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 AT0300007Tail Cone · inoperativeTAIL CONE DID NOT RELEASE FROM AIRCRAFT, STEP 12.1.4, EO09-5350-29-E1476 REV B. CORRECTIVE ACTION: REMOVED AND REPLACED TAIL CONE REF MM 53-50. DROP CHECK GOOD.Mar 19, 2003 · N831AT · Doug DC932 · Emergency ExitsSDR GTIA030164Beam · crackedEDDY CURRENT INSPECTION REVEALED 2.25 INCH CRACKS EMANATING FROM FASTENER HOLE IN OUTER PAN OF AFT LOWER CARGO DOOR FWD EDGE AT BEAM 1. STOP DRILLED CRACKS AND INSTALLED PATCH ON AFT CARGO DOOR.Mar 18, 2003 · N12536 · Doug DC932 · Cargo/Baggage DoorsSDR MWEA030135Seat Track · defectiveFIRST OFFICER SEAT HITS THE HI-LOCS ON SEAT TRACK OUTBOARD OF EXSISTING REPAIR. -- INSTALLED STAINLESS STEEL STRAP ON SEAT TRACK OUTBOARD AND REMOVED AND REPLACED SEAT TRACK.Mar 18, 2003 · N301ME · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MEX2003080Actuator · brokenDURING EXTERIOR INSPECTION, DETECTED A BREAK IN THE LEFT WING SLATS ACTUATORS ACCESS DOOR, THE FASTENER POINT OF THE UPPER SLAT ACTUATOR WAS BROKEN. BOTH CYLINDERS ACTUATORS WERE REPLACED IAW MM 27-80-5. (M)Mar 17, 2003 · N1003P · Doug DC932 · Leading Edge Slat ActuatorSDR 0300729606Clamp · brokenCLIMBING THROUGH FL 210 CREW FELT A THUMP IN THE FORWARD CABIN AND SUBSEQUENTLY LOST CONTROL OF CABIN PRESSURE. OUTFLOW VALVE INDICATED FULL CLOSED BUT THE CABIN CONTINUED TO CLIMB THROUGH 10,500 FEET. FLIGHT CONTINUED TO DESTINATION AT THIS LOWER ALTITUDE ANDMar 17, 2003 · N606NW · Doug DC932 · Cabin Cooling SystemSDR MWEA030133Windshield · failedFIRST OFFICER'S WINDSHIELD SHATTERED AT ALTITUDE (OUTER PANE). REMOVED AND REPLACED FIRST OFFICER'S WINDSHIELD.Mar 17, 2003 · N207ME · Doug DC932 · Flight Compartment WindowsSDR 0300799615Bracket · crackedDURING H-CHECK, FOUND CRACK IN FUSELAGE HORIZONTAL LEG BRACKET AT BS 69 RT SIDE. REPAIRED PER EA 96-190942.Mar 14, 2003 · N615NW · Doug DC932 · Fuselage Miscellaneous StructureSDR 0300809612Skin · crackedDURING L-CHECK, FOUND CRACKS ON FUSELAGE NOSE SKIN AT BS 69.5 AND BS 76.5. REPAIRED PER EA 96-190940.Mar 13, 2003 · N612NW · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030132Control Box · inoperativeWHILE ARMING ANTI-SKID RIGHT OUTBOARD AND INBOARD LIGHTS REMAINED ON. REMOVED AND REPLACED ANTI-SKID CONTROL BOX.Mar 13, 2003 · N209ME · Doug DC932 · Brake Anti-Skid SectionSDR MWEA030402Skin · canningEVIDENCE OF OIL CANNING ON LEFT SIDE OF FUSELAGE STATION 1025. INSTALLED DOUBLER.Mar 10, 2003 · N216ME · Doug DC932 · Fuselage Main, FrameSDR MEX2003062Thermostat · failedFLT 248 - MEX-GDL - DURING PUSH BACK, THE APU SHUT OFF ON RAMP. THE AIRCRAFT RETURNED TO POSITION. THE PNEUMATIC LOAD CONTROL THERMOSTAT WAS REPLACED IAW MM 49-52-1, TESTS CORRECT. (M)Mar 8, 2003 · N1003P · Doug DC932 · APU ControlsSDR AT0300006Duct · blownAFT LAVATORY SMOKE DETECTORS WENT OFF APPROXIMATELY F/L 220. AFT FLIGHT ATTENDANT REPORTED HEAVY ELECTRICAL SMELL. MINUTES LATER LEFT AFT LEFT LAV SMOKE DETECTOR WENT OFF. INSPECTED AIRCRAFT FOUND LT PACK OVERHEATED AND DUCT BLOWN OFF ACM. PRESSURIZED A/C TMar 8, 2003 · N831AT · Doug DC932 · Engine Bleed Air SystemSDR MWEA030129Engine · failedAT 32,500 FEET AIRCRAFT SUFFERED SEVERE ENGINE VIBRATION, RIGHT ENGINE OIL PRESSURE WENT TO ZERO AND RIGHT HYDRAULIC FLUIDS QUANTITY WAS AT ZERO. REMOVED AND REPLACED ENGINE.Mar 5, 2003 · N216ME · Doug DC932 · Engine Emergency Shutdown SystemSDR GTIA030114Fitting · leakingRIGHT WHEEL WELL AFT FUEL MANIFOLD INBOARD SIDE DRIPPING FUEL. RESECURED LOOSE FITTING AT APU FUEL LINE SHROUD CONNECTION. LEAK CHECK GOOD.Feb 28, 2003 · N12536 · Doug DC932 · Aircraft Fuel Distribution SystemSDR MWEA030120Warning Light · illuminatedRT START ENGINE VALVE ANNUNCIATOR STAYED ON. VERIFIED VALVE CLOSED, LIGHT IN COCKPIT OUT, COULD NOT DULPICATE AT THIS TIME.Feb 28, 2003 · N216ME · Doug DC932 · Engine CrankingSDR MWEA030122Computer · malfunctionedDURING TAXI, STALL INDICATION FAILURE LIGHT CAME ON. SWAPPED AOA SYSTEM, CHECKS GOOD. MARKED FAULTLY TRANSDUCER ON NR 1 SIDE, NOW IN NR 1 POSITION, RESET NR 2 COMPUTER VANE PIN.Feb 27, 2003 · N207ME · Doug DC932 · Stall Warning SystemSDR GTIA030105Uplock Switch · inoperativeRIGHT GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION AND REMAINS ON DURING UPLATCH CHECK AND REMAINDER OF FLIGHT. FOUND WIRE 2G206A24 ON TERMINAL C2 OF RELAY R2-29 (LANDING GEAR LEVER) SHORTED TO GROUND (=240HMS) WITH RT DOWNLOCK SWITCH CP P1-129 DISCONNFeb 25, 2003 · N133NK · Doug DC932 · Landing Gear Position and WarningSDR MWEA030112Throttle Switch · defectiveGEAR WARNING HORN SOUNDED. -- REMOVED AND REPLACED ON SWITCH UNIT AND INSTALLED LEFT THROTTLE SWITCH.Feb 25, 2003 · N401ME · Doug DC932 · Landing Gear Position and WarningSDR GTIA030104Switch · contaminatedDTW - FLT 1141 - FOUND SMOKE IN COCKPIT WHILE SITTING AT THE GATE. FOUND ARCING ON LANDING LIGHT SWITCH DUE TO DIRT CONTAMINATION CLEANED SWITCH CONTACTS COULD NOT DUPLICATE ORIGINAL PROBLEM. NO OTHER DEFECTS NOTED AT THIS TIME LIGHTING. OPS CHECK GOOD. (MFeb 24, 2003 · N133NK · Doug DC932 · Exterior LightingSDR AT0300004Outflow Valve · icedLOST CABIN PRESSURIZATION AT 20,000 FT IN ICING CONDITIONS. SELECTED MANUAL AND THE VALVE WOULD NOT CLOSE ALL THE WAY. MASKS DROPPED SUSPECT ICING AFTER 30 MINUTE HOLD. OPERATED OUTFLOW VALVE AND PRESSURIZED TO 3 PSI, OPS NORMAL REF MM 21-32. MASK DROPPED Feb 22, 2003 · N832AT · Doug DC932 · Pressure Regulator/Outflow ValveSDR MWEA030111Flange · elongatedFIRST OFFICER AFT INBOARD SEAT TRACK FOUND ENLONGATED HOLES. -- REMOVED AND REPLACED UPPER FLANGE OF FIRST OFFICER'S INBOARD SEAT TRACK.Feb 22, 2003 · N301ME · Doug DC932 · Flight Compartment EquipmentSDR 0300459614Former · crackedDuring "H" check found crack in outboard end of aft pressure bulkhead horizontal former at Z=34 and X=40. Repaired per EA 96-194267.Feb 19, 2003 · N614NW · Doug DC932 · Fuselage Main, BulkheadSDR MWEA030105Receiver · inoperativeFIRST OFFICER NR 2 NAV FAILED, VOR, GS, AND LOC FLAGS SHOWING. REMOVED AND REPLACED VOR/ILS RECEIVER.Feb 15, 2003 · N209ME · Doug DC932 · Localizer/VOR SystemSDR 0300329614Skin · corrodedDuring "H" check found corrosion on fuselage skin between BS 160-180 L28L-L28R. Repaired per EA 96-194258.Feb 14, 2003 · N614NW · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030108Outflow Valve · inoperativeFLOW LIGHT ILLUMINATED, FOLLOWED BY TRANSFER LOCKOUT LIGHT, STANDBY LIGHT ON PRESSURE CONTROLLER. DID QRH PROCEDURES. COULD NOT CONTROL CABIN PRESSURIZATION. REMOVED AND REPLACED OUTFLOW VALVE ACTUATOR AND TWO BELLY DRAINS. INSTALLED NEW SEAL FOR LEFT REVEFeb 14, 2003 · N502ME · Doug DC932 · Pressure Regulator/Outflow ValveSDR MWEA030072Drive Shaft · shearedWHEN ATTEMPTING TO START #2 ENGINE THE N2 WENT TO 10% THEN DROPPED OFF TO ZERO. -- REMOVED AND REPLACED STARTER DRIVE SHAFT.Feb 12, 2003 · N209ME · Doug DC932 · Engine StarterSDR MWEA030059Fillet · crackedCREW REPORTED LEFT SIDE WING AREA VIBRATION WITH FLAPS UP AND GEAR RETRACTED. FOUND FILLET CRACKS AND RIGHT ACM DUCT SUPPORT BRACKET BOLTS BROKE. REPAIRED FILLET PER SRM 53-01 AND WELDED REPAIR DUCT MOUNT FLANGES.Feb 8, 2003 · N401ME · Doug DC932 · Wing Miscellaneous StructureSDR ABXA030079Fitting · crackedRT FLAP INTERIOR FITTING AT INBOARD SIDE OF CENTER HINGE WAS CRACKED IN TWO PLACES BETWEEN RIVETS, BOTH ON UPPER SIDE OF FITTING. REPAIRED FITTING IAW DC-9 SRM 57-09.Feb 7, 2003 · N928AX · Doug DC932 · Trailing Edge FlapsSDR ABXA030078Fitting · crackedLEFT FLAP INBOARD HINGE, INTERNAL HINGE ATTACH FITTING WAS CRACKED ON THE OUTBOARD AFT CORNER. REMOVED AND REPLACED FLAP IAW DC-9 MM 27-51-01-4-0201.Feb 7, 2003 · N928AX · Doug DC932 · Trailing Edge FlapsSDR MWEA030052Bulkhead · crackedSTATION 965 RIGHT, FORWARD PYLON, BULKHEAD WEB HAS TWO SMALL CRACKS EMANATING FROM SNAPS AT OUTBOARD SIDE NEXT TO LONGERON 11 AND LONGERON 10. CUT OUT DAMAGE, FABRICATED DOUBLER, INSTALLED TWO EACH OF DOUBLERS AND PARTITION GUIDE.Feb 3, 2003 · N207ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA030054Bulkhead · crackedAT APPROXIMATELY STATION 965 RIGHT FORWARD BULKHEAD WALL HAS A CRACK APPROXIMATELY SIX INCHES INBOARD OF OUTSIDE BULKHEAD ATTACH ANGLE, CRACK IS EMITTING FROM BOLT HOLE FOR THE LOWER SPAR. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED WEB.Feb 3, 2003 · N207ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA030053Bulkhead · crackedSTATION 965 RIGHT FORWARD PYLON BULKHEAD HAS A CRACK GOING INBOARD OF LIGHTENING HOLE AT Z = 50.0. FABRICATED AND INSTALLED DOUBLER.Feb 3, 2003 · N207ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA030051Rib · crackedLEFT NR 5 SLAT OUTBOARD RIB IS CRACKED AT LOWER AFT CORNER. REMOVED CRACKED RIB AND INSTALLED NEW RIB.Feb 3, 2003 · N207ME · Doug DC932 · Leading Edge DevicesSDR MWEA030050Skin · crackedFUSELAGE SKIN CRACKED AT FRAME STATION 180 SHEAR TIE BETWEEN LONGERON 1&2 RIGHT. FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED DOUBLER.Feb 3, 2003 · N207ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA030043Transmitter · defectiveRIGHT OIL PRESSURE WAS AT ZERO. -- REMOVED AND REPLACED TRANSMITTER AND BUTT SPLICE.Jan 22, 2003 · N401ME · Doug DC932 · Engine Oil Indicating SystemSDR MWEA030039Seal · corrodedLOWER SEAL ON LEFT FORWARD OVERWING EMERGENCY EXIT DOOR IS CORRODED. -- LOCATED AND INSTALLED NEW SEAL RETAINER.Jan 20, 2003 · N401ME · Doug DC932 · Emergency ExitsSDR MWEA030038Spar · damagedLEFT WING STATION XRS 157 AFT SPAR REPAIR. -- FABRICATED AND INSTALLED REPAIR PARTS, FABRICATED AND INSTALLED NEW TEE.Jan 20, 2003 · N401ME · Doug DC932 · Wing SparSDR MWEA030037Frame · crackedCANTED FRAME AT STATION 1168 AT THE 2 O'CLOCK POSITION IS CRACKED. -- LOCATED,DRILLED AND INSTALLED NEW FRAME.Jan 20, 2003 · N401ME · Doug DC932 · Fuselage Main, FrameSDR MWEA030034Clip · crackedRUDDER POWER PACK SUPPORT TO FRAME ATTACH POINT IS CRACKED ON THE FRAME SIDE, RIGHT SIDE OF AFT ACCESSORY. -- REMOVED ATTACH POINT, FABRICATED AND INSTALLED NEW CLIP.Jan 16, 2003 · N401ME · Doug DC932 · Fuselage Main, FrameSDR MWEA030033Doubler · dentedFUSELAGE DENT AFT OF CARGO DOOR STATION 965 BETWEEN LONGERON 25-26 RIGHT. -- FABRICATED AND INSTALLED DOUBLER.Jan 16, 2003 · N401ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA030034Control Cable · lack of lubeWITH LANDING GEAR RETRACTED, GEAR DOOR OPEN LIGHT AND RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLING GEAR, HAD NO EFFECT ON THIS CONDITION. FERRIED AIRCRAFT BACK TO ILN UNDER FERRY PERMIT 002-003. REMOVED, CLEANED, LUBRICATED AND REINSTALLED DOOR SJan 15, 2003 · N988AX · Doug DC932 · Landing Gear Retraction/Extension SystemSDR ABXA030004Control Panel · defectiveAT CRUISE, SAW SMOKE COMING OUT AROUND CENTER INSTRUMENT AND PEDESTAL LIGHT PANEL. TURNED LIGHTS OFF. DECLARED EMERGENCY, RAN CHECKLIST AND RETURNED AIRPORT, AFTER SMOKE STOPPED. ISOLATED BURNING ODOR TO CENTER INSTRUMENT PANEL LIGHTING CONTROL PANEL. REPLACEDJan 7, 2003 · N903AX · Doug DC932 · Flight Compartment LightingSDR MWEA030009Filter · defectiveRIGHT HYDRAULIC SYSTEM FLUID QUANTITY DEPLETED AND LOST PRESSURE. REMOVED AND REPLACED AUXILIARY LINE FILTER HOUSING AND FILTERS.Jan 7, 2003 · N216ME · Doug DC932 · Hydraulic Filter, AuxiliarySDR ABXA030005Rib · crackedRIGHT ELEVATOR CRACKED ON INBOARD BULKHEAD COMMON TO FORWARD TORQUE TUBE. CRACK WAS IN LOWER FLANGE AT SPLICE AREA TO HINGE FITTING. VERIFIED WITH X-RAY AND BORESCOPE VISUAL. REPLACED RIGHT ELEVATOR IAW DC-9 MM.Jan 5, 2003 · N902AX · Doug DC932 · Elevator Control SystemSDR ABXA030007Wire · burnedDURING MAINTENANCE, NOTED 3 WIRES CONNECTED TO APU FEEDERS BEHIND GENERATOR CONTROL RACK WERE BURNED. REPLACED WIRES FROM S30-12 BURNDY BLOCK TO STA. 160 LEFT IAW REA D924-46054. WAS MISWIRED AT S30-12 WAS INSTALLED IN TERMINAL 26 INSTEAD OF 25. OPS CHECKED GJan 4, 2003 · N983AX · Doug DC932 · Electrical Power System WiringSDR AT0300002Ground Wire · damagedDURING B-CHECK FOUND AFT EMERGENCY EXIT (OVERWING) IDENTIFIERS DID NOT WORK. FOUND 3 AO RIVNUT GROUND UNDER LEFT AFT OVERWING EXIT, REPAIRED OPS CHECK GOOD.Jan 2, 2003 · N849AT · Doug DC932 · Light System WiringSDR MWEA020769Web · crackedFOUND TWO CRACKS IN WEB AT FUSELAGE STATION 1038 LEFT SIDE AT APPROXIMATELY LONGERON 12. -- REMOVED AND REPLACED NEW SECTION.Dec 31, 2002 · N401ME · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA030001Filter · leakingWHILE CLIMBING THRU 14,000 FT, LEFT OIL PRESSURE LOW LIGHT CAME ON. OIL PRESSURE SHOWED ABOUT 15 PSI. OIL QUANTITY RAPIDLY DECREASED TOWARDS ZERO. SHUT DOWN THE LT ENGINE. INSPECTED AND FOUND NR 1 ENGINE OIL FILTER HOUSING HAD 1 EA. STUD PULLED LOOSE, OIL DISPDec 30, 2002 · N902AX · Doug DC932 · Reciprocating Engine Oil SystemSDR AT0300001Battery · dischargedOVERWING EMERGENCY EXIT DOOR LIGHTS WILL NOT ILLUMINATE (SEAT ROW 18A & F). REMOVED AND REPLACED BATTERY AND POWER SUPPLY.Dec 28, 2002 · N845AT · Doug DC932 · Emergency LightingSDR MEX2002378Valve · failedAIRCRAFT RETURN, DUE TO NOSE LANDING GEAR UNSAFE INDICATION. AIRCRAFT WAS SENT TO THE HANGAR TO ATTEND THE FAIL. REPLACED NOSE LANDING GEAR O-RINGS IAW MM 32-21-2 AND LANDING WITH OVERWEIGHT INSPECTION WAS ACCOMPLISHED IAW MM 05-51-0. ADDITIONALLY THE FOLLOWDec 24, 2002 · N1003P · Doug DC932 · Landing Gear Retraction/Extension System
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