Lockheed 382G
Service difficulty reports · 5,734
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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 CA970226015Skin · puncture(CAN) FUSELAGE STA 902 RH AND WL 202 HAS SMALL PUNCTURE NEAR AN EXISTING REPAIR. EXISTING REPAIR REMOVED AND ENTIRE DAMAGED AREA REPAIRED.SDR CA970226014Web · cracked(CAN) FUSELAGE STA 597 TO 560, BL61 TO 84L AND WL 200 WHEEL WELL WEB FOUND CRACKED AT STA 575 - 2.75". REPAIRED.SDR CA970226013Web · cracked(CAN) FUSELAGE STA 597 TO 560, BL 61 TO 84R AND WL 200 WHEEL WELL WEB CRACKED AT STA 590 - 1.75" AND CORRODED BEYOND LIMITS. REPAIRED.SDR CA970226012Web · corroded(CAN) FUSELAGE STA 560 TO 517, BL 61 TO 84R AND WL 200, WHEEL WELL WEB HAS PITTING AND CORROSION BEYOND LIMITS. REPAIRED.SDR CA970226011Doubler · cracked(CAN) FUSELAGE STA 880, BL 61L AND WL 207 INBOARD CAP. WEB DOUBLER AND OUTBOARD CAP CRACKED. REPLACED.SDR CA970226010Skin · damage(CAN) FUSELAGE SKIN FROM STA 737-817OE AND WL 141 TO 190, LH AND RH MODERATE STONE DAMAGE. REPLACED.SDR SRAA970205Control Box · malfunctionedDURING TAXI OUT, BRAKES WENT INOP WITH ANTI-SKID ON. AIRCRAFT RETURNED TO BLOCK. FOUND ANTI-SKID CONTROL BOX MALFUNCTIONED. REPLACED ANTI-SKID CONTROL BOX, SYSTEM OPS CHECKED GOOD PER MM CH 32.SDR SRAA970114Control Box · malfunctionedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RECYCLED 3 TIMES, NO CHANGE. RETURNED AND AIRCRAFT LANDED WITHOUT INCIDENT. FOUND LANDING GEAR CONTROL BOX DEFECTIVE. REMOVED AND REPLACED IAW MM CH 32-33. RETRACTION AND EMERGENCY EXTENSION OPS CHECKED GOOD.SDR SRAA970112Temp Ctr Valve · inoperativeCARGO COMPARTMENT OVERHEAT ILLUMINATED ON TAXI. FOUND TEMPERATURE CONTROL VALVE INOPERABLE. REPLACED VALVE AND OPERATIONAL CHECK GOOD PER IAW MM CH 21.SDR SRAA961209Skin · crackedON WALKAROUND INSPECTION, FOUND RIGHT WING LEADING EDGE HAS A 5 INCH CRACK IN LOWER SURFACE AT O/B WING STATION 36. REPAIRED LEADING EDGE PER SRM FIG 51-140-12.SDR SRAA961206Tire · blownON TAXI OUT FOR FLIGHT 1008, RIGHT FORWARD MAIN WHEEL HAD A TIRE BLOWN OUT, SUSPECT RIM FAILURE, AIRCRAFT RETURNED TO BLOCK. VERIFIED RT FORWARD WHEEL ASSY HAD RIM FAILURE, REPLACED RT FORWARD AND AFT MAIN WHEELS, O/B MLG DOOR, SHEARED ACTUATOR ROD, 3 EACH DOSDR SRAA961202Batteries · dischargedDURING PREFLIGHT INSPECTION, FOUND EMERGENCY EXIT LIGHTS WEAK. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERIES IAW MM CH 33, OPS CHECKED GOOD.SDR SRAA961117Wheel · failedDURING TAXI OUT, THE LEFT FRONT MAIN WHEEL BLEW DUE TO FLANGE SEPARATION. AIRCRAFT RETURNED TO BLOCK. FOUND LEFT MLG OUTER DOOR DAMAGED, VERIFIED WHEEL FAILURE. REMOVED AND REPLACED LEFT FWD MAIN WHEEL ASSY. REMOVED LT MLG OUTER AND INNER DOOR PER AFM 1 TOSDR CA961128014Torquemeter · loose(CAN) IN CRUISE NR 3 ENGINE TORQUE INDICATION FAILED. POST FLIGHT MAINTENANCE INSPECTION FOUND THE TORQUE PICKUP TO BE RUBBING ON THE TORQUE SHAFT AND SOME TORQUEMETER ATTACHMENT NUTS MISSING AT THE REDUCTION GEARBOX ATTACH POINT. AIRCRAFT FERRIED FOR ENGINESDR SRAA961112Propeller · damagedON WALKAROUND, FOUND NR 2 PROPELLER HAD DAMAGE AT BLADE CUFFS TRAILING EDGES FROM CONTACTING AFTERBODY FAIRING. ACCOMPLISH THREE ENGINE FERRY TO MHZ. REPLACED NR 2 PROPELLER ASSEMBLY, AFTERBODY FAIRING PER SAT JOB CARDS 6101, 6101-1, 6102 AND PERFORMED OPS SDR SRAA961107Bushing · missingON APPROACH, RIGHT MAIN LANDING GEAR HAD UNSAFE WARNING INDICATION. FOUND AFT RT MAIN LANDING GEAR SHELF BRACKET BROKEN, TIED DOWN RT GEAR AND DECLARED EMERGENCY FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED RIGHT MAIN LANDING GEAR SHELF BRACKET,SDR SRAA961109Beam · crackedPOST-FLIGHT INSPECTION AT MHZ FOUND RIGHT WHEELWELL BOW BEAM CRACKED AT STA 557, WL 170. REPAIRED BOW BEAM CRACK PER SRM 53-40-12.SDR SRAA961106Strut · crackedON POST-FLIGHT INSPECTION, FOUND VERTICAL STRUT BRACE ON RHS AT FUSELAGE STATION 858 CRACKED. REPLACED STRUT ASSEMBLY PER M.M. CH 53.SDR SRAA961105Fitting · crackedPOST FLIGHT INSPECTION FOUND THE STRUT BRACE ATTACH FITTING AT STATION 938 CRACKED. REPAIRED AFT FUSELAGE LOWER LONGERON FITTING AT STATION 938 IAW SRM CH 53-50-26, OPS CHECKED RAMP AND DOOR, SYSTEM OPS CHECKED GOOD.SDR SRAA961104Cooling Turbine · inoperativeON TAXI OUT, CARGO COMPARTMENT OVERHEAT WARNING LIGHT CAME ON, AIRCRAFT RETURNED TO BLOCK. FOUND CARGO COMPARTMENT COOLING TURBINE INOPERATIVE, REPLACED COOLING TURBINE, SYSTEM OPS CHECKED GOOD PER M.M. CH 21-00.SDR SRAA961101Gasket · blownDURING FLIGHT, CARGO COMPARTMENT OVERHEAT LIGHT CAME ON AT FL230. SHUT OFF AIR CONDITIONING SYSTEM PER QUICK REFERENCE HANDBOOK, AIRCRAFT LANDED WITHOUT INCIDENT. FOUND UNDER FLOOR HEAT SHUTOFF VALVE HAD BLOWN GASKET. REPLACED GASKET, SYSTEM OPS CHECKED GOOSDR CA961104005Starter · worn jaws(CAN) #3 ENGINE WOULD NOT ENGAGE DURING START SEQUENCE. JAWS EXCESSIVELY WORN, REPLACED.SDR SRAA961015Valve · defectiveDURING FLIGHT, NR 2 ENGINE RPM DECAYED RAPIDLY. SHUT DOWN NR 2 ENGINE AND LANDED WITHOUT INCIDENT. FOUND NR 2 ENGINE VALVE HOUSING DEFECTIVE. REPLACED NR 2 PROP VALVE HOUSING, PERFORMED ENGINE RUN SYSTEM OPS CHECKED GOOD PER SAT J/C 6103, 7101 AND 7101-2.SDR CA961104006Starter · worn jaws(CAN) #1 STARTER WOULD NOT ENGAGE AT ENGINE START. TEETH ON STARTER JAWS WORN, REPLACED.SDR SRAA961013Propeller · oil leakNR 4 PROP LOW OIL LIGHT CAME ON WITH RPM OUT OF LIMITS, SHUT DOWN ENGINE IN FLIGHT AND AT THE SAME TIME NR 3 ENGINE PROP LOW OIL LIGHT CAME ON. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND NR 4 PROP LEAKING EXCESSIVELY AT NR 1 AND NR 2 BLADES, SERVISDR SRAA961012Track · crackedDURING WALK AROUND INSPECTION, FOUND ON RIGHT WING O/B FLAP VERTICAL BEAM I/B TRACK CRACKED FROM LOWER WING SURFACE AND TRAVELS UPWARD APPROX 50 PERCENT OF VERT FITT, SIMILAR CRACK WAS FOUND ON LEFT WING I/B FLAP O/B TRACK. ALSO, FOUND THE LT O/B TRACK FORMERSDR SRAA961088Frame · corrosionDURING C-CHECK, FOUND LEVEL 1 CORROSION AT RT O/B CARGO COMPARTMENT Z-FRAME AT FS 444, BL 61, WL 146. CUT OFF CORRODED END OF RING SEGMENT, FABRICATED FORMED AND INSTALLED 2 L-ANGLES AND 1 Z-FILLER IAW LAC SRM 51-140-21.SDR SRAA961083Support Beam · corrosionDURING C-CHECK FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS 297OE, BL ZERO HAS CORROSION AT FORWARD AND AFT SIDE OF UPPER CAP BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED NEW FILLER L-ANGLE AND STRAP IAW LAC SRM CHAPTER 51-140-SDR SRAA961081Angle · crackedDURING C-CHECK, FOUND A 2 INCH CRACK AT ACCESS PANEL SUPPORT ANGLE IN UPPER LEFT MLG WHEELWELL O/B SIDE OF WL 200, FS 507. CUT OUT CRACKED AREA, FABRICATED A FILLER TO EXISTING DOUBLER IAW LAC SRM 51-70-01, 53-60-02 AND 51-140-02.SDR SRAA961060Support Beam · corrosionDURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS 697, LBL 40 HAS CORROSION AT FORWARD AND AFT SIDE BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED FILLER AND L-ANGLE, DOUBLER AND STRAP DOUBLER IAW LAC SRM CHAPTER 51-40-SDR SRAA961051Support · corrosionDURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS 295, LBL 40 HAS CORROSION AT FORWARD SIDE BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED FLOORBEAM REPAIR AND 2 STRAPS LAC SRM CHAPTER 51-40-22.SDR SRAA961049Support · corrosionDURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS 275, LBL 40 HAS CORROSION AT FORWARD AND AFT SIDE BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED L-ANGLE AND STRAP IAW LAC SRM CHAPTER 51-140-22 AND 51-70-1.SDR SRAA961042Support · corrosionDURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS 697, RBL 20 HAS CORROSION AT FORWARD AND AFT SIDE BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED L-ANGLE AND STRAP IAW LAC SRM CH 51-140-22.SDR SRAA961035Frame · crackedDURING C-CHECK, FOUND RIGHT WHEEL WELL HAS A CRACK IN FRAME STA 667, TOP OF CORNER MEASURED 3 INCHES. STOP DRILLED CRACK, FABRICATED AND INSTALLED L-ANGLE. REPAIRED IAW LAC SRM 51-140-20 AND 51-60-12A, 51-80-08, AND 51-70-01.SDR SRAA961034Skin · crackedDURING C-CK, FOUND UPPER SECTION OF LT MAIN LANDING GEAR WHEEL WELL HAS A CRACK IN INNER SKIN NEAR ATTACH ANGLE ON O/B SIDE AT WL 200 STA 507. CRACK MEASURED 2 INCH LENGTH. FOUND CRACK OUT OF LIMITS, CUT OUT AREA FABRICATED AND INSTALLED FILLER TO EXISTING DSDR SRAA961030Fitting · crackedDURING C-CHECK, FOUND FITTING AT FUSELAGE STA. 1012 LHS BL 72.70 CRACKED COMPLETELY THROUGH. REMOVED CRACKED FITTING, INSTALLED NEW T-ANGLE FITTING, FABRICATED AND INSTALLED NEW WEB ASS'Y IAW LAC SRM CHAPTER 53-40-04 PG 10.SDR SRAA961007Fitting · crackedPOST FLIGHT INSPECTION, FOUND BOW BEAM FITTING ON LEFT HAND SIDE FS 557 CRACKED. ACCOMPLISHED BOW BEAM FITTING REPAIR PER LOCKHEED SRM 53-40-12.SDR SRAA1074Floorbeam · corrosionDURING C-CHECK, FOUND CORROSION ON CARGO COMPARTMENT FLOORBEAM AT TIE DOWN MOUNT HOLES FS 737E BL 0. REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED L-ANGLE AND STRAP IAW LAC SRM 51-140-22.SDR SRAA1070Support Beam · corrosionDURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS 537, RBL 20 HAS CORROSION AT FOWARD AND AFT SIDE BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED L-ANGLE, FILLER, STRAP AND DOUBLER IAW LAC SRM CHAPTER 51-140-22.SDR SRAA1066Support Beam · corrosionDURING C-CHECK, FOUND CARGO COMPARTMENT FLOOR PANEL SUPPORT BEAM AT FS.497, LBL 40 AND 20 HAS CORROSION AT FORWARD AND AFT SIDE BEYOND LIMITS. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED SECTION UPPER CAP, 2 L-ANGLES, STRAPS AND FILLER IAW LAC SRM CHASDR CA961112016Detection Unit · intermittent(CAN) IN CRUISE #3 ENGINE FIRE WARNING LIGHT CAME ON. ENGINE SHUT DOWN IN FLIGHT, AIRCRAFT LANDED WITHOUT INCIDENT. FAULT WITH FIRE DETECTION UNIT. REPLACED.SDR CA961024009Detection Unit · intermittent(CAN) IN CRUISE #3 ENGINE FIRE WARNING ILLUMINATED. ENGINE SHUT DOWN. LANDED WITHOUT INCIDENT. FIRE DETECTION UNIT REPLACED.SDR SRAA961005Retract Mech · out of adjustDURING FINAL APPROACH, LEFT MAIN LANDING GEAR FAILED TO LOCK IN DOWN POSITION USING NORMAL PROCEDURE. MANUALLY EXTENDED LEFT MLG TO DOWN AND LOCK BY AOM PROCEDURE. AIRCRAFT LANDED WITHOUT INCIDENT. PLACED AIRCRAFT ON JACKS AND PERFORMED GEAR RETRACTION CHECSDR CA961112015Wiring Harness · intermittent(CAN) ON ROTATION #3 CHIP DETECTOR LIGHT ON INTERMITTENTLY. POWER WAS REDUCED AND DETECTOR LIGHT OUT. LANDED WITHOUT INCIDENT. WIRING HARNESS PROBLEM. REPAIRED.SDR SRAA961002Fittings · crackedON PRE-FLIGHT INSPECTION AT HOW, FOUND AIRCRAFT FUSELAGE FITTINGS AT STA 780 AND 830 CRACKED. ADDITIONAL INSPECTION FOUND TOTAL OF THREE CARGO COMPARTMENT SUPPORT STRUTS ATTACH UPPER FITTINGS CRACKED AT FS 869 RT, FS 803 LT, AND FS 825 LT. REPLACED THREE SUPSDR SRAA960913Strut Shoe · defectiveAFTER TAKEOFF, RIGHT MAIN LANDING GEAR UNSAFE LIGHT CAME ON, CYCLED GEAR AND VERIFIED IN DOWN AND LOCKED POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED RIGHT MAIN LANDING GEAR, FOUND RT AFT STRUT SHOE FACINGS DEFECTIVE AND RT FORWARD STRUT BALL SCREW SDR CA961024007Screwjacks · dirty(CAN) ON APPROACH LH MAIN LANDING GEAR WOULD NOT EXTEND WHEN GEAR SELECTED DOWN. APPROACH WAS ABORTED AND ATC CONFIRMED LH MAIN LANDING GEAR DOOR WAS CLOSED AND GEAR NOT VISIBLE. LH GEAR MANUALLY LOWERED AND LANDING CARRIED OUT. SCREWJACK CONTAMINATED WITH MOISDR SRAA960910Switch · defectiveAFTER TAKEOFF, FOUND RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. ACCOMPLISHED AIR TURNBACK, AIRCRAFT LANDED WITHOUT INCIDENT. PERFORMED MLG RETRACTION TEST, FOUND UPLOCK SWITCH DEFECTIVE. REPLACED SWITCH AND CYCLED GEARS, SYSTEM OPS CHECKED GOOD.SDR SRAA960909Gaskets · leakingDURING CRUISE INTO PHL. FLT 9010, NR 2 NACELLE OVERHEAT LIGHT CAME ON, SHUT DOWN ENGINE AND LANDED WITHOUT INCIDENT AT PHL. FOUND SCOOP ANTI-ICE LINE ON LEFT HAND SIDE OF ENGINE LEAKING, REPLACED TWO GASKETS AND PERFORMED BLEED AIR LEAK CHECK, PER M.M. CH 75.SDR SRAA960907Duct Seal · failedDURING FLIGHT, NR 2 NACELLE OVERHEAT LIGHT CAME ON APPROXIMATELY FIVE MINUTES AFTER LEVELED OFF. SHUTDOWN ENGINE AND ACCOMPLISHED AIR TURNBACK TO CHS, AIRCRAFT LANDED WITHOUT INCIDENT. FOUND F-DUCT SEAL DETERIORATED. RESEALED F-DUCT PER MM CH 72 AND ACCOMPL
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