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 LR7A2013032500545Splice · crackedDURING SCHEDULED C-11 CHECK, FOUND LT UPPER MAIN WHEEL WELL BULKHEAD SPLICE AT FS 477 TO 497, LBL 62, WL 285 CRACKED. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500544Scuff Plate · corrodedDURING SCHEDULED C-11 CHECK, FOUND CARGO DOOR SCUFF PLATE HAD CORROSION FS 817E, LBL 42 TO RBL 42, WL 145.5 REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500543Strap · rustedDURING SCHEDULED C-11 CHECK, FOUND CABIN OVERHEAD FS 617 BULKHEAD UPPER FLANGE REINFORCEMENT STRAP CORRODED AND HOLE WITHOUT SUFFICIENT EDGE DISTANCE. RBL 26 TO 61. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500542Strap · corrodedDURING SCHEDULED C-11 CHECK, FOUND CABIN OVERHEAD FS 617 BULKHEAD UPPER FLANGE REINFORCEMENT STRAP CORRODED AND HOLE WITHOUT SUFFICIENT EDGE DISTANCE. LBL 26 TO LBL 61. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500541Riser · cutDURING SCHEDULED C-11 CHECK, FOUND LT OTBD WING LOWER PLANK KINGPIN RISER HAD MULTIPLE DEEP CUTS. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500540Fitting · damagedDURING SCHEDULED C-11 CHECK, DURING VISUAL INSPECTION, FOUND RT ATTACH ANGLE DAMAGED AT FS 617, RBL 61.625 AND WL 258.54. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500539Fitting · crackedDURING SCHEDULED C-11 CHECK, FOUND RT FS 477 RBL 61, WL 258 FITTING FASTENER HOLE CRACKED. REPAIRED IAW SMP583, 51-60 AND 51-70.SDR LR7A2013032500538Former · damagedDURING SCHEDULED C-11 CHECK, FOUND RT HORIZONTAL STABILIZER L/E INTERIOR FORMER HAD MULTIPLE FASTENER HOLES OVERSIZED AT HSS 90. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500537Bulkhead · bentDURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL INBD HINGE BULKHEAD WEB BENT, FS 507 TO 607, WL 132 TO 138, RBL 61. REPAIRED IAW SMP583, 51-60 AND 51-70.SDR LR7A2013032500536Stiffener · crackedDURING SCHEDULED C-11 CHECK, FOUND CARGO DOOR REAR BULKHEAD STIFFENER HAD .3750 INCH LONG CRACK AT RBL 26. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500535Bulkhead · crackedDURING SCHEDULED C-11 CHECK, FOUND CABIN FS 497 BULKHEAD REPAIR ANGLE HAD CRACKED; WL 262, LBL 58. REPAIRED IAW SMP583 SRM FIG 53-40-36.SDR LR7A2013032500534Former · elongatedDURING SCHEDULED C-11 CHECK, FOUND CENTER WING-TO-FUSELAGE AFT FAIRING FORMERS HAD ELONGATED FASTENER HOLES FS 597 TO 617, LBL 18, WL 285. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500533Former · damagedDURING SCHEDULED C-11 CHECK, FOUND CENTER WING-TO-FUSELAGE AFT FAIRING FORMERS HAD ELONGATED FASTENER HOLES FS 597 TO 617, LBL 22, WL 285. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500532Stiffener · crackedDURING SCHEDULED C-11 CHECK, FOUND FOUR CENTER WING-TO-FUSELAGE FAIRING STIFFENERS HAD CRACKED WITH ELONGATED FASTENER HOLES FS 497 TO 517, LBL 50 TO RBL 50, WL 285. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500531Stiffener · damagedDURING SCHEDULED C-11 CHECK, FOUND CENTER WING-TO-FUSELAGE FAIRING STIFFENERS CRACKED AND HOLES ELONGATED AT FS 497 TO 517, LBL 22, WL 285. REPAIRED IAW SMP 583 51-60 AND 51-70.SDR LR7A2013032500530Longeron · corrodedDURING SCHEDULED C-11 CHECK, FOUND FUSELAGE RT UPPER LONGERON HAD STRESS CORROSION AT FS 470 TO 476, RBL 60, WL 258 AT BAR FITTING ATTACHMENT. REPAIRED IAW SMP583, 51-60 AND 51-70.SDR LR7A2013032500529Longeron · corrodedDURING SCHEDULED C-11 CHECK, FOUND CABIN FS 617 TO 622 RT FUSELAGE LONGERON EXFOLIATED AT BL 60 BAR FITTING ATTACHMENT AT WL 250. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500528Fitting · corrodedDURING SCHEDULED C-11 CHECK, FOUND CARGO FLOORBEAM END FITTING HAD CORROSION AT FS 357, WL 142. REPAIRED IAW SMP583, 51-60 AND 51-70.SDR LR7A2013032500526Longeron · corrodedDURING SCHEDULED C-11 CHECK, FOUND LT LONGERON HAD CORROSION IN HOLES; FS 617 LBL 61 WL 260. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500525Longeron · crackedDURING SCHEDULED C-11 CHECK, FOUND LT FS 477, B L61 LONGERON HAD CRACKED; WL 260. REPAIRED IAW MEA 382-53-12-097.SDR LR7A2013032500524Doubler · corrodedDURING SCHEDULED C-11 CHECK, FOUND CABIN LT FRAME SEGMENT HAD CORROSION ON REINFORCEMENT DOUBLER AT FS 357, WL 142, LBL 61. REPAIRED IAW SMP583 51-60 & 51-70.SDR LR7A2013032500523Attach Angle · crackedDURING SCHEDULED C-11 CHECK, FOUND FUSELAGE ATTACH ANGLE HAD CRACKED FS 476, RBL 24 TO 62, WL 260 TO 280. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500521Skin · damagedDURING SCHEDULED C-11 CHECK, FOUND LT UPPER FUSELAGE SKIN HAD MULTIPLE EXCESS HOLES FOR FAIRING ATTACHMENT FS 446 TO 460, WL 282. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500519Bulkhead · damagedDURING SCHEDULED C-11 CHECK, FOUND CABIN LT BULKHEAD DAMAGED FS 477, LBL 20 TO LBL 61.5, WL258 TO WL270. REPAIRD IAW SMP583, 51-60 AND 51-70.SDR LR7A2013032500517Angle · crackedDURING SCHEDULED C-11, CHECK, FOUND AFT RT FUSELAGE UPPER L ANGLE CRACKED FS 1023, RBL 61, WL 270. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500516Channel · crackedDURING SCHEDULED C-11 CHECK, FOUND LT AFT FUSELAGE BULKHEAD CHANNEL UPPER FLANGE HAD A TWO INCH CRACK AT FS 1023, LBL 50, WL 285. REPAIRED IAW SMP583, SRM FIG 53-50-07.SDR LR7A2013032500515Tee Fitting · crackedDURING SCHEDULED C-11, FOUND RT AFT FUSELAGE FS935 BULKHEAD-TO-SLOPING LONGERON ATTACH TEE CRACKED FS 935, RBL 61, WL 250. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500514Splice · corrodedDURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL UPPER SPLICE HAD CORROSION FS 589 TO 597, W L250, AND RBL 61. REPAIRED IAW SMP583, CHAPTER 51-60 AND 51-70.SDR LR7A2013032500513Bulkhead · damagedDURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL REAR BULKHEAD HAD MULTIPLE MISDRILLED HOLES WITH INCORRECT METAL FS 617, WL 195 TO 220, RBL 61 TO 85. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500512Beam · corrodedDURING SCHEDULED C-11 CHECK, FOUND LT MAIN WHEEL WELL BEAM HAD STRESS CORROSION FS 588, WL 168, LBL 62. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500511Beam · corrodedDURING SCHEDULED C-11 CHECK, FOUND LT MAIN WHEEL WELL BEAM HAD STRESS CORROSION FS 588, WL 168, LBL 62, REPAIRED IAW SMP583, 51-60 AND 51-70.SDR LR7A2013032500510Post · crackedDURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD WEB INSPECTION WINDOW POST CRACKED AT FS 586, WL 185, RBL 61.5. REPAIRED IAW SMP583, 51-60 AND 51-70.SDR LR7A2013032500509Frame · crackedDURING SCHEDULED C-11 CHECK, FOUND CABIN OVERHEAD FRAME CRACKED AT FS 617, RBL 20, WL 285. REPAIRED IAW SMP583, 51-60 AND 51-70.SDR LR7A2013032500508Frame · crackedDURING SCHEDULED C-11 CHECK, FOUND CABIN OVERHEAD FRAME SPLICE CRACKED AT FS 477, RBL 20, WL 286. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500506Angle · crackedDURING SCHEDULED C-11 CHECK, FOUND LT HORIZONTAL STABILIZER L/E FRAME ANGLE CRACKED LT SIDE FS 1041, WL 283: HSS 115, HSS 186, AND HSS 198. REPAIRED IAW SMP583 SRM FIG 51-140-20.SDR LR7A2013032500505Bulkhead · corrodedDURING SCHEDULED C-11 CHECK, FOUND RT MAIN WHEEL WELL BULKHEAD WEB CORRODED FS 530 AND 575, WL 145 TO 146. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500504Bulkhead · damagedDURING SCHEDULED C-11 CHECK, FOUND CABIN BULKHEAD WEB HAD MULTIPLE OVERSIZED FASTENER HOLES. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500503Bulkhead · misrepairedDURING SCHEDULED C-11 CHECK, FOUND LEFT UPPER MAIN WHEEL WELL BULKHEAD WEB HAD MISALIGNMENT WITH THE NEWLY INSTALLED DRAG ANGLE FITTING FS 477 TO 617, WL 250 TO 270, BL 61.5. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500502Bulkhead · corrodedDURING SCHEDULED C-11 CHECK, FOUND NOSE WHEEL WELL REAR BULKHEAD HAD CORROSION AROUND THE INSPECTION WINDOW; FS 210, WL 148, LT AND RT. REPAIRED IAW SMP583 SRM 51-60 AND 51-70.SDR LR7A2013032500501Rib · warpedDURING SCHEDULED C-11 CHECK,, FOUND NOSE WHEEL WELL RIB WARPED AT FS 97, WL 166. REPAIRED IAW SMP583, SRM 51-60 AND 51-70.SDR LR7A2013032500500Frame · damagedDURING SCHEDULED C-11 CHECK, FOUND RT FUSELAGE RING SEGMENT HAD MULTIPLE MISDRILLED HOLES AND SURFACE CORROSION FS 351, WL 140-260. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500498Plate · corrodedDURING SCHEDULED C-11 CHECK, FOUND AFT FS 770 LT BULKHEAD-TO-SLOPING LONGERON GUSSET PLATE HAD CORROSION AND BOLT HOLE ELONGATED. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500497Skin · crackedDURING SCHEDULED C-11 CHECK, FOUND LT AFT FUSELAGE SKIN CRACKED FS 910, WL 200. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500496Skin · warpedDURING SCHEDULED C-11 CHECK , FOUND LT AFT FUSELAGE EXTERIOR SKIN WARPED FS 869 TO 902, WL 180 TO WL 220. REPAIRED IAW SMP583 SRM 51-60 AND 51-70.SDR LR7A2013032500495Stiffener · crackedDURING SCHEDULED C-11 CHECK UNDER JOB CARD HC5315, FOUND CARGO RAMP FLOORBOARD STIFFENER HAD A 20 INCH LONG CRACK. REPAIRED IAW SMP583 51-60 AND 51-70.SDR LR7A2013032500494Structure · crackedDURING SCHEDULED C-11 CHECK, FOUND CARGO RAMP INTERIOR BULKHEAD LOWER CAP CRACKED. REPAIRED IAW SMP583 SRM FIG 51-140-23.SDR LR7A2013032500493Skin · warpedDURING SCHEDULED C-11 CHECK, FOUND LT FUSELAGE SKIN WARPED FS 737E TO 777E, WL 140 TO WL 200. REPAIRED IAW SMP583 SRM 51-60 AND 51-70.SDR LR7A2013032500489Strap · elongatedDURING SCHEDULED C-11 CHECK, FOUND CABIN OVERHEAD BULKHEAD STRAP RUSTED AND MULTIPLE HOLES ELONGATED AT PRESSURE FAIRING ATTACHMENT, FS 477, LBL 20 TO LBL 60. REPAIRED IAW SMP583, 51-60 AND 51-70.SDR LR7A2013032500488Longeron · crackedDURING SCHEDULED C-11, FOUND NR 2 ENGINE RT LOWER HORIZONTAL QEC LONGERON HAD ONE CRACK AT FWD END LORD MOUNT ALIGNMENT HOLE. REPAIRED IAW SMP583, 51-60 AND 51-70.SDR LR7A2013032500487Frame · crackedDURING SCHEDULED C-11 CHECK, FOUND RT FS 528, BL 61, WL 258 SIDEWALL MAIN FRAME HOLE HAD TWO CRACKS AT 4 & 5 O'CLOCK POSITION RESPECTIVELY. REPAIRED IAW MEA 382-53-12-096.
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