Douglas DC-9-32
Service difficulty reports · 12,755
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 = 'DC932' 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 = 'DC932' 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 9516299926Blkhd Fitting · crackedDURING H-CHECK, FOUND A CRACK IN THE LOWER RIGHT HORIZONTAL STIFFENER END FITTING AT THE FS 521 BULKHEAD. REPLACED FITTING PER SRM 51-30-2.SDR 9516289603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FLOOR ATTACH FITTING AT FS 980, LONGERON 8L. REPLACED FITTING.SDR 9516279603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LOWER FLOORBEAM ATTACH FITTING AT FS 465, LBL 54. REPLACED FITTING (P/N 4911383-1), PER SRM 51-10-3.SDR 9516189921Up Latch Assy · malfunctionedDURING CLIMB, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR UPLATCH ASSSDR 9516169921Up Limit Switch · malfunctionedDURING CLIMB, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GEAR AND LIGHT REMAINED ILLUMINATED. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR UP LIMISDR CAL951054Door Jamb · crackedHOU - INSPECTION FOUND A 2 INCH CRACK AT LEFT LOWER CORNER OF AFT PRESSURE BULKHEAD DOOR JAMB. THE DOOR JAMB WAS REPAIRED IAW ECRA 5310-03176 AND EA 653A006. (M)SDR 96ZZZX918Control Cable · misroutedDUE TO CABLE MISRIGGING, LEFT THRUST REVERSER CABLE CHAFED THROUGH THE FORWARD PULLEY MOUNTING BRACKET UNDER THE COCKPIT PEDESTAL.SDR 95ZZZX6237Engine · malfunctionedATL/MDW - FLT 248 - THE CAPTAIN CALLED BACK WITH ENGINE VIBRATION. THE AIRCRAFT RETURNED TO ATL. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE. OPS CHECKED OK.SDR ABXA9600180Panel · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WING UPPER TRAILING EDGE PANEL AT XRS 531 DELAMINATED. REPLACED TRAILING EDGE PANEL IAW DC-9 SRM 51-30-1 AND 51-30-2.SDR ABXA9600178Longeron · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 30 CRACKED BETWEEN FS 560 AND FS 579. REPLACED LONGERON 30 IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR 95ZZZM646Pack · inopON FLT 440 - ATL - AIR RETURN, THE RIGH PACK OVERHEATED IN FLIGHT. THE TEMP CONTROL KNOB HAD NO EFFECT ON VALVE POSITION WHICH WAS IN FULL HOT. ASSIGNED MEL NR DM5116, SEQ 21-01 RIGHT PACK INOP.SDR 9518559926Frame · crackedDURING H-CHECK, FOUND CRACKS IN ALL FOUR OVERWING EMERGENCY EXIT DOOR PANS, BENEATH NR 14 SUPPORT. REPAIRED PANS (P/N 5913195-1) PER EA 99-103294, -103295, -103296 AND -103297.SDR MWEA95352Slide Cover · fell offDURING SERVICE CHECK, FOUND FWD GALLEY SERVICE DOOR EVACUATION SLIDE COVER HAD FALLEN OFF. MAINTENANCE REINSTALLED EVAC SLIDE COVER AND RETURNED A/C TO SERVICE.SDR ABXA9600159Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE INTERIOR FUSELAGE SKIN CORRODED AT LONGERON 17R BETWEEN FS 658 AND 680. REPAIRED SKIN IAW ABX REA D953-13156-MR.SDR 9516259920Fitting · corrodedDURING H-CHECK, FOUND CORROSION AND A CRACK IN THE FLOOR SUPPORT STRAP FITTINGS FS 896 AND 965 ABOVE LONGERON 28L. REPLACED FITTINGS PER SRM 53-11-3 FIG 3A.SDR 9516249601Mount Assy · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN BOTH THE LEFT AND RIGHT PYLON FORWARD ENGINE MOUNT ISOLATOR HOUSINGS. REPLACED BOTH YOKE ASSEMBLIES PER MM 71-20-3.SDR 9516239601Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE LEFT MAIN LANDING GEAR WHEEL WELL AFT KEEL BEAM FITTING. REPLACED FITTING PER SRM 51-30-2.SDR ABXA9500962Jamb · dentedDURING C-CHECK INSPECTION, FOUND SERVICE DOOR JAMB DENTED. REPAIRED IAW ABX REA D953-12952-MR.SDR 9522049601Spar Cap · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING REAR SPAR LOWER CAP XRS 477-509. REPAIRED CAP (P/N 5911301), PER EA 12-5720-9-C0486.SDR 9515649613Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A 1.2 INCH CRACK IN THE HORIZONTAL STABILIZER CENTER BOX T-FITTING AT THE FORWARD UPPER SPAR. REPLACED FITTING PER SRM 51-30.SDR MWEA95350Eel Battery · dischargedCREW REPORTED FORWARD CABIN EMERGENCY FLASHLIGHT DOES NOT FLASH THE TEST LIGHT. MAINTENANCE REMOVED AND REPLACED BATTERY. AIRCRAFT RETURNED TO SERVICE.SDR ABXA9600120Retainer · crackedDURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 56-11 REV 3, FOUND THE LEFT SLIDING WINDOW FRAME CRACKED IN THE UPPER AFT CORNER. REPLACED DOUBLERS IAW DC-9 SRM 56-01 AND ABX REA D956-13036-SB.SDR ABXA9500980Intercostal · damagedDURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN THE INTERCOSTAL AT STA 370, LONGERON 28R. REPAIRED IAW ABX REA D953-13047-MR.SDR ABXA9500979Former · misdrilledDURING C-CHECK INSPECTION, FOUND MISDRILLED HOLES IN THE FORMER AT STA 370, LONGERON 28R. REPAIRED IAW ABX REA D953-13047-MR.SDR 9522039601Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING STRINGERS 17L AND 19L OUTBOARD OF STA 58 WEB. REPAIRED STRINGER PER EA 12-5720-9-C0543.SDR 9522029601Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FUSELAGE SKIN FS 770 BETWEEN LONGERONS 18L TO 19L. REPAIRED SKIN PER EA 12-5330-9-C0603.SDR 9515639601Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND TWO CRACKS IN THE LEFT WING NR 5 SLAT INBOARD IDLER TRACK ATTACH FITTING. REPLACED FITTING PER SRM 51-30-2.SDR 9515629601Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LONGERON 18L TIE FITTING AT THE FS 980 FRAME. REPLACED FITTING PER SRM 51-30-2.SDR 9515619601Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 17L LONGERON TENSION TIE FITTING AT THE FS 996 FRAME. REPLACED FITTING PER SRM 51-30-05.SDR 9515609601Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 160 FRAME TO FLOOR FITTING AT LONGERON 17R TO 18R. REPLACED FITTING PER SRM 51-30-2.SDR 9515599601Fittings · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LBL 50 TO 55 FRAME TO FLOOR FITTINGS, FS 200 AND FS 208. REPLACED FITTINGS PER SRM 51-30-2.SDR 9515589601Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 795 FRAME TO FLOOR MOUNT FITTING AT LONGERON 18L. REPLACED FITTING PER SRM 51-30-3.SDR 9515319607Switch · malfunctionedDURING APPROACH, LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN LANDING GEAR DOOR SWITCH AND OPERATIONAL TEST GOOD.SDR ABXA9600131Frame · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND A PREVIOUS REPAIR ON FUSELAGE FRAME AT FS 1076 CRACKED BETWEEN LONGERONS 12R AND 13R. REPLACED FUSELAGE FRAME AT FS 1076 IAW DC-9 SRM 51-10-2, 51-10-5 AND 51-30-1.SDR 9515309607Connector · looseDURING APPROACH, LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. RESECURED CANNON PLUG ON LANDING GEAR DOOR INDICATOR SWITCH AND OPERATIONAL CHECK GOOD.SDR 9515299940Warning Light · illuminatedON APPROACH, THE LANDING GEAR LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. A GO-AROUND WAS ACCOMPLISHED, RECYCLED LANDING GEAR AND LIGHT EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED GEAR DOOR SWITCHES FOR SECURITY. OPERATIONAL CHECK GOOD.SDR ABXA9600157Spar · damagedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT WING LOWER REAR SPAR HAD A PREVIOUS REPAIR BETWEEN XRS 509 AND XRS 531 WITH FURTHER DAMAGE. REPAIRED REAR SPAR IAW DC-9 SRM 57-09 FIG 11 AND ABX REA D957-13115-MR.SDR 95ZZZX6368Brake Assy · leakingATL - FLT 522 - FLT RETURNED TO ATL DUE TO HYDRAULIC LEAK. REMOVED AND REPLACED NR 1 BRAKE ASSEMBLY PER MM 32-40.SDR 95ZZZM588Cover · not sealedFLT NR 572 - ATL-MCI - CREW NOTICED FUEL LEAKING FROM RIGHT WING FUEL TANK ACCESS PLATE. FLIGHT RETURNED TO ATL FOR REPAIRS. ATL MAINTENANCE RESEALED RIGHT WING UPPER TANK PLATE BL 1426.SDR ABXA9500955Doubler · corrodedDURING C-CHECK INSPECTION, FOUND EXCESSIVE CORROSION ON AFT LOWER CARGO DOOR DOUBLER. REPAIRED DOUBLER IAW ABX REA D953-12953-MR.SDR ABXA9500954Skin · corrodedDURING C-CHECK INSPECTION AND PSE INSPECTION 53.09.035A, AD 94-03-01, FOUND EXCESSIVE CORROSION ON THE FUSELAGE SKIN. REPAIRED SKIN IAW ABX REA D953-12953-MR.SDR 95ZZZX6370Manifold Valve · out of positionATL - FLT 505 - FUEL STREAMING OUT OF RIGHT WING TIP, NOTED ON TAKEOFF AND CLIMB-OUT. AIRCRAFT RETURNED TO ATL. FOUND MANIFOLD DRAIN VALVE STUCK OPEN, REPOSITIONED VALVE. VALVE WAS CLEANED AND OPERATION WAS CHECKED FOR FREEDOM OF MOVEMENT PER MM 28-12.SDR 9515569613Blkhd Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 996 AFT PRESSURE BULKHEAD LOWER FRAME FITTING. REPLACED FITTING PER SRM 51-10-03, 51-30.SDR 95ZZZX6375Supply Line · failedFLT 520 - CENTER TANK VENTED 3,000 POUNDS OF FUEL THROUGH FUEL VENT. REPLACED LEFT WING FUEL SUPPLY PIPE ASSEMBLY.SDR CA951129507Oil Line · leaking(CAN)ON CLIMB OUT, LEFT ENGINE OIL PRESSURE FLICKERED & OIL QUANTITY LOST. LEFT ENGINE SHUT DOWN. AIRCRAFT RETURNED TO DEPARTURE TERMINAL. MAINTENANCE ACTION INVOLVED CHANGING OIL LINE AT OIL FILTER DIFFER ENTIAL PRESSURE SWITCH. AIRCRAFT CHECKED FOR LEAKS ON SDR ABXA9600147Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD UPPER FUSELAGE SKIN HAD CORROSION UNDER THE NR 1 AND NR 2 ADF ANTENNAS. REPAIRED FUSELAGE SKIN IAW ABX REA D953-12833-MR.SDR ABXA9600136Skin · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD UPPER FUSELAGE SKIN HAD CORROSION UNDER THE NR 1 AND NR 2 ADF ANTENNAS. REPAIRED FUSELAGE SKIN IAW ABX REA D953-12833-MR.SDR ABXA9500971Skin · damagedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 94-03-01, FOUND FUSELAGE SKIN DENTED AND CRACKED AT STA 105, LONGERON 18L. REPAIRED IAW ABX REA D953-13037-MR.SDR ABXA9500960Web · cutDURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR.SDR ABXA9500959Web · cutDURING C-CHECK INSPECTION, IT WAS NECESSARY TO CUT CUSP WEB FOR ACCESS TO DO OTHER REPAIRS. REPAIRED CUSP WEB IAW ABX REA D953-13050-MR.
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