JASC 5730
Service difficulty reports · 27,269
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 ASOA20130308027Skin · crackedDURING A-CHECK INSP THE LT WING TE SKIN WAS FOUND TO BE CRACKED IN THE GROUND SPOILER CENTER HINGE OTBD FWD RADIUS EXTENDING 22MM (.86IN). REMOVED DAMAGED SECTION AND PERFORMED A FILLER/DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR REXA2013030900386Skin · chafedREMOVED CHAFE ON RIGHT WING FUEL CUTOUT PANEL LANDING 640BB, HOLE NR 1, IN THE NON-CRITICAL AREA WITHIN LIMITS IAW BOMBARDIER REO 601R-57-21-030 REV J.SDR GLBA2013030700200Skin · dentedDURING A SCHEDULED ROUTINE INSPECTION, FOUND DENT ON THE RT WING OTBD L/E AT WS 290.06, DAMAGE APPROX 17.5". REPAIRED IAW EO 13-1900-57-001. MAJOR REPAIR.SDR SWAA2013032013896Rub Strip · corrodedUPPER RIGHT WING CUTOUT FOR FUEL PANEL 620FT, MATING SURFACE CORRODED. REMOVED AND REPLACED RUB STRIP IAW SRM.SDR SWAA2013032013895Rub Strip · corrodedUPPER RIGHT WING CUTOUT FOR FUEL ACCESS PANEL 620DT, MATING SURFACE CORRODED. REMOVED AND REPLACED RUB STRIP IAW SRM.SDR IPXA13M77534Doubler · corrodedINSPECTION TYPE:1C RT WING L/E LOWER PANEL LANDING CORRODED AT UPPER SURFACE NEAR XORS 820 (XOS 926). REPAIRED RT WING L/E LOWER DOUBLER AT XOS926 IAW EA 011-5710-01- A4516 REV IR AND EO MD11-5730-50171-A.SDR DALA13010889243Panel · corrodedRT WING T/E, LOWER INBD FIXED PANEL, AFT STIFFENER IS DEEPLY CHAFED. REMOVED CORROSION ON WING T/E. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 57-00-01, FIG 3. CUTOUT DAMAGED AREA. FABRICATED, DRILLED INSTALLED DOUBLER AND FILLER IAW 51-70-01 FIG 1, 51-10-01SDR WRLA20130304586Door · nickedCRACK - DURING 4C CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND TWO NICKS ON THE SKIN OF LEFT WING SLAT ACTUATOR DOOR PANEL 518FB.SDR FDEA201303030492Skin · corrodedLEFT, AFTER REMOVAL OF OVERWING FILL PORT ADAPTER, FOUND UPPER SKIN CORRODED AT MATING SURFACE TO OVERWING FILL PORT ADAPTER. REPAIRED IAW EA F-5710-155960. MAJOR REPAIR.SDR SWAA2013031113546Skin · crackedLEFT WING LEADING EDGE SKIN AT WBL 208 CRACKED. REPAIRED LEADING EDGE PER EA.SDR UALA2013030101238Skin · gougedRIGHT WING UPPER EXTERNAL SKIN HAS A DENT GOUGE BS 1017, BBL 87 STR U5 FOUND TO BE OUT OF LIMITS. MAJOR REPAIR ACCOMPLISHED. DAMAGE AT RIGHT WING UPPER SKIN BS 1017 BBL 87 STR U5. TRIMMED CUT DAMAGE AND INSTALLED REPAIR PER ESR#23 PER AAR EA 130182 & ECRA 5SDR SWAA2013032113939Skin · crackedRIGHT WING LEADING EDGE SKIN CRACKED AT FS 542. REPAIRED SKIN IAW SRM.SDR SWAA2013031913788Skin · crackedRIGHT WING INBOARD FIXED LEADING EDGE SKIN CRACKED. REPAIRED SKIN IAW SRM.SDR SIMA20130226010Skin · crackedRT WING SKIN AT SPOILER HINGE CRACKED. REPAIRED IAW EO EM-57MR-661.SDR SIMA20130226009Skin · crackedRT WING SKIN AT SPOILER HINGE CRACKED. REPAIRED IAW EO EM-57MR-661.SDR QXEA2013022600512Skin · dentedRT WING HAS A DENT ON UNDERSIDE JUST INBD OF NR 5 FLAP TRACK. DENT MEASURED 1.5" X 1.3" X .020" DEEP. DAMAGE IS OUT OF LIMITS IAW SRM 57-20-30-01-01, REV 12. CONFIRMED WING SKIN CRACK FREE IN AFFECTED AREA REF NTM 51-00-01-250-801, PT 6, REV 7. CUT AWAY SDR IPXA3M77490Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E BEADED DOUBLER AT XOS669.7174 CRACKED. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER AT XOS669.7174 REF MD11 57-40-02, REPAIR 15, FIG 203.SDR IPXA3M77489Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E BEADED DOUBLER AT XOS665.2174 IS CRACKED. REPAIRED LT WING FIXED L/E COMPT. BEADED DOUBLER AT XOS665.2174 REF SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA3M77488Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E BEADED DOUBLER CRACKED AT XOS544.5878. REPAIRED LT WING FIXED L/E BEADED DOUBLER AT XOS544.5878 REF SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA3M77487Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E BEADED DOUBLER CRACKED AT XOS755.8529. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER AT XOS755.8529 REF SRM 57-40-02, REPAIR 15, FIG203.SDR IPXA3M77486Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E BEADED DOUBLER CRACKED AT XOS696.2851. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER AT XOS696.2851 REF SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA3M77485Doubler · crackedINSPECTION TYPE:4C RT WING FIXED L/E BEADED DOUBLER CRACKED AT APPROX XOS 696. REPAIRED RT WING FIXED L/E COMPT BEADED DOUBLER FROM XOS692 TO XOS703 REF SRM 57-40-02, REPAIR 15, FIG. 203.SDR IPXA3M77484Doubler · crackedINSPECTION TYPE:4C LT WING FIXED L/E XOS732.2851 BEADED DOUBLER FOUND WITH CRACKS. REPAIRED LT WING FIXED L/E BEADED DOUBLER AT XOS732.2851 REF EO MD11-5730-48222-A.SDR IPXA3M77466Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT XOS 618.1502. REPAIRED IAW 5730-48222-A, APPX A.SDR IPXA3M77465Doubler · crackedINSPECTION TYPE:1C LT WING FIXED L/E COMPT BEADED DOUBLER CRACKED AT XOS 655.2174. REPAIRED LT WING FIXED L/E COMPT BEADED DOUBLER AT XOS 655.2174 REF SREO MD11-5730-48222-A.SDR IPXA3M77464Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E COMPT BEADED DOUBLER AT XOS 627.1502 CRACKED. REPAIRED LT WING BEADED DOUBLER IAW SRM 51-33-01, REPAIR 15, FIG 203.SDR IPXA3M77463Doubler · crackedINSPECTION TYPE:1C, RT WING FIXED L/E BEADED DOUBLER CRACKED AT APPROX XOS 496. REPAIRED BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA3M77462Skin · crackedINSPECTION TYPE:1C, RT WING FIXED L/E COMPT PANEL LANDING CRACKED AT APPROX XOS 546. FABRICATED AND INSTALLED RT WING L/E PANEL LANDING REPAIR IAW SRM 51-33-01, PAGE 1.SDR SBAA2013022700003Panel · deformedDURING VISUAL INSPECTION NOTICED THAT LEFT WING INBOARD AND RIGHT WING INBOARD TKS PANELS WERE SLIGHTLY DEFORMED ALONG LEADING EDGE FROM WS 37.00 TO WS 47.00. TKS PANELS DID NOT APPEAR LOOSE AND SEEMED TO OPERATE NORMALLY.SDR SWAA2013032013897Rub Strip · corrodedRIGHT WING UPPER RIGHT CUTOUT FOR ACCESS PANEL 620AT, MATING SURFACE CORRODED. REMOVED AND REPLACED RUB STRIP IAW SRM.SDR SWAA2013030813495Rub Strip · corrodedRIGHT WING UPPER CUTOUT FOR ACCESS PANEL 620FT, MATING SURFACE RUBSTRIP CORRODED. REMOVED AND REPLACED RUBSTRIP PER SRM.SDR ABXA20130223399Skin · corrodedRIGHT WING UPPER SKIN HAS AREA OF CORROSION AT FWD SPAR ATTACH POINT WS 433 APROX FORWARD OF VORTEX GENERATORS. REMOVED CORROSION IAW B767 SRM 51-10-02 & 57-20-01. C/W REA 657-60480-MR, ACFT WAS GROUNDED.SDR UHLA2013022000107Skin · damagedMAJOR REPAIR - DRILL START IN UPPER WING SKIN FROM RIGHT RIB 10 EXTENSION STOP DRILL. REMOVED UPPER SKIN DOUBLER, DRILLED OUT DAMAGE, INSTALLED DOUBLE FLUSH PLUG IAW ETD 2013-170-003239 REV 1. RE-INSTALLED UPPER SKIN DOUBLER AND RESTORED TOP COAT IAW ETD 201SDR QXEA2013022200429Access Panel · corrodedCORROSION AROUND SCREW HOLES OF MATING SURFACE ON PANEL 622BT. REMOVED CORROSION AS MARKED IAW SRM 57-10-35-02-02, REV 12. MECHANICALLY MEASURED, MAX MATERIAL LOSS OF .009" IS WITHIN LIMITS IAW SRM REV 12-57-10-35-02-02. CONFIRMED AFFECTED AREAS CRACK FREE SDR FXGA201302211306Skin · crackedRE-ENFORCING RING, SKIN & DOUBLER CRACKED AT CTR WING SECTION. CRACKS WERE FOUND IN THE WING SKIN, STATION 60 TO 60 DOUBLER & RE ENFORCING RING FOR PANEL PN 3479163, DOOR, CTR WING FUSELAGE FRAME CUT OUT, IN THE CTR WING SECTION OF THE AIRPLANE. THE CRACK ISDR FDEA201302210399Skin · crackedFOUND NINE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS 683.4 AND XORS 713.6. REPAIR CARRIED OUT IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 51. REPAIR CLASSIFIED SDR FDEA201302210398Skin · crackedFOUND CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS 683.4 AND XORS 713.6. REPAIR CARRIED OUT IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 51. REPAIR CLASSIFIED AS MAJSDR DXTA2013030105302Skin · corrodedTOP OF RT WING SKIN HAS CORROSION AND CORROSION ALL AROUND FUEL FILLER WING SKIN. REMOVED NON-MEASURABLE CORROSION FROM FASTENERS AND AROUND THE FUEL FILLER CAP AND REPLACED CORRODED FASTENERS ON THE WING FUEL PANELS W219, W206, W208 & W212 IAW SRM 51-73-00 SDR QXEA2013021900513Access Panel · corrodedCORROSION ON ACCESS PANEL 624BT MATING SURFACE. REMOVED CORROSION IAW SRM 57-20-35-02-02, REV 12. WITHIN LIMITS IAW SRM 57-20-35-02-02, REV 12. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801, PT 1, REV 7. INSTALLED NEW OUTER SEAL IAW SRM REV 1SDR QXEA2013021900418Access Panel · corrodedCORROSION ON PANEL 624AT MATING SURFACE. REMOVED CORROSION FROM PANEL 624AT IAW SRM 57-20-35-02-02, REV 12. MINIMUM REMAINING ON PAD IS .115 IS WITHIN LIMITS IAW SRM 57-20-35-02-02, REV 12. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT1, SDR QXEA2013021900417Skin · corrodedCORROSION ON RT WING LANDING INBD AND OTBD SIDE FOR PANEL 624AT. REMOVED CORROSION IAW SRM 57-20-35-02-05, REV 12 MIN THICKNESS NOTED .005" CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801, PT 1 AND 51-00-06-910-801, PT 1, REV 7. FOUND BLENDS TO SDR QXEA2013021900416Skin · corrodedCORROSION ON RT WING LANDING INBD AND OTBD FOR PANEL 624BT. REMOVED CORROSION IAW SRM 57-20-35-02-05, REV 12. MIN THICKNESS NOTED .085", CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801, PT 1 AND 51-00-06-910-801 PT 1, REV . FOUND BLENDS TO BE WISDR QXEA2013021900415Skin · corrodedCORROSION ON RT WING LANDING INBD SIDE FOR PANEL 624CT. REMOVED CORROSION IAW SRM 57-20-35-02-05, REV 12 MIN THICKNESS NOTED .084", CONFIRMED AFFECTED AREA CRACK FREE NTM 51-00-04-910-801 AND 51-00-06-910-801 PT 1, REV 7. FOUND BLENDS TO BE WITHIN LIMITS IAWSDR QXEA2013021900414Access Panel · corrodedCORROSION AROUND SCREW HOLES OF MATING SURFACE ON PANEL 522BT. REMOVED CORROSION AND ALODINED MIN THICKNESS REMAINING .217, PANEL IS WITHIN LIMITS IAW SRM 57-10-35-02-02, REV 12. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1, REV 7. APPLIESDR QXEA2013021900412Skin · corrodedCORROSION ON PANEL 524DT MATING SURFACE. REMOVED CORROSION AND BLENDED IAW SRM REV 12 57-20-35-02-02. MIN THICKNESS REMAINING .118 IS WITHIN LIMITS IAW SRM REV 12 57-20-35-02-02. ALODINED, PAINTED AND RE IDENTIFIED IAW SRM REV 12 57-20-35-02-02. CONFIRMED SDR QXEA2013021900411Skin · corrodedCORROSION ON PANEL 524CT MATING SURFACE. REMOVED CORROSION AND BLENDED IAW SRM REV 12 57-20-35-02-02 MIN REMAINING THICKNESS .116 WITHIN LIMITS IAW SRM REV 12 57-20-35-02-02. ALODINED AND RE IDENTIFIED PANEL IAW SRM REV 12 57-20-35-02-02. CONFIRMED CRACK FREESDR QXEA2013021900408Skin · corrodedCORROSION ON LT WING LANDING INBD AND OTBD SIDE FOR PANEL 524AT. REMOVED DAMAGE IAW SRM 57-20-35-02-05, REV 12. MIN THICKNESS NOTED .079" CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1 AND 51-00-04-910-801, PT 1 REV 7. FOUND BLENDS TO BE WSDR QXEA2013021900407Skin · corrodedCORROSION ON LT WING LANDING INBD SIDE FOR PANEL 524BT. REMOVED DAMAGE IAW SRM 57-20-35-02-05, REV 12 MIN THICKNESS NOTED .085", CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801, PT 1 AND 51-00-06-910-801 PT 1, REV 7. FOUND BLENDS TO BE WITHIN LIMSDR QXEA2013021900406Skin · corrodedCORROSION ON LT WING LANDING INBD SIDE FOR PANEL 524CT. REMOVED CORROSION ON LANDING IAW SRM 57-20-35-02-05, REV 12 MIN THICKNESS NOTED .081" CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801, PT 1 AND 51-00-06-910-801 PT 1, REV 7. FOUND BLENDS TO SDR QXEA2013021900405Skin · corrodedCORROSION ON LT WING LANDING INBD SIDE FOR PANEL 524DT. REMOVED CORROSION AS MARKED IAW SRM 57-20-35-02-05, REV 12 MIN THICKNESS NOTED .079" CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801, PT 1 REV 7. FOUND BLENDS TO BE
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