JASC 5753
Service difficulty reports · 31,513
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 REXA2014090900787Flap · chafedRIGHT INBD FLAP LE CHAFED UP TO 0.010 INCHES DEEP. REPAIRED IAW REO 601R-57-52-004.SDR SWAA2014090231449Flap · delaminatedLEFT WING OTBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW MM.SDR SWIA201439327Vane · chafedRT INBD FLAP VAN MIDDLE SECTION OF L/E IS CHAFED. R & R RT INBD FLAP VANE MIDDLE SECTION,. BLENDED CHAFE AND FOUND NOT IN LIMITS IAW REO. R & R THE FLAP VANE MIDDLE SECTION IAW SRM AND DWG.SDR ASOA2014090311176Fitting · wornLEFT OTBD FLAP ALIGNMENT FITTING, HAS WEAR DAMAGE DUE TO ROLLER FITTING ASSY CONTACT. AFTER ATTEMPT TO APPLY GREO 601R-57-51-143 REPAIRS, IT WAS FOUND THAT FURTHER EVALUATION OF DAMAGE IS REQUIRED. BLENDED OUT DAMAGE ON LT FLAP ALIGNMENT FITTING IAW REO 60SDR FDEA201408292357Skin · puncturedLEFT INBD MAIN FLAP TE HONEYCOMB TOP SKIN PUNCTURE REPAIR IAW SRM 57-53-01 & SRM 51-70-07.SDR DALA2017061604775Channel · damagedLEFT WING OTBD FLAP AFT HINGE FAIRING CHANNEL HAS AN ELONGATED HOLE, REPAIRED IAW ERA 525967-14, REV ORIGSDR TSAA20141015023Carriage · corrodedRIGHT OTBD FLAP OTBD SPINDLE BODY CORRODED. R & R RT OTBD FLAP, OTBD CARRIAGE IAW AMM 27-51-81.SDR FDEA201408282339Spar · chafedRIGHT WING REFER TO SNRM N00617, AFTER CARRIAGE SUPPORT REMOVAL, OTBD TE. MAIN FLAP FRONT SPAR WEB FOUND CHAFE MARK AT NR 8 CARRIAGE FWD SUPPORT FITTING MATING AREA. REPAIRED IAW EA F-550-T0312509. REPAIR CLASSIFIED AS MINOR.SDR UIEA2014082800407Carriage · damagedNUMBER 5 FLAP CARRIAGE FWD BOGIE, BOTH FWD LOWER ROLLERS CRACKED, SPLIT & DAMAGED & OTBD ROLLER ARM BENT. R & R NR 5 FLAP CARRIAGE FWD BOGIE IAW AMM 27-51-43. NO DEFECTS NOTED IN FLAP TRACK.SDR UIEA2014082800408Support · crackedNUMBER 1 TE FLAP CARRIAGE ASSEMBLY GENEVA TRACK IND SUPPORT ASSEMBLY IS CRACKED. REPLACED IAW AMM 20-51-01.SDR SWIA201439335Vane · chafedRIGHT INBD FLAP VANE L/E CHAFED ON OTBD SIDE. BLENDED FLAP VANE L/E OTBD SIDE IAW REO AND FOUND TO BE WITHIN LIMITS IAW REO.SDR SWIA201439334Vane · chafedLEFT INBD FLAP VANE L/E CHAFED ON INBD SIDE. BLENDED CHAFE IAW REO AND FOUND TO BE WITHIN LIMITS IAW REO.SDR SWIA201439333Vane · chafedLT INBD FLAP VANE L/E CHAFED ON CENTER SECTION. BLENDED IAW REO AND FOUND TO BE WITHIN LIMITS IAW REO.SDR SWAA2014091131841Skin · delaminatedLEFT WING INBD FORE FLAP DELAMINATED ON LOWER SKIN. REPAIRED FORE FLAP IAW SRM.SDR REXA2014082700865Cover · wornRIGHT INBD FLAP VANE INBD ACTUATOR END COVER HAS WEAR 684 ET. DRILLED NEW RT INBD FLAP VANE ACTUATOR END COVER 684 ET IAW SRM 57-52-01-101-001-A01 & 51-40-11-001-001-A01. PANEL 684 ET WILL BE INSTALLED ON OPERATIONS 192 PANEL.SDR FDEA201408272335Nut Plate · corrodedRIGHT WING OTBD FLAP STRESS PANEL NUTPLATE CORROSION IN SEVERAL PLACES. CORROSION REPAIRED IAW EA F-5750-T0310492.SDR USAA2014090200011Skin · delaminatedC3 CHECK DELAMINATION ON RT INBD FLAP UPPER SKIN AT APPROX 77 INCHES INBD FROM OTBD END & 5.75 INCHES FWD OF TE. REPAIRED RT INBD FLAP UPPER SKIN IAW SRM 51-70-10-2R-4.SDR FDEA201408272327Spar · corrodedRIGHT OTBD MAIN FLAP CORROSION ON FWD SPAR INTERNAL LOWER FLANGE. REPAIR IAW EA F-5750-T0310699.SDR FDEA201408272325Angle · corrodedLEFT OTBD FLAP CORROSION ON INTERNAL FRONT SPAR LOWER ANGLE CORROSION REMOVED IAW EA F-5750-T0310561.SDR REXA2014082600864Panel · wornLEFT WING INBD FLAP VANE UPPER PANEL 584 FT HAS WEAR. EVALUATED LT WING INBD FLAP VANE ACTUATOR PANEL 584 FT, FOUND TO BE OUT OF LIMITS IAW SRM 57-52-01-101-001-A01. RECEIVED NEW PANEL FROM STOCK DRILLED HOLES & PAINTED IAW SRM 51-40-11-001-001-A01 & IAW SRMSDR SWAA2014082831396Flap · delaminatedRIGHT WING OTBD AFT TE FLAP DELAMINATED. REPAIRED AFT FLAP IAW AMM.SDR SWAA2014090931749Flap · delaminatedLEFT WING INBD TE AFT FLAP DELAMINATED. R & R AFT FLAP IAW MM.SDR IPXA2014091084230Skin · chafedINSPECTION 3C, RT INBD FLAP UPPER SKIN REPAIR DOUBLER IS CHAFED BETWEEN RIB 11 AND RIB 14, STR 2.1-2.3 ACCOMPLISHED REPAIR ON RT INBD FLAP UPPER SKIN BETWEEN RIB 10 AND RIB 15 STR 2.1-2.3 IAW VT, EA 300-5753-01-A5574, REV A AND EO A300-5750-55467-B.SDR ASOA20140823263Fitting · crackedDURING C-CHECK THE RT OTBD FLAP INBD FLAP TRACK ROOT FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE FITTING IAW EC5750-01631. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20140823262Fitting · crackedDURING C-CHECK, THE LT OTBD FLAP INBD FLAP TRACK ROOT FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE FITTING IAW EC5750-01630. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR SWAA2014090831635Stiffener · crackedLEFT WING NR 3 FLAP TRACK FAIRING STIFFENER CRACKED. R & R STIFFENER IAW SRM & DWG.SDR IPXA201409084190Skin · chafedINSPECTION 3C, RT OTBD FLAP, INBD BULLNOSE SKIN IS CHAFED. ACCOMPLISHED REPAIR ON RT OTBD FLAP INBD BULLNOSE SKIN IAW SRM 57-50-00, FIG 208.SDR GR4D201408220001Flap Track · corrodedLT FLAP TRACK CORRODED, REPLACED FLAP TRACK.SDR SWAA2014092332234Flap · delaminatedLEFT WING OTBD FORE FLAP INBD TE CORNER DELAMINATED. REPAIRED FORE FLAP IAW WO.SDR FDEA201408202239Repair · debondedAGING INSPECTION EXISTING REPAIR ON RT WING INBD FLAP TE RIB 5 - 7 LOWER SURFACE, REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR PATCH DISBONDED REMOVED OLD REPAIR PATCH & DAMAGE CORE IT EXCEEDED THE REPAIRABLE LIMIT PER A310SRM57-52-12 FIG 204 REPORTED TO ENSDR FDEA201408202238Repair · debondedAGING INSPECTION EXISTING REPAIR ON RT WING INBD FLAP TE RIB 3 - 5 LOWER SURFACE, REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED AND FOUND THE OLD REPAIR PATCH DISBONDED. REMOVED OLD REPAIR PATCH & DAMAGE CORE REPORTED TO ENGINEER. REPAIRED TSDR A6WA201441912Vane · chafedRIGHT INBD FLAP VANE LE HAS CHAFES.SDR A6WA201441911Vane · chafedLEFT INBD FLAP MOVEABLE VANE LE HAS CHAFE MARKS.SDR IPXA2014090384141Vane · chafedINSPECTION 3C, CHAFE DAMAGE ON RT INBD FLAP VANE UPPER SURFACE STA XIFH137. REPAIRED RT INBD FLAP VANE IAW SRM 57-50-80, REPAIR 2, PARA 2, WET LAY-UP.SDR DALA2014081804687Structure · crackedDURING MAINTENANCE, FOUND OTBD BUTTE DOOR ON LT INBD FLAP CRACKED. DAMAGE WAS REMOVED IAW SRM 57-01, FIG 5 DOUBLERS AND FILLER WERE FABRICATED IAW SRM 57-01, FIG 5 AND DWG 5936802, REV D. REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3 PAR 14 AND 21. SDR R61A201408160991Torque Tube · corrodedDURING HEAVY CHECK, LT FLAP TORQUE TUBE F-5 HAS CORRODED AND WORN SPLINES. MX R & R LT FLAP TORQUE TUBE IAW AMM 27-51-03.SDR R61A201408160990Torque Tube · corrodedDURING HEAVY CHECK, LT FLAP TORQUE TUBE F-6 HAS CORRODED AND WORN SPLINES. MX R & R LT FLAP TORQUE TUBE IAW AMM 27-51-03.SDR R61A201408160989Bearing Support · corrodedDURING HEAVY CHECK, LT FLAP TORQUE TUBE BEARING SUPPORT BETWEEN F-5 AND F-6 TORQUE TUBES IS PITTED AND CORRODED. MX RT & R LT FLAP TORQUE TUBE BEARING SUPPORT BETWEEN F-5 AND F-6 TORQUE TUBES IAW AMM 27-51-04, PN 1702961 BEARING SUPPORT.SDR A6WA201441870Skin · chafedLEFT INBD FLAP VANE SKIN LE IS CHAFED IN 3 LOCATIONS FROM STOPS.SDR ASAA2014081409107Structure · chafedAFT OF FIXED FAIRING BETWEEN INBD AND OTBD FLAP CHAFED IN THE INBD. ACFT GROUNDED. BLENDED AREA FOUND TO BE OUT OF LIMITS ACCOMPLISHED REPAIR IAW EA 57EA 13370 TO NR 3 IF O/T FAIRING.SDR FDEA201408142167Hinge · damagedRIGHT WING INBD FLAP ASSEMBLY OTBD HINGE FOUND SURFACE DAMAGED. SURFACE DAMAGED AT RIGHT HAND WING - INBOARD FLAP ASSEMBLY OUTBOARD HINGE REWORKED PER MD10 SRM 57-20-00 VOLUME I REVISION 101. MATERIAL REMOVED: LENGTH 0.650 INCH X WIDTH 0.090 INCH X DEPTH 0.0SDR FDEA201408142162Skin · bulgedLEFT INBD FLAP HAS SKIN BULGE AT UPPER CTR TE. REPAIRED LT INBD FLAP IAW SRM 57-20-00 FIG 13. CURRENTLY BEING TRACKED ON EA 8-5710-T0310431. FABRICATED FILLER 2024-T3 BATCH 2550453 & DOUBLER 2024-T3 BATCH 264264. INSTALLED AT UPPER SKIN 177.300 TO 189.300.SDR ASAA2014081309106Skin · chafedRIGHT INBD MIDFLAP CHAFED ON INBD UPPER EDGE. ACFT GROUNDED. DAMAGE FOUND TO BE OUT OF LIMITS, R & R RT INBD MID FLAP UPPER AFT SKIN PANEL IAW SRM 51-40-02-0G-0.SDR ASAA2014081309088Skin · chafedMID FLAP ON LT WING INBD PHNOLIC STRIP TORN, METAL SKIN CHAFED. ACFT GROUNDED. REPLACED 3 RUBSTRIPS AND REPAIRED MIDFLAP LT WING OTBD FLAP SLIP IAW SRM 51-70-10-2R-4 TYPE EA 57-50-01185, REV C.SDR DALA2014081404558Skin · wornWORN SKIN ON INBD BUTTE DOOR OF LT INBD FLAP. SKIN REPLACED IAW SRM 57-01, FIG 3 51-10-3, PAR 14 AND 21 51-30-1, 51-30-2.SDR DALA2014081404557Structure · wornWORN REPAIR ON INBD EDGE OF LT INBD BUTTE DOOR AT OTBD FLAP. DOUBLER REPLACED IAW SRM 57-01, FIG 3, SRM 51-30-2, 51-30-1, SRM 51-10-3 PAR 14 AND 21.SDR SWAA2014081530907Flap · delaminatedLEFT WING INBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.SDR ASAA2014081208898Skin · chafedLEFT INBD MID FLAP IS CHAFED AT INBD UPPER EDGE. ACFT GROUNDED. REPAIRED LT INBD MID FLAP INBD UPPER SKIN IAW SRM 57-53-01-2R-3.SDR DALA2014081304568Bearing · corrodedDURING INSPECTION, FOUND CORROSION ON BEARING AT LT WING INBD FLAP. REPLACED BEARING IAW CMM 57-52-21-410-011-A01. .SDR SWAA2014091131829Skin · delaminatedRIGHT WING OTBD LOWER SURFACE INBD END OF OTBD AFT FLAP DELAMINATED. REPAIRED AFT FLAP IAW SRM.
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