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 SWAA053339Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RIGHT WING T/E OUTBOARD AFT FLAP DELAMINATED AT INBOARD END. REMOVED AND REPLACED FLAP ASSY PER MM.SDR QXEA200501495Beam · corrodedPDX - LEFT NR 4 FLAP BEAM HAS SURFACE RUST AND LIGHT PITTING OVER ENTIRE LENGTH OF INBOARD SURFACE "E". REPAIRED IAW RD 8/57/988.SDR QXEA200501494Beam · corrodedPDX - LEFT NR 4 FLAP BEAM HAS SURFACE RUST AND LIGHT PITS OVER ENTIRE LENGTH OF OUTBOARD SURFACE "E". REPAIRED IAW RD 8/57/988.SDR QXEA200501493Beam · corrodedPDX - LEFT NR 4 FLAP BEAM HAS TWO PITS THROUGH PITTING IN SURFACE C OUTBOARD, AT O POSITION AND 4" AFT OF O. REPAIRED IAW RD 8-57-988.SDR QXEA200501492Beam · corrodedPDX - LEFT NR 4 FLAP BEAM HAS TWO PITS THROUGH PLATING ON SURFACE OUTBOARD, AT O POSITION AND 4" AFT OF O. REPAIRED IAW RD 8/57-988.SDR SWAA053302Skin · delaminatedDURING SCHEDULED RON, FOUND RT INBD T/E AFT FLAP DELAMINATED. REPAIRED FLAP PER SWA EA.SDR QXEA200501375Failsafe · damagedLT INBOARD FLAP AFT FAIL SAFE CATCHER FOR THE INBOARD AFT ROLLER HAS CRACKED AND JAMMED AGAINST THE ROLLER. MAINTENANCE REPAIRED IAW HORIZON EA 6-27-117 AND MOD SUM IS4Q-2700001, STEPS 4-9.SDR QXEA200501374Failsafe · wornPDX: LT INBOARD FLAP AFT FAIL SAFE CATCHER FOR THE OUTBOARD AFT ROLLER HAS HEAVY WEAR, REF AMM 27-54-01 PG 427, ITEM 26. MAINTENANCE REPAIRED IAW HORIZON EA 6-27-177 AND MOD SUM IS4Q-2700001 STEPS 4-9.SDR AWXA200501395Carriage · corrodedMCN - DURING C18 CHECK DISCOVERED CORROSION ON THE RT INBOARD MID-FLAP, INBOARD CARRIAGE, INBOARD AND OUTBOARD FORE FLAP SEQUENCE CARRIAGE TRACKS. NO CORROSION REMOVAL LIMITS ARE AVAILABLE. MAINTENANCE REMOVED AND REPLACED THE RT INBOARD MID-FLAP, INBOARD CASDR AWXA200501394Carriage · corrodedMCN - DURING C18 CHECK DISCOVERED CORROSION ON THE LT INBOARD MID-FLAP, OUTBOARD CARRIAGE, OUTBOARD FORE FLAP SEQUENCE CARRIAGE TRACK. NO CORROSION REMOVAL LIMITS ARE AVAILABLE. MAINTENANCE REMOVED AND REPLACED THE LT INBOARD MID-FLAP, OUTBOARD CARRIAGE, OUTSDR AWXA200501326Cam · corrodedMCN - DURING C18 CHECK DISCOVERED CORROSION ON THE RT INBOARD MID FLAP, OUTBOARD CARRIAGE, INBOARD FORE FLAP SEQUENCE CAM TRACK. MAINTENANCE REMOVED AND REPLACED THE RT INBOARD MID FLAP, OUTBOARD CARRIAGE, INBOARD FORE FLAP SEQUENCE CAM TRACK IAW BOEING SOPM SDR AWXA200501267Track · corrodedMCN - DURING C18 DISCOVERED CORROSION ON THE LT AND RT INBOARD MIDFLAP, INBOARD AND OUTBOARD CARRIAGE, INBOARD FORE FLAP SEQUENCE CAM TRACK AT WBL 71L AND 71R. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CAM TRACK. MAINTENANCE REMOVED CAM TRACKS AND INSTALSDR AWXA200501266Track · corrodedDURING C18 DISCOVERED CORROSION ON THE LT INBOARD MIDFLAP, OUTBOARD CARRIAGE, INBOARD FORE FLAP SEQUENCE CAM TRACK AT WBL 185. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CAM TRACK. MAINTENANCE REMOVED CAM TRACK AND INSTALLED NEW CAM TRACK ON THE LT INBOARSDR AWXA200501280Track · corrodedMCN - MAJOR REPAIR - DURING C16, DISCOVERED CORROSION ON THE RT INBOARD FLAP, INBOARD CAM TRACK AT WBL 71.00R. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CAM TRACK. MAINTENANCE REMOVED CAM TRACK AND INSTALLED NEW CAM TRACK ON THE RT INBOARD FLAP, INBOARD SDR AWXA200501279Track · corrodedMCN - MAJOR REPAIR - DURING C16 DISCOVERED CORROSION ON THE RT INBOARD FLAP, OUTBOARD CAM TRACK AT WBL 185.00R. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CAM TRACK. MAINTENANCE REMOVED CAM TRACK AND INSTALLED NEW CAM TRACK ON THE RT INBOARD FLAP, OUTBOARSDR AWXA200501278Track · corrodedMCN - MAJOR REPAIR - DURING C16, DISCOVERED CORROSION ON THE LT INBOARD FLAP, INBOARD CAM TRACK AT WBL 71.00L. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CAM TRACK. MAINTENANCE REMOVED CAM TRACK AND INSTALLED NEW CAM TRACK ON THE LT INBOARD FLAP, INBOARD SDR AWXA200501277Track · corrodedMCN - MAJOR REPAIR - DURING C16 DISCOVERED CORROSION ON THE LT INBOARD FLAP, OUTBOARD CAM TRACK AT WBL 185L. NO CORROSION REMOVAL LIMITS ARE AVAILABLE FOR CAM TRACK. MAINTENANCE REMOVED CAM TRACK AND INSTALLED NEW CAM TRACK ON THE LT INBOARD FLAP, OUTBOARD TSDR MWEA050116Flap Track · corrodedRIGHT HAND WING MOST INBOARD FLAP TRACK HAS PITTING ON UPPER AND LOWER SURFACE WHERE ROLLERS RIDE. REMOVED AND REPLACED FLAP TRACK.SDR LR7A05147Cap · corrodedDURING C-6 CHECK PER HC5711, FOUND RIGHT HAND INBOARD FLAP CENTER LOWER SPAR CAP CORROSION, 7-05-074, NR 0407.SDR LR7A05146Cap · corrodedDURING C-6 CHECK PER HC5711, FOUND RIGHT HAND OUTBOARD FLAP CENTER LOWER SPAR CAP CORROSION. REPAIRED IAW DRAWING R05-025-03 PER LAC MEA382-57-05-073. NR 0404.SDR UPS05M45623Web · crackedFOUND 6 INCH CRACK OF INBD LT FLAP OUTBD CLOSURE WEB. IAW EO MD11-5750-23071-A CUT OUT DAMAGE AREA. ACCOMPLISHED EFEC, NO CRACKS FOUND. INSTALLED REPAIR DOUBLER PER EO MD11-5350-23071-A CONSIDERED PERMANENT REPAIR PER EO REPEAT INSP REQ'D EVERY C CK. EVERY C SDR QXEA200501398Guide · chafedYYC - LEFT WING AFT SHROUD AREA AT STA 169, ON O/B FLAP ROLLER GUIDE FITTING CHAFED BY FLAP ROLLER FITTING. MAINTENANCE REPAIRED IAW REO 670-57-51-036, CRJ-700 NDTM PT 1, 51-20-006, SRM TASK 51-24-11-001-001-A01 AND FIELD P.S.18.0, CRJ 700/900 SRM 51-21-16, ASDR DHL2005365500Rib · crackedDURING ACCOMPLISHMENT OF EA57530001-001-A WHILE AT AVBORNE HEAVY MAINTENANCE INC LEFT INBOARD FLAP RIB NR 7 (FITTING} OUTBOARD SIDE FOUND CRACKED. REMOVED AND REPLACED NR 7 RIB IAW S/B A300-57-0242 REF ASTAR NON ROUTINE 034345.SDR ASAA0540544Skin · damagedOKC - FOUND RIGHT OUTBOARD AFT FLAP IS DAMAGED. REMOVED DAMAGE, FABRICATED AND INSTALLED CORE AND DOUBLER PER B737-200 SRM 51-70-10. (M)SDR ASAA0540543Skin · puncturedOKC - FOUND DURING RIGHT WING INBOARD MID FLAP T/E PANEL LOWER SKIN IS PUNCTURED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PIECES PER B737-200 SRM 51-70-10. (M)SDR IXXA05SMN244SVane · damagedDURING C CHECK INSPECT, RT WING INNER L/E SLOT VANE HAS ELONGATED HOLES AT STA XOLDO 67.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05463. REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPM PARSDR IXXA05SMN243SVane · elongatedDURING ROUTINE C CHECK INSPECTION, RT WING CTR L/E SLOT VANE HAS ELONGATED HOLES AT STA XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 05461 DATED 10-10-05, SEMAN DWG NR ED-4081 DATED 10-08-05, EO SEMAN NR 20051290 DATED 10-10-05. REMOVED FASTENERSSDR 05FDEA03431Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP OUTBOARD HINGE FITTING OUTBOARD NR 3 BOLT HOLE FROM FORWARD FOUND CORROSION. REPAIR ACCOMPLISHED PER EA 1-5750-93248.SDR 05FDEA03430Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP INBOARD HINGE FITTING INBOARD NR 2 BOLT HOLE FROM FORWARD FOUND CORROSION. REPAIR ACCOMPLISHED PER EA 1-5750-93247.SDR 05FDEA03429Hinge Fitting · corrodedLEFT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD NR 3 BOLT HOLE FROM FORWARD FOUND CORROSION. REPAIR ACCOMPLISHED PER EA 1-5750-93247.SDR 05FDEA03428Hinge Fitting · corrodedLT WING OUTBOARD FLAP INBOARD HINGE FITTING OUTBOARD NR 1 BOLT HOLE FROM FORWARD FOUND CORROSION. REPAIR ACCOMPLISHED PER EA 1-5750-93247.SDR 05FDEA03400Skin · chafedLEFT WING TRAILING EDGE SUBSTRUCTURE LOWER SURFACE 7 EA RIVET HEADS CHAFING INTO UPPER SURFACE, INTO THE O/B FLAP (LOCATED BETWEEN SPOILER 3 AND 4) DAMAGE ON SUBSTRUCTURE AND ON FLAP. COMPLIED WITH EA 6-5750-93356 REF N00077.SDR USAA051198Wedge · delaminatedRIGHT WING O/B AFT FLAP BEHIND NR 8 FLAP TRACK DELAMINATED. INJECTED WEDGE SPLIT WITH TWO PART ADHESIVE IN DISBOND. NO FURTHER ACTION REQUIRED IAW SRM 57-53-01, DEFECT SIZE 3 X 5 INCHES.SDR SWAA053135Skin · delaminatedDURING SCHEDULED RON CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA053126Skin · delaminatedDURING SCHEDULED C1 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA053133Skin · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING INBOARD T/E FOREFLAP DELAMINATED. REMOVED AND REPLACED FOREFLAP PER MM.SDR SCNA05007Bolt · shearedON POST FLIGHT WALKAROUND, MAINTENANCE FOUND LT INBOARD AFT FLAP DROOPING WITH FLAPS RETRACTED. AFT FLAP ASSY BOLTS WERE SHEARED. MAINTENANCE REPLACED LT INBOARD AFT FLAP LINKAGE MOUNT BOLTS WITH BOLTS, WASHERS & NUTS.SDR 05FDEA03331Rib · crackedR/W I/B MID FLAP TE RIB IS CRACKED AT IB AFT FLAP PUSHROD CUT OUT. REMOVED CRACKED SECTION & INSTALLED NEW SECTION IAW SRM 51-40-4.SDR AWXA200501273Skin · debondedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND ARE ON THE UPPER SURFACE OF THE RT OUTBOARD FORE FLAP, 92" FROM INBOARD END AT WBL 293.69L TO WBL 299.69L. MAINTENANCE CUT OUT AND REMOVED DAMAGE AREA IAW BOEING 737-300 SRM 51-70-10-2R3. FABRICATED RESDR AWXA200501254Wedge · debondedMCN - MAJOR REPAIR - DURING C16 DISCOVERED AREA OF DEBOND ON UPPER AND LOWER SURFACES OF THE LT INBOARD AFT FLAP, 37 INCHES FROM INBOARD END FROM WBL 110.00 TO WBL 114.00. MAINTENANCE REMOVED DAMAGED SKIN AND CORE IAW BOEING 737-300 SRM 51-700-10-2R4. FABRICSDR AWXA200501251Skin · debondedMCN - DURING C16 CHECK DISCOVERED DISBOND AREA AT AFT EDGE OF LT OUTBOARD FORE FLAP, 72-76 INCHES FROM INBOARD END. MAINTENANCE REMOVED DISBOND AREA ON THE LT OUTBOARD FOREFLAP IAW BOEING 737-300 SRM 51-70-10-2R. FABRICATED FILLER AND DOUBLER IAW BOEING 737-SDR 05FDEA03310Skin · chafedLT WING CENTER FLAP UPPER SKIN HAD 4 SMALL CHAFED AREAS. INSTALLED REPAIR DOUBLER PER EA NR 6-5750-92547.SDR EIA2005234Tie Rod · crackedLHW NR 4 FLAP TRACK TIE ROD UPPER MOUNT FTG FLANGE CRACKED. REPAIRED DEFECTIVE CHORD PER SRM 51-40-04, FIG 3.SDR EIA2005228Tie Rod · crackedLHW NR 4 FLAP TRACK TIE ROD UPPER MOUNT FTG FLANGE CRACKED. REPAIRED DEFECTIVE CHORD PER SRM 51-40-04, FIG 3.SDR USAA051187Wedge · wornFOUND LEFT HAND INBOARD MID FLAP INBOARD END WORN. REMOVED DAMAGED FLAP WEDGE AND REINSTALLED NEW WEDGE IAW BOEING DWG 65-46486U155, FLAP WEDGE WORN DUE TO CONTACT WITH THE CONTROL ROD. DAMAGE MEASURES .5" BY 2.75".SDR MWEA050110Skin · crackedLEFT OUTBOARD FLAP AT STATION 262, UPPER SKIN IS CRACKED. FABRICATED AND INSTALLED DOULBER.SDR SWAA053074Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA053072Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND RT WING OTBD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR 05FDEA03249Flap Track · corrodedLEFT WING FLAP TRACK NR 1 FWD ATTACH POINT INSIDE HAS CORROSION. REMOVED AND REPLACED NR 1 FLAP TRACK IAW MM 27-51-031-4.SDR CA051011007Skin · crackedSEVERAL CRACKS IN SKIN THROUGH RIVET HOLES IN TRAILING EDGE. THIS SKIN IS IN THE FLAP BAY. SUSPECT FAILURE IS DUE TO FLEXING OF TRAILING EDGE, CAUSED BY TURBULENCE IN SLOW FLIGHT WITH FLAPS LOWERED. AIRCRAFT IS USED SOLELY FOR FLIGHT TRAINING.
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