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 SWIA201334275Vane · chafedLT INBD FLAP VANE LE CHAFFED IN THE CENTER BEYOND LIMITS. C-CHECK REPLACED PN 601R14303-51 IAW SRM.SDR SWIA201334271Skin · chafedLT INBD FLAP VANE LE CHAFED ON THE OTBD SIDE. C-CHECK REPAIRED IAW REO.SDR SWIA201334270Skin · chafedLT INBD FLAP VANE LE CHAFED IN THE CENTER. C-CHECK BLENDED IAW REO.SDR IPXA13179782Skin · chafedINSPECTION TYPE:3C, LT CENTER FLAP UPPER SKIN IS CHAFED BETWEEN RIB 13 AND 15. ACCOMPLISHED REPAIR ON LT CENTER FLAP UPPER SKIN BETWEEN RIB 13 AND RIB 15 STGR 2, 6 TO STGR 2.8 IAW STASA EA 300-5753-01-A4829 AND EO A300-5750-51792-A, PARA 6A.SDR IPXA13B79611Skin · puncturedPUNCTURE IN LOWER SKIN LT INBD FLAP COVE PANEL 2.5" FWD OF AFT END AND 1 2.0" OTBD OF INBD EDGE. REPAIRED IAW EO B747-5750-51098-B.SDR SWIA201334269Skin · chafedRT INBD FLAP VANE LE SKIN CHAFED AT OTBD END. C-CHECK REPAIRED IAW REO.SDR SWIA201334268Skin · chafedRT INBD FLAP VANE LEADING SKIN CHAFED NEAR CENTER. C-CHECK REPAIRED IAW REO.SDR SWIA201334267Skin · chafedRT INBD FLAP VANE LE SKIN CHAFED. C-CHECK REPLACED IAW REO.SDR QXEA2013082101269Structure · corrodedTHREE RIVETS CORRODED ON THE RT INBD FLAP UPPER L/E. REMOVED CORRDED RIVETS ON RT FLAP IAW SRM 51-42-15, PROCEDURE 5, TIEM G, STEP 1. INSTALLED NEW RIVETS IAW SRM 51-42-15 PROCEDURE 5, ITEM E, STEPS 1-3.SDR SWAA2013081919296Flap · delaminatedLT WING OTBD AFT FLAP DELAMINATED AT AFT INBD CORNER. REPAIRED AFT FLAP IAW MM.SDR FDEA201308021745Skin · dentedRIGHT WING INBD FLAP LOWER SURFACE FOUND DENTED AT XIFH 250 AND ONE INCH FROM T/E. REPAIRED IAW SRM 57-50-01, REPAIR 1, FIGURE 201, REV 53 AND EA 1-5750-T0301707, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR SWAA2013081319171Stiffener · crackedRT WING NR 6 AFT FLAP TRACK STIFFENER CRACKED. R&R STIFFENER IAW SRM.SDR SWAA2013080718935Flap · delaminatedLT WING OTBD AFT FLAP DELAMINATED AT INBD END LOWER SIDE. R&R AFT FLAP IAW MM.SDR SWAA2013080618888Flap · delaminatedLT WING INBD AFT FLAP DELAMINATED. R&R AFT FLAP IAW AMM.SDR SWAA2013080618887Flap · delaminatedRT WING OTBD AFT FLAP DELAMINATED ON INBD END. R&R AFT FLAP IAW AMM.SDR DALA13037480971Vane · corrodedDURING ROUTINE INSPECTION, THE LT WING OTBD T/E FLAP FIXED VANE WAS NOTED TO HAVE EXFOLLIATION CORROSION ON THE LOWER SURFACE. THE FLAP VANE WAS REPLACED IAW AMM 27-51-03-501 AND THE REQUIRED INSPECTIONS WERE COMPLETED.SDR SWIA201334308Hinge Fitting · chafedRT WS54.55 HINGE BOX AFT FITTING HAS OTBD FITTING LUGS CHAFED. C-CHECK REPAIRED FLAP HINGE BOX WING FITTING IAW STS.SDR IPXA13179803Skin · gougedINSPECTION TYPE:3C, RT INBD FLAP UPPER SKIN IS GOUGED BETWEEN RIB 16 AND 17 STGR 2.2 TO STGR 2.4. ACCOMPLISHED REPAIR ON RT INBD FLAP UPPER SKIN BETWEEN RIB 16 AND 17 STR 2.2 TO STGR 2.4 IAW EO A300-5750-51803-A PARA 6A.SDR IPXA13179801Skin · chafedINSPECTION TYPE:3C, RT INBD FLAP UPPER SKIN IS CHAFED IN 2 PLACES BETWEEN RIB 11 AND 12 STR 2.1 TO STR 2.4. ACCOMPLISHED REPAIR ON RT INBD FLAP UPPER SKIN BETWEEN RIB 11 AND 12 STR 2.1 TO STR 2.4 IAW EO A300-5750-51802-A, PARA 6A.SDR IPXA3579588Skin · puncturedINSPECTION TYPE: C-CK, RT INBD MAIN FLAP HAS A SMALL PUNCTURE ON THE UPPER SURFACE. REPAIRED IAW SRM 51-53-01 2R AND 51-70-07-OG.SDR A6WA20134M1176Panel · damagedLEFT FLAP PANEL 584AB HAS 1 EA ELONGATED FASTENER HOLE TOP RB CORNER. REMOVED ELONGATED HOLE AND INSTALLED FREEZE PLUG, PN 05-2013-056 IAW SRM 57-52-00-02.SDR SWIA201334248Skin · chafedLT INBD FLAP VANE LE SKIN CHAFED AT INBD VANE ACTUATOR. C-CHECK REPAIRED CHAFE BY BLENDING ON LT INBD FLAP VANE LE SKIN AT INBD VANE ACTUATOR IAW REO.SDR SWIA201334247Skin · chafedLT INBD FLAP VANE LE SKIN CHAFED AT CENTER VANE ACTUATOR. C-CHECK REPAIRED CHAFE BY BLENDING ON LT INBD FLAP VANE LE SKIN AT CENTER VANE ACTUATOR IAW REO.SDR SWIA201334246Skin · chafedLT INBD FLAP VANE LE SKIN CHAFED AT OTBD VANE ACTUATOR. C-CHECK REPAIRED CHAFE BY BLENDING ON LT INBD FLAP VANE LE SKIN AT OTBD VANE ACTUATOR IAW REO.SDR IPXA13579683Skin · damagedINSPECTION TYPE: C1S3, LT INBD MAIN FLAP UPPER SKIN DAMAGED AT APPROX 44.75 FROM INBD END. REPAIRED IAW RCD 012190.SDR SWAA2013080118745Flap · delaminatedLT WING OTBD AFT FLAP DELAMINATED. R&R AFT FLAP IAW MM.SDR SWIA201334249Hinge Fitting · gougedLT WING OTBD FLAP INBD FWD HINGE FITTING AFT SIDE HAS A GOUGE. C-CHECK BLENDED GOUGE ON LT WS178.00 FLAP HINGE BOX OTBD AFT SIDE OF AFT HINGE FITTING IAW STS.SDR SWAA2013080718928Stiffener · crackedLT WING NR 3 STIFFENER CRACKED ON INBD SIDE OF FLAP TRACK FAIRING. R&R STIFFENER IAW SRM & DRAWING.SDR IPXA3579535Panel · puncturedRT INBD MAIN FLAP COVE PANEL LWR SURFACE 3 DAMAGE AREAS 81" OTBD OF INBD EDGE 3.1" FWD OF AFT EDGE. REPAIRED IAW EO B757-5750-51606-A.SDR CALA2013072990026Fairing · crackedFLAP CANOE FAIRING, 571DB HAS 1 INCH CRACK INBD SIDE. PERFORMED PERMANENT REPAIR IAW SRM 57-53-70, 1 PAGE, 103 NOTE A.SDR WRLA20130727601Wedge · debondedDISBOND WAS FOUND ON LT WING OTBD FLAP, NRC6753-503L, WEDGE UPPER SKIN AT STA X OF 614.25 TO 676.5. PERFORM THE LT WING OTBD FLAP WEDGE UPPER SKIN REPAIR IAW EI W2013A57B-2048, REV: 0. CHECK CONDITION SATISFACTORY.SDR SWAA2013080918987Angle · crackedRT WING FLAP TRACK NR 6 UPPER SURFACE ANGLE CRACKED AT WBL 183.49. R&R ANGLE IAW & DRAWING.SDR CALA2013072990036Skin · delaminatedRT INBD T/E FLAP DELAMINATED ALONG THE EDGEBAND. 12 INCHES INBD FROM THE BODY. AREA REMOVED OF MOISTURE, R & R RT AFT T/E FLAP IAW MM. RIG AND OPS CHECKED GOOD.SDR DALA13036413138Strut · corrodedCORROSION AT INTERNAL STRUCTURE OF INTERCONNECTING STRUT OF LT FLAP. R & R INTERCONECTING STRUT.SDR AALA20130726001Flap · puncturedRT INBD FLAP HAS PUNCTURE ON THE LOWER INBD FLAP HAS PUNTURE ON THE LOWER INBD SIDE APPROXIMATLEY 10 INCHES FROM INBD END. ACCOMPLISHMENTS HOT BOND REPAIR IAW SRM 57-53-01-01-2, 51-70-10-2R-2 & SRM 51-70-10-2R.SDR ASOA2013081608876Fitting · damagedOVERSIZED HOLES ON LT & RT FWD FLAP FITTING ASSY. REPAIRED IAW REO 670-57-21-575, REV P1. REPAIR CLASSIFIED AS MAJOR.SDR SWAA2013072618605Flap · delaminatedLT WING INBD AFT FLAP DELAMINATED ON OTBD CORNER. R&R FLAP ASSEMBLY IAW MM.SDR IPXA13B79634Skin · delaminatedINSPECTION TYPE:C, LT WING INBD T/E FORE FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 26.SDR A6WA2013073141117Skin · chafedTE FLAP SKIN PANEL 594PB CHAFED. R & R SKIN IAW SRM 51-40-11 AND 51-42-06.SDR IPXA13579682Skin · damagedINSPECTION TYPE: C1S3, LT INBD MAIN FLAP UPPER SURFACE COMPOSITE SKIN DAMAGED FROM CONTACT WITH WING T/E FIXED PANEL. REPAIRED IAW RCD 011892.SDR IPXA13B79633Skin · delaminatedINSPECTION TYPE:C, RT WING INBD T/E MID FLAP T/E COVE PANEL HAS DELAMINATION. FIBERGLASS PREPREG LAY-UP REPAIR PERFORMED IAW SRM 51-70-07, PAR5A (1), FIG 5, REV 25.SDR FDEA201307221632Tee Fitting · corrodedLT OTBD FLAP VANE TEE FITTING "B" MOUNTING HOLE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW SRM 57-50-02 REPAIR 5 FIG.201 REV 53. REPAIRED IAW EA 1-5750-T0301579 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.SDR FDEA201307221631Tee Fitting · corrodedRT OTBD FLAP VANE TEE FITTING "F" MOUNTING HOLE CORRODED. FOUND EXCEEDED LIMIT IAW SRM 57-50-02, REPAIR 5, FIG 201, REV 53. REPAIRED IAW EA 1-5750-T0301580, PART 1 STEP 1.B. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307221630Tee Fitting · corrodedRIGHT OTBD FLAP VANE TEE FITTING "C" MOUNTING HOLE CORROSION. FOUND EXCEEDED LIMITS IAW SRM 57-50-02, REPAIR 5, FIG 201, REV 53. REPAIRED IAW EA1-5750-T0301580, PART 1 STEP 1.A. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307221629Hinge Fitting · corrodedRT WING OTBD FLAP, OTBD AFT (FLAP) HINGE PIVOT HOLE INBD BORE CORRODED. REWORKED AND FOUND EXCEEDED LIMITS IAW CMM 57-52-04, REV 76. REPAIRED IAW EA 1-5750-166144. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201307221628Bushing · wornRIGHT WING FLAP OTBD HINGE (FLAP SIDE), PIVOT OTBD BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76 AND FOUND EXCEEDED LIMITS IAW CMM 57-52-03, REV 76. NEW BUSHING FABRICATED BY MACHINING AND INSTALLED EA 1-5750-102153C, PART 3, STEP 2. REPAIRSDR FDEA201307221627Bushing · wornRIGHT WING: RT INBD FLAP OTBD HINGE (FLAP SIDE) , PIVOT INBD BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 76. FOUND EXCEEDED LIMIT IAW CMM 57-52-03, REV 76. NEW BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-102153C, PART 3, STEP SDR IPXA201307229437Skin · puncturedRIGHT WING INBD FLAP LOWER T/E PUNCTURE DAMAGED. REPAIRED IAW EO B747-5750-51514-A.SDR IPXA201307229433Skin · puncturedRT INBD MID FLAP LWR SURFACE PUNCTURE 1.4" FROM INBD EDGE. REPAIRED IAW EO B747-5750-51513-A.SDR A6WA2013073141118Vane · chafedCHAFE TO L/T INBD FLAP VANE UPPER SKIN T/E AT WS 55.49. BLENDED IAW REO 601R-57-52-2028.
Back to JASC 5753