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 VJ970340Battery Pack · dischargedFORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED CHARGER NICAD BATTERIES IAW MM 33-50.SDR VJ970339Smoke Detector · malfunctionedSMOKE DETECTOR CHIRPING IN RT AFT LAVATORY. REPLACED SMOKE DETECTOR, OPS CHECKS NORMAL IAW MM 26-00.SDR VJ970338Cover · looseMAIN PASSENGER DOOR EMERGENCY SLIDE COVER CAME LOOSE. REINSTALLED IAW MM 25-60 AND PERFORMED REQUIRED INSPECTION.SDR ABXA9701791Longeron · crackedDURING C-CHECK, FOUND LONGERON 17R CRACKED AT STA 980. REPAIRED LONGERON IAW DC9 SRM 53-02.SDR MWEA97823Temp Sensor · defectiveDURING CLIMB, THE AIRCRAFT TEMP HIGH LIGHT STAYED ON WITH SYSTEM OFF. MTC REMOVED AND REPLACED LT AIRFOIL TEMP HIGH SENSOR.SDR MWEA97822Windshield · crackedTHE CENTER WINDSHIELD WINDOW OUTER PANE CRACKED PASSING THROUGH 10,500 FT. MTC REMOVED AND REPLACED CENTER WINDSHIELD IAW SRM 56-10-1.SDR MWEA97821Skin · crackedDURING C-CHECK, FOUND TWO CRACKS AND A DENT ALONG LOWER EDGE OF AFT CARGO DOOR EXTERIOR SKIN. MTC REPAIRED IAW SRM 52-05 FIG 4.SDR MWEA97820Doubler · crackedDURING C-CHECK, FOUND CRACK ON FWD CARGO DOOR INNER PAN. MTC REPAIRED IAW SRM 52-05 FIG 26A AND 27A.SDR MWEA97819Fitting · crackedDURING C-CHECK, FOUND A CRACKED WEB END FITTING AT FWD CARGO DOOR LOWER AFT DOOR STOP AND CORROSION UNDER FITTING. MTC REPAIRED IAW SRM 51-10-3 AND SRM 52-01 PAGE 1.SDR MWEA97818Fitting · crackedDURING C-CHECK, FOUND AFT CARGO DOOR NR 5 FRAME FWD END END CLIP CRACKED AND CORRODED. MTC REMOVED AND REPLACED FITTING IAW SRM 51-30.SDR GTIA9700398Bulbs · missingPIE - FORWARD SECTION OF RED FLOOR TRACK LIGHTING MISSING 2 LENSES AND LAMPS. REPLACED 2 RED LENSES AND LAMPS IN FORWARD SECTION OF FLOOR TRACK LIGHTING. OPS CHECKS OK PER DC-9 MM CHAPTER 33. (M)SDR CALA9701581Longeron · corrodedINSPECTION FOUND LONGERON 25R CORRODED IN FORWARD CARGO COMPARTMENT AT STA 218. THE LONGERON WAS REMOVED IAW SRM 53-10-03. A NEW LONGERON AND SPLICE SECTION WERE FABRICATED AND INSTALLED IAW SRM 53-02, 51-10-3 AND 51-30-2.SDR CALA9701580Doubler · gougedINSPECTION FOUND GOUGED DOUBLER AT FORWARD PASSENGER DOOR CUTOUT FOR DOOR LATCH HOOK ASSEMBLY. THE OLD DOUBLER WAS REMOVED IAW SRM 51-30-2. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-05, 51-10-3, 51-30-1, AND 51-30-2.SDR CALA9701579Longeron · crackedINSPECTION FOUND A 1 INCH CRACK IN LONGERON 2L AT STA 1079. THE CRACKED SECTION OF LONGERON WAS CUT OUT IAW SRM 53-02. A REPAIR SECTION, SPLICE AND ATTACH BRACKET WERE FABRICATED AND INSTALLED IAW SRM 53-02, 51-30-5 AND ECRA 5310-03589.SDR CALA9701578Cover · crackedINSPECTION FOUND A 1 INCH CRACK IN RT ELEVATOR FLIGHT TAB MECHANISM CONTROL COVER AT STA XHS 95. THE CRACKED AREA WAS REMOVED, DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 55-03, 51-10-3, 51-30-2, AND 51-30-8.SDR CALA9701577Skin · dentedINSPECTION FOUND RT FUSELAGE SKIN DENTED AT FS 360 BETWEEN LONGERON 21R AND 22R. THE DENTED AREA WAS CUT OUT, A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND 51-30-2.SDR ABXA9701773Window · bindingCAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. FOUND WINDOW TRIM BINDING WINDOW ACTUATING ROD. RESECURED TRIM, WINDOW OPERATED NORMAL.SDR CA971125009Air Cyc Machine · inoperative(CAN) AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. QUICK REFERENCE HANDBOOK (QRH) DRILL CARRIED OUT AND SMOKE CLEARED WITHIN ONE MINUTE. RT PACK REMAINED OFF FOR REMAINDER OF FLIGHT. MAINTENANCE ACTION INVOLVED CHANGING RT CYCLING MACHINE AND COSDR ABXA9701776Tab · delaminatedDURING C-CHECK, FOUND THE LEFT AILERON CONTROL TAB DELAMINATED. REPLACED LEFT AILERON CONTROL TAB IAW DC-9 MAINT MANUAL CHAPTER 27-10-2.SDR 9720649606Battery · dischargedDURING PERIODIC CHECK, MAIN CABIN DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE.SDR VJ970337Slide · not securedSLIDE IN GALLEY NEEDS TO BE SECURED IN CASE. REINSTALLED SLIDE IAW MM 25-60 AND PERFORMED REQUIRED INSPECTION.SDR CALA9701551Control Valve · out of adjustTHE AIRCRAFT WAS RETURNED TO DTW FOR REPORTS OF A RUBBER ODOR OBSERVED IN THE CABIN. THERE WERE NO VISIBLE SIGNS OF SMOKE. THE ODOR BEGAN TO DISSIPATE WITHIN THREE MINUTES. THERE WERE NO ENGINE OR AIRCRAFT SYSTEM PROBLEMS NOTED. THE AIRCRAFT LANDED WITHOUTSDR ABXA9701775Spar Cap · corrodedDURING C-CHECK, FOUND THE RIGHT WING REAR SPAR CRACKED AT STATION 164 FLAP HINGE FITTING, LOWER INBOARD ATTACH STUD. REPAIRED RIGHT WING REAR SPAR IAW ABX EA 57110027-002, SERVICE BULLETIN 57-146 AND DOUGLAS SERVICE REWORK DRAWING J060271.SDR 9720749614Connector · looseNOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED AND CLEANED NOSE GEAR SENSOR CANNON PLUG, OPERATIONSDR 9720729606Battery Packs · dischargedDURING PERIODIC CHECK, RIGHT AND LEFT NACELLE EMERGENCY LIGHT BATTERY PACKS FAILED TEN MINUTE TEST. REPLACED BATTERY PACKS, OPERATIONAL CHECK NORMAL.SDR VJ970336Power Supply · inoperativeFORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES IAW WITH MM 33-50; OPS CHECKED GOOD.SDR MWEA97815Check Valve · leakingINFLIGHT NOTICED LARGE FUEL LEAK FROM LEFT WING AROUND AILERON PANEL. MTC FOUND RT FWD BOOST PUMP VOLUTE CHECK VALVE CAUSING LEAK AND DISASSEMBLED AND REASSEMBLED.SDR CALA9701519Intercostal · dentedINSPECTION FOUND INTERCOSTAL DENTED BETWEEN STA 560 AND 579 AT LONGERON 28R. THE INTERCOSTAL WAS REMOVED. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, 51-10-3, AND 51-30-1.SDR CALA9701518Intercostal · corrodedINSPECTION FOUND INTERCOSTAL CORRODED AT STA 680-699, LONGERON 16L. THE INTERCOSTAL WAS REMOVED IAW SRM 51-30-2. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-11-3, 51-11-2, 51-10-3, AND 51-30-2.SDR CALA9701517Intercostal · crackedINSPECTION FOUND INTERCOSTAL CRACKED INSIDE R-1 DOOR AT CENTER OF DOOR BELOW LATCH MECHANISM. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.SDR CALA9701516Skin · dentedINSPECTION FOUND RT WING NR 1 LEADING EDGE SLAT SKIN DENTED. THE DENTED AREA WAS CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 57-06 AND 51-10-3.SDR CALA9701515Stiffener · crackedINSPECTION FOUND A 2 CRACK IN HORIZONTAL STIFFENER ON FORWARD FACE OF AFT PRESSURE BULKHEAD AT L13R. THE STIFFENER WAS REMOVED. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-30-5.SDR CALA9701514Skin · dentedINSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 284, LONGERON 24. THE DENTED AREA WAS CUT OUT. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-04 AND 53-04, FIGURE 12.SDR ABXA9701751Skin · chafedDURING C-CHECK, FOUND THE VERTICAL STABILIZER CHAFED AND GOUGED ON THE RIGHT SIDE. REPLACED SKIN PANEL IAW DC9 SRM 51-30-2 AND 51-30-8.SDR ABXA9701750Bulkhead Gusset · corrodedDURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB LOWER LEFT GUSSET CORRODED. REPLACED GUSSET IAW DC9 SRM 51-30-1 AND 51-30-5.SDR ABXA9701749Rib · corrodedDURING C-CHECK, FOUND THE RIGHT WING TRAILING EDGE RIB CORRODED AT WING STA XRS 133. REPLACED RIB IAW DC9 SRM 51-30-2 AND 51-30-5.SDR VJ970335Battery · dischargedFORWARD OVERWING EMERGENCY EXIT DOOR SIGNS INOPERATIVE. RESEATED BATTERIES IN BATTERY PACK; OPS CHECKED GOOD.SDR MWEA97814Lights · defectiveDURING B-CHECK, FOUND 1ST SEGMENT OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. MTC REPLACED 1ST SEGMENT FLOOR TRACK AND MISSING 2ND RED LAMP IAW DC9MM 33-50-00.SDR ABXA9701707Air Distribution · odorON APPROACH HAD A BURNING SMELL IN COCKPIT. SMELLED LIKE VINYL OR PLASTIC HOT SMELL. POSSIBLY ASSOCIATED WITH USE OF AIRFOIL ANTI-ICE. COULD NOT DUPLICATE DISCREPANCY. PRESSURIZED AIRCRAFT USING BOTH AIR CONDITIONING PACKS, RAN APU AND BOTH ENGINES. INSPESDR 9720459611Longeron · crackedDURING L-CHECK, FOUND CRACK IN LONGERON 2R, FS 1076 AT INBOARD FASTENER IN FRAME. REPAIRED PER EA 96-151793.SDR 9720449611Longeron · crackedDURING L-CHECK, FOUND CRACK IN LONGERON 2L, FS 1076 AT OUTBOARD FASTENER. REPAIRED PER EA 96-151793.SDR GTIA9700389Tire · failedACY - FLT 201 - NR 2 MAIN WHEEL BLEW ON LANDING. REMOVED AND REPLACED NR 2 MAIN WHEEL ASSEMBLY PER MM 32-40-1. (M)SDR 9720069611Slide · low batteryDURING PERIODIC CHECK, FOUND FORWARD SERVICE DOOR EMERGENCY EVACUATION SLIDE BATTERY LOW. REPLACED SLIDE.SDR VJ970334Engine · damagedDURING CLIMBOUT, EXPERIENCED LOSS OF POWER NR 1 ENGINE. REDUCED POWER TO 1.3 EPR AND 61 PERCENT N1. ENGINE WAS NOT SHUTDOWN AND NO EMERGENCY DECLARED. ELECTED TO LAND AT MSO AS PRECAUTIONARY MEASURE. PERFORMED VISUAL INSPECTION AND FOUND 4TH STAGE LPT DAMSDR MWEA97810Cover · fell offTHE ENTRANCE DOOR EMERGENCY SLIDE COVER FELL OFF. MTC REINSTALLED THE FORWARD EMERGENCY SLIDE COVER.SDR 9720109982Power Supply · failedDURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.SDR VJ9800022Cusp · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION AT LEFT CUSP STA 229. REMOVED CORROSION AND REPAIRED IAW DC9 SRM 53-05, FIG 55, SHEET 2, ACMI REA 97865 AND DAC FAX FILE AJC01097.SDR VJ970333Longeron · chafedSTATION 1019 FRAME CHAFED APPROXIMATELY .015 DEEP AT 14L. CUT OUT CHAFED AREA, INSTALLED FILLER AND DOUBLERS IAW SRM 53-03, FIG 4.SDR MWEA97812Fuel/Oil Cooler · defectiveAIRCRAFT DISCONTINUED TAKEOFF DUE TO LEFT ENGINE INDICATING HIGH OIL PRESSURE 63 PSI. MTC REMOVED AND REPLACED LEFT OIL PRESSURE PUMP AND LEFT FUEL OIL COOLER.SDR 9720059985Uplatch Roller · out of adjustLEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED WIRES 1F875D24 AND D264A24. ALSO, RESHIMMED LEFT UPLATCH ROLLER AND REPLACED CABLE ROD END. OPERATIONAL CHECK NOR
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