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 SRAA98A0116Fitting · leakingAFTER LANDING DURING ROLL OUT AND TURN OFF TO PARKING AT DNA FLIGHT 407, NOTICED FUEL ODORS IN CARGO COMPARTMENT. AFTER PARKING AIRCRAFT FOUND FUEL DRIPPING FROM CENTER WING AREA CAVITY DRAIN LINE. TURNED OFF ALL AIRCRAFT POWER, EVACUATED AIRCRAFT AND FIRE DSDR LR7A9822Cap · crackedDURING C-CHECK/BRIDGING INSPECTION, FOUND CRACKED TANG AT HSS 180.0. DAMAGE AREA CLEANED UP AND TANG REPLACED WITH LS30661 EXTRUSION.SDR LR7A9821Bulkhead · crackedDURING C-CHECK/BRIDGING INSPECTION, FOUND 2 CRACK RADIATING ACROSS THE NR 1, 2, 3 AFT NACELLE BULKHEAD ASSY LOWER OUTBOARD SIDE, FS 485.9, PPWL 3.5. STOP DRILLED AND INSTALLED REPAIR DOUBLER.SDR LR7A9820Angle · crackedDURING C-CHECK/BRIDGING INSPECTION, FOUND ANGLE AT LOWER AFT NACELLE ASSY CRACKED NEAR FORWARD MOST SPOT WELD NR 1, 2, 3, 4 ENGINES FS 517, PPBL 5.0.SDR LR7A9819Skin · wornDURING C-CHECK/BRIDGING INSPECTION, LT AUX TANK CAVITY LOWER WING SKIN UPPER AND LOWER SURFACE HAS WEAR MARKS. WEAR MARKS BLENDED SMOOTH, EDDY CURRENT INSPECTED, AND ROTO-PEENED.SDR LR7A9818Beam · crackedDURING C-CHECK/BRIDGING INSPECTION, FOUND CENTER WING REAR BEAM CRACKED AT CWS 72R, FS 597, APPROX WL 268. INSTALLED NEW INBD SECTION OF WEB, DOUBLER, AUXILIARY DOUBLER, SPACER STRAP, RADIUS BLOCK, REPAIR FINISHED.SDR LR7A9817Chine Cap · damagedDURING C-CHECK/BRIDGING INSPECTION, FOUND SEVERAL CHINE CAPS, FS 245E TO 817E LT AND RT, WITH ELONGATED HOLES AT 10K TIE DOWNS, CORROSION, CRACKS, ANCHOR NUT RIVET HOLES. REPLACED ALL CHINE CAPS, EXCEPT ONE REPAIRED.SDR LR7A9816Web · crackedDURING C-CHECK/BRIDGING INSPECTION, CRACKS LOCATED IN THE WEB AT WL 200, FS 590 ON BOTH LT AND RT SIDES. REPLACED WEB.SDR LR7A9815Fairing · crackedDURING C-CHECK/BRIDGING INSPECTION, CENTER WING LEADING EDGE TO INBOARD ENGINE NACELLE FAIRING ASSY WEB HAS 2 CRACKS AT CW STA 174. TRIMMED OUT CRACKS, INSTALLED FILLER AND DOUBLER.SDR LR7A9814Skin · crackedDURING C-CHECK/BRIDGING INSPECTION, SPIDER CRACKS FOUND ON THE MLG WHEEL WELL RT PANEL SKIN, FS 480 AND WL 198. CRACKS IN SKIN PANEL TRIMMED OUT, REPAIR DOUBLER INSTALLED.SDR LR7A9813Bulkhead · wornDURING C-CHECK/BRIDGING INSPECTION, NR 4 ENGINE QEC FRONT BULKHEAD ASSEMBLY WORN ON BOTH SIDES OF FILLER, TOP CENTER. REPLACED EXISTING FILLER, INSTALLED WEAR STRIP.SDR LR7A9812Extrusion · wornDURING C-CHECK/BRIDGING INSPECTION, FOUND TEE EXTRUSION WORN 0.025 THICKNESS AND GOUGED TO DEPTH OF 0.045 AT NR 4 ENGINE, LHS, FS 410, 11.0. WORN AREA BLENDED SMOOTH, EPOXY FILLER APPLIED, STAINLESS STEEL WEAR STRIP INSTALLED.SDR LR7A9811Longeron · crackedDURING C-CHECK/BRIDGING INSPECTION, LT SLOPING LONGERON FOUND CRACKED AT RS1 RETAINER HOOK. LONGERON REPLACED.SDR LR7A9810Firewall Cap · wornDURING C-CHECK/BRIDGING INSPECTION, FOUND NR 3 ENGINE FIREWALL CAP WORN AT WL 225. BLENDED GROOVE, APPLIED FILLER, INSTALLED DOUBLER.SDR LR7A9809Tee · wornDURING C-CHECK/BRIDGING INSPECTION, TEE EXTRUSION IS WORN, NR 3 ENGINE, FS 410, PPBL 0.0 AND PPWL 11.0, AT THE TOP OF THE BULKHEAD. THE WORN AREA WAS BLENDED SMOOTH, EPOXY FILLER APPLIED, STAINLESS STEEL WEAR STRIP INSTALLED.SDR LR7A9808Longeron · crackedDURING C-CHECK/BRIDGING INSPECTION, FOUND CRACKS ON A LONGERON, NR 2 AND NR 3 ENGINE, FS 410 TO FS 485, PPBL 10.00L, AND WEAR ALONG THE LONGERON WHICH IS .030 TO .035 INCHES DEEP. EXISTING REPAIR REMOVED, CRACKED PORTION OF LONGERON TRIMMED OUT, FILLER INSTASDR LR7A9807Web · crackedDURING C-CHECK/BRIDGING INSPECTION, A CRACK AT WEB CTR FUS, FS 597.0 TO 617.0, BL 61.625 UPPER, EXTENDING FROM ONE WIRE BUNDLE CUTOUT HOLE TO ANOTHER, APPROXIMATELY 1 INCH LENGTH AND AN ADDITIONAL CRACK WHICH HAS EXTENDED JUST PAST A CREW HOLE ABOVE THE 1 INCSDR SRAA98A0114Heat Exchanger · defectiveAFTER 40 MINUTES OUT OF HNL FLIGHT 2039, AIRCRAFT LOST PRESSURIZATION, COULD ONLY MAINTAIN 10,000 FT, CARGO COMPARTMENT OVERHEAT LIGHT CAME ON SHORTLY AFTER. ACCOMPLISHED AIR TURN BACK TO HNL. REMOVED AND REPLACED CARGO COMPARTMENT AIRCONDITIONING HEAT EXCHASDR SRAA98B0107Engine · damagedON LANDING AT MYU FLIGHT 1902, AIRCRAFT LANDED ON ICY SURFACE AND DEPARTED FROM RUNWAY. AIRCRAFT SUSTAINED NR 4 ENGINE AND PROP DAMAGE. DUE TO CONTACT WITH SNOW BANK NR 4 ENGINE FIRE, EXTINGUISHED WITH NR 1 BOTTLE. AIRCRAFT HAS BEEN REMOVED FROM SNOW BANK ASDR LR7A9801Thermostat · failedPRECAUTIONARY SHUTDOWN NR 3 ENGINE AT 0400Z DUE TO HIGH OIL TEMP. FERRIED AIRCRAFT TO ANC, REPLACED NR 3 ENGINE OIL COOLER THERMOSTAT PER LOCKHEED MM CHAPTER 79-20, PAGE 203. GROUND RUNS ACCOMPLISHED, SYSTEM OPERATIONALLY TESTS OK.SDR LR7A9734Thermostat · failedPRECAUTIONARY SHUTDOWN NR 3 ENGINE AT 0400Z DUE TO HIGH OIL TEMP. FERRIED AIRCRAFT TO ANC, REPLACED NR 3 ENGINE OIL COOLER THERMOSTAT PER LOCKHEED MM CHAPTER 79-20, PAGE 203. GROUND RUNS ACCOMPLISHED, SYSTEM OPERATIONALLY TESTS OK.SDR SRAA971206Latch · unlockedDURING CLIMBOUT, MASTER DOOR WARNING LIGHT ILLUMINATED AND AIRCRAFT WOULD NOT PRESSURIZE, ACCOMPLISHED AIR TURNBACK. INSPECTED CARGO DOOR LATCH SYSTEM AND FOUND THE LEFT LATCH DOES NOT GO TO FULL OVER CENTER AND LATCH. RECYCLED CARGO DOOR AND VERIFIED DOOR CSDR SRAA971108Check Valve · crackedON CLIMB-OUT OF AYTU FOR FLIGHT 503 TO WWK AFTER GEAR RETRACTION, UTILITY HYDRAULIC SYSTEM DUMPED ALL PRESSURE, UNABLE TO ESTABLISH SYSTEM PRESSURE. DURING MANUAL GEAR EXTENTION FOUND THE RIGHT MLG MANUAL GEARBOX DIFFICULT TO ENGAGE, PERFORMED EMERGENCY GEARSDR SRAA971104Mount · brokenPOST FLIGHT, THE LEFT HAND HORIZONTAL STABILIZER TIP FOUND LOOSE ON UPPER AND LOWER ATTACHMENT POINTS. INSPECTION FOUND THE UPPER AND LOWER FORWARD MOUNTS ON THE HORIZONTAL STABILIZER ON THE LEFT HAND SIDE BROKEN. PERFORMED INTERIM REPAIR PER EAM8255005 APPRSDR SRAA971102Ball Screw · contaminatedAFTER TOUCHDOWN, RIGHT MAIN LANDING GEAR WENT INTO TRANSIT WITH HORN AND LIGHT IN THE HANDLE. INSPECTED AND FOUND FOREIGN MATERIAL WRAPPED AROUND BALL SCREW. JACKED AIRCRAFT MANUALLY CRANKED RIGHT MAIN LANDING GEAR UP, REMOVED FOREIGN MATERIAL FROM BALL SCRESDR SRAA971101Valve Housing · failedDURING FLIGHT, NR 4 PROP FLUX IN NORMAL GOVERNING STEADY AND WITHIN LIMITS IN MECHANICAL. RPM WENT OUT OF LIMITS IN MECHANICAL GOVERNING. PROP WAS NOT PITCHLOCKED, SHUTDOWN IAW AOM. REMOVED AND REPLACED NR 4 VALVE HOUSING PER IAW JOB CARD NR 6103, GROUND RSDR LR7A9726Fire Detector · out of positioinINTERMITTENT FAINT FIRE WARNING LIGHT BOTH HANDLE AND MASTER LIGHT NR 2 ENGINE. CHECKED FIRE DETECTOR ELEMENTS IAW LAC MM 26-10. REPOSITIONED ELEMENT IN HORSECOLLAR, GROUND TEST NORMAL.SDR SRAA971013Control Rod · strippedDURING LANDING, NR 1 PROP WOULD NOT GO INTO THE BETA RANGE. ON INSPECTION FOUND THREADS ON THE CONTROL ROD AND ROD ENDS STRIPPED. REPLACED CONTROL ROD ON PROP CONDITION CONTROLS IAW MM 61, OPS CHECK GOOD.SDR LR7A9724Blade Seal · leakingNR 3 PROP LOW OIL LIGHT FOLLOWED BY OUT OF LIMITS FLUX. ENGINE SHUTDOWN IAW AFM. REMOVED AND REPLACED NR 3 PROPELLER ASSY PER JC6101. OPS OK PER JC7101.SDR SRAA971009Overheat Det · defectiveDURING FLIGHT, NR 1 TURBINE OVERHEAT LIGHT CAME ON, RETARDED THROTTLE TO 977 AND LIGHT WENT OUT. AIRCRAFT ARRIVE AT DESTINATION WITHOUT INCIDENT. INSPECTED OVERHEAT DETECTORS AND FOUND ELEMENTS DEFECTIVE. REPLACED DETECTORS AND OPS CHECKED GOOD PER MM CH 26SDR SRAA971007Bracket · bentON TAKEOFF FROM STL TO YIP FLIGHT 9020, NR 1 ENGINE OVERHEAT WARNING LIGHT CAME ON INTERMITTENTLY FOR 2 TO 3 SECONDS, ALL OTHER PARAMETERS INDICATED NORMALLY. INSPECTED NR 1 ENGINE, FOUND FIRE DETECTION LOOP BRACKET BENT, REPOSITIONED BRACKET, BY TURBINE AREASDR SRAA971008Control Unit · failedDURING CRUISE FROM MCI, FLIGHT 9021, NR 3 ENGINE FIRE WARNING LIGHT CAME ON, SHUT DOWN NR 3 ENGINE AND DISCHARGED FIRE EXTINGUISHING BOTTLE, LIGHT REMAINED ON. A SECOND BOTTLE WAS ALSO DISCHARGED, AIRCRAFT DIVERTED TO SPI AND LANDED WITHOUT INCIDENT. FOUND NSDR LR7A9722Prop Assy · leakingNR 3 ENG PROP LOW OIL LIGHT, ENGINE SHUTDOWN AT 1833Z. REMOVED AND REPLACED NR 3 PROPELLER ASSY PER FORM M-6101. OPS CHECK OK PER CARD 7101.SDR SRAA971006Hyd Fitting · crackedAFTER TAKEOFF, NR 1 ENGINE LOST ALL HYDRAULIC PRESSURE, DUMPED FUEL AND ACCOMPLISHED AIR TURNBACK TO STN. FOUND NR 1 HYD PUMP PRESURE FITTING CRACKED. REPLACED NR 1 HYD PUMP AND FITTING, SYSTEM OPS CHECKED GOOD PER MM CH 2901-2.SDR CA971015025Frame · cracked(CAN) 2.5 INCH CRACK FOUND IN BULKHEAD AT BS.968 BL ZERO WL.283. RACK REPAIRED PER SRM.SDR SRAA971005Gasket · leakingON FINAL APPROACH TO IKN FOR FLIGHT 407, CARGO COMPARTMENT OVERHEAT LIGHT CAME ON, DEACTIVATED COOLING SYSTEM AND LIGHT WENT OUT. INSPECTED AIR PNEUMATIC SYSTEM AND FOUND BLEED AIR DUCT GASKET LEAKING, TRANSFERRED ITEM TO DMI PER MEL 21-1.SDR SRAA971002Wire · looseON APPROACH, MASTER NACELLE OVERHEAT WARNING LIGHT CAME ON WHEN LANDING GEAR HANDLE WAS PLACED IN THE DOWN POSITION. FOUND NACELLE MASTER WARNING LIGHT WIRING LOOSE. REPAIRED WIRING TO SWITCH AND REFORMED OPS CHECK PER MM CH 26.SDR SRAA970916Gasket · leakingDURING TEST FLIGHT, FOUND THE RIGHT WHEEL WELL GOT VERY HOT WITH CARGO COMPARTMENT AIR CONDITIONING SYSTEM OFF. THERE WERE SIGNS OF FUMES AND SMOKE IN THE CARGO COMPARTMENT. CLOSED ALL ENGINE BLEED VALVES AND THE CONDITION CEASED TO EXIST. FOUND LEAKING CLASDR SRAA970915Temp Contl Vlv · stuckDURING DESCENT, FLIGHT DECK AIR CONDITION WENT TO FULL HOT AND SMOKE WAS COMING OUT OF AIR CONDITION SYSTEM. FLIGHT CREW AND PASSENGERS WENT ON OXYGEN, TURNED OFF AIR CONDITIONING AND DESCENDED FROM 8,000 TO 3,000 FT. SMOKE HAD COMPLETELY CLEARED BY 3,000 FTSDR SRAA971105Skin · damagedWHILE ON THE GROUND, AIRCRAFT WAS STRUCK BY A FORKLIFT. INSPECTED AIRCRAFT AND FOUND BOTTOM SKIN OF LEFT WING HAD GOUGING AND SCRAPES. PERFORMED INTERIM REPAIR AND FERRIED TO BHM FOR REPAIR. REMOVED AND REPLACED LEFT OUTER WING PER SAT JOB CARD 5715, ALL SSDR SRAA970907Valve · inoperativeDURING FLIGHT, AIRCRAFT WOULD NOT PRESSURIZE, NOTICED BLEED AIR LEAK IN RIGHT WHEEL WELL. DUMPED 3,000 LBS OF FUEL AND LANDED WITHOUT INCIDENT AT DEPARTURE STATION. FOUND UNDERFLOOR HEAT VALVE STUCK OPEN AND LEAKING AT GASKET. REPLACED VALVE AND GASKET OPS SDR SRAA970815Air Cond · smokeDURING FLIGHT FOR OKO, FLIGHT NR 408, FOUND FLIGHT DECK AIR CONDITIONING SYSTEM EMITS SMOKE WHEN DRIVEN IN WARM, SYSTEM OPERATED GOOD IN COLD MODE. INSPECT AIRCRAFT AND OPERATED SYSTEM IN FULL RANGE TEMPERATURE, NO FAULT FOUND PER MM CH 21.SDR SRAA 970814Wire · brokenDURING ENGINE START, NR 3 TURBINE OVERHEAT WOULD NOT TEST. ABORTED ENGINE START. INSPECTED NR 3 ENGINE FIRE DETECTION SYSTEM AND FOUND BROKEN WIRE IN THE HARNESS AT TURBINE AREA. REPAIRED BROKEN WIRE AND OPS CHECKED GOOD PER MM CH 26-10.SDR LR7A97019Battery · dischargedREPLACED BATTERIES IN FLIGHT DECK EMERGENCY EXIT LIGHT PER 33-50-01. OPS OK.SDR SRAA970810Bulkhead · crackedDURING CLIMB-OUT FROM FAI AT 17000 FT, FLT NR 1930, HEARD A LOUD BANG FOLLOWED BY A/C DEPRESSURIZATION, A/C DESCENT TO 10,000 FT. THEN DUMPED 19,000 LBS OF FUEL FOR LANDING. A/C LANDED WITHOUT INCIDENT. INSPECTED A/C AND FOUND A 42 IN CRACK ALONG THE LHS OFSDR CA970904022Controller · failed(CAN) NR 2 ENG FIRE WARN ILLUMINATED ON APPROACH. IN-FLIGHT SHUTDOWN C/W. INVESTIGATION REVEALED A FIRE DETECTION UNIT HAD FAILED IN THE FIRE POSITION. UNIT REPLACED.SDR CA970815005Gearbox · contaminated(CAN) IN CRUISE FLIGHT, NR2 CHIP DETECTOR LIGHT ILLUMINATED. LIGHT PULSED OUT BUT RE-ILLUMINATED MINUTES LATER AND WOULD NO LONGER PULSE OUT. PRECAUTIONARY ENGINE SHUT-DOWN WAS CARRIED OUT AND 3 ENGINE LANDING CARRIED OUT. MAINTENANCE FOUND FERROUS PARTICLES OSDR CA970807006Engine · faulty(CAN) SHORTLY AFTER REACHING ALTITUDE, CHIP LIGHT ON NR2 POWER SECTION ILLUMINATED. ATTEMPTS WERE MADE TO "PULSE" LIGHT OUT, BUT IT REMAINED ON. PRECAUIONARY IN-FLIGHT SHUT DOWN WAS CARRIED OUT AND 3 ENGINE LANDING CONDUCTED WITHOUT INCIDENT. POWERPLANT CHANGESDR SRAA970802Valve · malfunctionedDURING FLIGHT APPROX 50 MILES FROM DESTINATION, NR 4 ENGINE DROPPED TO 97 PERCENT, THEN PROP LOW OIL LIGHT CAME ON. SHUT DOWN NR 4 ENGINE AS PRECAUTIONARY AND LANDED WITHOUT INCIDENT. SUSPECT DEFECTIVE VALVE HOUSING. REPLACED BOTH VALVE HOUSING AND PUMP HOUSDR SRAA970719Light · inoperativeDURING REMOVAL OF THE COMBI UNIT FROM AIRCRAFT AT ANC, FOUND RT LOWER SIDE EMERGENCY EXIT LIGHT INOP. COMBI UNIT REMOVED FROM AIRCRAFT AND ITEM TRANSFERRED TO COMBI LOG BOOK TO BE CORRECTED.
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