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 SWAA2015070841593Flap Track · crackedRIGHT WING NR 6 FLAP TRACK AFT FAIRING TAIL CONE AFT END CRACKED. REPAIRED FLAP TRACK IAW SRM & EA.SDR SWAA2015052039876Roller · corrodedRIGHT WING BELOW FLAP CTR MOVABLE VANE INBD TRACK ROLLER ON TRACK CORRODED, R & R ROLLER IAW SRM.SDR IPXA2015051989228Structure · crackedINSPECTION TYPE:C, 10 CRACK AND DISBOND ON THE LT WING OTBD FLAP L/E AT OTEF STA 61.98 - 75.23. REPAIR IAW SRM 57-53-01-2R-1, REPAIR 1, FIG 201, REV:62.00 & 767-300F, SRM 51-70-05-0G-0-GENERAL FIG REV:62.00.SDR SWAA2015051839750Flap · delaminatedRIGHT WING OTBD AFT FLAP INBD AFT END DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR SWAA2015051839749Flap · delaminatedLEFT WING OTBD AFT FLAP INBD AFT END DELAMINATED. REPAIRED AFT FLAP IAW SRM.SDR SWAA2015051139526Flap · delaminatedLEFT WING INBD AFT FLAP DELAMINATED ON INBD END. R & R AFT FLAP IAW AMM.SDR FXGA201505071520Skin · wornLOWER FLAP SKIN WORN AT WS 250R. TO REPAIR WORN SKIN AT 250R AT CTR SPAR ATTACH FASTENERS. REMOVE DAMAGE & REPAIR IAW OVERHAUL MANUAL FIG 1347.SDR SWIA201541212Panel · chafedRT WING INBD FLAP PANEL 684 GB IS CHAFED. REPLACED, LOCATED AND DRILLED NEW PANEL 684GB IAW SRM.SDR FDEA201505061393Fairing · delaminatedLEFT OTBD FLAP, INBD HINGE FAIRING PANEL 535AR DISBONDED AT FWD EDGE. REPAIRED LT OTBD FLAP, INBD HINGE FAIRING PANEL 535AR AT FWD EDGE IAW SRM 51-71-00 VOL 2.SDR DALA2015050403048Skin · dentedLEFT WING INBD T/E FLAP AFT FLAP FOUND 15 EA DENT. ALL THE DENT IS WITHIN LIMIT IAW SRM 57-53-01, FIG 101. HFEC INSPECTION CARRIED OUT IAW NDTM D634T301, REV 109, PART 6. 51-00-19 ON DENT AREA, 15 EA AND FOUND NO CRACK EVIDENT. DENT AREA PROTECTED IAW SRM 5SDR IPXA2015052289338Skin · corrodedINSPECTION TYPE:3C, RT INBD FLAP HAS CORROSION ON UPPER SKIN AT RUBSTRIP FS XIFH 133.900 TO XIFH 140.600. REPAIRED THE FLAP UPPER SKIN IAW EA 011-5753-01-A5812, REV I/R AND EO MD11-5750-57528-A.SDR IPXA2015052089295Hinge · corrodedINSPECTION TYPE:3C, RT OTBD FLAP INBD HINGE FITTING CORRODED. REPAIRED HINGE FITTING IAW VTSAA EA 011-5753-01-A5817, REV IR AND EO MD11-5710-57513-A.SDR SWAA2015051439662Skin · delaminatedRIGHT WING INBD FORE FLAP DELAMINATED AT 36.5" INBD OF OTBD EDGE ON UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.SDR SWAA2015051439661Skin · delaminatedRIGHT WING INBD FORE FLAP DELAMINATED 43.5" INBD OF OTBD EDGE ON UPPER SURFACE. REPAIRED FORE FLAP IAW SRM.SDR A6WA201542731Skin · chafedLEFT INBD FLAP VANE LE CHAFED.SDR IXXA20150726102Support Fitting · damagedNUMBER 8 OTBD ROTARY ACT SUPPORT FITTING HAS 1 EACH DEFECTIVE HOLE AT APPROX THE 3:00 O CLOCK POSITION. HOLE REAMED TO .453", FREEZE PLUG INSTALLED IAW ENGINEERING DOCUMENT 47158REA04.SDR IXXA20150726101Support Fitting · corrodedNUMBER 7 OTBD ROTARY ACT SUPPORT FITTING HAS 1 EACH DEFECTIVE HOLE APPROX AT THE 12:00 POSITION. HOLE REAMED TO .393", FREEZE PLUG INSTALLED IAW ENGINEERING DOCUMENT 47158REA04.SDR IPXA2015050988872Skin · chafedINSPECTION TYPE:5YR, LEFT WING, CENTER FLAP, UPPER SKIN, REPAIR DOUBLER CHAFED, 75"-78" FROM INBD EDGE, 44" FROM T/E. R & R DOUBLER IAW A300-600, SRM 57-50-00, FIG 205.SDR IPXA2015050988870Skin · debondedINSPECTION TYPE: C10, DISBOND DAMAGE ON RT WING INBD AFT FLAP UPPER SKIN, AT IFS 112 REPAIR IAW SRM 57-53-01-2R-1, REPAIR 1 AND SRM 51-70-10-2R-4, REPAIR 4.SDR IPXA2015050988869Skin · debondedINSPECTION TYPE: C10, DISBOND DAMAGE ON LT WING INBD AFT FLAP UPPER SKIN AT IFS 107. REPAIR IAW SRM 57-53-01-2R-1, REPAIR 1 AND SRM 51-70-10-2R-4, REPAIR 4.SDR FDEA201504301330Skin · damagedLEFT INBD FLAP VANE LE EDGE SKIN MISSING, HONEYCOMB MATERIAL EXPOSED. INSTALLED NEW LT INBD FLAP VANE IAW 27-50-03-2.SDR SWAA2015052039868Skin · delaminatedLEFT WING INBD FLAP ON UPPER SURFACE DELAMINATED. REPAIRED FLAP IAW SRM.SDR SWAA2015051139549Flap · delaminatedLEFT WING OTBD AFT FLAP LOWER INBD CORNER DELAMINATED. R & R AFT FLAP IAW AMM.SDR SWAA2015050439279Flap Track · looseRIGHT WING OTBD AFT FLAP NR 4 TRACK AFT ATTACH POINT LOOSE. R & R FLAP TRACK IAW AMM.SDR SWAA2015050439278Flap Track · looseRIGHT WING OTBD AFT FLAP NR 2 TRACK AFT ATTACH POINT LOOSE. R & R FLAP TRACK IAW MM.SDR SWAA2015050439277Flap Track · looseRIGHT WING INBD AFT FLAP OTBD TRACK AFT ATTACH POINT LOOSE. R & R FLAP TRACK IAW AMM.SDR SWAA2015050439276Flap Track · looseRIGHT WING INBD AFT FLAP INBD TRACK AFT ATTACH POINT LOOSE. R & R FLAP TRACK IAW AMM.SDR A6WA201542688Skin · chafedLEFT INBD FLAP VANE SKIN CHAFED IN 3 SPOTS.SDR SWAA2015043039143Flap · delaminatedRIGHT WING OTBD AFT FLAP DELAMINATED AT AFT INBD CORNER. REPAIRED AFT FLAP IAW SRM.SDR SWAA2015051439660Skin · debondedLEFT WING INBD FORE FLAP UPPER SURFACE DEBONDED 46" FROM INBD END. REPAIRED FORE FLAP IAW SRM.SDR SWAA2015051439659Skin · debondedRIGHT WING INBD FORE FLAP UPPER SURFACE DEBONDED 46" FROM INBD END. REPAIRED FORE FLAP IAW SRM.SDR SWIA201541208Vane · chafedRT INBD FLAP VANE CHAFED L/E MIDDLE. INSTALLED NEW RT INBD FLAP VANE MIDDLE L/E IAW SRM.SDR SWIA201541202Vane · chafedRIGHT INBD FLAP VANE CHAFED L/E OTBD. R & R RT INBD FLAP VANE OTBD L/E PANEL 601R14303-44 IAW SRM.SDR SWIA201541197Vane · chafedLEFT INBD FLAP VANE CHAFED L/E OTBD. INSTALLED NEW LT INBD FLAP VANE OTBD L/E PANEL IAW SRM.SDR SWIA201541196Vane · chafedLEFT INBD FLAP VANE CHAFED L/E MIDDLE. REPLACED LT INBD FLAP VANE L/E MIDDLE SECTION IAW REO.SDR SWAA2015050839455Flap Track · corrodedRIGHT WING NR 5 FLAP TRACK MOUNT HOLE CORRODED. REPAIRED FLAP TRACK IAW CMM.SDR REXA2015042500444Panel · chafedTASK CARD 900-27-680-100 RT FLAP PANEL 684EB CHAFED. RT FLAP PANEL PNL 684EB IAW SRM'S 51-40-11 & 57-52-01.SDR ABXA20150424060Support · corrodedNUMBER 1 FLAP SUPPORT NR 1, 2 & 4 HOLES HAVE DEFECT INDICATION WITH ROTARY SCAN, POSSIBLE CORROSION. NR 1 SUPPORT HOLES REAMED IAW REA-B657-61484-MR. SDR INFO, PN 113T1345-43, PART NAME, NR 1 FLAP SUPPORT, CORRODED LEVEL 2, FROM NR 1 FLAP SUPPORT. ACFT WAS SDR ABXA20150424059Support · corrodedNUMBER 7 FLAP SUPPORT NR 3 HOLE HAS DEFECT INDICATION WITH ROTARY SCAN, POSSIBLE CORROSION. NR 7 SUPPORT HOLES REAMED IAW REA-B657-61484-MR. SDR INFO, PN A13T1345-48, PART NAME NR 7 FLAP SUPPORT, CORRODED LEVEL 2, FROM NR 7 FLAP SUPPORT. ACFT WAS GNDED.SDR R61A201504240302Skin · damagedMAINTENANCE REPORTED A LIGHTNING STRIKE DAMAGE TO THE LT INBD FLAP ASSY. TOP SKIN ALONG THE REAR SPAR BETWEEN YW90 TO YW112. MAINTENANCE PERFORMED A "MAJOR" REPAIR TO THE LIGHTNING STRIKE DAMAGE ON THE LT INBD FLAP ASSY, TOP SKIN ALONG THE REAR SPAR BETWEEN YWSDR SWAA2015052740095Flap · delaminatedLEFT WING OTBD AFT FLAP INBD TE DELAMINATED. R & R AFT FLAP IAW SRM.SDR ASAA2015042311634Skin · chafedLEFT OTBD FOREFLAP INBD L/E CHAFED. ACFT GROUNDED. R & R L/E SKIN IAW SRM 57-53-01-01-2 AND 51-40-02-0G-0.SDR REXA2015042300441Panel · chafedTASK CARD 900-27-580-100 LT FLAP VANE PANEL 584ET CHAFED ACROSS RIVETS HEAD. DRILLED FASTENER HOLES IN NEW PANEL 584ET IAW SRM 51-40-11-001-001-A01. INSTALLED RIVETS IN NEW PANEL 584ET FOR NUTPLATES IAW SRM 51-42-06. PRIMED & TOP COATED NEW PANEL IAW SRM 51SDR WX0A072552Skin · dentedRAMP CREW REPORTED POSSIBLE DENT IN LT OTBD FLAP, 18 1/2 X 9 1/2 X 0.3125. REPLACED TWO EACH DAMAGED RIBS & DENT RELIEVED IAW SRM 51-30-2, 51-10-02 & CMM 27-50-02. NO FURTHER INSPECTIONS REQUIRED. THIS IS A MINOR REPAIR.SDR ASOA20150427012Fitting · crackedTHE RT OTBD FLAP HAS A CRACK ON THE INBD ROOT FITTING. REPAIRED USING PRINCIPALES OF TECH INSTRUCTIONS TI-145-13-200, REV U. GENERATED A DMI TO PERFORM AN INTERNAL AND EXTERNAL DVI AT A 2C OR 10,000 FLT HRS WHICHEVER OCCURES FIRST.SDR DALA2015042402908Skin · delaminatedLEFT WING T/E OTBD FLAP LOWER SURFACE CENTER SECTION FOUND DELAMINATION. LT WING T/E OTBD FLAP LOWER SURFACE CENTER SECTION DELAMINATION AREA DETERMINED DAMAGED SIZE AND REPAIRED IAW SRM 57-53-01, REPAIR 1, FIG 201, SRM 51-70-17. 1916816.SDR SWAA2015042438922Flap · delaminatedLEFT WING INBD AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.SDR DALA2017041102916Crank Assy · corrodedCORROSION LEVEL 2, AT C CHECK, PITTING WAS FOUND ON THE NR 2 CRANK ARM ASSY OF THE LT OUTBOARD FLAP. REPLACED CRANK.SDR SWIA201541133Skin · failedLT INBD FLAP VANE CENTER L/E SKIN FAILED. R & R LT INBD FLAP VANE CENTER L/E REF SRM.SDR SWAA2015042739026Skin · crackedLEFT WING INBD TE AFT FLAP LE SKIN CRACKED FROM INBD EDGE. R & R AFT FLAP IAW AMM.
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