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 LR7A99106Web · dentedDURING C CHECK/BRIDGING INSPECTION PER HSP57108, FOUND RMLG FS 583 ACCESS PANEL OPENING DENTED BEYOND LIMITS AT WL 155. REPAIRED IAW SMP 583 51-140-17.SDR LR7A99105Press Panel · dentedDURING C CHECK/BRIDGING INSPECTION PER HC3208, FOUND RMLG FS 593 SIDE PRESSURE PANEL DENTED BEYOND LIMITS AT WL 150. REPLACED PANEL IAW SMP 583-51-70 AND DWG 3311015. NR 360.SDR LR7A99104Longeron · corrodedDURING C CHECK/BRIDGING INSPECTION PER HSP7180 FOUND NR 3 QEC RT UPPER SLOPING LONGERON CORRODED. REPLACED LONGERON IAW SRM 583-54-20-08 AND SB 382-71-12, REV 92. NR 349 AND 959.SDR LR7A99103Fitting · crackedDURING C CHECK/BRIDGING INSPECTION PER HST5302, FOUND FS 617 BULKHEAD SIDE SUPPORT FITTING CRACKED AT RBL 61. REPLACED FITTING IAW SMP 583-51-70, NR 350.SDR LR7A99102Fitting · crackedDURING C CHECK/BRIDGING INSPECTION PER HSP5297, FOUND FS 617 RT AND FS 717 RT 25K TIE DOWN END FITTINGS CRACKED. REPLACED FITTINGS IAW SMP 583-51-70. NR 323.SDR LR7A9910Bulkhead · damagedDURING C CHECK BRIDGING INSPECTION, FOUND FS 617 LT AFT MLG BULKHEAD ASSY DAMAGED BEYOND 2.5 IN LIMIT AT BL 61.62L, WL 200. REPLACED BULKHEAD ASSY IAW SPAR MPP L100-404-99-009. LAC MEA 382-53-99-011.SDR LR7A9909Bulkhead · damagedDURING C CHECK BRIDGING INSPECTION, FOUND FS 617 RT AFT MLG BULKHEAD ASSY DAMAGED BEYOND 2.5 IN LIMIT AT BL 61.62R, WL 200. REPLACED BULKHEAD ASSY IAW SPAR MPP L100-404-99-008. LAC MEA 382-53-99-010.SDR LR7A9908Frame · corrodedDURING C CHECK BRIDGING INSPECTION, FOUND CENTER FUSELAGE RT FS 297 RING SEGMENT CORRODED FROM WL 166 - 190. REPAIRED IAW SPAR MPP L100-404-99-005. LAC MEA 382-53-99-007.SDR LR7A9907Channel · crackedDURING C CHECK BRIDGING INSPECTION, FOUND NR 2 UPPER AFT NACELLE LOWER LT CHANNEL CRACKED AT FS 512.64, PP WL -5.38. REPAIRED BY INSTALLING REPAIR DOUBLER IAW SPAR MPP L100-404-99-004. LAC MEA 382-53-99-006.SDR LR7A9906Beam · crackedDURING C CHECK BRIDGING INSPECTION, FOUND FS 528 RT MLG BEAM, INNER BEAM CRACKED AT BL62R, WL 256. REPAIRED BY CUTTING OUT CRACK AND INSTALL FILLER, STRAPS AND ANGLES IAW SPAR MPP L100-404-99-001. LAC MEA 382-53-99-004.SDR AU990416025Bolt · wrong part(AU) PART STSBG013-1 HEX HEAD BOLT FOUND INSTALLED IN THE REAR ENGINE MOUNT. THE BOLT HAD BEEN SUBSTANTIALLY GROUND DOWN OF MATERIAL AFT OF THE THREAD AREA. THE GRINDING HAD BEEN PERFORMED BY A ROTARY DISK AND WAS NOT UNIFORM ON THE CIRCUMFERENCE. PART NR 3SDR LR7A9982Web · crackedDURING SCHEDULED C1 INSPECTION PER HC2704, FOUND FWD CENTER WING WEB CRACKED 1.25 INCH AT RBL 20 RADIATING FROM FASTENER HOLE UNDER SUPPORT FITTING. REPAIRED PER MPP 401-1999-L100-57-107.SDR LR7A9981Floorbeam · corrodedDURING SCHEDULED C1 INSPECTION PER HSP53161, FOUND FS 257 FLOORBEAM CAP CORRODED AROUND ANCHOR NUT LOCATION AT WL 146, RBL 43. REPLACED FLOORBEAM CAP IAW SMP 583-53-40-01.SDR LR7A9987Angle · crackedDURING SCHEDULED C1 INSPECTION PER HC5303, FOUND FS 817 CHINE CRACKED AT WL 146, LBL 60. REPAIRED IAW SRM SMP 583-53-40-26/27.SDR LR7A9986Fitting · crackedDURING SCHEDULED C1 INSPECTION PER HSP71189, FOUND NR 4 ENGINE SUPPORT FITTING CRACKED. REPLACED FITTING IAW SRM SMP 583-54-20-10 USING P/N 3331795-3.SDR LR7A9985Fitting · crackedDURING SCHEDULED C1 INSPECTION PER HSP71189, FOUND NR 2 ENGINE SUPPORT FITTING CRACKED. REPLACED FITTING PER SRM 583-54-20-10 USING P/N 3331795-3.SDR LR7A9984Angle · crackedDURING SCHEDULED C1 INSPECTION PER HSP53224 (SP-224), FOUND FS 490 UPPER PRESSURE FAIRING CAP ANGLE CRACKED AT LBL 61. REPAIRED IAW SRM SMP 583-53-40-35B.SDR LR7A9983Angle · crackedDURING SCHEDULED C1 INSPECTION PER HSP53224 (SP-224), FOUND FS 490 UPPER PRESSURE FAIRING CAP ANGLE CRACKED AT RBL 61. REPAIRED IAW SRM SMP 583-53-40-35B.SDR LR7A9980Fitting · crackedDURING SCHEDULED C1 INSPECTION PER HSP5372 (SP-72), FOUND FS 617 RT STRUT SUPPORT FITTING CRACKED AT WL 150. REPLACED FITTING IAW SRM SMP 583-53-40-01 AND DWG 339394-3.SDR LR7A9979Fitting · crackedDURING SCHEDULED C1 INSPECTION PER HSP53224 (SP-224), FOUND FS 477 UPPER BULKHEAD SPLICE CRACKED AT RBL 20. REPLACED PER DWG 340043-12.SDR LR7A9978Channel · crackedDURING SCHEDULED C1 INSPECTION PER HSP53224 (SP-224), FOUND FS 477 C CHANNEL CRACKED AT RBL 25. REPLACED CHANNEL PER DWG 340043.SDR LR7A9905Fitting · crackedBUTTERFLY FITTING CRACKED LT FS 946. REPLACED FITTING IAW SRM 51-10.SDR LR7A9904Fitting · crackedFS 990 RT CRACKED TEE (P/N 353042-8R), WEB CRACKED, FS 990 LT FITTING CRACKED (P/N 353059-8). REMOVED AND REPLACED FITTINGS, TEE AND WEB IAW HERC SRM CH51-10 PG 4.SDR LR7A9903Fitting · crackedCRACKED FITTINGS AT STA 990 BOTH LT AND RT SIDE. REPLACED FITTINGS IAW SMP 583 51-10. (P/N 353059-4L,-4R, 353042-8L).SDR LR7A9902Speed Control · failedON TAKEOFF, NR 2 ENGINE WOULD NOT EXCEED 830 DEG TIT, SELECTED NULL AND PULLED IGNITION CONTROL CB ENGINE TIT STAYED AT 830 DEG. TIT, SHUTDOWN ENGINE AT 1226Z. RETURNED TO DEPARTURE AIRPORT. REMOVED AND REPLACED NR 2 SPEEDSENSE CONTROL IAW ALLISON 501 D22 MMSDR LR7A9901Cable · out of adjREJECTED T/O, DOOR WARNING LIGHT CAME ON DURING ROLL, ADJUSTED CARGO DOOR DOWN LOCK CABLES IAW SMP 58152-30 PAGE 206.SDR LR7A9848Fitting · crackedFS 345E LT END FITTING CRACKED IN THE RADIUS 0.3 INCH LENGTH. REPAIRED PER MAINT PRODUCTION PERMIT L100-401-98-010 AND COTNEY COMPANY DOC NR F68 REV1R DATED 11/6/98.SDR LR7A9847Fitting · crackedFS 858 RT FITTING CRACKED. REPLACED FITTING PER SMP583-53-50.SDR LR7A9846Web · crackedFS 990 RT WEB CRACKED. REPLACED WEB IAW SMP583-53-50.SDR LR7A9845Fitting · crackedFS 990 RT ATTACH FITTING CRACKED. REPLACED FITTING IAW SMP 583 53-50.SDR LR7A9844Fitting · corrodedRT FWD STA 737 (817E) FITTING HAS STRESS CORROSION BEYOND LIMITS. REPLACED END FITTING PER SMP 583 53-50-4 AND SMP 52-30.SDR LR7A9843Fitting · corrodedRT FWD STA 737 (817E) END FITTING CORRODED BEYOND LIMITS. REPLACED END FITTING PER SMP 583 53-10-10.SDR LR7A9842Stringer · crackedINNER CAP (P/N 342582-24R) WAS DISCOVERED CRACKED DURING MAINTENANCE. CRACK WAS .15 INCH LENGTH AT WL 203 FS 880 RT BL 63R. REPAIRED PER MAINT PRODUCTION PERMIT L100-401-98-008 COTNEY DOC NR F68 REV 1R DATED 11/6/98.SDR LR7A9841Fitting · crackedDURING ROUTINE MAINT, THE LT OWS 241 FLAP TRACK ATTACH FITTING WAS DISCOVERED CRACKED. REMOVED AND REPLACED FITTING IAW SMP 583 51-10 PARA G, AND 57-10-04.SDR LR7A9839Longeron · crackedDUE TO CRACKED SLOPING LONGERON DOUBLER RT FS 858. ONE TIME FERRY UNPRESSURIZED FERRY AUTHORIZED IAW COTNEY EDF 60-1.SDR LR7A9838Web · crackedRT GEAR WELL AFT PRESSURE WEB AT STA 617 HAS CRACKS ON THREE RISERS. REPAIRED IN ACCORDANCE WITH ED NR EDF49-1.SDR LR7A9836Seal · failedNR 2 ENG SHUTDOWN IN FLIGHT DUE TO OIL LOSS STARTER GARLOC SEAL LEAKING. REPLACED STARTER GARLOC SEAL IAW 501-D22 MM 72-0 PG 221. REPLACED SCAVANGE OIL FILTER IAW 501-D22 72-2-5 DUE TO PIN BEING POPPED (BYPASS).SDR LR7A9834Clamp · looseCARGO COMPARTMENT REFRIG OVERHEAT LIGHT CAME ON IN CLIMBOUT. SWITCHED CARGO COMPARTMENT AIR CONDITION SHUT OFF TO OFF PER EMERG CHECKLIST. OVERHEAT LIGHT WENT OUT. TIGHTENED CLAMP ON CARGO COMPT FLOW CONTROL VALVE SYS LK, OP AND PRESS CK GOOD PER MM CHAP 21SDR LR7A9833Oil Cooler · inoperativeSHUTDOWN NR 2 ENG DUE TO HIGH OIL TEMP. REMOVED AND REPLACED NR 2 ENG OIL COOLER, SEE SPAR WO NR 20-431-101-001. INOPERATIVE THERMOSTATIC BYPASS AND RELIEF VALVE.SDR LR7A9832Uplock · crackedLOSS OF UTILITY HYD SYSTEM. NLG UPLOCK ASSY REPLACED IAW 32-30 PG 231-232. LEAK CHECK GOOD, OPS CHECK GOOD IAW 32-32 PG 201. EMERGENCY EXT OPS CHECK GOOD IAW 32-00 PG 201.SDR LR7A9831Hyd Line · brokenLOSS OF UTILITY HYD SYSTEM. REMOVED AND REPLACED LAND GEAR DOWN HYD LINE WHICH WAS BROKEN. ALSO, REPLACED THE EMERGENCY DOWN HYD LINE, WEATHER BEATING BAD. PRESSURE TESTED GOOD IAW LOCKHEED MM CHAPTER 32. REFILLED HYD RES UTILITY HYD SYSTEM.SDR LR7A35Angle · corrodedEXFOILATION CORROSION STA 258 RT CHINE, INSPECTED DAMAGED AREA PER ENGINEERING IN DIRECTIVE EDF07-1 STEP 1 AND STEP 2 DAMAGE WITHIN PERMISABLE LIMITS PER STEP 2 OK FOR INTENDED FERRY FLT RT CHINE ANGLE, FS 257, BLR 61, WL 146, (P/N 372322-1). REPAIRED IAW SMPSDR LR7A9830Fire Loop · shortedNR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED AFTER T/O, FIRE EMERGENCY HANDLE PULLED AT 2200Z, RETURNED TO BRW. REMOVED AND REPLACED NORMAL AFT FIRE BOTTLE AND SQUIBB, INSPECTED NR 1 ENGINE NO EVIDENCE OF FIRE. THREE ENGINE FERRY AUTHORIZED IAW LYNDEN AIR CARGSDR LR7A9829Fitting · crackedDURING B-CHECK, THE RT FS 617 25000 LB TIE DOWN FITTING WAS DISCOVERED CRACKED DURING EDDY CURRENT INSPECTION PER CARD SP-262. THE CRACK WAS .75 INCHES LONG, LOCATED IN THE AFT RADIUS. THE FITTING WAS REPAIRED IAW LOCKHEED SRM SMP 583 CHAP 53-40-40, PAGES 11SDR LR7A9828Switch · intermittentLT MLG IND STAYED UP WHEN GEAR SELECTED DOWN, OK ON SECOND TRY. REMOVED AND REPLACED LEFT DOWN LIMIT SWITCH PER MM 32-33-202, OPS CHECKED OK.SDR LR7A9825Oil Pump · failedNR 4 ENGINE LOW AND DECREASING OIL QUANTITY. PRECAUTIONARY SHUTDOWN. REPLACED TURBINE REAR SCAVANGE OIL PUMP PER 72-2-3 201-204. SERVICED OIL TANK, RUNUP AND LEAK CHECK NORMAL PER 72-2-3 204-205.SDR LR7A9826Diffuser · crackedNR 4 ENGINE LOW AND DECREASING OIL QUANTITY, PRECAUTIONARY SHUTDOWN. INSPECTED NR 4 ENGINE, AIRCRAFT IN SAFE CONDITION FOR INTENDED FERRY FLIGHT TO ANC, 3 ENGINE FERRY. REMOVED QEC, BORESCOPE INSPECTED ENGINE AND SUPSPECT CRACKED DIFFUSER.SDR LR7A9823Cap · looseNR 2 ENGINE SHUTDOWN IN CLIMB AT 1750 Z DUE TO PROP OIL LOW LIGHT ON. RESECURED PRESSURIZED CAP ON NR 2 PROP. RESERVICED IAW HAM STD MM PARA 7-10, 7-11 PF 706 AND 707, OPS CHECK NORMAL.SDR LR7A9805Blade · leakingNR 2 PROP LOW OIL LIGHT FOLLOWED BY FLUX. SHUTDOWN IAW AFM. INSPECTED AND FOUND NR 2 BLADE LEAKING. PROP REMOVED FOR DETAILED INSPECTION BY VENDOR.SDR LR7A9803Seal · leakingNR 2 PROP LOW OIL LIGHT FEATHERED IN FLIGHT. REMOVED PROPELLER, HUB RESEALED BY PACIFIC PROPELLER, REINSTALLED AND TESTED PER HN6101.
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