Lockheed 382G
Service difficulty reports · 5,734
Newest first. General aviation reporting is voluntary.
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 LR7A2015080300603Angle · corrodedDURING SCHEDULED C-2 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CARGO DOOR FWD LOWER ANGLE, CAP, CORRODED BEYOND LIMITS. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CHAPTER 51-60 & 51-70.SDR LR7A2015080300602Stiffener · crackedDURING SCHEDULED C-2 CHECK, FOUND RAMP DOOR LT LOWER STIFFENER HAD 2" LONG CRACK. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, SRM, CHAPTER 51-60 & 51-70.SDR LR7A2015080300601Rib · crackedDURING SCHEDULED C-2, FOUND THE HORIZONTAL STABILIZER LT L/E HAD CRACKED REINFORCEMENT RIBS AT HSS146L, FS1041. REPAIR BY REPLACEMENT, ACCOMPLISHED IAW SMP583, SRM, CHAPTER 51-60 & 51-70 AND FIG 55-20-04.SDR LR7A2015080300600Skin · corrodedDURING SCHEDULED C-2 CHECK, FOUND THE LT INBD WING LOWER NR 2 AND NR 3 PLANK AREAS HAD PITTING CORROSION BEHIND NR 2 ENGINE EXHAUST AREA. REPAIRED IAW LAC MEA 382-57-15-034.SDR LR7A2015080300599Skin · crackedDURING SCHEDULED C-2 CHECK, FOUND THE LT OTBD FLAP LOWER L/E SKIN HAD A ONE INCH LONG CRACK AT OWS 238. REPAIRED IAW SMP583, SRM FIG. 51-140-12.SDR LR7A2015080300598Seat Track · elongatedDURING SCHEDULED C-2 CHECK, FOUND THE CO-PILOT'S SEAT TRACK LT AND RT POSITION HOLES ELONGATED. REPAIRED IAW LAC MEA 382-53-99-164(R3).SDR LR7A2015080300597Seat Track · damagedDURING SCHEDULED C-2 CHECK, FOUND THE PILOT'S SEAT TRACK LT AND RT POSITION HOLES ELONGATED. REPAIRED IAW LAC MEA 382-53-99-164(R3).SDR LR7A2015080300596Bulkhead · crackedDURING SCHEDULED C-2 CHECK, FOUND THE AFT FUSELAGE BS 836 LT SIDE BULKHEAD OTBD FLANGE CRACKED AT WL175, LBL72. REPAIRED IAW SMP583, SRM FIG 51-140-19.SDR LR7A2015062700595Skin · corrodedDURING SCHEDULED B-2 CHECK, FOUND HORIZONTAL STABILZER LOWER SKIN CRACKED & CORRODED. REPAIRED IAW SRM 51-60 & 51-70, AND DWG 370247.SDR LR7A2015062700594Skin · corrodedDURING SCHEDULED B-2 CHECK, FOUND HORIZONTAL STABILZER LOWER SKIN FS1066, RBL36 HAD CRACK & CORROSION. REPAIRED IAW SRM, 51-60 & 51-70, AND DWG 370372.SDR LR7A2015062700593Strap · corrodedDURING SCHEDULED B-2 CHECK UNDER FOUND BELT FRAME STRAP CORRODED AT BS 200 - 236, LBL 60 AT FORWARD LOWER CORNER OF ENTRY DOORWAY. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM 51-70.SDR LR7A2015062700592Web · wornDURING SCHEDULED B-2 CHECK UNDER JC HB5302, FOUND THE CARGO DOOR WEB WORN THROUGH AT STA 1, FS 880, LBL 33. REPAIR BY WEB REPLACEMENT ACCOMPLISHED IAW SRM 51-60 & 51-70, AND DWG 342582.SDR LR7A2015062700591Bulkhead Web · crackedDURING SCHEDULED B-2 CHECK, FOUND FS 924 BULKHEAD WEB CRACKED, RBL 62, WL 254. REPAIR BY WEB REPLACEMENT ACCOMPLISHED IAW SMP 583, SRM 51-60 & 51-70, AND DWG 359091. NR N-14, WO 1391418.SDR LR7A2015062700590Bulkhead Web · crackedDURING SCHEDULED B-2 CHECK, FOUND CARGO DOOR BS 4 BULKHEAD WEB HAD 3 CRACKS AT FS 946, LBL 30 TO LBL 37. REPAIR BY WEB REPLACEMENT ACCOMPLISHED IAW SMP583 SRM 51-60 & 51-70, AND DWG 372552.SDR LR7A2015062700589Bulkhead · crackedDURING SCHEDULED B-2 CHECK, FOUND BS 880 RT SIDE BULKHEAD INBD CAP CRACKED, RBL 62, WL 199. REPAIRED IAW SRM FIG 53-50-17.SDR LR7A2015060100588Apu · malfunctionedWITH APU NOT OPERATING, NORMAL FLIGHT OPERATIONS, APU FIRE WARNING LIGHT WOULD INTERMITTENTLY COME ON DURING FLIGHT.SDR LR7A2015051200587Skin · corrodedDURING SCHEDULED C-12 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND THE HORIZONTAL STABILZER LOWER SKIN INNER DOUBLER AT FS 1067, LBL 61 - RBL 61, WL 256 HAD EXFOLIATION CORROSION. REPAIRED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200586Intercostal · crackedDURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RAMP DOOR'S LOWER INTERCOSTAL BEAM ASSY CRACKED AT RAMP FS 6, RBL2. REPAIR BY BEAM & WEB DOULBER REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CHAPTER 51-60 AND 51-70.SDR LR7A2015051200585Bulkhead · crackedDURING SCHEDULED C-12 CHECK, FOUND THE CARGO BAY RT FS 497, BULKHEAD CRACKED, WL 260, RBL 55. REPAIRED IAW SRM 53-40-37.SDR LR7A2015051200584Former · corrodedDURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND LT MAIN WHEELWELL AFT FAIRING INNER RIB, FORMER, CORRODED AND MULTIPLE ELONGATED HOLES AT FS 617, LBL 48 - 74. REPAIRED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200583Stiffener · corrodedDURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE LT MAIN WHEEL WELL AFT FAIRING FOR BS 617 LOWER CAP ACCESS HAD INNER TWO STIFFENERS, WITH PITTING CORROSION0. REPAIRED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200582Skin · chafedDURING SCHEDULED C-12 CHECK, FOUND THE HORIZONTAL STABILIZER'S LT & RT L/E SKINS HAD DEEP CHAFED. REPAIRED SKIN IAW SRM 51-60 AND 51-70.SDR LR7A2015051200581Skin · corrodedDURING SCHEDULED C-12 CHECK, FOUND THE HORIZONTAL STABILZER LOWER FORWARD SKIN INNER DOUBLER HAD EXFOLIATION CORROSION. REPAIR IAW SRM 51-60 AND 51-70.SDR LR7A2015051200580Window Frame · crackedDURING SCHEDULED C-12 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND THE RT WINDOW POST, FRAME AT FS 105, WL 253 WAS CRACKED. REPAIR BY INTERIOR WINDOW POST REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200579Skin · corrodedDURING SCHEDULED C-12 CHECK, FOUND THE HORIZONTAL STABILIZER LOWER SKIN'S INNER SKIN DOUBLER HAD AREAS OF DEEP PITTING CORROSION. REPAIR BY INNER SKIN REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200578Skin · corrodedDURING SCHEDULED C-12 CHECK, FOUND THE HORIZONTAL STABILIZER LOWER SKIN HAD AREAS OF CORROSION. REPAIR BY SKIN REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200577Skin · corrodedDURING SCHEDULED C-12 CHECK, FOUND THE HORIZONTAL STABILIZER LOWER SKIN HAD AREAS OF EXFOLIATION CORROSION; FS1066 TO FS1095, LBL61 TO RBL61, WL256. REPAIR BY SKIN REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200576Bulkhead · corrodedDURING SCHEDULED C-12 CHECK, FOUND THE LT MAIN WHEEL WELL INBD BULKHEAD HAD EXFOLIATION CORROSION AT TEE SPLICE BS 528 - 537, WL 175, LBL 62. REPAIR BY TEE SPLICER REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200575Stiffener · crackedDURING SCHEDULED C-12 CHECK, UNDER JC HC5511, FOUND THE HORIZONTAL STABILIZER LOWER SKIN'S INTERIOR STIFFENERS CRACKED, QTY 3 EA AT FS1093; LBL10, BL0, & RBL10; WL256. REPAIR BY STIFFENER REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200574Pressure Blkhd · corrodedDURING SCHEDULED C-12 CHECK, FOUND THE LT MAIN WHEEL WELL INBD BULKHEAD, PRESSURE WEB, HAD CORROSION AT FS 537, WL 185 - 195, RBL 82. REPLACEMED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200573Intercostal · corrodedDURING SCHEDULED C-12 CHECK, FOUND THE LT MAIN WHEEL WELL FS 557 - 577 INTERCOSTAL TEE CAP HAD CORROSION AT WL 158 AND WL 175, LBL 62. REPLACED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200572Intercostal · corrodedDURING SCHEDULED C-12 CHECK, FOUND THE LT MAIN WHEEL WELL FS 588 - 597 INTERCOSTAL BEAM WEB, OTBD CAP HAD CORROSION LBL 62, WL 175. WEB REPLACEMED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200571Skin · corrodedDURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR FWD L/E SKIN HAD EXFOLIATION CORROSION AT RAMP FS 0, LBL 28 TO RBL 28. SKIN REPLACED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200570Intercostal · crackedDURING SCHEDULED C-12 CHECK, FOUND THE RAMP DOOR INTERIOR RS6 TO RS8, LBL 3 TO RBL 3 UPPER INTERCOSTAL BEAM WEB HAD 1.5 INCH LONG CRACK. REPLACEMED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200569Skin · chafedDURING SCHEDULED C-12 CHECK, FOUND THE RT INBD FLAP L/E SKIN HAD DEEP CHAFING AT CWS 86R. REPAIRED IAW SRM 57-70-10.SDR LR7A2015051200568Floorbeam · corrodedDURING SCHEDULED C-12 CHECK, FOUND THE BS 657 FLOORBEAM LOWER CAP HAD CORROSION AT LBL 20, WL 140. REPLACED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200567Gusset · crackedDURING SCHEDULED C-12 CHECK, FOUND THE LT AFT FUSELAGE BS 946 GUSSET BUTTERFLY FITTING WAS CRACKED; LBL 53 - 66, WL 264 - 276. GUSSET FITTING REPLACED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200566Bulkhead Web · crackedDURING SCHEDULED C-12 CHECK, FOUND LT UPPER MAIN WHEEL WELL FS 477 PRESSURE BULKHEAD WEB CRACKED AT WL 235, LBL 77. BULKHEAD WEB REPLACED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200565Cap · corrodedDURING SCHEDULED C-12, FOUND FS 617 UNDERFLOOR BULKHEAD LOWER CAP HAD CORROSION AT RBL 32, WL 140. CAP REPLACED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200564Fitting · crackedDURING SCHEDULED C-12 CHECK, FOUND FS 577 LT PORK CHOP FITTING CRACKED, WL 142 LBL 61. FITTING REPLACED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200563Bulkhead Web · crackedDURING SCHEDULED C-12, CHECK, FOUND THE RT UPPER MAIN WHEEL WELL FS 477, BULKHEAD WEB HAD CRACKED AT RBL 77, WL 235. REPAIR BY PRESSURE WEB REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200562Stiffener · crackedDURING SCHEDULED C-12 CHECK UNDER JC HC5321, FOUND THE FS 93 BULKHEAD LOWER STIFFENER HAD CRACKED AT LBL 20 AND RBL 20, WL 150. REPAIR BY STIFFENER REPLACEMENT ACCOMPLISHED IAW SRM 51-60 AND 51-70.SDR LR7A2015051200561Stiffener · crackedDURING SCHEDULED C-12, AFTER REMOVING THE RAMP DOOR PEDESTAL FAIRING FOR ACCESS, FOUND CRACKED STIFFENER AT RAMP FS 9, RBL12. REPAIR BY STIFFENER REPLACEMENT ACCOMPLISHED IAW SMP 583 SRM, CHAPTER 51-60 AND 51-70. NR 2022.SDR LR7A2015051200560Manifold · crackedDURING SCHEDULED C-12 CHECK, FOUND THE RT MAIN WHEEL WELL MANIFOLD WAS CRACKED AT FS 567, RBL 62, WL 146. REPLACED THE MANIFOLD IAW SRM 51-60 AND 51-70.SDR LR7A2015051200559Bulkhead Web · crackedDURING SCHEDULED C-12 CHECK UNDER JC HC5315, FOUND THE AFT FUSELAGE FS 880 RT INTERIOR BULKHEAD WAS CRACKED AT WL 190, RBL 65. REPAIRED IAW SRM 51-140-17.SDR LR7A2015031800556Floorbeam · unknownDURING SCHEDULED C-11 CHECK, WHILE PERFORMING OTHER MAINTENANCE, FOUND CABIN FS637 FLOORBEAM WEB LBL18 TO RBL18, WL140 HAD MULITPLE ACCESS HOLES. REPAIRED BY REPLACEMENT, ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70. NR 2292.SDR LR7A2015031800555Spar · crackedDURING SCHEDULED C-11 CHECK, WHILE PERFORMING SB 382-57-85, R2 APPENDIX D NDI AND SB 382-57-86 R1, FOUND THE RT CENTER WING FRONT SPAR, WEB AT CWS58R, WL256-WL275, FS517 BEAM ATTACHMENT AREA HAD 6 CRACKS EVIDENT. REPAIRED IAW LAC MEA 382-57-15-005. NR 2291.SDR LR7A2015031800554Floorbeam · corrodedDURING SCHEDULED C-11 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND CABIN FS597 FLOORBEAM UPPER CAP HAD EXFOLIATION CORROSION AT LBL1 TO RBL1 TIEDOWN POINT. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70. NR 2290.SDR LR7A2015031800553Brace · crackedDURING SCHEDULED C-11 CHECK UNDER JOB CARD HC5712, FOUND NR 4 DRY BAY BRACE ASSY AT OWS197R HAD CRACKED. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583, CHAPTER 51-60 AND 51-70. NR 2288.SDR LR7A2015031800552Rib · crackedDURING SCHEDULED C-11, CHECK UNDER JOB CARD HC5511, FOUND THE LT HORIZONTAL STABILIZER L/E HAD A CRACKED FORMER, RIB AT FS1038, HSS267.5L, WL260. REPAIRED IAW SMP583 SRM FIG 51-140-20 F. NR 2277.
Back to Lockheed 382G