JASC 5730
Service difficulty reports · 27,262
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 DALA2015121207574Access Panel · corrodedCORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1335C. FUEL ACCESS 1335C WAS REPLACED IAW SRM 51-22-2A AND WILL BE INSTALLED WITH CARD 2800-0120, JOB 001-0445.SDR FXGA201512071547Skin · crackedUPPER WING SKIN CRACKED AT NR 2 AT FUEL TANK ACCESS DOOR NR 90. TO REPAIR A CRACK IN THE UPPER WING SKIN AT THE AFT OTBD CORNER OF NR 2 ALT FUEL TANK ACCESS DOOR NR 90 & REPLACING THE CRACKED ACCESS DOOR DOUBLER. THE WING SKIN CRACKED EXTENDS BEYOND THE LIMISDR DALA2015121107538Access Panel · corrodedCORROSION AT SETTLEMENT AND COUNTERSINK AREAS OF FUEL ACCESS PANEL 1472C. FUEL PANEL WAS REPLACED.SDR FOTR20151210001Skin · dentedLEFT WING NR 1 SLAT UPPER SURFACE OF THE T/E WEDGE HAS A DENT THAT IS OUT OF LIMITS DUE TO OVERLAPPING DENTS WS 785-800.SDR SWAA2016012248304Skin · crackedRIGHT WING UPPER SKIN, CRACKED AT APPROX RSS 255.5 RT, FASTENER HOLE 1" FROM AFT EDGE. REPAIRED SKIN IAW EA.SDR SWAA2016012248303Skin · crackedRIGHT WING UPPER SKIN, CRACKED AT APPROX RSS 251 RT, FASTENER HOLE 1" FROM AFT EDGE. REPAIRED SKIN IAW EA.SDR SWAA2016012248302Skin · crackedRIGHT WING UPPER SKIN, CRACKED AT APPROX RSS 239.5 RT, FASTENER HOLE 1" FROM AFT EDGE. REPAIRED SKIN IAW EA.SDR SWAA2016012248301Skin · crackedRIGHT WING UPPER SKIN, CRACKED AT APPROX RSS 238 RT, FASTENER HOLE 1INCH FROM AFT EDGE. REPAIRED SKIN IAW EA.SDR SWAA2016012248300Skin · crackedRIGHT WING UPPER SKIN, CRACKED AT APPROX RSS 237 RT, FASTENER HOLE 1 INCH FROM AFT EDGE. REPAIRED SKIN IAW EA.SDR SWAA2016012248264Skin · crackedRIGHT WING UPPER SKIN AT APPROX RSS 236 RT, FASTENER HOLE 1" FROM AFT EDGE CRACKED. REPAIRED SKIN IAW EA.SDR SWAA2016010647679Skin · crackedLEFT WING UPPER SKIN REAR SPAR CRACKED IN FASTENER AREA AT RSS 247. REPAIRED SKIN IAW EA.SDR SWAA2016010647686Skin · crackedLEFT WING UPPER SKIN CRACKED AT REAR SPAR AREA, AFT FASTENER ROW, IN FASTENER AT RSS 267. REPAIRED SKIN IAW EA.SDR SWAA2016010647685Skin · crackedLEFT WING UPPER SKIN REAR SPAR AREA CRACKED AFT FASTENER ROW, IN FASTENER AT RSS 253. REPAIRED SKIN IAW EA.SDR SWAA2016010647684Skin · crackedLEFT WING UPPER SKIN CRACKED IN REAR SPAR AREA, AFT FASTENER ROW, IN FASTENER AT RSS 248. REPAIRED SKIN IAW EA.SDR ASOA2015120914261Skin · corrodedWING PLANK HOLE FUEL PANEL 640BB LAND SURROUND HAS CORROSION/PITTING. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV L. COMPLIED WITH REO 601R-57-21-2392. RECEIVED AND COMPLIED WITH ECTC REO 601R-57-21-2392.SDR ASOA2015120914260Skin · corrodedWING PLANK ACCESS HOLE FOR FUEL PANEL 540BB LAND SURROUND HAS CORROSION PITTING. COMPLIED WITH ECTC EO 000-57-81.SDR DALA2015121007532Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620EB. NEW BUSHING WAS FABRICATED AND INSTALLED IAW SRM 57-00-04.SDR ABXA20151208199Skin · corrodedSUSPECTED CORROSION ON RT WING AT REAR SPAR & WS 912. REMOVED PANELS, REMOVED CORROSION & NDT INSPECTED. PERFORMED REPAIR ON REA B657-61824-MR. REINSTALLED PANELS IAW SRM 51-40-02 & REA B657-61824-MR. TOUCH UP PAINT TO BE DONE ON NR 1241. DANGER TAG REMOVSDR ABXA20151208198Skin · corrodedSUSPECTED CORROSION ON RT WING AT REAR SPAR & WS 1025. REPAIRED CORRODED AREA ON RT WING AT REAR SPAR & WS 1030 IAW REA B657-61825-MR. REINSTALLED FIXED PANELS IAW SRM 51-40-02 & REA 657-61825. REPAIR AREA TO BE PAINTED ON NR 1241. FUEL PANEL 652BB TO BE LSDR ABXA20151208196Skin · corrodedLEFT WING SURFACE CORRODED AFT OF OVERWING EXIT AT WING TO BODY FAIRING AT APPROX STATION 938. REMOVED CORROSION & REPAIRED AREA IAW REA B657-61841-MR. SDR INFORMATION, CORRODED LEVEL 2, PN 112T3229-11, SN N/A, PART NAME RIB CHORD, EXACT FS & BS LOCATION ON SDR DALA2015120907527Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PLATE 620JB. REAMED HOLES, FABRICATED AND INSTALLED BUSHINGS IAW SRM 51-10-03.SDR DALA2015120907461Access Panel · corrodedCORROSION OUT OF LIMITS ON 2 COUNTERSINK HOLES ON FUEL ACCESS PLATE NR. 1371C. SRM 51-22-2A. FUEL ACCESS PLATE AND BUSHINGS WERE TREATED IAW SRM 51-10-3, NEW BUSHINGS WERE INSTALLED.SDR FDEA201512073931Skin · chafedRIGHT WING FIXED LEADING EDGE SKIN LOWER EDGE FOUND CHAFFED JUST OUTBOARD OF DROOP LEADING EDGE. REPAIRED IAW EA 1-5730-T0321987 PT 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR DALA2015120807523Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PANEL 620FT. BUSHINGS WERE REPLACED IAW SRM 57-00-04 AND 51-10-03.SDR DALA2015120807522Access Panel · corrodedCORROSION ON CONTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 620FT. BUSHING FABRICATED AND INSTALLED IAW SRM 57-00-01.SDR FDEA201512073929Skin · chafedPANEL 655AR EXTERNAL SKIN HAS CHAFED. REPAIRED IAW EA F5750-T0320958. MAJOR REPAIR.SDR DALA2015120807450Access Panel · corrodedCORROSION AT SETTLEMENT AND COUNTERSKIN AREAS OF FUEL ACCESS PANEL 1409C. FUEL ACCESS 1409C WAS REPLACED IAW SRM 51-22-2A CONDITION II PARAGRAPH, B.SDR SWAA2016012248308Skin Panel · crackedRIGHT WING UPPER SKIN PANEL, CRACKED AT RSS 254, MOST AFT OPENED ATTACH STRUCTURE. REPAIRED SKIN IAW EA.SDR SWAA2016012248307Skin Panel · crackedRIGHT WING UPPER SKIN PANEL, CRACKED AT RSS 238, MOST AFT OPENED STRUCTURE ATTACH FASTENER HOLE. REPAIRED SKIN IAW EA.SDR SWAA2016012148256Skin Panel · crackedRIGHT WING UPPER SKIN PANEL CRACKED AT RSS 191. REAR SPAR UPPER CHORD TO WING SKIN FWD FASTENER HOLE. REPAIRED SKIN IAW EA.SDR SWAA2016012148238Skin Panel · crackedRIGHT WING UPPER SKIN PANEL CRACKED AT RSS 250, MOST AFT OPENED STRUCTURE ATTACH FASTENER HOLE. REPAIRED SKIN IAW EA.SDR SWAA2016012148237Skin Panel · crackedRIGHT WING UPPER SKIN PANEL TE CRACKED AT RSS 221. REPAIRED SKIN IAW EA.SDR SWAA2016012148236Skin Panel · crackedRIGHT WING UPPER SKIN PANEL CRACKED AT RSS 208, MOST AFT STRUCTURE ATTACH FASTENER HOLE. REPAIRED SKIN IAW EA.SDR UIEA2015120800697Skin · corrodedCORROSION ON THE RT WING INTERIOR LOWER SKIN UPPER SURFACE NEAR OLES 1308. REMOVE DAMAGE AREA IAW SRM 51-10-02 REV 32. REPAIR DAMAGE AREA IAW EI NR T2015 A 578 - 2597 REV 2. JOB COMPLETED & CONDITION CHECKED NORMAL.SDR UIEA2015120800698Skin · corrodedCORROSION DAMAGE ON THE RT WING INTER SPAR LOWER SKIN UPPER SURFACE NEAR OLES 1308. REMOVED DAMAGED AREA IAW SRM 51-10-02 REV 32. REPAIR DAMAGED AREA IAW EI NR T2015 A 578 - 2597 REV 2. JOB COMPLETED & CONDITION CHECKED.SDR UIEA2015120900702Skin · corrodedCORROSION FOUND RT WING UPPER SKIN UPPER SURFACE HAD CORROSION AFT OF REAR SPAR WS 582.2. REPAIR CORROSION IAW E I NR T2015 A 57B - 2603 REV 4&. CONDITION CHECKED NORMAL & JOB COMPLETED.SDR UIEA2015120800700Fairing · corrodedCORROSION SURFACE, FOUND SURFACE RT WING INBD DOOR FAIRING UPPER WAS CORRODED. BLENDED OUT THE DAMAGE AREA & MEASURED REWORKED AREA L X W X D = 2X1.5X0.0044. ORIGINAL THICKNESS WAS 0.071 WHICH WAS WITHIN THE ALLOWABLE LIMIT IAW SRM 52-80-02, ALLOWABLE DAMAGESDR UIEA2015120900703Skin · corrodedREPAIR CORROSION ON THE WING INTER SPAR LOWER SKIN, PANEL NR 3, LOWER SIDE NEAR FSS 1305. BLENDED OUT THE DAMAGED AREA, MEASURED & REWORKED. THE DEEPEST THICKNESS WAS 0.216 INCHES, WHICH WAS NOT ALLOWABLE IAW SRM 57-20-01, ALLOWABLE DAMAGES FIG 101 CHART I RSDR UIEA2015120900711Skin · corrodedCORROSION, SKIN, LT WING UPPER SKIN AT WBL 849. BLEND OUT THE DAMAGED AREA & MEASURED REWORK AREA LX WXD = 1.1" X 0.9" X 0.007" WHICH IS WITHIN ALLOWABLE LIMIT IAW SRM 57-20-01-1A-1 FIG 101 DETAIL II REV 32. DETAIL DATA REA TO J/C ATTACHING SHEET NO. 0069538SDR DALA2015120707448Access Panel · corrodedCORROSION ON SETTLEMENT AND COUNTERSINK AREA OF FUEL ACCESS PANEL NR 520EB. FOUND TO BE OUT OF LIMITS. REPLACED FUEL PANEL IAW SRM 57-00-04.SDR RAIA2018091250001Skin · crackedLEFT WING LE NR 3 HAS CRACKS ABOVE THE O/B 2 VORTILONS. REMOVED AND REPLACED LT NR 3 LE STORAGE. A/C REPAIRED 8/30/18 A/C NOT YET RELEASED.SDR SWAA2015120946953Skin · crackedRIGHT WING LE, CRACKED IN DEFLECTOR DOOR CUT OUT, JUST INBD OF PYLON. REPAIRED CUT OUT IAW SRM.SDR SWAA2016010647683Skin · crackedLEFT WING UPPER SKIN FASTENER HOLES CRACKED, BETWEEN RSS 248 - 254. REPAIRED SKIN IAW EA.SDR HKGA2016F00044Skin · corrodedAN AREA OF CORROSION ON THE RT LOWER WING SKIN JUST INBD OF THE ENGINE NACELLE WAS IDENTIFIED. IT IS LOCATED ON THE AFT SKIN EDGE WERE IT IS SECURED TO THE SPAR, IN THE DRY AREA, AROUND WS 72.548 AND APPROXIMATELY 1.0" IN DIAMETER.SDR SWAA2015123147560Skin · crackedRIGHT WING UPPER SKIN TE CRACKED AT RSS 270.5. REPAIRED SKIN IAW EA.SDR SWAA2015123147559Skin · crackedRIGHT WING UPPER SKIN TE CRACKED AT RSS 251. REPAIRED SKIN IAW EA.SDR SWAA2015123147558Skin · crackedRIGHT WING UPPER SKIN TE CRACKED AT RSS 241. REPAIRED SKIN IAW EA.SDR ABXA20151203197Skin · corrodedCORROSION SUSPECTED AT LT WING REAR SPAR WS 854. BLEND OUT FOR CORROSION REMOVAL WAS ACCOMPLISHED ON REA 657-61837-MR, WS 810-815. BLEND OUT & TRIM OUT FOR CORROSION REMOVAL WAS ACCOMPLISHED ON REA B657-61838-MR, WS 850 - 859. SDR INFORMATION CORRODED LEVELSDR FDEA201512033877Doubler · crackedRIGHT WING LE BEADED DOUBLER AT STATION XOS 643 - 648 FOUND CRACKED. CRACKED BEADED DOUBLER AT CARRIED OUT REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201512033876Doubler · crackedRIGHT WING LE BEADED DOUBLER AT XOS 768 - 772 FOUND CRACKED. CRACKED BEADED DOUBLER CARRIED OUT REPAIR IAW SRM 57-40-02-2R FIG 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
Back to JASC 5730