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 UALA2012030601414Flaperon · damagedREMOVED DAMAGED LT FLAPERON PER MM. REMOVED AND REPLACED R57039. ACP SMC 058 ON WU U8736K LT WING FLAPERON REMOVED. INSTALLED FLAPERON AND TORQUE MOUNTS BOLTS AND ACTUATOR BOLTS. ACP PER AMT. ADJUSTED FLAPERON, OP CHECK GOOD.SDR UALA2012030601413Seal · missingFOUND LEFT WING UPPER INBOARD FLAPERON SEAL MISSING. FOUND ABOUT 4 FEET MISSING. REPLACED FLAPERON SEAL.SDR UALA2012030501374Fairing · damagedLEFT I/B FLAP O/B FWD CANOE FAIRING IS DAMAGED. REMOVED CANOE PER MM.SDR UALA2012030501373Fairing · damagedLEFT I/B FLAP O/B AFT CANOE FAIRING IS DAMAGE. REMOVED CANOE PER MM.SDR SWAA2012031902309Flap · delaminatedRT WING I/B AFT FLAP DELAMINATED AT T/E ON FORWARD AND AFT SIDE. REMOVED AND REPLACED AFT FLAP IAW AMM.SDR VNAA2012020500002Skin · dentedDURING SCHEDULED MAINTENANCE THE LEFT INBOARD LOWER SKIN WAS DENTED. THE LEFT INBOARD FLAP LOWER SKIN WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.SDR DALA1213393119Panel · chafedDURING NON ROUTINE CHECK, MAINTENANCE FOUND LEFT INBD FLAP SLIDING PANEL UPPER SURFACE HAS CHAFED MARK. BLENDED CHAFED MARK AREA IAW A319 SRM 51-73-00. FOUND TO BE IN LIMITS IAW ER/A 13 484369-14MA. REPAIR ACCOMPLISHED IAW ER/A 13 484369-14MA. IDENTIFIED SDR A6WA201240428Rib · damagedRIGHT INBD FLAP HAS 2 EA MISDRILLED HOLES UNDER INBD SEAL. R & R INBD FLAP INBD RIB IAW REO 601R-57-52-1871.SDR DALA1212051503Skin · delaminatedO/B MAIN FLAP LWR SURFACE MUD SECTION FOUND DELAM. REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE II AND SRM 51-70-07 PARA 5A(1) FIG 9.SDR IPXA2172296Skin · dentedINSPECTION TYPE: 10YR, RIGHT WING INBD FLAP OTBD UPPER SURFACE BETWEEN STR 2.1 & 2.2, RIB 3 HAS DENTED AND GOUGED. REPAIRED RT WING INBD FLAP IAW SRM 57-50-00, PARA 4 E, FIG 205, REV 21.SDR UALA2012022901252Skin · corrodedLEFT INBOARD FLAP UPPER SURFACE HAS CORROSION AT MID POINT. REPAIRED LEFT MAIN FLAP UPPER SKIN PER ECRA 5750-04424. NEED TO ACCOMPLISH PERMANENT REPAIR ON OR BEFORE 24 MONTHS. RII ACCOMPLISHED.SDR SWAA2012030501914Flap · delaminatedLT WING INBOARD AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY PER AMM.SDR QXEA2012030200196Flap Track · damagedLEFT NR 2 FLAP TRACK MISSING TUNGSTEN COATING ON AFT END OF TOP TRACK, UPPER FLANGE. COMPLIED WITH RD 8//4-57-1771.SDR SWAA2012031602268Skin · puncturedLT WING I/B FORE FLAP LOWER SURFACE PUNCTURED. REPAIRED FLAP PER SRM.SDR FDEA201202280698Vane · corrodedLEFT WING OTBD FLAP VANE NR 3 TEE FITTING TRACK ATTACH HOLE FOUND CORRODED. HOLE REWORKED AND FOUND EXCEED LIMIT IAW SRM 57-50-02 REPAIR 5 FIGURE 201 REVISION 48. EXISTING HOLE SIZE: 0.873" X 0.597". FINAL SIZE: 0.964"X0.696". MAXIMUM ALLOWABLE SIZE: 0.94SDR FDEA201202280697Vane · corrodedRIGHT WING OTBD FLAP VANE NR 2 TEE FITTING TRACK ATTACH HOLE FOUND CORRODED. HOLE REWORKED AND FOUND EXCEED LIMITS IAW SRM 57-50-02 REPAIR 5 FIGURE 201 REVISION 48. EXISTING HOLE SIZE: 0.894" X 0.670". FINAL HOLE SIZE: 0.995" X 0.726". MAXIMUM ALLOWABLE SISDR SWAA2012030501876Skin · puncturedRT WING I/B AFT FLAP LOWER SURFACE PUNCTURED. REPAIRED AFT FLAP IAW SRM.SDR QXEA2012030100193Flap Track · damagedRT WING NR 4 FLAP TRACK HAS CHIPPED/MISSING TUNGSTEN CARBIDE COATING ON INBD SURFACE OF VERTICAL LEG. BLENDED NR 4 FLAP TRACK IAW RD 8/4-57-1238. CONFIRMED TRACK CRACK FREE REF NTM 51-00-04-910-801 PT 4. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-57SDR SWAA2013030113192Tail Cone · delaminatedRIGHT WING NR 7 CANOE TAIL CONE ASSY FOUND TO BE DELAMINATED ON BOTTOM. REMOVED AND REPLACED TAIL CONE ASSY PER MM.SDR USAA2012032600002Flap · corroded2S CHECK - LEFT OUTBOARD FLAP INTERNAL AREA CORRODED BETWEEN WS 486 TO WS 1166 & BETWEEN RIB 9 TO RIB 22. REPLACED LEFT OUTBOARD FLAP IAW A319 AMM 27-54-62.SDR SWIA201229861Skin · dentedDENT FROM BIRD STRIKE AT RIGHT WING OUTBOARD FLAP LEFT SIDE OF INBOARD FAIRING. (SERVICE) REPAIRED OUTBOARD FLAP LOWER SKIN PER REO. REBUSHED LOWER CENTERFLAP TRACK PER SRM.SDR USAA2012022800018Carriage · fracturedWHEN FLAPS WERE SELECTED TO 25 FOR LANDING (FLT 1700), FELT A POP AND AC ROLLED LEFT. FLAPS RETRACTED TO 15 AND SITUATION IMPROVED BUT LEFT ROLL PERSISTED. LANDED WITHOUT INCIDENT. LEFT FLAPS EXTENDED. MX INSPECTED FLAPS AT VARIOUS SETTINGS, RAN UP AND DOWSDR USAA2012032600004Spar · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT OUTBOARD FLAP FRONT SPAR AT RIB 15 & ATTACHMENT AREA AT TRACK NR 4. REPLACED RIGHT OUTBOARD FLAP IAW A319 AMM 27-54-62-400-001.SDR SWAA2012022801796Flap · delaminatedRT WING O/B AFT FLAP I/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA12411210Skin · delaminatedRT OUTBOARD AFT FLAP HAS DELAM AT T/E. REPAIRED RT OUTBOARD AFT FLAP T/E IAW B737 400 SRM 51 70 10 REPAIR 4.SDR QXEA2012030100195Flap Track · damagedLEFT NR 1 FLAP TRACK, RUB MARKS ON VERTICAL SURFACE OF THE TOP TRACK. BLENDED RUB MARKS IAW RD 8/4-57-1352. CONFIRMED TRACK CRACK FREE MIN REMAINING THICKNESS NOTED .190" REF RD 8/4-57-1352. FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-1352. PRIMED AND PAINTED SDR QXEA2012030100194Flap Track · damagedLEFT NR 3 FLAP TRACK TUNGSTEN COATING MISSING ON AFT END OF LOWER TRACK. POLISHED DAMAGED AREAS ON NR 3 TRACK IAW RD 8/4-57-1511. CONFIRMED CRACK FREE REF NTM 8.2.1.1. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-1511.SDR A6WA201240392Beam · wornLEFT INBD FLAP VANE ACTUATOR OTBD AND CENTER SLIDING BEAM HAS WEAR. REPAIRED WEAR IAW REO 601R-57-52-1863.SDR A6WA201240394Beam · wornRIGHT INBD FLAP VANE ACTUATOR SLIDING BEAM HAS WEAR DAMAGE. REPAIRED WEAR DAMAGE IAW REO 601R-57-52-1864.SDR FDEA201202240679Hinge Fitting · corrodedCORROSION FOUND DURING FPI ON LT WING (FLAP SIDE) INBD FLAP, OTBD AFT HINGE BRACKET PIVOT INBD LUG BORE. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03 REVISION 72. EXISTING DIAMETER 1.256",FINAL DIAMETER 1.261", MAXIMUM ALLOWABLE DIAMETER 1.220". BUSSDR FDEA201202240678Hinge Fitting · corrodedCORROSION FOUND DURING FPI ON LT WING (FLAP SIDE) INBD FLAP, OTBD AFT HINGE BRACKET PIVOT OTBD LUG BORE. REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-52-03 REVISION 72. EXISTING DIAMETER 1.329",FINAL DIAMETER 1.335", MAXIMUM ALLOWABLE DIAMETER 1.220"SDR DALA1211093359Attach Fitting · chafedRT OUTBOARD FLAP, INBOARD DRIVE ROD ATTACH FITTING FOUND CHAFED. REPAIRED AS PER PRI 499108-14 REV 0.SDR DALA1211063359Attach Fitting · chafedLT OUTBOARD FLAP, INBOARD DRIVE ROD ATTACH FITTING FOUND CHAFED. REPAIRED AS PER PRI 499108-14 REV 0.SDR SWAA2012022901815Flap · puncturedLT WING O/B FORE FLAP PUNCTURED. REPAIRED FORE FLAP IAW SRM.SDR SWAA2012022701758Flap · delaminatedRIGHT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER M/M.SDR FDEA201202230674Skin · delaminatedLT INBD AFT T/E FLAP LOWER SKIN HAS PREVIOUS REPAIR THAT IS CRACKING. REPAIRED LT INBD AFT T/E FLAP LOWER SKIN IAW SRM 51-70-06. REF EA F-5750-157259 ISSUED FOR TRACKING-WINGS -FLIGHT SURFACES -EO F-5100-7-5001 LT INBD AFT FLAP-RSC REPAIR TRACKING. MAJOR RESDR A6WA201240367Hinge Fitting · chafedLT INBD FLAP INBD FLAP HINGE BOX IS CHAFING LWR INBD BRACKET. R & R LT INBD FLAP INBD FLAP HINGE BOX INBD BRACKET.SDR R61A201202220156Bolt · corrodedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RT WING INBD FLAP FAIRING 623BB AFT MOUNTING HARDWARE. MAINTENANCE REMOVED AND REPLACED RT WING INBD FLAP FAIRING 623BB AFT MOUNTING HARDWARE IAW EMB 190/195 AMM 57-58-23. AIRCRAFT IS SDR R61A201202220155Bushing · corrodedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RT WING INBD FLAP FAIRING 623BB AFT MOUNTING HARDWARE. MAINTENANCE REMOVED AND REPLACED RT WING INBD FLAP FAIRING 623BB AFT MOUNTING HARDWARE IAW EMB 190/195 AMM 57-58-23. AIRCRAFT IS SDR R61A201202220154Bolt · corrodedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE RT WING INBD FLAP FAIRING 622BB AFT MOUNTING HARDWARE. MAINTENANCE REMOVED AND REPLACED RT WING INBD FLAP FAIRING 623BB AFT MOUNTING HARDWARE IAW EMB 190/195 AMM 57-58-23. AIRCRAFT IS SDR AALA20120303005Skin · damagedLEFT WING OUTBOARD MAIN FLAP UPPER SURFACE AFT OF NUMBER 1 SPOILER HAS SMALL AREA OF EXPOSED HONEYCOMB. REMOVED DAMAGE PLIES, LAYED UP REPAIR PLIES AND CURED, APPLIED SEALER RESIN AND CURED PER SRM 57-53-01 AND SRM 51-70-07.SDR SWAA2012022701749Skin · puncturedLT WING I/B FOREFLAP PUNCTURED ON LOWER SURFACE. REMOVED AND REPLACED FORE FLAP PER M/M.SDR IPXA2172007Structure · chafedINSPECTION TYPE:4C, RT WING OTBD FLAP INBD BULLNOSE CHAFED. REPAIRED RT WING OTBD FLAP INBD BULLNOSE IAW SRM 57-50-00, PARA 4-H, FIG 208, REV 21.SDR SWAA2012022901829Wedge · delaminatedLT WING O/B AFT FLAP I/B CORNER TRAILING EDGE WEDGE DELAMINATED. REPAIRED WEDGE IAW SRM.SDR AALA20120222018Skin · delaminatedRIGHT WING OUTBOARD FLAP UPPER SURFACE HAS DELAMINATION. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.SDR SWAA2012022401739Flap · delaminatedRT WING O/B FORE FLAP I/B END DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR UIEA2012022300058Skin · damagedDURING WALKAROUND INSPECTION, FOUND DAMAGE TO THE RT INBD MID FLAP L/E EXTERNAL SKIN. DAMAGE EXCEEDED THE LIMITS OF SRM 57-60-01, FIG 101.SDR QXEA2012022700181Skin · chafedLEFT INBD FLAP UPPER SKIN HAS AREAS OF CHAFED PAINT BETWEEN STA YW-42.000 AND YW-157.825. BLENDED OUT CHAFE IAW RD 8/4-57-1595. REMAINING THICKNESS .023", CONFIRMED CRACK AND DISBOND FREE REF RD 8/4-57-1595. BLENDED AREAS FOUND TO BE OUT OF LIMITS IAW RD 8/SDR AALA20120224009Wedge · delaminatedLEFT WING MAIN INBOARD FLAP TRAILING EDGE WEDGE HAS DELAMINATION ON UPPER SKIN APPROXIMATELY 41.5 INCHES FROM OUTBOARD END OF WEDGE. FABRICATED AND INSTALLED DOUBLER PER SRM 51-70-10.SDR SWAA2012022101602Skin · damagedLT WING O/B AFT FLAP UPPER SKIN MATERIAL DAMAGED FROM UPPER SURFACE O/B CORNER. REMOVED AND REPLACED AFT FLAP PER MM.
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