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 GTIA96NK212Power Supply · inoperativeFORWARD RIGHT AND LEFT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY, OPS CHECKS GOOD IAW 33-53-0. (M)SDR 9622909606Fuel Control · out of adjustWHEN APPLYING POWER FOR TAKEOFF, THE RIGHT ENGINE WOULD NOT REACH TAKEOFF POWER. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TRIMMED THE RIGHT ENGINE, LEAK AND OPERATIONAL CHECK OK.SDR CALA9601522Frame · crackedINSPECTION FOUND LT FRAME AT STA 737 CRACKED IN THREE PLACES. TWO CRACKS WERE 3.125 INCHES LONG AND ONE CRACK WAS 0.25 INCH LONG. THE FRAME WAS REMOVED AND REPLACED IAW ENGINEERING ORDER 1830 AND TASK CARD 05-5310-1-0019.SDR 9622939951Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON BOTH THE LEFT AND RIGHT OUTBOARD BATHTUB FITTINGS IN THE MAIN LANDING GEAR WHEELWELLS. REPLACED FITTINGS PER SRM 51-01, PAR.1C.SDR CALA9601530Skin · puncturedA MAINTENANCE LIFT TRUCK STRUCK THE FUSELAGE CREATING A HOLE THROUGH SKIN AT STA 140.038, 3 INCHES BELOW LONGERON 20R. THE HOLE WAS APPROXIMATELY .875 L BY .5 W. THE AREA WAS REPAIRED IAW SRM 53-04 FIGURE 12B PAGE 608A SHEET 15.SDR 9622929618Fitting · corrodedDURING M-CHECK, FOUND CORROSION ON THE INTERCOSTAL AND SUPPORT FITTING AT LONGERON 27R, FS 980 - 996. REPLACED BOTH PER SRM 53-01.SDR 9622919618Fitting · corrodedDURING M-CHECK, FOUND CORROSION ON THE LEFT SLIDING WINDOW LOWER AFT STOP PLATE. REPLACED FITTING AND PLATE PER SRM 51-30-2.SDR CALA9601523Skin · corrodedINSPECTION FOUND CORROSION ON RT WING SKIN PANEL NR 1244. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-31-1, FIGURE 1.SDR 9622629618Fitting · corrodedDURING M-CHECK, FOUND CORROSION ON THE LEFT WING NR 1 SLAT OUTBOARD END FITTING. REPLACED FITTING PER SRM 51-30-2.SDR VJ960001R1Relay · failedWHEN POWER WAS TRANSFERRED FROM EXTERNAL POWER UNIT TO APU, A LOUD ARCING NOISE WAS HEARD FROM BEHIND CAPTAINS SEAT. CABIN LIGHTS WENT OUT AND GROUND SENSE BUS CONTROL CIRCUIT BREAKER POPPED AND SMOKE APPEARED FROM CIRCUIT BREAKER PANEL. REMOVED AND REPLACED SDR 9622729941Downlock Sw · malfunctionedDURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS EXTENDED. CREW EXECUTED GO-AROUND PROCEDURES AND RECYCLED GEAR FOUR TIMES. NORMAL INDICATIONS WERE ACHIEVED ON FOURTH ATTEMPT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RECYCLED SDR 9622699612Battery Pack · dischargedDURING LINE MAINTENANCE INSPECITON, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR 9622649605Latch Assy · failedLEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAITNENANCE REPLACED LEFT MAIN GEAR DOOR UPLATCH ASSEMBLY, OPERATIONAL CHECK NORMAL.SDR CALA9601491Controller · inoperativeSHORTLY AFTER TAKEOFF, THE LT PACK VALVE WENT TO FULL HOT IN AUTO, THE CONTROL WAS SWITCHED TO MANUAL AND MODULATED TO COLD. THE PACK VALVE DID NOT RESPOND AND THE CABIN AND COCKPIT BEGAN TO FILL WITH SMOKE. THE PACK AUTO SHUTDOWN, BUT THE SMOKE CONTINUED. SDR 9622369609Amplifier · malfunctionedAUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF. OUTFLOW VALVE WENT FROM FULL OPEN TO FULL CLOSED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CABIN PRESSURE AMPLIFIER, OPERATIONAL CHECK NORMAL.SDR CALA9601490Bulbs · failedTHE RT MLG DID NOT INDICATE DOWN AND LOCKED WITH GEAR HANDLE DOWN NOR WITH ALTERNATE EXTENSION WHILE ON APPROACH. THE GEAR WAS CONFIRMED DOWN AND LOCKED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH LANDING GEAR ANNUNCIATOR LAMPS BURNED OUSDR 96ZZZX5873Oil Line · crackedCMH - FLT 425 - DURING CRUISE, SHUT DOWN NR 1 ENGINE, SN 2146, DUE TO LOSS OF OIL QUANTITY. FOUND CRACKED OIL LINE, MFG PN 814776-01. REPLACED OIL LINE, SERVICED ENGINE OIL. ENGINE OPERATION CHECKED NORMAL. ENGINE TOTAL TIME: 58,369 HOURS; 68,640 CYCLES. SDR ZIAA969006Skin · crackedDURING WALK AROUND INSPECTION, FOUND 1 INCH CRACK ON THE LOWER FUSELAGE AT APPROX STATION 208 ON THE LEFT SIDE FUSELAGE 2ND RIVET ROW ABOVE THE BELLY SKIN LAP SEAM. REPAIRED CRACK AT FUSELAGE STATION 210 LEFT SIDE. FABRICATED FILLER AND DOUBLER AND INSTALLEDSDR CA961104013Oven Plug · burnt(CAN) DURING CRUISE AN ELECTRICAL BURNING SMELL WAS NOTICED COMING FROM THE FRONT AREA OF THE AIRCRAFT NEAR THE FLIGHT DECK. INVESTIGATION REVEALED PLUG OF GALLEY OVEN #4 BURNT. PLUG REPLACED.SDR 9622259951Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE LEFT WHEEL WELL ATTACH FITTING FS 690 AT THE KEEL SKIN. REPLACED FITTING PER SRM 53-01 FIG 1.SDR 9622169618Fitting · crackedDURING M-CHECK, FOUND CORROSION ON THE VERTICAL STABILIZER LEFT RUB STRIP ATTACH FITTING AND A CRACK IN THE RIGHT RUB STRIP ATTACH FITTING. REPLACED BOTH FITTINGS PER SRM 51-30-5.SDR 9622029618Fitting · corrodedDURING M-CHECK, FOUND CORROSION ON THE LONGERON 23L AND LONGERON 30 TIE FITTINGS AT FS 990 TO 996. REPLACED TIE FITTINGS PER SRM 51-10-03.SDR 9621899925Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT MAIN CABIN DOOR AND FLOOR PROXIMITY LIGHTS AT RIGHT GALLEY ACROSS FROM LAVATORY INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL.SDR MWEA96613Wire · detachedDURING SERVICE CHECK, FOUND EMERGENCY LIGHTS OVER TAIL EVACUATION SLIDE WOULD NOT ILLUMINATE. MAINTENANCE FOUND WIRE SEPARATED FROM TERMINAL RESECURED WIRE IAW DC9MM 33-51-01, OPS CHECK GOOD.SDR 9621819607Wire · looseFLIGHT ATTENDANT REPORTED ELECTRICAL SMELL IN AFT CABIN DURING TAKEOFF. FLIGHT RETURNED TO YWG AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED CEILING AREA BETWEEN AFT LAVATORIES AND FOUND WIRE CONDUITS LOOSE. RECLAMPED CONDUITS, OPERATIONAL CHECK NORMALSDR 9621989614Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE AFT ENTRY DOOR FRAME FITTING, LEFT AFT SIDE. REPLACED FITTING PER SRM 51-10-3.SDR 9621799926Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS IN TAILCONE INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK, OPERATIONAL CHECK NORMAL.SDR 9621779883Pt2 Line · leakingDURING CLIMB, THE RIGHT ENGINE EPR WAS INDICATING A HIGH READING. CREW PERFORMED AN AIR TURNBACK WHERE THEY LANDED AT MSP WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED A LEAK ON THE PT2 LINE, LEAK AND OPERATIONAL CHECK OK.SDR MWEA96531Batteries · dischargedDURING A CHECK, FOUND FWD CABIN EMERGENCY CEILING LIGHTS WOULD NOT EXTINGUISH. MAINT. REPLACED D-CELL BATTERIES IN POWER SUPPLY. OPS CHECK GOOD.SDR GTIA96NK211Fuse · blownAFT SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED BLOWN FUSE IN BATTERY PACK, OPERATIONAL CHECK GOOD IAW DC-9 MM CH 33-53-01. (M)SDR 9621759604Batteries · dischargedDURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS AT ROWS 6 THROUGH 10 INOPERATIVE. REPLACED BATTERIES IN BATTERY PACKS, OPERATIONAL CHECK NORMAL.SDR CALA9601426Wire · damagedINSPECTION FOUND EMERGENCY TRACK LIGHTING IN FIRST CLASS SECTION OF CABIN COMING UP AND INOPERATIVE. MAINTENANCE FOUND DAMAGED TRACK LIGHT WIRING. THE WIRING WAS REPAIRED AND THE TRACK WAS REINSTALLED.SDR CALA9601424Actuator · inoperativeWHEN GEAR WAS RETRACTED ON TAKEOFF, THE GEAR DOOR OPEN AND RIGHT MAIN GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. APPROXIMATELY 15 SECONDS LATER THE SPEED BRAKE SPOILER HANDLE SOUNDED AS THOUGH IT CYCLED TO AIR MODE AND BOTH GEAR UNSAFE LIGHTS EXTINGUISHED. THE SDR ABXA9600634Connector Pin · looseUPON LOWERING LANDING GEAR, NO RIGHT MAIN GEAR INDICATION NOR RIGHT GEAR UNSAFE LIGHT. RECYCLED, CHANGED BULBS TO NO EFFECT. ALTERNATE MAIN GEAR INDICATION NORMAL. LANDED WITHOUT INCIDENT. VERIFIED PIN 5 ON CANNON PLUG PL-129 NOT SECURED. RESEATED PIN, SSDR 9621019983Fuel Control · failedDURING CLIMB, THE LEFT ENGINE EPR AND FUEL FLOW INDICATIONS BEGAN FLUCTUATING. CREW RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE FUEL CONTROL AND TRIMMED ENGINE, LEAK AND OPERATIONAL CHECK OK.SDR CA961112037Bearing · leaking oil(CAN) INFLIGHT SHUTDOWN CARRIED OUT ON #1 ENGINE DUE TO LOSS OF OIL QUANTITY. POST FLIGHT INSPECTION FOUND NO OIL IN #1 ENGINE OIL RESERVOIR. OIL WAS COMING FROM THE ENGINE EXHAUST. #1 ENGINE CHANGED. THE OIL LOSS WAS DUE TO #6 BEARING FAILURE AND THE OIL WAS SDR CA961018013Engine · failed(CAN) INFLIGHT SHUTDOWN OF #1 ENGINE DUE TO TOTAL LOSS OF OIL QUANTITY. POST FLIGHT INSPECTION FOUND NO OIL IN #1 ENGINE RESERVOIR. FOUND OIL COMING FROM TURBINE EXHAUST. #1 ENGINE REPLACED.SDR ABXA9700670Angle · crackedDURING C-CHECK, THE VERTICAL STABILIZER INTER SPAR BOX FORWARD LOWER ATTACH ANGLE WAS FOUND CRACKED. REPAIRED IAW REA D955-16656-MR.SDR ABXA9700669Frame · crackedDURING C-CHECK, THE CANTED FRAME AT STA 1074 WAS FOUND CRACKED AT LONGERON 4 LT. REPAIRED IAW REA D953-16684-MR.SDR ABXA9700668Frame · crackedDURING C-CHECK, THE CANTED FRAME AT STA 1121 WAS FOUND CORRODED AND CRACKED AT LONGERON 5 LT. REPAIRED IAW DC-9 SRM.SDR ABXA9700667Frame · crackedDURING C-CHECK, THE CANTED FRAME AT STA 1104 WAS FOUND CRACKED AT LONGERON 4 LT. REPAIRED IAW REA D953-16685-MR.SDR ABXA9700666Frame · crackedDURING C-CHECK, THE CANTED FRAME AT STA 1155 WAS FOUND CRACKED AT LONGERON 4 LT. REPAIRED IAW REA D953-16713-MR.SDR ABXA9700665Frame · crackedDURING C-CHECK, THE CANTED FRAME AT STA 1155 WAS FOUND CRACKED AT LONGERON 4 RT. REPAIRED IAW REA D953-16713-MR.SDR ABXA9700685Angle · crackedDURING C-CHECK, A CRACK WAS FOUND IN THE UPPER PYLON TO FUSELAGE ATTACH ANGLE. REPLACED ANGLE IAW DC-9 SRM.SDR ABXA9700684Frame · crackedDURING C-CHECK, THE FUSELAGE MAIN FRAME AT STA 718 RT WAS FOUND CRACKED BEYOND A PREVIOUS REPAIR. REPAIRED IAW REA D953-16620.SDR ABXA9700681Longeron · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LONGERON 17L CRACKED AT FRAME 965. REPLACED IAW DC-9 SRM.SDR ABXA9700672Longeron · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LONGERON 17R CRACKED AT FRAME 980. REPLACED IAW DC-9 SRM.SDR ABXA9700671Longeron · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LONGERON 17L CRACKED AT FRAME 980. REPLACED IAW DC-9 SRM.SDR 9621329614Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE AFT ENTRY DOOR, AFT LEFT FRAME FITTING. REPLACED FITTING PER SRM 51-30-2.SDR GTIA96NK210Door Lock · out of adjustREF - CABIN LOG ENTRY NR 1 FROM C/N 8113 EMERGENCY EXIT HATCH ROW 15. AIRCRAFT RIGHT COMES LOOSE ON LANDING. INSPECTED AND ADJUSTED DOOR LOCK BAR IAW DC-9 MM 52-20-0. (M)
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