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 SRAA970717Duct · failedON ENGINE START, FLIGHT 514 OUT OF LTBA, NR 1 ENGINE NACELLE OVERHEAT LIGHT CAME ON. ENGINE START TERMINATED AS QRH. REMOVED AND REPLACED AIR DUCT BETWEEN START VALVE AND STARTER. OPS CHK AND LEAK CHK GOOD IAW MM CH 80.SDR SRAA970716Fire Loop · brokenON PREFLIGHT OUT OF AAB, FLIGHT 513, NR 3 ENGINE FIRE WARNING WOULD NOT TEST. REPLACE FIRE WARNING ELEMENT IAW MM CH 26, OPS CK GOOD.SDR SRAA970702Connector · looseAT DEPARTURE, FOUND NR 4 FIRE WARNING SYSTEM WOULD NOT TEST. FOUND LOOSE CONNECTION AT FIREWALL. SECURED CONNECTOR AND SYSTEM OPS CHECKED GOOD PER MM CH 26.SDR SRAA970701Connector · looseAT DEPARTURE, FOUND NR 4 FIRE WARNING SYSTEM WOULD NOT TEST. FOUND LOOSE CONNECTION AT FIREWALL, SECURED CONNECTOR AND SYSTEM OPS CHECKED GOOD PER MM CH 26.SDR SRAA970616Indicator Socket · defectiveNR 4 ENGINE LOW OIL PRESSURE LIGHT CAME ON DURING CRUISE, OIL PRESSURE GAUGE READ 240 PSI, FOR GEARBOX, 50 PSI FOR ENGINE, QUANTITY AT 10.5 GAL AND OIL TEMP AT 80 DEG. SHUTDOWN ENGINE AS PRECAUTIONARY AND LANDED WITHOUT INCIDENT. FOUND LIGHT SOCKET ON OIL PRSDR SRAA970612Window · short circuitDURING FLIGHT, CO-PILOT'S CENTER SIDE WINDOW NESA SMOKED AND SPARKED. PULLED CIRCUIT BRAKER, SPARKING CONDITION CEASED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED WINDOW AND DEFERRED PER MEL 30-12.SDR SRAA970611Fire Loop · wornON TAXI OUT, NR 1 ENGINE FIRE WARNING FLICKERED ON. AIRCRAFT RETURNED TO BLOCK. FOUND FIRE LOOP IN DRY BAY NR 1 DEFECTIVE. REPLACED FIRE LOOP, SYSTEM OPS CHECKED GOOD PER MM CH 26.SDR SRAA970607Atc Transponder · inoperativeAFTER TAKEOFF, ATC TRANSPONDER WENT INOP. ACCOMPLISHED AIR TURNBACK TO CHS WITHOUT INCIDENT. REPLACED TRANSPONDER, SYSTEM OPS CHECKED GOOD PER MM 34.SDR SRAA970519Battery · dischargedDURING DEBRIEF AT MHZ, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT WEAK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY, SYSTEM OPS CHECKED GOOD PER MM CH 33.SDR SRAA970516Valve Housing · defectiveDURING FLIGHT 527 FROM LERT TO LEMO, NR 4 PROPELLER RPM DECAYED TO 975, SHUT DOWN ENGINE AS PRECAUTIONARY AND LANDED WITHOUT INCIDENT. FOUND NR 4 PROPELLER VALVE HOUSING DEFECTIVE, REPLACED VALVE HOUSING IAW SAT J/C'S 6101, 6101-1, AND PERFORMED ENGINE RUN PESDR SRAA970511Engine · failedFLIGHT 527 REPORTED NR 1 ENGINE CAUSES FUMES FROM BOTH AIR CONDITIONING SYSTEMS WHEN BLEED IS OPEN. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY PER J/C 7101 AND 7101-2 AND RETURNED TO SERVICE.SDR SRAA970420Valve Housing · bearing failedSHUTDOWN OF NR 4 ENGINE DUE TO SUSPECTED DECOUPLE APPROX 30 MIN. AFTER TAKEOFF FROM LCK. RETURNED TO LCK AND LANDED WITHOUT INCIDENT. FOUND NO DECOUPLE CONDITION, NR 4 PROPELLER VALVE HOUSING ASS'Y HAD FAILED BEARING. REPLACED NR 4 PROP AND VALVE HOUSING SDR SRAA970419Light · inoperativeON PREFLIGHT, FOUND 1 EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY EXIT LIGHT ASS'Y AND OPS CHECK GOOD PER MM CH 33.SDR SRAA970417Downlock Switch · failedON APPROACH, INTERMITTENT INTRANSIT INDICATION ON NLG. VISUALLY CONFIRMED GEAR DOWN AND LANDED WITHOUT INCIDENT. REPLACED NLG DOWNLOCK SWITCH AND OPS CHECKED PER MM 32-33 AND RETURNED TO SERVICE.SDR SRAA970416Wire · brokenNLG INDICATION WENT INTRANSIT ON TAXI IN AFTER LANDING. REPAIRED BROKEN WIRE ON NLG DOWNLOCK SWITCH AND OPS CHECK PER MM 32-33 AND RETURNED TO SERVICE.SDR SRAA970403Wire · brokenON PRE-FLIGHT INSPECTION FOUND NR 2 NACELLE OVERHEAT WOULD NOT TEST. FOUND LOWER RIGHT AFT SIDE OVERHEAT DETECTOR HAD BROKEN WIRE, REPAIRED BROKEN WIRE, SYSTEM OPS CHECKED GOOD PER M.M. CH 26-10-4.SDR SRAA970401Switch · stickingDURING FLIGHT 1901, FOUND RUDDER TRIM INOP. DUMPED 5,000 LB OF FUEL AND ACCOMPLISHED AIR TURNBACK TO ANC. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED RUDDER TRIM, FOUND TRIM SWITCH STICKING. REMOVED TRIM SWITCH, CLEANED AND REINSTALLED UNIT, SYTSTEM OPS CSDR SRAA970307Light · dimDURING PREFLIGHT INSPECTION, FOUND FLIGHT DECK ESCAPE HATCH EMERGENCY LIGHT DIM. REMOVED AND REPLACED FLIGHT DECK EMERGENCY LIGHT ASSEMBLY, SYSTEM OPS CHECKED GOOD PER MM CH 33-10.SDR SRAA970301Engine · defectiveDURING TAXI IN FROM FLIGHT 507 AT MHZ, NOTICED OIL FUMES COMING FROM AIR CONDITIONING SYSTEM, SHUT DOWN AIR CONDITIONING SYSTEM. REPLACED NR 3 ENGINE, PERFORMED ENGINE RUN-UP PER J/C 7101, 7101-2 AND 7103 NO DEFECTS FOUND.SDR SRAA970208Fitting · crackedPOST FLIGHT INSPECTION, FOUND A .75 INCH CRACK AND A 2 INCH CRACK IN THE VERTICAL SUPPORT FITTING AT FS 858. ITEM IS BEING REPAIRED.SDR SRAA970207Fitting · looseON ENGINE START AT RMS FOR FLIGHT 507, FOUND SMOKE IN COCKPIT WHILE NR 3 ENGINE WAS RUNNING, ABORTED ENGINE START. MOTORED NR 3 ENGINE, FOUND ENGINE OIL LEAK AT GEARBOX OIL PUMP FITTING. TIGHTENED FITTING IAW MM CH 79 AND CLEANED INTAKE AREA. PERFORMED ENGSDR CA970226044Stringer · cracked(CAN) CENTRE WING STRINGER 18, BL 57 AND FS 559 INSIDE CENTRE DRY BAY CRACKED - 2.0" ON THE LOWER FLANGE. REPAIRED.SDR CA970226043Rib Cap · cracked(CAN) CENTRE WING STA 178.8 R/H INBOARD UPPER RIB CAP FITTING CRACKED AT UPPER FORWARD TRUSS MOUNT ATTACHMENT HOLE. REPLACED.SDR CA970226042Sword Fitting · cracked(CAN) R/H WING OWS 303 SWORD FITTING CRACKED. REPLACED.SDR CA970226041Spar Web · cracked(CAN) CENTRE WING FORWARD SPAR WEB CRACKED - 0.75" AT C.W.S. 17.5R AND WL 274. REPAIRED.SDR CA970226040Ring · cracked(CAN) FUSELAGE STA 807OE, BL 63L AND WL 160, RING SEGMENT CRACKED - 1.5". REPLACED.SDR CA970226039Beam · cracked(CAN) FUSELAGE STA 597, L/H VERTICAL LANDING GEAR BEAM CRACKED - 1.25", AT VERTICAL LEG CUTOUT. REPLACED.SDR CA970226038Beam · cracked(CAN) FUSELAGE STA 528, L/H VERTICAL LANDING GEAR BEAM OUTBOARD CAP CRACKED AT HORIZONTAL TIE POINT. REPAIRED.SDR CA970226037Beam Web · cracked(CAN) FUSELAGE STA 517, AND WL 230, LH VERTICAL LANDING GEAR BEAM WEB AND OUTBOARD CAP CRACKED. REPAIRED.SDR CA970226036Splice · cracked(CAN) FUSELAGE STA 617, BL 20L AND R, LONGERON SPLICE FITTING CRACKED. REPLACED.SDR CA970226035Frame · cracked(CAN) FUSELAGE STA 617, BL 25L, UPPER FRAME CRACKED - 2.75" BETWEEN THREE FASTENERS. REPAIRED.SDR CA970226034Fitting · cracked(CAN) FUSELAGE STA 617, BL 60R AND WL 146 FITTING CRACKED - 0.25". REPLACED.SDR CA970226033Skin · cracked(CAN) CARGO DOOR SKIN CRACKED AT SAFETY VALVE LOCATION. REPAIRED.SDR CA970226032Web · cracked(CAN) FUSELAGE STA 1040, BL 25R CARGO DOOR BULKHEAD WEB CRACKED IN THREE LOCATIONS. REPLACED.SDR CA970226031Chine Cap · corroded(CAN) CARGO RAMP RH CHINE CAP CORRODED BEYOND LIMITS. REPLACED.SDR CA970226030Chine Cap · cracked(CAN) CARGO RAMP LH CHINE CAP CRACKED - 1.5", AND CORRODED BEYOND LIMITS. REPLACED.SDR CA970226029Chine Cap · corroded(CAN) FUSELAGE STA 737 TO 817OE, BL 60R AND WL 146, AFT CHINE CAP CORRODED BEYOND LIMITS. REPLACED.SDR CA970226028Cap · cracked(CAN) FUSELAGE STA 557, BL 58R AND WL 146, CENTRE CHINE CAP CRACKED - 1.0". REPLACED.SDR CA970226027Fitting · cracked(CAN) FUSELAGE STA 817OE, BL 60L AND WL 146, FLOOR RING BULKHEAD FITTING CRACKED - 1.5". REPLACED.SDR CA970226026Cap · corroded(CAN) FUSELAGE STA 817OE, BULKHEAD LOWER CAP CORRODED BEYOND LIMITS. REPLACED.SDR CA970226025Upper Cap · cracked(CAN) FUSELAGE STA 817OE, BULKHEAD UPPER CAP CRACKED IN THE RADIUS AND CORRODED BEYOND LIMITS. REPLACED.SDR CA970226024Web · corroded(CAN) FUSELAGE STA 817OE, BULKHEAD WEBS (3) CORRODED BEYOND LIMITS. REPLACED.SDR CA970226023Ramp Hinge · corroded(CAN) FUSELAGE STA 817OE, BL 31.9L AND R, RAMP HINGE SUPPORTS CORRODED BEYOND LIMITS. REPLACED.SDR CA970226022Web · cracked(CAN) FUSELAGE STA 902, BL 60R AND WL 225, BULKHEAD WEB CRACKED - 3.0". REPLACED.SDR CA970226021Cap · cracked(CAN) FUSELAGE STA 930, BL 60L AND WL 230, BULKHEAD INBOARD CAP CRACKED - 1.5". REPLACED.SDR CA970226020Web · cracked(CAN) FUSELAGE STA 930, BL 60R AND WL 235, BULKHEAD WEB UPPER END CRACKED - 2.5". REPAIRED.SDR CA970226019Cap · cracked(CAN) FUSELAGE STA 990, BL 60R AND WL 240, BULKHEAD WEB AND INBOARD CAP CRACKED -2.25". REPLACED.SDR CA970226018Frame · cracked(CAN) FUSELAGE STA 836, BL 6L AND R UPPER FRAME CRACKED - 0.5 AT DORSAL FIN ATTACH FASTENER LOCATIONS. REPAIRED.SDR CA970226017Bulkhead · cracked(CAN) FUSELAGE STA 950, BL 60L AND WL 262 BULKHEAD INBOARD CAP CRACKED - 0.75". NEW CAP INSTALLED.SDR CA970226016Web · cracked(CAN) FUSELAGE STA 990, BL 60L AND WL 265 BULKHEAD WEB AND INBOARD CAP CRACKED, REPAIRED.
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