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 SRAA960906Gimble Assy · jammedON DESCENT, FLT 1908 INTO AED, NR 4 THROTTLE LEVER WOULD NOT ADVANCE ABOVE 2 POUND/INCH PAST FLIGHT IDLE, OCCURED AT 7,000 FEET, ENGINE AT 6,900 INCH/POUNDS TORQUE, AND 720 DEGREES TIT. AIRCRAFT DIVERTED TO OTZ AND LANDED WITHOUT INCIDENT. INSPECTED NR 4 TSDR SRAA960901Hyd Hose · leakingON APPROACH, LOST UTILITY HYDRAULIC PRESSURE WHILE LOWERING GEARS, NOSE LANDING GEAR DID NOT FULLY EXTEND. USED ALTERNATE GEAR EXTENSION WITH AUX HYDRAULIC PRESSURE, ALL GEARS CAME DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NOSE GEAR EXTENSIONSDR SRAA960812Bulb · failedON PREFLIGHT, FOUND CARGO EMERGENCY EXIT LIGHT WEAK, FOUND P2 LIGHT BULB DEFECTIVE. REPLACED BULB, OPS CHECKED GOOD PER MM CH 33.SDR SRAA960811Controller · defectiveDURING FLIGHT, AIRCRAFT WOULD NOT PRESSURIZE OVER 4 AT 14,000 FT IN AUTO OR MANUAL. ACCOMPLISHED AIR TURNBACK TO LCK AND LANDED WITHOUT INCIDENT. FOUND PRESSURE CONTROLLER DEFECTIVE. REPLACED CONTROLLER, SYSTEM OPS CHECKED GOOD PER MM CH 21.SDR SRAA960810Gaskets · leakingDURING FLIGHT, CARGO COMPARTMENT OVERHEAT LIGHT CAME ON GOING THROUGH 11,000 FT. TURNED SYSTEM OFF AFTER ONE MINUTE AND LIGHT WAS STILL ON, ISOLATED SYSTEM, LIGHT WENT OUT. ACCOMPLISHED AIR TURNBACK, AIRCRAFT LANDED WITHOUT INCIDENT AT 146,900 LBS. FOUND UPSDR SRAA960809Pump · failedDURING FLIGHT, NR 1 HYDRAULIC PUMP PRESSURE WENT TO O PSI WHEN RAISING MLG. ACCOMPLISHED AIR TURNBACK, AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NR 1 HYD PUMP FAILED. REPLACED PUMP AND FILTER, INSPECTED UTILITY SYSTEM MAIN AND DRAIN FILTERS, NO CONTAMINATION SDR SRAA960808Retract Mech · malfunctionedON APPROACH, LEFT MAIN LANDING GEAR WOULD NOT EXTEND, DIVERTED TO FAI AND PREPARED TO HAND CRANK THE LANDING GEAR ON APPROACH. LOWERED GEAR HANDLE AND ALL GEARS CAME DOWN AND LOCKED NORMALLY. ACCOMPLISHED LANDING WITHOUT INCIDENT AND ITEM IS UNDER INVESTIGATSDR SRAA960806Control Unit · defectiveDURING PRE-FLIGHT, NR 3 FIRE HANDLE AND MASTER DISPLAY FLASHED INTERMITTENTLY WITHOUT NR 3 ENGINE RUNNING. FOUND NR 3 ENGINE FIRE CONTROL UNIT DEFECTIVE, REPLACED FIRE CONTROL UNIT, SYSTEM CHECKED GOOD PER M.M. CH 26.SDR CA960826042Valve Housing · cover cracked(CAN) DURING FLIGHT SMOKE BEGAN TO FILL THE CABIN. THE AIR CONDITIONING SYSTEM AND RH AC BUS WERE ISOLATED. FLIGHT CONTINUED TO DESTINATION. POST FLIGHT INSPECTION FOUND #3 PROPELLER VALVE HOUSING COVER WAS CRACKED AND LEAKING OIL. FRICTION ON SLIP RING GENERASDR CA960812009Valve Housing · cover cracked(CAN) DURING CRUISE SMOKE BEGAN FILLING THE CABIN. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. MAINTENANCE INVESTIGATION FOUND #3 PROPELLER VALVE HOUSING COVER WAS CRACKED AND LEAKING OIL. FRICTION ON SLIP RINGS GENERATED SMOKE WHICH WAS INGESTED BY THE PRESSDR SRAA960803Light · inoperativeON PREFLIGHT, FOUND EMERGENCY EXIT LIGHT BY CREW DOOR NOT WORKING. REPLACED EMERGENCY EXIT LIGHT, OPS CHECKED GOOD PER MM CH33. (M)SDR SRAA960706Gen Ctl Pnl · failedDURING FLIGHT, AFTER 3.8 HOURS INTO FLIGHT, NR 1 GENERATOR CONTROL PANEL EMITS SMOKE. TURNED OFF NR 1 GENERATOR CONTROL PANEL AND REMOVED FROM RACK, RESUMED NORMAL OPERATION AFTER TWO MINUTES WITH OXYGEN MASK. AIRCRAFT LANDED WITHOUT INCIDENT, NR 1 GENERATORSDR SRAA960705Ballscrew · wornAFTER TAKEOFF, NOTICED RIGHT MLG WAS SLOW TO RETRACT. RECYCLED GEAR AND ACCOMPLISHED AIR TURNBACK, LANDING WITHOUT INCIDENT. CONTINUED A SERIES OF 3 FLIGHTS WITH GEARS DOWN, AT ANC THE FINAL DESTINATION THE RIGHT MLG WAS INSPECTED AND FOUND THE FORWARD BALLSSDR CA960703008Indicator · malfunction(CAN) ON DESCENT WITH RUDDER TRIM AT ZERO IT WAS NOTED THAT THE TRIM INDICATOR HAD DRIFTED TO 10 DEGREES RIGHT. A FEW MINUTES LATER INDICATION RETURNED TO ZERO WITH NO EFFECT TO FLIGHT CONTROL IN EITHER INSTANCE. INDICATOR REPLACED.SDR SRAA69608Jackscrew · failedAFTER TAKING OFF FROM ILL FOR ANC ON FLIGHT 956, FOUND RIGHT MAIN LANDING GEAR WOULD NOT RETRACT, CONTINUED FLIGHT WITH GEARS DOWN AND LANDED IN ANC WITHOUT INCIDENT. FOUND RIGHT MAIN LANDING GEAR JACKSCREW FAILED. REMOVED AND REPLACED JACKSCREW AT RIGHT AFTSDR SRAA69604Valve Hsg · damagedON TAKEOFF ROLL OUT OF GAL NR 1 PROPELLER WENT TO 104 PERCENT RPM (PTICH LOCKED). NR 1 ENGINE WAS SHUT DOWN AND TAKEOFF ABORTED, AIRCRAFT RETURNED TO BLOCKS WITHOUT INCIDENT. FOUND NR 1 PROP VALVE HOUSING HAD METAL SHAVINGS. REPLACED NR 1 PROPELLER ASSEMBLYSDR SRAA69602Valve Hsg · bad bearingON CLIMB-OUT FROM AVB TO AAB - NR 1 ENGINE RPM FLUCTUATED FROM 105 PERCENT TO 95 PERCENT IN LESS THAN ONE SECOND, NO LOW OIL LIGHT AND MECHANICAL GOVERNING HAD NO EFFECT ON CONDITION, SHUT DOWN NR 1 ENGINE AS PRECAUTIONARY, AIRCRAFT LANDED SAFELY AT AAB. FOUNSDR SRAA69603Pressurize Sleev · failedDURING TAXIING OUT OF ANC, HYDRAULIC LINE (BETWEEN THE 245 BULKHEAD AND COMBI MODULE) BLEW, CAUSING FUMES AND HYDRAULIC MIST TO ENTER THE CABIN, FOLLOWED BY UTILITY HYD SYSTEM PRESSURE LOSS. SHUT DOWN HYDRAULIC SYSTEM AND DE-PLANED ALL PASSENGERS. FOUND UTILSDR SRAA69601Attach Fitt · crackedON APPROACH TO YIP, FLIGHT 9003 - HAD TO USE FULL RIGHT AILERON TRIM AND 10 DEGREE RIGHT RUDDER TO FLY LEVEL. FOUND LHS FLAP TRACK ATTACH FITTING CRACKED AT FS 241.60, REPLACED FLAP TRACK. SYSTEM OPS CHECKED GOOD PER MM CH 57-10 AND CH 27. (M)SDR CA960508004Lines · blocked(CAN) DURING CLIMBOUT, THERE WAS AN OIL LOSS INDICTION FOR NR 4 ENGINE. IN-FLIGHT SHUTDOWN WAS CARRIED OUT AND A 3 ENGINE LANDING CONDUCTED WITHOUT INCIDENT. REAR COMPRESSOR, FRONT TURBINE BEARING SCAVENGE LINES WERE FOUND BLOCKED WITH CARBON. LINES WERE BLSDR SRAA59604Turbine Blade · damagedDURING CRUISE TO ARI FLT NR 1204, NR 2 ENGINE HAD LOW TORQUE AND HIGH FUEL FLOW, ACCOMPLISHED ENGINE SHUT DOWN AS PRECAUTIONARY PRIOR TO LANDING, AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NR 2 ENGINE HAD TURBINE BLADES DAMAGED. REPLACED NR 2 ENGINE AND PERFORMSDR CA960508003Propeller · failed(CAN)IN CRUISE, #4 PROPELLER PITCH LOCKED ENGINE SHUTDOWN. UNDER INVESTIGATIONSDR CA960508005Valve Housing · malfunction(CAN)ON APPROACH, TORQUE ON #4 ENGINE COULD NOT BE REDUCED BELOW 5000 LBS. ON LANDING, PROP FAILED TO GO INTO BETA RANGE, ENGINE SHUTDOWN. #4 VALVE HOUSING REPLACED.SDR SRAA49604Valve Housing · defectiveFLT 1201 - DURING CRUISE, NR 4 PROPELLER RPM DECREASING BELOW 98 PERCENT, PRECAUTIONARY SHUT DOWN NR 4 ENGINE AND ACCOMPLISHED AIR TURN-BACK TO LIM. LANDED SAFELY. FOUND NR 4 PROPELLER VALVE HOUSING DEFECTIVE. REPLACED VALVE HOUSING PER MM, CHAPTER 61. OPSSDR CA960409001Presure Line · cracked(CAN)IN CRUISE, LOW OIL QUANTITY LIGHT ILLUMINATED FOR THE #2 ENGINE. ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED. MAINTENANCE INVESTIGATION CONFIRMED CRACKED OIL PRESSURE LINE. LINE REPLACED.SDR CA960325008Trim Actuator · failed(CAN)ON CLIMB THE ELEVATOR TRIM TAB BECAME UNRESPONSIVE IN NORMAL MODE. AIRCRAFT RETURNED TO BLOCKS. ELEVATOR TRIM TAB ACTUATOR REPLACED.SDR CA960222006Seal · cut(CAN) AT TOP OF DESCENT, #4 PROP LOW OIL LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INVESTIGATION REVEALED A LEAKING BLADE ROOT SEAL. THE PROPELLER ASSEMBLY WAS REPLACED FOR COMPANY CONVENIENCE.SDR SRAA29601Detector · malfunctionedFLT ADT07 - ON TAKEOFF ROLL FROM MHZ, MASTER TURBINE OVERHEAT ILLUMINATED, ABORTED TAKEOFF AND RETURNED TO BLOCK. FOUND NR 3 ENGINE AT 7 O'CLOCK OVERHEAT DETECTOR DID NOT FUNCTION PROPERLY, REPLACED NR 7 DETECTOR. SYSTEM OPS CHECKED GOOD PER MM, CHAPTER 26. SDR CA960111014Blade · missing(CAN)DURING A ROUTINE A-CHECK, A CRACK WAS FOUND IN THE #3 ENGINE TAIL PIPE AND TURBINE REAR BEARING SUPPORT. FURTHER INVESTIGATION SHOWED A PIECE MISSING FROM THE FOURTH STAGE TURBINE BLADE. DAMAGE WAS CONTAINED. TURBINE SENT FOR STRIP REPORT.SDR SRAA129504Switch · out of adjustPILOT REPORT DURING LANDING APPROACH, RT MLG WOULD NOT EXTEND WITHOUT G-FORCE. SUPPORT AIRCRAFT ON JACKS, INSPECT MAIN LANDING GEAR RETRACTION MECHANISM, FOUND SWITCH OUT OF ADJUSTMENT, ADJUSTED POSITION INDICATOR IAW CH 32, OPS CHECKED GOOD. (X)SDR CA951206007Blades · damaged(CAN)DURING A THREE ENGINE FERRY FLIGHT ON TAKEOFF, A LOUD BANG WAS HEARD, FOLLOWED BY 1000 DEGREES C TIT INDICATION. THE THROTTLE WAS PULLED BACK AND NO OTHER INDICATIONS WERE NOTED. ON DESCENT, WHEN POWER WAS PULLED BACK, AN NTS OCCURRED WITH HIGH FUEL FLOW SDR CA951206006Starter · worn drive(CAN)DURING CRUISE, THE #1 ENGINE REDUCTION GERABOX CHIP DETECTOR LIGHT ILLUMINATED AND THE ENGINE WAS SHUT DOWN AS A PRECAUTION. MAINTENANCE INVESTIGATION REVEALED THAT THE DRIVE TEETH ON THE STARTER WERE WORN OUT. THE DRIVE WAS REPLACED AND THE OIL SYSTEM FLSDR CA951204026Beam · cracked(CAN)LH MAIN LANDING GEAR BEAM STA 528 WL220 CRACKED. REPAIRED SRM 53-40-20.SDR CA951204025Former · corroded(CAN)LH WHEEL WELL FAIRING STRUCTURE STA 497 WL165 CRACKED. REPAIRED SRM 51-140-20.SDR CA951204024Skin · cracked(CAN)RH SIDE FUSELAGE SKIN STA 695 BL62.5 WL256 CRACKED. REPAIRED DWG SK 382-53-274.SDR CA951204023Rib Brace · cracked(CAN)LH WING OWS.108 RIB BRACE CRACKED. REPLACED.SDR CA951204022Rib Brace · cracked(CAN)LH WING OWS.90 RIB BRACE CRACKED. REPLACED.SDR CA951204021Rib Cap · cracked(CAN)RH OUTER WING LOWER RIB CAP CRACKED. REPAIRED SRM 57-50-38.SDR CA951204020End Rib · cracked(CAN)RH OUTBOARD FLAP INBOARD END RIB STA.0 CRACKED. REPLACED.SDR CA951204019End Rib · cracked(CAN)LH OUTBOARD FLAP INBOARD END RIB STA.0 CRACKED. REPLACED.SDR CA951204018Skin · cracked(CAN)RH INBOARD FLAP CRACKED IN THREE LOCATIONS. REPAIRED IN ACCORDANCE WITH SRM 51-140-10.SDR CA951204017Doubler · cracked(CAN)LH ELEVATOR TRAILING EDGE BEAM ASSEMBLY CRACKED. REPLACED.SDR CA951204016Rib · cracked(CAN)RH ELEVATOR LEADING EDGE HSS.58 CRACKED. REPLACED.SDR CA951204015Skin · cracked(CAN)LH HORIZONTAL STABILIZER LEADING EDGE OUTER SKIN AT STA 89 CRACKED. REPAIRED SRM 51-140-14.SDR CA951204014Mounts · cracked(CAN)LH HORIZONTAL STABILIZER LEADING EDGE ASSEMBLY STA 156 AND STA 162 COMPENSATOR MOUNTS CRACKED. REPAIRED SRM 51-140-20.SDR CA951204013Skin · cracked(CAN)LH HORIZONTAL STABILIZER STA 219 UPPER SKIN CRACKED. REPAIRED DWG #SK382-55-024.SDR CA951204012Skin · cracked(CAN)RH SIDE FUSELAGE SKIN STA 437-477 WL200 DOUBLER CHANNEL CRACKED. REPLACED.SDR CA951204011Panel · cracked(CAN)LH WHEEL WELL STA 617 WL170-195 BL61-82 PANEL CRACKED. REPLACED.SDR CA951204010Cline Cap · cracked(CAN)BL61 LH AND RH STA 697-737 WL146 CLINE CAP FLOOR "Z" CRACKED REPLACED.SDR CA951204009Panel · cracked(CAN)LH ATTIC WEB PANEL STA 596-617 BL61.6 WL270-284 CRACKED. REPAIRED IN ACCORDANCE WITH TRANSPORT CANADA APPROVAL W-RA95-106 ISSUE 1.
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