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 CALA2016012895050Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L10, BETWEEN WS 1209 - 1264. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.125, BLEND OUT REMAIN 0.089. HFEC INSPECTION, FLUORESCENT PENETRANT INSPSDR CALA2016012895049Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L14, BETWEEN WS 942 - 995. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.244, BLEND OUT REMAIN 0.236. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECSDR CALA2016012895048Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L10, BETWEEN WS 863 - 916. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.280, BLEND OUT REMAIN 0.284. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECSDR CALA2016012895047Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT NEAR SPAR, BETWEEN WS 864 - 916. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.350, BLEND OUT REMAIN 0.319. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTIOSDR CALA2016012895046Skin · corrodedRIGHT LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT STRINGER L14, BETWEEN WS 810 - 916. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-0. SKIN ORIGINAL THICKNESS 0.280, BLEND OUT REMAIN 0.241. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CSDR CALA2016012895045Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION, AT STRINGER L14, BETWEEN WS 1182 - 1209. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & 51-20-01. SKIN ORIGINAL THICKNESS 0.155, BLEND OUT REMAIN 0.131. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTSDR CALA2016012895044Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION, AT STRINGER L14, BETWEEN WS 1021 - 1074. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.220, BLEND OUT REMAIN 0.200. HFEC INSPECTION, FLUORESCENT PENETRANT INSSDR CALA2016012895043Skin · corrodedRIGHT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, BETWEEN WS 995 - 1047. CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.310 & BLEND OUT REMAIN 0.286. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTSDR CALA2016012895042Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION, AT STRINGER 14, WS 960 - 1000 AREA. REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.245, BLEND OUT REMAIN 0.200. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CARRIED SDR CALA2016012895041Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, WS 1095 - 1105 AREA. REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.256, BLEND OUT REMAIN 0.247. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CARRIED OUSDR CALA2016012895040Skin · corrodedRIGHT WING CTR TANK MEASURING STICK 1, SURROUNDING SKIN FOUND CORRODED. REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.557, BLEND OUT AREA REMAIN 0.511. HFEC INSPECTION, FLUORESCENT PENETRANT INSPECTION CARRIED OUT, NO DEFECTSDR CALA2016012895039Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, WS 1270 & WS 1280 AREA. LT WING LOWER SKIN EXTERIOR SURFACE CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.106, BLEND OUT REMAIN 0.091. HFEC INSPECSDR CALA2016012895038Skin · corrodedLEFT WING LOWER SKIN EXTERIOR SURFACE, FOUND CORROSION AT REAR SPAR, WS 1065 - WS 1080 AREA. LT WING LOWER SKIN EXTERIOR SURFACE CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.268, BLEND OUT REMAIN 0.226. HFEC INSPESDR CALA2016012895037Skin · corrodedLEFT WING LOWER SKIN, EXTERIOR SURFACE FOUND CORROSION AT REAR SPAR, BETWEEN WS 1020 & WS 1050. LT WING LOWER SKIN EXTERIOR SURFACE CORROSION REMOVED & PROTECTED IAW SRM 51-10-02 & SRM 51-20-01. SKIN ORIGINAL THICKNESS 0.300, BLEND OUT REMAIN 0.290. HFEC INSDR SWAA2016022549423Skin · crackedRIGHT WING UPPER SKIN TE HOLES CRACKED, BETWEEN LOCATION RSS 228 - 267. REPAIR SKIN IAW EA & ER.SDR SWAA2016022549375Skin · crackedLEFT WING UPPER SKIN AT TE, AFT OF REAR SPAR RSS 239, FASTENER HOLE CRACKED. REPAIRED SKIN IAW ER & EA.SDR SWAA2016022549374Skin · crackedLEFT WING UPPER SKIN AT TE, AFT OF REAR SPAR, RSS 251 FASTENER HOLE CRACKED. REPAIRED SKIN IAW ER & EA.SDR SWAA2016022549373Skin · crackedLEFT WING UPPER SKIN AT TE, AFT OF REAR SPAR, RSS 255.5 FASTENER HOLE CRACKED. REPAIRED SKIN IAW ER & EA.SDR SWAA2016022349255Skin · crackedRIGHT WING UPPER SKIN AFT OF REAR SPAR, CRACKED FASTENER HOLE AT RSS 249.5. REPAIRED SKIN IAW ER & EA.SDR SWAA2016021949251Skin · crackedRIGHT WING UPPER SKIN AFT OF REAR SPAR, CRACKED FASTENER HOLE AT RSS 240. REPAIRED SKIN IAW ER & EA.SDR SWAA2016021949250Skin · crackedRIGHT WING UPPER SKIN AFT OF REAR SPAR, CRACKED AT FASTENER HOLE AT RSS 256. REPAIRED SKIN IAW ER & EA.SDR SWAA2016021949249Skin · crackedRIGHT WING UPPER SKIN AFT OF REAR SPAR, CRACKED FASTENER HOLE AT RSS 266. REPAIRED SKIN IAW ER & EA.SDR SWAA2016021949248Skin · crackedRIGHT WING UPPER SKIN AFT OF REAR SPAR, CRACKED FASTENER HOLE AT RSS 271. REPAIRED SKIN IAW ER & EA.SDR CA160129005Access Panel · corroded(CAN) CORROSION ON 4 EACH FUEL ACCESS PANEL LANDINGS NUMBER 510AB, 640BB, 540BB AND 650HB AS SHOWN IN THE ATTACHED FIGURE 1. MAINTENANCE HAS REMOVED ALL CORROSION DAMAGE IAW REO 601R-57-21-030, THE MATERIAL LOSS ON THE PANEL LANDINGS WOULD BE WITHIN LIMITS OF SDR FDEA201601260318Skin · damagedLEFT WING, AFT OVERWING ATTACH FITTING, ABOVE FRONT SPAR & NR 4 SLAT INBD MAIN TRACK REMOVAL, FOUND OSS 346 LE FIXED RIB COMMON TO WING UPPER SKIN LE LOCK FASTENER HOLE, ONE EACH, ELONGATED. LT WING OSS 346 LE FIXED RIB COMMON TO WING UPPER SKIN LE LOCK FASTESDR KO0R201601260035Skin Panel · crackedOUTER WING LOWER SKIN PANEL ACCESS DOOR CUT OUT, RT WING HAS 4 CRACK INDICATIONS IN FASTENER HOLES. WING STATION XORS 700.SDR KO0R201601260034Skin Panel · crackedOUTER WING LOWER SKIN PANEL ACCESS DOOR CUT OUT, LT WING HAS 3 EACH CRACK INDICATIONS IN FASTENER HOLES. WING STATION XORS 700.SDR CA160126009Skin · cracked(CAN) LEFT WING LOWER PLANK 601R10045-11 DRAIN HOLE AT WS 85.5 BETWEEN S-14 AND S-15 HAS TWO (2) EACH CRACKS. THE FORWARD CRACK EMANATES FROM THE EDGE OF THE DRAIN HOLE TO THE FORWARD AND MEASURES 0.4 INCHES LONG. THE AFT CRACK EMANATES FROM THE EDGE OF THE DRSDR ASOA2016012414390Skin · crackedCRACK FOUND AT RT LOWER WING PLANK, WS 148.019. COMPLIED WITH ECTC REO 601R-57-21-130 01 AND REO 601R-57-21-131. REMOVED UPPER PIE PANEL IAW SRM 51-42-06 & 51-42-13. INSTALLED UPPER PIE PANEL IAW CRJ 200 SRM 51-42-06, 51-42-13. COMPLIED WITH ECTC REO 601R-5SDR ASOA2016012414389Skin · crackedCRACK FOUND AT LT LOWER WING PLANK WS 148.019 CRACK LENGTH IS .7170. COMPLIED WITH ECTC REO 601R-57-21-130 AND REO 601R-57-21-131. REMOVED UPPER AND LOWER PIE SKIN PANELS IAW SRM 51-42-06 AND 51-42-15 AND 511-42-21. INSTALLED PIE PANELS IAW SRM 51-41-02 ANDSDR SIMA20160123001Skin · crackedRIGHT UPPER WING SKIN CRACKED AT GND SPOILER, CTR HINGE CUT OUT, 1.17 INCHES LONG. TRANSFERRED TO NRWC 603 MQT 02576. REPAIRED AREA IAW ERS-EM-57MR-569.SDR DALA2016012300545Access Panel · corrodedCORROSION AT COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1460C. FUEL ACCESS DOOR 1460C WAS REPLACED IAW 57-30-00 AND FUEL MEASURING STICK WAS INSTALLED UNDER CARD 343, ZONE 100.SDR DALA2016012300535Access Panel · corrodedCORROSION ON FUEL ACCESS DOOR COUNTERSINK/SETTLEMENT AREA NR 1460C AT RT WING. FUEL ACCESS DOOR 1460C WAS FOUND OUT OF LIMITS THEN WAS REPLACED.SDR DALA2016012200526Access Panel · corrodedCORROSION AT COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 1335. FUEL ACESS DOOR 1335C WAS REPLACED IAW IPC: 57-30-00.SDR DALA2016012200523Access Panel · corrodedCORROSION ON RT WING HEATER BLANKET FUEL SECONDARY ACCESS PLATE NR 1409C. RT WING HEATER BLANKET FUEL SECONDARY ACCESS PLATE NR 1409C WAS REPLACED IAW IPC 57-30-00.SDR SWAA2016021649105Skin · crackedRIGHT UPPER WING SKIN CRACKED FASTENER HOLES IMMEDIATELY FWD OF THE UPPER REAR SPAR FASTENERS AT RSS 220. REPAIRED SKIN IAW EA.SDR SWAA2016021649091Skin · crackedRIGHT WING UPPER SKIN CRACKED, IN AFT ROW OF OPEN FASTENER HOLES, AT RSS 238. REPAIRED SKIN IAW EA.SDR SWAA2016021649090Skin · crackedRIGHT WING UPPER SKIN, CRACKED IN AFT ROW OF OPEN FASTENER HOLES, BETWEEN RSS 254 - 264. REPAIRED SKIN IAW EA.SDR DALA2016012200532Access Panel · damagedDAMAGE FUEL SECOND ACCESS PLATE 1307C. FUEL SECOND ACCESS PLATE WAS REPLACED.SDR SWAA2016021849170Skin · crackedLEFT UPPER WING SKIN HOLE CRACKED AT RSS 220, 5" FWD OF TE. REPAIRED SKIN IAW EA.SDR SWAA2016021849169Skin · crackedLEFT UPPER WING SKIN HOLE CRACKED AT RSS 249 AFT ROW, .5" FWD OF TE. REPAIRED SKIN IAW ER & EA.SDR SWAA2016021849168Skin · crackedLEFT UPPER WING SKIN HOLE CRACKED AT RSS 253 AFT ROW, .5" FWD OF TE. REPAIRED SKIN IAW EA.SDR SWAA2016012648384Skin · crackedRIGHT WING INSPAR SKIN, CRACKED AT WBL 175 AT FASTENER HOLE REAR SPAR. REPAIRED SKIN IAW EA.SDR SWAA2016022349294Skin · crackedLEFT WING AFT UPPER SKIN CRACKED, BETWEEN RSS 235 - 275, IN FASTENER HOLE REAR SPAR AFT ROW. REPAIRED SKIN IAW EA.SDR SWAA2016021649150Skin · crackedRIGHT WING AFT UPPER SKIN TE, CRACKED AT RSS 255. REPAIRED SKIN IAW EA.SDR SWAA2016021649149Skin · crackedRIGHT WING AFT UPPER SKIN TE, CRACKED AT RSS 253.5. REPAIRED SKIN IAW EA.SDR SWAA2016021649148Skin · crackedRIGHT WING AFT UPPER SKIN TE SKIN, CRACKED AT RSS 247.5. REPAIRED SKIN IAW EA.SDR SWAA2016021649147Skin · crackedRIGHT WING AFT UPPER SKIN TE CRACKED AT RSS 237. REPAIRED SKIN IAW EA.SDR SWAA2016012248305Skin · crackedRIGHT WING INSPAR SKIN, CRACKED AT WBL 175 AT FASTENER HOLE REAR SPAR. REPAIRED SKIN IAW SRM.SDR DALA2016011900422Access Panel · corrodedCORROSION ON FUEL ACCESS DOOR COUNTERSINK/SETTLEMENT AREA NR 1361C AT LT WING. FUEL ACCESS WAS REPLACED IAW SRM 51-22-2A. ANGLE ON NEW FUEL ACCESS WAS INSTALLED IAW SRM 51-30-05.
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