTERCONNECT ROD TO WING REAR SPAR CORRODED. (C-CHECK) REPLACED LEFT I/B FLAP LOWER INTERCONNECT ROD TO WING REAR SPAR.SDR MALA090104Skin · corrodedNOTED 20 SPOTS OF CORROSION UNDER WEAR STRIP NR 9 ON LT FLAP UPPER SKIN PANEL 541AT. REPAIRED IAW EO S57263.SDR FDEA200907252753Angle · crackedRT WING INBD MID-FLAP, LOWER CHORD ANGLE IS CRACKED BELOW INBD MECHANISM, WBL 90. OPENED INBD MIDFLAP INNER PANEL IAW SRM 51-30-2. CUT OUT DAMAGED SECTION DIM 47" IAW SRM 51-10-1 AND 51-40-4 FABRICATED CHORD SECTION FROM BAC1503-100046, PO NR 9008728 DISDR FDEA200907252752Structure · crackedLT IB MIDFLAP LWR AFT CHORD IS CRACKED 4 PL. ON IB CARRIAGE TRACK CUT OUT AND IB ACT ROD CUT OUT. REMOVED INNER SKIN AND TEARDROP FAIRING IAW SRM 51-30-2. REMOVED PREVIOUS REPAIR SECTION DIM 48" IAW SRM 51-30-2, FABRICATED NEW ANGLE FROM BAC 1503 - 100046 SDR A6WA200940447Abrasion Strip · contaminatedACFT ROLLS TO RIGHT WHEN FLAPS ARE EXTENDED TO 45 DEG. REQ`D JUST UNDER 50 PERCENT STRAIGHT/LEVEL FLT ON APPROACH. REMOVED PAINT AND PAINTED FLAPS LEADING EDGE TEFLON ABRASION STRIP IAW SRM 51-25-26 AND REO 601R-51-25-002. OPS CK OF FLAPS GOOD. (K)SDR USAA2009072791912Carriage · corrodedPHL - RON - MAJOR REPAIR - CORROSION FOUND ON FORWARD END OF LEFT WING OUTBOARD FLAP SPINDLE ON FRONT OF TIE AT WBL 355 AND BROKEN BOLT HEAD ON TOP OF SAME CARRIAGE ASSEMBLY INBOARD SIDE. REPLACED LEFT OUTBOARD FLAP CARRIAGE IAW B737 AMM 27-51-34-825-001.SDR SWAA094760Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA094735Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR FDEA200907232714Hinge Fitting · damagedSCRATCH MARK, LT WING INBD FLAP AFT OUTBD HINGE INBD PIVOT BORE. REWORKED AS PER E.A. 1-5750-132705, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200907232713Hinge Fitting · corrodedCORROSION RT WING INBD FLAP AFT OUTBD HINGE OUTBD PIVOT SPOT FACE. REWORKED AS PER E.A. NO. 1-5750-132706, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200907232712Hinge Bracket · damagedRIGHT HAND WING INBOARD FLAP AFT OUTBOARD HINGE OUTBOARD PIVOT BORE FOUND CORROSION. RIGHT WING INBOARD FLAP AFT OUTBOARD HINGE OUTBOARD PIVOT BORE REWORKED AS PER EA 1-5750-132706, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.SDR FDEA200907232711Hinge Bracket · damagedUNABLE TO CARRY OUT HFEC INSPECTION ON INBD PIVOT HOLE AT RT WING INBD FLAP OUTBD HINGE (FLAP SIDE) DUE TO HOLE CORROSION. REWORKED AS PER E.A. NO. 1-5750-132706, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 107.SDR CA090723009Stud · broken(CAN) FLAP MOTOR MOUNTING STUD SHEARED.SDR IPXA09656876Fairing · delaminatedINSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 44. THIS CLASSIFIED AS MAJOR REPAIR WITH REPAIR MATERIAL RESIN EY3804PT AND GLASSFIBER BMS9-3TYH3CSDR SWAA094822Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING O/B AFT FLAP T/E DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA094758Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING O/B TRAILING EDGE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA094690Flap · puncturedDURING SCHEDULED MV2 CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.SDR FDEA200907222705Hinge Fitting · chafedRIGHT HAND WING INBOARD FLAP OUTBOARD HINGE INBOARD FACE AFT OF ACTUATOR MOUNT HOLE FOUND WITH CHAFING MARK. COMPLIED WITH E.A. 1-5750-132126, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 107.SDR FDEA200907222704Hinge Fitting · chafedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) INBOARD FACE, AROUND AFT ATTACHMENT FITTING FOUND WITH CHAFING MARK. REPAIR CARRIED OUT AS PER E.A. 1-5750-132125, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR FDEA200907222703Hinge Fitting · chafedLEFT HAND WING INBOARD FLAP OUTBOARD HINGE (FLAP SIDE) INBOARD FACE, AFT OF ACTUATOR MOUNT FITTING FOUND WITH CHAFING MARK. REPAIR CARRIED OUT AS PER E.A. 1-5750-132125, THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 107.SDR ASAA0946330Rib · crackedRIGHT INBOARD MID FLAP INBOARD AFT RIB CRACKED. REMOVED DAMAGED RIB, INSTALLED NEW RIB.SDR ASAA0946329Plate · crackedRIGHT INBOARD MID FLAP ELEPHANT EAR MOUNT PLATE CRACKED AT LOWER AFT BOLT HOLE. REMOVED DAMAGED PART, INSTALLED NEW PART.SDR IPXA09656858Fairing · delaminatedINSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 44. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL RESIN EY3804PT AND GLASS FIBER BMS 9-3TYHSDR SWAA094804Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING O/B TRAILING EDGE FLAP I/B END DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0946224Skin · dentedRIGHT I/B AFT FLAP LOWER SURFACE DENTED AT WBL 116. PREPPED DAMAGED AREA, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER.
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