Lockheed 382G
Service difficulty reports · 5,734
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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 aircraft_model_key = '382G' 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 aircraft_model_key = '382G' 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 LR7A2015031800551Rib · crackedDURING SCHEDULED C-11 CHECK UNDER JOB CARD HC5511, FOUND THE LH HORIZONTAL STABILIZER LEADING EDGE HAD A CRACKED FORMER, RIB AT FS1038, HSS256L, WL260. REPAIRED IAW SMP583 SRM FIG 51-140-20, F. NR 2276.SDR LR7A2015031800550Beam · damagedDURING SCHEDULED C-11 CHECK, WHILE PERFORMING SB 382-57-85, R2 NDI, FOUND THE RT FS 528 MLG BEAM MAIN HOLE AT WL 256 WAS OVERSIZED WHERE IT ATTACHES TO THE DRAG ANGLE FITTING, RBL 62. REPAIRED IAW LAC MEA 382-53-14-059, NR 2274.SDR LR7A2015031800549Rib · crackedDURING SCHEDULED C-11 CHECK UNDER JOB CARD HC5712, FOUND THE RT OTBD FLAP RIB HAD MULTIPLE CRACKS AT OWS0 TO FRONT SPAR WEB ATTACHMENT. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70. NR 2271.SDR LR7A2015031800548Stringer · mechanic errorDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85, R2 NDI, FOUND 3 MISDRILLED HOLES WITH DOUBLE FLUSH RIVETS PLUGGING THEM AT NR 2 DRY BAY LOWER RIB CAP AT CWS178.78L PLANK STRINGERS 17 & 18 AT DRAG FITTING ATTACHMENT, WL256. REPAIRED IAW LAC MEA 382-SDR LR7A2015031800547Stringer · mechanic errorDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85 R2 NDI, FOUND 3 MISDRILLED HOLES WITH DOUBLE FLUSH RIVETS PLUGGING THEM AT NR 3 DRY BAY LOWER RIB CAP AT CWS178.78R PLANK STRINGERS 16, 17, & 18 AT DRAG FITTING ATTACHMENT, WL256. REPAIRED IAW LAC MEA SDR LR7A2015031800546Skin · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85 R2 APPENDIX A NDI AND SP-141 NDI, FOUND 2 CRACKS EVIDENT ON THE RT CENTER WING LOWER PLANK LAYER AT FS596, CWS59R WL256 AND 1 CRACK EVIDENT ON THE RT CTR WING REAR BEAM LOWER CAP LAYER AT FS596 CWS59R. SDR LR7A2015031800545Bulkhead · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85 R2 APPENDIX A NDI AND SP-141 NDI, FOUND 3 CRACKS EVIDENT ON THE RT FS577-FS617 SIDEWALL AT FS576, FS577, & FS588, RBL61. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70. NR 2267.SDR LR7A2015031800544Bulkhead · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85 R2 APPENDIX A NDI AND SP-141 NDI, FOUND 2 CRACKS EVIDENT ON THE RT FS528-FS577 SIDEWALL AT FS528, RBL61. REPAIR BY SIDEWALL REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70. NR 2266.SDR LR7A2015031800543Beam · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85 R2 APPENDIX D NDI AND SB 382-57-86 R1, FOUND 1 CRACKED FASTENER HOLE EVIDENT ON THE RT FS517 MLG BEAM'S INBD AND OTBD CAPS COMMON TO THE ATTACH ANGLE AT CWS 62R, WL256. REPAIR BY BEAM REPLACEMENT ACCOMSDR LR7A2015031800542Skin · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85, R2 APPENDIX D NDI AND SB 382-57-86 R1, FOUND 2 CRACKS EVIDENT AT RT CENTER WING LOWER PANEL NR 1 COMMON TO THE RT ATTACH ANGLE AT FS518, CWS72R, WL256. REPAIRED IAW LAC MEA 382-57-14-053. NR 2261.SDR LR7A2015031800541Skin · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85 R2 APPENDIX D NDI AND SB 382-57-86 R1, FOUND 1 CRACK EVIDENT AT LT CENTER WING LOWER PANEL NR 1 COMMON TO THE LT ATTACH ANGLE AT FS518, CWS72L, WL256. REPAIRED IAW LAC MEA 382-57-14-052. NR 2260.SDR LR7A2015031800540Skin · crackedDURING SCHEDULED C-11 CHECK, WHILE PERFORMING SB 382-57-85, R2 APPENDIX B NDI, FOUND 1 CRACKED FASTENER HOLE EVIDENT ON RT CENTER WING LOWER NR 1 PANEL AT FS538, CWS 178R, WL 256. REPAIRED IAW LAC MEA 382-57-14-051, NR 2259.SDR LR7A2015031800539Tee Fitting · corrodedDURING SCHEDULED C-11 CHECK UNDER JOB CARD HC 2111, FOUND THE APU COMPARTMENT INTERIOR RIB CLIP HAD EXFOLIATION CORROSION AT FS 477 AND FS 491, WL 200, LBL 85. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60 AND 51-70, NR 2242.SDR LR7A2015031800538Longeron · brokenDURING SCHEDULED C-11 CHECK, FOUND THE APU COMPARTMENT LONGERON BROKEN AT FS 477, WL 200, LBL 85. REPAIRED IAW SMP 583, SRM FIG 53-40-49, NR 2241.SDR LR7A2015031800537Bulkhead · crackedDURING SCHEDULED C-11 CHECK, FOUND THE RT MAIN WHEEL WELL BULKHEAD WEB HAD CRACKED AT FS 599, WL 190, RBL 62. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60 AND 51-70, NR 2240, PSE 53-40-17, AD 2012-06-09.SDR LR7A2015031800536Structure · corrodedDURING SCHEDULED C-11 CHECK, FOUND THE LT OTBD FLAP LOWER CAP HAD EXFOLIATION CORROSION AT OWS 163L TO OWS 203L. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 CHAPTER 57-70-09, NR 2238.SDR LR7A2015031800535Panel · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85 R2, APPENDIX A NDI, FOUND 1 CRACK EVIDENT ON THE E533 SIDEWALL AT FS 528, LBL 61 WL 252, UNDER THE WING ATTACH ANGLE. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60 AND 51-70. NR 2237.SDR LR7A2015031800534Panel · crackedDURING SCHEDULED C-11 CHECK WHILE PERFORMING SB 382-57-85 R2 APPENDIX A NDI, FOUND 1 CRACK EVIDENT ON THE LT SIDEWALL AT FS 484, LBL 61, WL 252 UNDER THE WING ATTACH ANGLE. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60 AND 51-70, NR 2235.SDR LR7A2015031800533Skin · crackedDURING SCHEDULED C-11 CHECK, WHILE PERFORMING SB 382-57-85 R2 APPENDIX A NDI, FOUND THE LT CENTER WING LOWER SURFACE PANEL UNDER THE LT WING ATTACH ANGLE HAD 1 CRACK EVIDENT; FS 570, CWS 60L, WL 256. REPAIRED IAW LAC MEA 382-57-14-040, NR 2234.SDR LR7A2015031800532Skin · crackedDURING SCHEDULED C-11 CHECK, FOUND THE LT FWD FUSELAGE EXTERIOR SKIN HAD CRACKED AT THE BATTERY PANEL CUTOUT ACCESS AT THE REAR UPPER CORNER; FS 155, WL 180, LBL 55. REPAIRED IAW SMP 583, SRM FIG 51-140-12, NR 2232, PSE 53-30-08, AD 2012-06-09.SDR LR7A2015031800531Fitting · crackedDURING SCHEDULED C-11 CHECK, FOUND THE LT FS 497 BOW BEAM'S UPPER FITTING CRACKED AT WL 260, LBL 63. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60 AND 51-70, NR 2229.SDR LR7A2015031800530Longeron · corrodedDURING SCHEDULED C-11 CHECK, FOUND APU COMPARTMENT'S UPPER LONGERON HAD STRESS CORROSION BEYOND LIMITS; FS 447 TO FS 491, LBL 85, WL 180. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60 AND 51-70, NR 2226.SDR LR7A2015031800529Stiffener · crackedDURING SCHEDULED C-11 CHECK, FOUND THE FS 93 NOSE RADOME BULKHEAD STIFFENER HAD CRACKED AT RBL 27, WL 150. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583 CHAPTER 51-60 AND 51-70, NR 2203, PSE 53-30-15, AD 2012-06-09.SDR LR7A2015031800528Skin · corrodedDURING SCHEDULED C-11 CHECK, FOUND THE RT CENTER WING LOWER PLANKS HAD SURFACE CORROSION AROUND PIN RIVET HEADS AT BEHIND NR 3 ENGINE EXHAUST, ABOVE NACELLE; FS 576 TO FS 590, CWS 188R TO CWS 206R, WL 256. REPAIRED IAW LAC MEA 382-57-14-056, NR 2199.SDR LR7A2015031800527Former · crackedDURING SCHEDULED C-11 CHECK, FOUND THE RT HORIZONTAL STABILIZER L/E HAD A CRACKED FORMER AT HSS 198R, UPPER; FS 1038, WL 285. REPAIRED IAW SMP 583, SRM FIG 51-140-20, NR 2158.SDR LR7A2015031800526Former · crackedDURING SCHEDULED C-11 CHECK, UNDER JOB CARD HC 5511, FOUND THE LT HORIZONTAL STABILIZER L/E HAD A CRACKED FORMER AT HSS 140L, LOWER; FS 1038, WL 256. REPAIRED IAW SMP 583, SRM FIG 51-140-20 F, NR 2154.SDR LR7A2015031800525Former · crackedDURING SCHEDULED C-11 CHECK, FOUND FS 477 OVERHEAD BULKEAD FORWARD FACE, BULKHEAD FORMER, HAD CRACKED AT LBL26. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60 AND 51-70, NR 2118, PSE 53-40-19, AD 2012-06-09.SDR LR7A2015031800524Intercostal · damagedDURING SCHEDULED C-11 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND CARGO RAMP INTERIOR FRAME CAP, INTERCOSTAL WARPED AND CRACKED AT RS 9, LBL 25 TO RBL 25. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60 AND 51-70, NR 2112.SDR LR7A2015031800523Bulkhead Web · crackedDURING SCHEDULED C-11 CHECK, FOUND THE LT AFT FUSELAGE INTERIOR FS880 BULKHEAD WEB HAD CRACKED AT WL 200, LBL66. REPAIR BY WEB REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60, 51-70 AND 51-140-17. NR 2102.SDR LR7A2015031800522Beam · crackedDURING SCHEDULED C-11 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND FS 577 MLG BEAM INBD CAP CRACKED AT WL 260, LBL 62. REPAIR BY BEAM REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60 AND 51-70. NR 2075.SDR LR7A2015031800521Intercostal · crackedDURING SCHEDULED C-11 CHECK, FOUND CABIN INTERCOSTAL RIB CRACKED, FS 205, WL 195, LBL 59. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60 AND 51-70, NR 2049.SDR LR7A2015031800520Beam · crackedDURING SCHEDULED C-11 CHECK, FOUND THE RT UPPER MAIN WHEEL WELL FS 537 BOW BEAM HAD CRACKED AT WL 202, RBL 63. REPAIRED IAW SMP 583, SRM FIG 53-40-14, NR 2043.SDR LR7A2015031800519Plate · corrodedDURING SCHEDULED C-11 CHECK, FOUND RAMP DOOR RT CHINE PLATE HAD PITTING CORROSION AT R S0, RS 2, AND RS 10; RBL 50 TO RBL 60. REPAIR BY CHINE PLATE REPLACEMENT ACCOMPLISHED IAW SMP 583, CHAPTER 51-60 AND 51-70, NR 2035.SDR LR7A2015031800518Skin · crackedDURING SCHEDULED C-11 CHECK, FOUND RT PARATROOP DOOR INNER SKIN HAD A TWO INCH LONG CRACK AT BS 699, RBL 65, WL 165. REPAIRED IAW SMP 583, SRM FIG 51-140-12, NR 2030.SDR LR7A2015031800513Duct · crackedDURING SCHEDULED C-11 CHECK, FOUND THE APU AFT EXHAUST DUCT ASSY WAS CRACKED. REPAIRED IAW LAC MEA 382-49-15-001, NR 1057.SDR LR7A2015031800512Duct · crackedDURING SCHEDULED C-11 CHECK, FOUND THE APU FWD EXHAUST DUCT HAD MULTIPLE CRACKS. REPAIRED IAW LAC MEA 382-49-14-043, NR 1056.SDR LR7A2015020600511Wire · chafedDURING SCHEDULED FLIGHT, APU FIRE LIGHT ILLUMINATED IN FLIGHT. REPAIRED CHAFING WIRE IN APU FIRE DETECTION SYS IAW SMP 581 26-10, OPS CHECK GOOD.SDR LR7A2015020500510Former · crackedDURING SCHEDULED A-1 CHECK, UNDER JC HA120, FOUND THE RT OTBD WING FLAPWELL HAD A CRACKED FORMER. FORMER LOCATED AT OTBD FLAP. REPAIRED IAW SRM 57-60-10.SDR LR7A2015020500509Skin · puncturedDURING SCHEDULED A-1 CHECK, FOUND THE RT OTBD FLAP LOWER SURFACE WAS PUNCTURED AT FLAP STATION 141R, 35 INCHES FORWARD FROM THE T/E, AT WL256. REPAIRED IAW SRM 57-70-10.SDR LR7A2015020500508Skin · damagedDURING SCHEDULED A-1 CHECK, FOUND THE LT AILERON LOWER SKIN WAS DAMAGED. REPAIRED IAW SRM FIG 51-140-12.SDR LR7A2015020500507Skin · crackedDURING SCHEDULED A-1 CHECK, FOUND THE HORIZONTAL STABILIZER BOX STRUCTURE'S LOWER SKIN WAS CRACKED. REPAIRED IAW SRM 51-140-12.SDR LR7A2014122000506Volt Regulator · smokeDURING SCHEDULED FLIGHT, THE CREW NOTED A SMOKEY ODOR IN COCKPIT AND OBSERVED LIGHT SMOKE FROM THE NR 1 VOLTAGE REGULATOR. VOLTAGE REGULATOR STOPPED SMOKING AFTER BRIEF INTERVAL. REPLACED VOLTAGE REGULATOR AND NR 1 GENERATOR CONTROL UNIT IAW SMP 581 24-20.SDR LR7A2014121600505Plenum · crackedDURING SCHEDULED B-3 CHECK, UNDER JOB CARD HB5701, FOUND NR4 ENGINE'S LOWER AFT NACELLE PLENUM HAD CRACKED ON THE INBD SIDE; FS536, PPWL0 TO PPWL-6, PPBL8.4L TO PPBL12.5L. REPAIRED IAW MEA 382-54-14-042.SDR LR7A2014121600504Longeron · crackedDURING SCHEDULED B-3 CHECK, UNDER JOB CARD HB2703, FOUND THE DORSAL FIN'S LH FUSELAGE ATTACH ANGLE (LONGERON) HAD CRACKED; FS902, WL285, LBL12.5. REPAIRED IAW SRM FIG 51-140-22.SDR LR7A2014121600503Stiffener · crackedDURING SCHEDULED B-3 CHECK, UNDER JC HB3200, FOUND NLG BAY'S BLUKHEAD WEB STIFFENER PN 370027-83 HAD CRACKED; FS204, WL150, BL0. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70.SDR LR7A2014121600502Skin · crackedDURING SCHEDULED B-3 CHECK UNDER JC HB5301, FOUND THE RT PARATROOP DOOR SURROUND'S FORWARD LOWER CORNER HAD CRACKED; FS697, WL146, RBL61. REPAIR BY REPLACEMENT OF SKIN PANEL ACCOMPLISHED IAW LM DWG 373161 IAW SMP583 CHAPTER 51-60 AND 51-70.SDR LR7A2014121600501Skin · crackedDURING SCHEDULED B-3 CHECK UNDER JC HB5301, FOUND THE LT PARATROOP DOOR SURROUND'S FORWARD LOWER CORNER HAD CRACKED; FS697, WL146, LBL61. REPAIR BY REPLACEMENT OF SKIN PANEL ACCOMPLISHED IAW DWG 373161 IAW SMP 583, 51-60 AND 51-70.SDR CA150118001Longeron · cracked(CAN) DURRING ROUTINE B CHECK INSPECTION , CRACK WAS FOUND ON SLOPING LONGERON AT BS 869 LT SIDE. LONGERON WAS REPLACED AIRCRAFT WAS RETURNED TO SERVICE.SDR LR7A2014111700500Skin · crackedDURING SCHEDULED A CHECK, FOUND PREVIOUSLY REPORTED CRACK ON THE RT INBD L/E PROPAGATED CWS118R, BS 502.25, WL 285-287.SDR LR7A2014111700499Skin · crackedDURING SCHEDULED A CHECK, FOUND PREVIOUSLY REPORTED CRACK ON THE RT INBD L/E PROPAGATED CWS124R, FS505-FS514.5, WL285-WL287.
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