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 SWAA2012100408253Flap · delaminatedRIGHT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY IAW MM.SDR USAA2012102300006Strut · corroded2S CHECK - CORROSION ON LEFT WING INTERCONNECTING STRUT BETWEEN WS 4862 & WS 5512 & BETWEEN WING RIB 9 TO RIB 10. REPLACED LEFT WING INTERCONNECTING STRUT IAW A319 AMM 27-51-44-001-A.SDR CA120925006Housing · damaged(CAN) RT OTBD SECONDARY DRIVE CABLE OUT HOUSING FOUND SHEARED OFF AT CABLE SWAGGED END. SWAGGED FITTING SEPARATED FROM CABLE SHEATH. RESOLVED ON W/O: 354198, TASKCARD: NR-00008, REPLACED RT OTBD SECONDARY FLEX DRIVE SHAFT, PN-745581A IAW AMM.SDR FDEA201209233408Bushing · wornLEFT INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT INBD BUSHING WORN. WORN BUSHING REMOVED AS PER CMM 20-20-07 REVISION 74. FOUND EXCEED LIMITS AS PER CMM 57-52-03 REVISION 74. NEW BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-162592 PART 1. REPAIR CLSDR SWAA2012102308724Skin · delaminatedLEFT WING O\B AFT FLAP LOWER SURFACE I\B AFT CORNER OF FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP IAW AMM.SDR SWAA2012092708068Flap · damagedRIGHT WING I/B AFT FLAP DAMAGED. REMOVED AND REPLACED AFT FLAP PER MM.SDR UALA2012092405388Fitting · faultyDURING REWORK OF RIGHT I/B FLAP TORQUE TUBE SLOT DOOR ARM REF CF0580. REMOVED AND REPLACED FITTING PER SRM 51-40-02 AND ECRA5750-04490.SDR SWAA2012092608034Spindle · crackedRIGHT WING O/B MID FLAP NR 7 SPINDLE CRACKED. REMOVED AND REPLACED SPINDLE ASSY IAW MT.SDR FDEA201209233411Bushing · wornRIGHT INBD FLAP, OTBD AFT (FLAP SIDE) PIVOT OTBD BUSHING WORN. WORN BUSHING REMOVED IAW CMM 20-20-07, REV 74. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING HOLE DIAMETER 1.258", MAXIMUM HOLE DIAMETER 1.220". NEW BUSHING FABRICATEDSDR FDEA201209233410Bushing · wornRT INBD FLAP OTBD AFT (FLAP SIDE) HINGE PIVOT INBD BUSHING WORN. WORN BUSHING REMOVED IAW CMM 20-20-07 REV 74. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03 REV 74. EXISTING HOLE DIAMETER 1.255", MAXIMUM HOLE DIAMETER 1.220". NEW BUSHING FABRICATEDSDR FDEA201209233409Bushing · wornLEFT INBD FLAP, OTBD AFT (FLAP SIDE) HINGE PIVOT OTBD BUSHING WORN. REMOVED IAW CMM 20-20-07, REV 74. HOLE MEASURED AND FOUND EXCEED LIMIT IAW CMM 57-52-03, REV 74. EXISTING HOLE DIAMETER 1.254", MAXIMUM HOLE DIAMETER 1.220". NEW BUSHING FABRICATED AND INSSDR SWAA2012092608031Flap · delaminatedRIGHT WING I/B MID FLAP DELAMINATED. REMOVED AND REPLACED MID FLAP ASSY PER MM.SDR SWAA2012092607982Flap · damagedRIGHT WING I/B FORE FLAP DAMAGED. REMOVED AND REPLACED FORE FLAP PER MM.SDR AALA20120921015Skin · damagedCENTER PIN ON BLIND FASTENER ON DOUBLER REPAIR LOWER SURFACE OF INBOARD AFT FLAP. FABRICATED DOUBLER AND HOT BONDED DOUBLER REPAIR AREA PER SRM 51-70-10.SDR CA120921004Skin · delaminated(CAN) DURING HEAVY MAINTENANCE INSPECTION, RT INB FLAP T/E HAS A LARGE AREA OF DELAMINATION,30" LENGTH. RIVET HOLES ELONGATED AND HEADS PULLED THROUGH THE COMPOSITE STRUCTURE. T/E REPLACED IAW AMM.SDR REXA2012101701118Skin · chafedLEFT INBOARD FLAP VANE AT TRAILING EDGE AND UPPER OUTER SKIN CHAFED. REPAIRED IAW SRM 57-52-00 AND SRM 57-00-31.SDR SWAA2012100408273Skin · crackedRIGHT WING NR 6 SLAT SKIN CRACKED. REPAIRED SKIN IAW SRM.SDR USAA2012092600038Fastener · looseQ6 CHECK - LOOSE FASTENERS ON RIGHT OUTBOARD FORE FLAP AT WS 280, RBL 141. REPLACED RIGHT OUTBOARD FORE FLAP AT WS 280, RBL 141 IAW JOB CARD 03C40927013.SDR QXEA2012092001092Roller · erodedRT WING NR 2 LOWER FLAP TRACK ROLLER CONTACT SURFACE HAS ERODED, FLAKED COATING. FOUND TRACK TO BE IN LIMITS IAW RD 8/4-57-1907. INSPECTED BLENDED AREA USING HFEC REF NDTM 51-00-06-910-801 PT 1, NO CRACKS NOTED. COMPLIED WITH TASK CARD RD 8/4-57-1907.SDR QXEA2012092001090Flap Track · crackedLEFT WING, NR 3 LOWER FLAP TRACK HAS MISSING COATING ON ROLLER CONTACT MATING SURFACE AFT END OF TRACK. REMOVED DAMAGE AND FOUND DAMAGE BEYOND LIMITS IAW RD 8/4-57-1511. CONFIRMED BLENDED AREA CRACK FREE REF NDTM 51-00-06-910-801 PT 1. MIN REMAINING THICKNSDR SWAA2012101708599Skin · puncturedRIGHT WING INBOARD AFT FLAP LOWER SKIN PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA2012092407926Flap · delaminatedRIGHT WING O/B AFT FLAP DELAMINATED AT THE INBOARD CORNER. REMOVED AND REPLACED AFT FLAP PER AMM.SDR A6WA20120921543Lug · gougedLEFT O/B FLAP CENTER HINGE AFT LUG IS GOUGED ON ALL ATTACHING POINTS. BLENDED 4 GOUGED AREAS IAW REO 601R-57-21-1753.SDR DALA1249040182Skin · delaminatedRIGHT WING INBD MAIN FLAP OTBD L/E FAIRING IS DELAMINATED. REPAIRED IAW SRM 57-53-01, REPAIR 1, FIG 201 AND 51-70-05 FIG 5.SDR DALA1249030182Skin · delaminatedLEFT WING INBD MAIN FLAP OTBD L/E FAIRING IS DELAMINATED, REPAIRED IAW SRM 57-53-01, REPAIR 1, FIG 201 AND 51-70-05, FIG 5.SDR CA120921007Lock Fastener · sheared(CAN) INSPECTION REVEALED A SHEARED LOCK FASTENER PIN ON THE FWD ROW OF FASTENERS OF THE INBD FLAP HINGE FITTING 600-10317-6, INSTALLED AT WS 76.50.SDR FXGA201209181271Skin · crackedRIGHT FLAP CRACKED AT W STA 149. REPAIRED IAW EO 1271.SDR SWAA2012101808652Flap · corrodedRIGHT WING INBOARD MID FLAP BORE OF OUTBOARD CARRIAGE CORRODED. REPAIRED MID FLAP IAW AMM.SDR IPXA2B75570Fairing · delaminatedINSPECTION TYPE: C, LT WING O/B T/E MID FLAP I/B L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 63.SDR QXEA2012091801083Skin · damagedRT INBD FLAP LOWER SURFACE HAS 9 SMOKING RIVETS. R & R RIVETS IAW SRM 51-42-05-02-01.SDR USAA2012091900010Skin · delaminatedC4 CHECK - DELAMINATION ON LEFT WING INBOARD FORE FLAP UPPER SURFACE 35 INCHES INBOARD OF OUTBOARD END & 8.5 INCHES UP FROM AFT TRAILING EDGE. REPLACED LEFT WING INBOARD FORE FLAP IAW B737 AMM 27-51-07-404-010 TO STEP D.(9).SDR DALA1248630182Skin · puncturedLEFT WING INBD AFT FLAP UPPER SURFACE IS PUNCTURED AND REPAIRED IAW SRM 57-53-01 REPAIR 1, FIG 201 AND 51-70-10, REPAIR 4 FIG 201.SDR UALA2012091905301Seal · damagedCREW REPORTS SEAL BETWEEN LEFT INBOARD AND OUTBOARD FLAP LOWER SURFACE IS DAMAGED AT THE AFT AFT END. SEAT HAS SMALL TEAR AT AFT SIDE, NO LOOSE PIECES. NEEDS LEFT WING FLAP KINK SEAL (110-1856) ITEM #180 OF IPC 57-52-21 PG6A. REPLACED FLAP SEAL.SDR AALA20120918012Skin · dentedRIGHT WING OUTBOARD FLAP LOWER SURFACE HAS 2 DENTS ON TRAILING EDGE WEDGE 31 AND 43 INCHES FROM OUTBOARD END. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-70-07.SDR AALA20120918011Flap · delaminatedDELAMINATION FOUND ON OUTBOARD TRAILING EDGE FLAP 31 INCHES FROM INBOARD EDGE. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-70-07.SDR IPXA12B75343Skin · dentedRT WING INBD AFT FLAP LOWER SKIN DENTED. REPAIRED IAW EO B747-5750-48266B.SDR UALA2012091805257Fitting · damagedNEED TO INITIATE A CF FOR ECRA 5750-04484 LEFT WING I/B MAIN FLAP I/B ATTACH FITTING.SDR IPXA2B75569Fairing · delaminatedINSPECTION TYPE: C, LT WING OTBD T/E FORE FLAP L/E FAIRING DELAMINATION AT MOST INBD AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 63.SDR IPXA2B75568Fairing · delaminatedINSPECTION TYPE: C, RT WING OTBD T/E MID FLAP L/E FAIRING DELAMINATED AT MOST INBD AREA. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 63.SDR A6WA20120921541Fitting · chafedLEFT O/B FLAP ROLLER FITTING CHAFED AND ROLLER WORN. REPAIRED LEFT O/B ROLLER FITTING IAW BOMBARDIER REO 601R-57-53-948. REMOVED WORN ROLLER INSTALLED NEW SERVICEABLE ROLLER (P/N NAS562-5R5) IAW CRJ 200 SRM 51-41-04.SDR QXEA2012091601065Skin · chafedCHAFE DAMAGE ON RT OTBD FLAP, LOCATED AT NR 4 FLAP TRACK CARRIAGE FWD MOUNT FITTINGS. SMOOTHED OUT DAMAGED AREA IAW SRM 51-14-00-02-04. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1, REMAINING THICKNESS NOTED .290" REF NTM 51-00-04-910-801SDR USAA2012091700039Strut · wornRON - RIGHT TRAILING EDGE FLAP INTERCONNECTING STRUT WORN. REMOVED AND REPLACED STRUT IAW A319 AMM 27-51-44-000-001-A.SDR SWAA2012111509438Strip · crackedCRACK ON STRIP LOCATED AT UPPER STRUCTURE OUTBOARD SIDE OF FLAP TRACK FAIRING NR 6 RT WING. REMOVED AND REPLACED STRIP IAW SRM AND DRAWING.SDR IPXA2M75685Vane · chafedINSPECTION TYPE: 4C, CHAFE DAMAGE ON UPPER SURFACE OF LT INBD FLAP VANE NEAR INBD END. REPAIRED CHAFE DAMAGE ON LT INBD FLAP VANE UPPER SURFACE T/E NEAR XIFH 138 IAW SRM 57-50-80. REPAIR 2 WET LAYUP BONDED REPAIR. (MAJOR)SDR USAA2012091700035Skin · delaminatedC5 CHECK - DELAMINATION ON RIGHT OUTBOARD AFT FLAP, INBOARD UPPER SKIN, 6 INCHES FROM INBOARD END & 6 INCHES FROM TRAILING EDGE. REPLACED RIGHT OUTBOARD AFT FLAP IAW B737 AMM 27-51-39-404-002.SDR AALA20120912018Flap · puncturedPUNCTURE ON LEFT OUTBOARD FLAP TRAILING EDGE 108 INCHES FROM OUTBOARD AND 17 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01.SDR AALA20120912002Skin · delaminatedOUTBOARD FLAP AT LEFT TRAILING EDGE, ON UPPER SKIN HAS A SMALL DELAMINATION AROUND 112 INCHES FROM INBOARD END AND 11 INCHES FROM TRAILING EDGE. ACCOMPLISHED BONDED REPAIR PER SRM 57-53-01-2R.SDR A6WA20120920014Vane · chafedRIGHT I/B FLAP VANE CHAFED ON LEADING EDGE WHERE VANE HITS STOPS. REMOVED AND REPLACED CTR VANE LEADING EDGE P/N 601R14303-52 IAW CRJ 51-40-11 AND 51-42-13, I/B AND O/B VANE LEADING EDGE BLENDED OUT DAMAGE AND FOUND TO BE WITHIN LIMITS IAW REO 601R-57-52-004 SDR SWAA2012091407619Spindle · corrodedLEFT WING NR 2 FLAP CARRIAGE SPINDLE THERMAL COATING AND BASE METAL CORRODED. REMOVED AND REPLACED NR 2 SPINDLE FLAP CARRIAGE ASSY PER MT.SDR TRBA20120910004Guide · corrodedDURING B INSPECTION, FOUND THE RT WING HAS 2 EXTERNAL FLAP CAM GUIDES WITH CORROSION OUT OF LIMITS. THE ACFT WAS REMOVED FROM SERVICE. REMOVAL AND INSTALLATION OF RT WING 2 EXTERNAL FLAP CAM GUIDES COMPLETED IAW MM 57-53-12. THE ACFT WAS RETURNED TO SERVICE.
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