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.

SDR ABXA030410Rib · crackedRIGHT SIDE OF REMOVABLE LEADING EDGE HAD A CRACK ON A RIB AT THE BOTTOM OF THE PANEL. REPAIRED AREA IAW DC-9 SSRM DWG K05159.Oct 14, 2003 · N982AX · Doug DC932 · Vertical Stabilizer, Spar/RibSDR MWEA030421Control Panel · inoperativeON START OF RT ENGINE, AC CROSS-TIE LOCK OUT CAME ON, UNABLE TO RESET. REMOVED AND REPLACED AC BUSS CONTROL PANEL.Oct 13, 2003 · N209ME · Doug DC932 · AC Generation SystemSDR MWEA030422Smoke Detector · inoperativeDURING FLIGHT THE MASTER WARNING CAME ON WITH NO OTHER ANNUNCIATIONS FOUND, NO POWER TO CARGO DETECTION PANEL. REMOVED AND REPLACED CARGO SMOKE DETECTORS, OHMED AND MEGGED ALL WIRING TO CARGO SMOKE DETECTOR.Oct 12, 2003 · N207ME · Doug DC932 · Smoke DetectionSDR MWEA030420Control Panel · inoperativeMASTER WARNING CAME ON WITH NO OTHER ANNUNCIATIONS. SMOKE DETECTOR PANEL CIRCUIT BREAKER POPPED. INSPECTED OVERHEAD PANEL WIRING AND CARGO FIRE SUPPRESSION CONTROL PANEL. NO VISIBLE DEFECTS NOTED, ALSO INSPECTED CARGO PIT SMOKE DETECTOR. NO VISIBLE DEFECTSOct 10, 2003 · N207ME · Doug DC932 · Smoke DetectionSDR MWEA030412Wire · brokenAFTER CONTROL CHECK, THE RUDDER TRAVEL UNRESTRICTED LIGHT WENT OUT, WHEN LEFT RUDDER IS MOVED 3 INCHES THE LIGHT ILLUMINATED AND WHEN THE RIGHT PEDAL IS MOVED FULL TRAVEL THE LIGHT STAYS OUT. REMOVED AND REPLACED SWITCH AND BROKEN WIRES.Oct 8, 2003 · N302ME · Doug DC932 · Flight Control System WiringSDR 0301889921Acm · failedSHORTLY AFTER TAKEOFF, THE RIGHT AIR CONDITIONING PACK AIR FLOW STOPPED. THE LEAD FLIGHT ATTENDANT REPORTED SMOKE IN THE CABIN. AIRCRAFT RETURNED TO BIL AND MADE AN EMERGENCY OVERWEIGHT LANDING WITHOUT ANY FURTHER INCIDENT. NO COMMENTS ABOUT COM OR ATTEMPTEOct 3, 2003 · N943N · Doug DC932 · Cabin Cooling SystemSDR MWEA030400Thrust Reverser · corrodedLIGHT CORROSION ON OUTER FACE OF LEFT DRIVE ARM, TOP BUCKET IN FLANGE RADIUS. REMOVED AND REPLACED THRUST REVERSER.Oct 1, 2003 · N209ME · Doug DC932 · Engine Thrust ReverserSDR CA030930014Housing · cracked(CAN) THIS FUEL PUMP WAS INSTALLED TO REPLACED A TIME (X) FUEL PUMP, AFTER MANY ATTEMPS TO REPAIRED A FUEL LEAK,THE TECH DISCOVERED A CRACK IN THE PUMP HOUSING.THE CRACK FOUND LOCATED AT THE BOLTS FLANGE ATTACHMENT. THE PUMP WAS O/H IN NOV/02 THIS PUMP WAS RESep 30, 2003 · Doug DC932 · Fuel Boost PumpSDR MWEA030401Switch · inoperativeNO SLAT EXTEND LIGHT WITH SLATS OUT, SLAT DISAGREEMENT LIGHT INTERMITTENT. REMOVED AND REPLACED LEFT SLAT EXTEND SWITCH.Sep 30, 2003 · N202ME · Doug DC932 · Leading Edge Slat Position Indicating SystemSDR AT0300028Engine · unserviceableLOW OIL PRESSURE AND LOSS OF QUANTITY DURING CLIMB OUT AT 16,000 AND 300 KNOTS. REMOVE AND REPLACED THE NR 2 ENGINESep 27, 2003 · N836AT · Doug DC932 · Engine (Turbine/Turboprop)SDR 0301829612Cooling Turbine · failedIMMEDIATELY AFTER TAKEOFF, SMOKE WAS REPORTED IN THE CABIN AREA AND LAV SMOKE DETECTORS WERE IN ALARM. CREW COMPLIED WITH COM, DONNED OXYGEN MASKS, & RETURNED TO AN UNEVENTFUL LANDING AT GFK. SMOKE HAD DISSIPATED BEFORE LANDING & THERE WAS NO EVIDENCE OF ANY FSep 27, 2003 · N612NW · Doug DC932 · Cabin Cooling SystemSDR ABXA030370Wire · burnedLEFT AFT BOOST PUMP AND RADIO RACK COOLING VALVE WIRES CHARRED AT STATION 237 (P1-1061L). REPAIRED WIRES HV-Q 13A20B, HV-Q 12A20C, H 211A24 IAW W.D. MANUAL 28-21-00 AND 21-21-00. LEFT AFT BOOST PUMP AND RADIO RACK COOLING VALVE. OPS CHECK GOOD.Sep 25, 2003 · N989AX · Doug DC932 · Fuel System WiringSDR MWEA030395Skin · dentedFUSELAGE SKIN HAS A DENT AT STATION 967, 2 INCHES ABOVE LONGERON 27 LEFT. FABRICATED AND INSTALLED DOUBLER AND FILLERS.Sep 25, 2003 · N209ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030393Longeron · crackedWHILE REPLACING DOME NUTS FOR FUSELAGE FILET PANEL, FOUND SUSPECT CRACK ON AFT END OF LONGERON 26 RT FRAME STATION 604. FABRICATED AND INSTALLED FITTING.Sep 25, 2003 · N209ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA030392Skin · dentedFUSELAGE SKIN HAS A DENT AT STATION 388 AT LONGERON 5 RIGHT. FABRICATED AND INSTALLED FILLER AND DOUBLER.Sep 25, 2003 · N209ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030391Skin · gougedLEFT SIDE OF VERTICAL STABILIZER SKIN UNDER VERTICAL TO HORIZONTAL STABILIZER, FAIRING HAS A GOUGE FROM TOP SKIN RADIUS EXTENDING DOWN AT 1.5 INCHES. FABRICATED AND INSTALLED REPAIR DOUBLER.Sep 25, 2003 · N209ME · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR MWEA030377Start Valve · inoperativeRIGHT ENGINE HIGH-PRESSURE COMPRESSOR SHAFT SPEED WOULD NOT RISE ABOVE 13 PERCENT, HIGH-PRESSURE COMPRESSOR SHAFT SPEED ABORTED START. REMOVED AND REPLACED RIGHT ENGINE START VALVE.Sep 17, 2003 · N301ME · Doug DC932 · Engine Start Valves/ControlsSDR ABXA030362Connector · looseNO INDICATION OF NOSE GEAR DOWN AND LOCKED. CHANGED LIGHT BULBS AND RAN ABNORMAL CHECK-LIST. DETERMINED INDICATION PROBLEM. FOUND CONNECTOR PLUG LOOSE ON THE NOSE DOWNLOCK SWITCH. CLEANED AND RECONNECTED PLUG. SYSTEM OPS CHECK GOOD IAW DC-9 MM 32-60-00.Sep 12, 2003 · N989AX · Doug DC932 · Landing Gear Position and WarningSDR MWEA030367Skin · canningSTATION 959 LONGERON 18 RIGHT & LONGERON 16 RIGHT EVIDENCE OF OIL CANNING UNDER RIGHT PYLON. FABRICATED AND INSTALLED REPAIR DOUBLER.Sep 9, 2003 · N216ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030366Skin · canningEVIDENCE OF OIL CANNING ON RIGHT SIDE OF FUSELAGE UNDER PYLON STATION 988 LONGERON 17,18 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER.Sep 9, 2003 · N216ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030365Skin · canningEVIDENCE OF OIL CANNING RIGHT SIDE OF FUSELAGE UNDER PYLON STATION 1006 LONGERON 8 RIGHT AND LONGERON 17 RIGHT. FABRICATED AND INSTALLED REPAIR SPLICE AND DOUBLER.Sep 9, 2003 · N216ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030364Doubler · corrodedCORROSION FOUND ON COVER PLATE AND ON FUSELAGE. REMOVED AND REPLACED REPAIR DOUBLER.Sep 7, 2003 · N301ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030363Wire · brokenRUDDER TRAVEL UNRESTRICTED LIGHT NOT ON. FOUND WIRE BROKEN NEAR RUDDER, REPAIRED WIRE.Sep 6, 2003 · N302ME · Doug DC932 · Flight Control System WiringSDR 0301819613Doubler · crackedDURING L-CHECK FOUND CRACK IN EXISTING REPAIR DOUBLER ON AFT CARGO DOOR JAMB AT BS 897. REPAIRED PER EA 96-195991.Sep 3, 2003 · N612NW · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA030367Fitting · corrodedSLANT PANEL OUTBOARD ATTACH ANGLE WAS EXFOLIATED. REPLACED DAMAGED FITTING WITH NEW FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.Sep 2, 2003 · N985AX · Doug DC932 · Fuselage, Landing Gear Attach FittingsSDR 0301909941Skin · crackedDURING APB WEB INSPECTION FOUND 1.5 IN CRACK IN SKIN 4 IN OUTBOARD OF THE DOOR JAMB. REPAIRED IAW EA 99-195996.Aug 31, 2003 · N3324L · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030351Proximity Switch · faultyRED LEFT GEAR UNSAFE LIGHT CAME ON ALONG WITH HORN. REMOVED AND REPLACED PROXIMITY SWITCH CONTROL BOX.Aug 28, 2003 · N202ME · Doug DC932 · Landing Gear Position and WarningSDR MWEA030331Amplifier · inoperativeCAPTAIN'S ATTITUDE INICATOR SHOWS GYRO FLAG DURING ANY ATTITUDE CHANGE. REMOVED AND REPLACED NR 1 INSTRUMENT AMPLIFIER.Aug 26, 2003 · N302ME · Doug DC932 · Attitude and Direction Data SystemSDR ABXA030344Fitting · corrodedFLAP HINGE STUDS AT FLAP FITTING STA. 267 HEAVILY CORRODED. REPLACED FLAP HINGE IAW DC-9 MM 57-40-01-2-0001.Aug 21, 2003 · N939AX · Doug DC932 · Trailing Edge FlapsSDR ABXA030343Intercostal · crackedCABIN FLOORBEAM INTERCOSTAL BETWEEN STA. 256 AND 275, BUTT LINE O, CRACKED FORWARD END. REPLACED INTERCOSTAL IAW DC-9 SSRM K05159.Aug 20, 2003 · N939AX · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA030317Wire · openUNABLE TO GET A GREEN DOWN LIGHT. FOUND OPEN WIRES IN RIGHT GEAR DOWN CONNECTOR, ALL ASSOCIATED WIRES WERE REPLACED.Aug 18, 2003 · N301ME · Doug DC932 · Landing Gear System WiringSDR MWEA030316Relay · failedAFTER ROTATION STICK SHAKERS AND STALL INDICATION LIGHT CAME ON. REMOVED AND REPLACED RIGHT RELAY.Aug 18, 2003 · N207ME · Doug DC932 · Stall Warning SystemSDR MWEA030311Relay · failedSLAT EXTEND LIGHT INOPERATIVE. REMOVED AND REPLACED RELAY.Aug 17, 2003 · N207ME · Doug DC932 · Leading Edge Slat Control SystemSDR MWEA030310Connector · defectiveSTALL INDICATION FAILURE LIGHT CAME ON. REMOVED AND REPLACED FIRST OFFICER'S STICK SHAKER CONNECTOR.Aug 15, 2003 · N207ME · Doug DC932 · Stall Warning SystemSDR MWEA030309Transmitter · faultySTALL INDICATION FAILURE LIGHT CAME. REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER. PERFORMED ADJUSTMENT TEST OF STALL SYSTEM CHECKED GOOD.Aug 14, 2003 · N207ME · Doug DC932 · Trailing Flap Position Indicating SystemSDR ABXA030331Longeron · crackedLONGERON 17 CRACKED ON AFT SIDE OF BULKHEAD FS 965. REPLACED LONGERON IAW DC-9 SRM.Aug 8, 2003 · N903AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA030305Transceiver · inoperativeUNABLE TO TRANSMIT ON NUMBER ONE COMMUNICATION. REMOVED AND REPLACED NUMBER ONE COMMUNICATION TRANCEIVER.Aug 7, 2003 · N501ME · Doug DC932 · VHF Communications SystemSDR MWEA030303Computer · malfunctionedSTALL INDICATION FAILURE ANNUCIATOR COMES OFF AND ON. REMOVED AND REPLACED STALL WARNING COMPUTER.Aug 1, 2003 · N207ME · Doug DC932 · Stall Warning SystemSDR 0301409617Duct · out of positionTHE CABIN ALTITUDE BEGAN TO CLIMB FOLLOWING A MUFFLED REPORT. AIRCRAFT WAS IN CRUISE AT FL330 WHEN MASTER WARNING ILLUMINATED AND PRESSURE LOSS BEGAN. CREW INITIATED AN EMERGENCY DESCENT TO FL100 WHEN CABIN PRESSURE GRADUALLY RECOVERED. FLIGHT CONTINUED TO Jul 30, 2003 · N617NW · Doug DC932 · Air Distribution SystemSDR MWEA030289Door · noisyPASSENGER REPORTED LARGE AMOUNTS OF AIRFLOW AROUND EMERGENCY EXIT DOOR. INSPECTED EMERGENCY DOOR, SEALS AND LATCHING MECHANISMS. OPERATIONS CHECK GOOD NO DEFECTS FOUND.Jul 24, 2003 · N502ME · Doug DC932 · Emergency ExitsSDR MWEA030288Fire Bottle · dischargedEXTIGUISHING AGENT TWO LOW LIGHT ILLUMINATED, THERMAL BOTTLE DISCHARGED TO ZERO PSI. REMOVED AND REPLACED BOTTLE.Jul 22, 2003 · N202ME · Doug DC932 · Fire Bottle, FixedSDR ABXA030288Wire · damagedDURING TAXI, WHEN FIRST OFFICER PERFORMED TAXI CHECK LIST, THERE WAS A POPPING SOUND AND SPARKS EMITTING FROM THE OVERHEAD ON THE CAPTAIN'S SIDE. REPLACED LEFT WINDSHIELD ANTI-ICE TEMPERATURE SENSOR WIRING IAW DC-9 MM 20-50-01-2. OPS CHECKED GOOD.Jul 21, 2003 · N902AX · Doug DC932 · Ice/Rain Protection System WiringSDR AT0300021Wire · disconnectedEMERGENCY PATH WIRING OPEN-UNDER LIGHT TRACK/ONE SECTION OF LIGHTS WAS INOPERATIVE. RECONNECTED WIRING.Jul 18, 2003 · N837AT · Doug DC932 · Light System WiringSDR MWEA030282Skin · damagedFUSELAGE SKIN AT STATION 1164 ON RIGHT SIDE OF AFT OF LOUVER HAS DAMAGE TO THE INTERNAL SIDE. FABRICATED AND INSTALLED DOUBLER.Jul 18, 2003 · N401ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030281Yoke · corrodedEVIDENCE OF CORROSION AND GALLING INSIDE LOWER HALF OF RIGHT PYLON MOUNT YOKE CUP. REMOVED AND REPLACED RIGHT ENGINE YOKE MOUNT.Jul 12, 2003 · N203ME · Doug DC932 · Engine Mount SectionSDR MWEA030273Flex Line · crackedAT 35,000 FEET RED MASTER WARNING LIGHT ILLUMINATED ALONG WITH THE RED CABIN ANNUCIATOR, MASK DROPPED -- REPLACED COALESER BAG AND CLEANED BOTH WATER OUTLET SCEENS, ALSO PERFORMED A CABIN PRESSURIZATION CONTROL ADJUST, REMOVED AND REPLACED WATER SEPERATOR TEJul 10, 2003 · N207ME · Doug DC932 · Pneumatic Distribution SystemSDR AT0300020Wire · damagedONE SET OF EMERGENCY LIGHTS NEAR AFT WALKING IS INOPERATIVE. REPAIRED WIRE TO CONNECTOR OPS CHECK GOOD IAW DC-9 MM 20-50.Jul 9, 2003 · N833AT · Doug DC932 · Light System WiringSDR 0301279615Controller · malfunctionedAT FL330, THE CABIN ALTITUDE BEGAN CLIMBING AS PRESSURIZATION BECAME UNCONTROLLABLE. A RAPID DESCENT WAS NOT NECESSARY BECAUSE THE CABIN HAD REACHED 14,500 FT AND ALL OF THE PASSENGER OXYGEN MASKS DEPLOYED. COMPLIED WITH COM PROCEDURES AND FLT CONTINUED TO DJul 8, 2003 · N615NW · Doug DC932 · Cabin Pressure ControllerSDR MWEA030272Connector · faultyLEFT ENGINE LOOP A FIRE INDICATION CAME ON. REMOVED AND REPLACED BOTH FIRE EXTINGUISHER BOTTLE,1 EACH SQUIBS,LEFT ENGINE B AND REPLACED FAULTY CONNECTORS,Jul 8, 2003 · N209ME · Doug DC932 · Fire DetectionSDR 0301249614Shutoff Valve · crackedRIGHT HYDRAULIC SYSTEM FLUID QUANTITY WENT TO ZERO DURING TAXI OUT. FUMES ENTERED THE CABIN BUT CREW WAS ABLE TO CLEAR THE AIR.CREW STATED THAT THE RED EMERGENCY WARNING LIGHT DID NOT ILLUMINATE. AIRCRAFT WAS TOWED BACK TO THE GATE WITHOUT FURTHER INCIDENT. MAJul 7, 2003 · N614NW · Doug DC932 · Rudder Control System
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