Douglas DC-9-32

Service difficulty reports · 12,755

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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"

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SDR MWEA010161Clip · brokenTAIL CONE AFT INTERIOR HANDLE HAS A BROKEN CLIP AND FAILS PULL CHECK (25 - 35 LBS). REMOVED AND REPLACED CLIP.Feb 19, 2001 · N212ME · Doug DC932 · Aerodynamic FairingsSDR MWEA010169Stall Warning · malfunctionedAFTER GEAR UP, AIRCRAFT FAILED TO PRESSURIZE AND STALL INDICATION FAILURE LIGHT CAME ON AT FLAPS 5 DEGREES. MAINTENANCE FOUND OUTFLOW VALVE WAS INLOCKED OPEN/MANUAL POSITION ON PEDESTAL. RETURNED TO OPEN/AUTO POSITION. ALSO REMOVED AND REPLACED LEFT ANGLE OFeb 19, 2001 · N602ME · Doug DC932 · Stall Warning SystemSDR MWEA010166Skin · dentedRUDDER LEFT SKIN HAS .75 INCH BY .75 INCH DENT .010 INCH DEEP AT ZR 28.936. REMOVED AND REPLACED DOUBLER.Feb 19, 2001 · N212ME · Doug DC932 · Rudder, Plate/SkinSDR MWEA010165Skin · damagedAFT CARGO BAG FUSELAGE SKIN HAS MECHANICAL DAMAGE FROM STATION 876 - STATION 890 BETWEEN LONGERON 23 THRU LONGERON 22 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS.Feb 19, 2001 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA010164Belt · corrodedNR 20 LEFT WINDOW FRAME CORRODED IN BOTH LOWER, INNER CORNERS. REMOVED AND REPLACED WINDOW BELT.Feb 19, 2001 · N212ME · Doug DC932 · Fuselage Main, StructureSDR MWEA010162Panel · dentedLEFT WING UPPER TRAILING EDGE PANEL IS DENTED, STATION 419, 4 INCHES AFT OF REAR SPAR. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER.Feb 19, 2001 · N212ME · Doug DC932 · Wing, Plate/SkinSDR MWEA010160Ring · crackedLEFT WINDOW RING CRACKED, STATION 639 - 658. REMOVED AND REPLACED WINDOW RING.Feb 19, 2001 · N212ME · Doug DC932 · Passenger Compartment WindowsSDR MWEA010159Skin · dentedFUSELAGE SKIN DENTED STATION 980, 2 INCHES BELOW LONGERON 2 RIGHT. FABRICATED AND INSTALLED DOUBLER.Feb 19, 2001 · N212ME · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0100085Seat Track · corrodedFOUND LEFT INBOARD SEAT TRACK AT BS 918 - 965 CORRODED BEYOND LIMITS. REPLACED CORRODED SECTION OF SEAT TRACK IAW DC9 SRM 53-05 FIG 4B & 4F.Feb 16, 2001 · N824AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA010167Regulator Valve · stuckDURING CLIMBOUT FROM MILWAUKEE, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT CAME ON. AIRCRAFT RETURNED TO MILWAUKEE. MAINTENANCE REMOVED AND REPLACED THE RIGHT PRESSURE REGULATOR VALVE FOR STICKING OPEN.Feb 16, 2001 · N302ME · Doug DC932 · Airfoil Anti/De-ice SystemSDR AT0100094Warn Panel · malfunctionedFOUND SMOKE DETECTOR LOOP LIGHT ON IN FLIGHT, FORWARD CARGO COMPARTMENT LOOP-B. CREW REPORTED LOWER CARGO COMPARTMENT SMOKE DETECTION SYSTEM DID NOT TEST AFTER B-LOOP LIGHT ILLUMINATED. INSPECTED FORWARD AND AFT CARGO COMPARTMENT, NO DEFECTES NOTED. CHECKEDFeb 15, 2001 · N830AT · Doug DC932 · Detection SystemSDR AT0100099Longeron · crackedFOUND LONGERON IN E&E COMPARTMENT CRACKED AT BS 200 LONGERON 29 RIGHT. INSTALLED LONGERON SPLICES IAW DC9 SRM 53-02 FIG 18.Feb 14, 2001 · N824AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0100092Floor Panel · corrodedFOUND FORWARD CABIN FLOOR PANEL BS 155 CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 51-10-02, 51-10-03, 51-10-04, 53-21 FIG 20 AND DC9 MM 53-20-01.Feb 14, 2001 · N824AT · Doug DC932 · Fuselage Floor PanelSDR AT0100084Skin · dentedREPLACE TEMPORARY REPAIR WITH PERMANENT REPAIR AT BS 976. REPLACED REPAIR IAW DC SRM 53-04 FIG 12B, 51-10-03, AND 51-20.Feb 14, 2001 · N824AT · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA010163Throttle Cable · stuckSTARTED DESCENT FROM FLIGHT LEVEL 350 AND LEFT THROTTLE STUCK AT 80 PERCENT N2. THROTTLE FREED UP PRIOR TO LANDING. MAINTENANCE DISASSEMBLED LEFT THROTTLE CABLE, CLEANED AND LUBRICATED INNER ELEMENT. ALSO FOUND CABLE CLAMPED IN A WAY CAUSING MISALIGNMENT. Feb 14, 2001 · N401ME · Doug DC932 · Power LeverSDR CA010321009Receptacle · burned(CAN) ON TAKEOFF, BURN SMELL REPORTED IN THE GALLEY AREA. CIRCUIT BREAKER PULLED NO APPARENT SMOKE. FOUND NR 16 OVEN RECEPTACLE BURNT. REPLACED NR 16 RECEPTABLE.Feb 13, 2001 · Doug DC932 · Air Distribution SystemSDR AT0100102Skin · crackedFOUND AFT PIT CARGO DOOR INNER SKIN TORN AT AFT HINGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 52-05, 51-30-01, 51-30-02, AND 51-30-05.Feb 13, 2001 · N824AT · Doug DC932 · Cargo/Baggage DoorsSDR AT0100091Floor Panel · corrodedFOUND FLOOR PANEL 47 CORRODED BEYOND LIMITS. REPLACED FLOOR PANEL IAW DC9 SRM 53-21 AND 51-20-02.Feb 13, 2001 · N824AT · Doug DC932 · Fuselage Floor PanelSDR ABXA010052Wire · damagedTHE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED INTERMITTANTLY. THE FLIGHT RETURNED TO ILN TO COMPLETE REPAIRS. MAINTENANCE INSPECTED AND REPAIRED A WIRE FOR CONNECTOR P1-130 PIN NR 4. LANDING GEAR OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS Feb 13, 2001 · N939AX · Doug DC932 · Landing Gear System WiringSDR MWEA010154Web · crackedVERTICAL WEB CRACKED IN RIGHT PYLON OUTBOARD OF 13TH STRINGER. BLEED NUT ACCESSIBLE THROUGH PANEL 8204A. FABRICATED AND INSTALLED REPAIR DOUBLERS.Feb 13, 2001 · N212ME · Doug DC932 · Nacelle/Pylon, Main FrameSDR MWEA010153Longeron · corrodedCORROSION ON LONGERON 12 LEFT AT STATION 1104. FABRICATED AND INSTALLED LONGERON AND ANGLE.Feb 13, 2001 · N212ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA010152Floor Panel · crackedFLOOR PANEL E-6 IS CRACKED ON AFT OUTBOARD CORNER. FABRICATED AND INSTALLED DOUBLER.Feb 13, 2001 · N212ME · Doug DC932 · Fuselage Floor PanelSDR MWEA010151Angle · crackedCRACK AT STATION 1121 AT LONGERON 17 RIGHT. DRILLED AND INSTALLED REPAIR ANGLES.Feb 13, 2001 · N212ME · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0100176Proximity Sensor · out of adjAIRCRAFT WOULD NOT TRANSFER TO FLIGHT MODE. AIRCRAFT WAS FERRIED FOR TROUBLESHOOTING. RIGGED AND ADJUSTED GROUND SENSE MECHANISM AND SERVICED NOSE STRUT IAW DC9 MM 32-23-1, 32-21-2.Feb 12, 2001 · N866AT · Doug DC932 · Landing Gear Position and WarningSDR 0100439610Apu · overservicedDURING CLIMB, FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN. FORWARD LAV DETECTOR SOUNDED. FLIGHT CREW RETURNED TO DEPARTURE AIRPORT. SMOKE BEGAN TO DISSIPATE DURING RETURN TO DEPARTURE AIRPORT. AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE FOUND APU OIL OFeb 12, 2001 · N610NW · Doug DC932 · APU Oil SystemSDR MWEA010158Elevator · damagedLEFT ELEVATOR HAD LIGHTNING STRIKE EXIT DAMAGE OUTBOARD OF LAST STATIC WICK MOUNT ON TRAILING EDGE. REMOVED DAMAGED PARTS, FABRICATED, LOCATED AND INSTALLED NEW PARTS.Feb 10, 2001 · N205ME · Doug DC932 · Elevator StructureSDR AT0100101Longeron · crackedFOUND LONGERON 27R CRACKED AT BS 258. FABRICATED AND INSTALLED REPAIR SPLICES IAW DC9 SRM 51-10-05, 51-10-04, AND 53-02 FIG 18.Feb 9, 2001 · N824AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR AT0100096Web · damagedFOUND HOLE AT NUT PLATE IN FORWARD PIT WEB BS 370 LONG 24R. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-03, 51-10-04, 53-01 FIG 2, 53-30-02, AND REO-L00408.Feb 9, 2001 · N824AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0100089Pan · corrodedFOUND G4 GALLEY FLOOR PAN CORRODED BEYOND LIMITS. FORMED AND INSTALLED FLOOR PAN AND HAT CHANNELS IAW DC9 SRM 51-10-03, 51-30-02, 53-01 FIG 1, AND 53-20 FIG 5C.Feb 9, 2001 · N824AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0100088Door Frame · gougedFOUND FORWARD GALLEY DOOR JAMB GOUGED BEYOND LIMITS. REMOVED GOUGED SECTION AND INSTALLED REPAIR IAW DC9 SRM 53-05 FIG 55, 51-10-02, 51-10-03, 51-10-04, 51-30-01, 51-30-02, 51-30-05, AND 53-01 FIG 1.Feb 9, 2001 · N824AT · Doug DC932 · Fuselage Main, StructureSDR MWEA010155Skin · lightning strikeFOUND LIGHTNING STRIKE DAMAGE TO LEFT ELEVATOR OUTBOARD TRAILING EDGE. MAINTENANCE FABRICATED AND INSTALLED ELEVATOR SKIN REPAIR.Feb 9, 2001 · N501ME · Doug DC932 · Elevator StructureSDR MWEA010148Fitting · crackedFITTING CRACKED AT VERTICAL WEB AT LEFT ENGINE PYLON STRUCTURE, VIEWED THROUGH PANEL 8105A. REMOVED AND REPLACED FITTING.Feb 9, 2001 · N212ME · Doug DC932 · Nacelle/Pylon, Attach FittingsSDR MWEA010149Rib · wornLEFT NR 4 SLAT OUTBOARD BUSHINGS AT THE COMMON LINK WORN. REMOVED AND REPLACED RIB.Feb 9, 2001 · N212ME · Doug DC932 · Leading Edge DevicesSDR AT0100104Panel · chafedFOUND VERTICAL STABILIZER UPPER FAIRING CHAFED OUT OF LIMITS. REPLACED SKIN PANEL IAW DC9 SRM 55-01 FIG 1, 55-31, 51-10-02, 51-10-03, 51-10-04, AND 51-30-02.Feb 8, 2001 · N824AT · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR AT0100103Door Frame · crackedFOUND AFT CARGO DOOR FRAME CRACKED. STOP DRILLED CRACK AND FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-10-02, 51-10-03, 51-10-04, 51-30-02, 51-30-01, AND 52-03.Feb 8, 2001 · N824AT · Doug DC932 · Fuselage Main, StructureSDR AT0100100Skin · gougedFOUND AFT PIT CARGO DOOR SKIN GOUGED BEYOND LIMITS. INSTALLED REPAIR DOUBLER IAW DC9 SRM 52-05 FIG 3, 52-01 FIG 1, 51-10-04, 51-10-02, AND 51-10-03.Feb 8, 2001 · N824AT · Doug DC932 · Cargo/Baggage DoorsSDR AT0100097Angle · corrodedFOUND RIGHT NOSE LANDING GEAR WHEEL WELL LOWER ANGLE CORRODED BEYOND LIMITS AT BS 109 RBL 27. INSTALLED REPAIR IAW REO-L00405.Feb 8, 2001 · N824AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0100093Floor Support · corrodedFOUND FORWARD CABIN FLOOR SUPPORT AT BS 200 CORRODED. REPLACED FLOOR SUPPORT IAW DC9 SRM 53-21, 53-11-01, AND 53-30-05.Feb 8, 2001 · N824AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0100077Engine · failedON CLIMBOUT CAPTAIN REPORTED NR 2 ENGINE PARAMETERS ACCELERATED WITH N1/N2 CLIMBING THRU 99 PERCENT AND EGT AT 750C FOR 30 SECONDS. SHUT DOWN ENGINE AND SECURED AIRCRAFT FOR ENGINE OUT APPROACH. REMOVED AND REPLACED NR 2 ENGINE DUE TO EGT LIMITS EXCEEDING TEFeb 8, 2001 · N816AT · Doug DC932 · Engine (Turbine/Turboprop)SDR AT0100087Door Frame · corrodedFOUND AFT CARGO DOOR JAMB CORRODED BEYOND LIMITS. INSTALLED NEW DOOR JAMB IAW DC9 SRM 53-05 FIG 44, 51-30-01, 51-30-02, 51-30-04, 51-10-03, 51-30-05, AND RES 01-220.Feb 7, 2001 · N824AT · Doug DC932 · Fuselage Main, StructureSDR AT0100086Web · crackedFOUND R-1 DOOR JAMB LOWER CORNER SKIN CRACKED. CUT OUT CRACK AND INSTALLED REPAIR IAW EO 09-5310-29-E1472.Feb 7, 2001 · N824AT · Doug DC932 · Fuselage Main, StructureSDR AT0100090Cargo Track · corrodedFOUND FORWARD PIT CARGO TRACK BS 239 - 340 CORRODED BEYOND LIMITS. INSTALLED NEW SECTION OF CARGO TRACK IAW DC9 SRM 51-10-03, 51-10-04, 53-05 FIG 4C, AND 53-21.Feb 6, 2001 · N824AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA010038Socket · intermittentTHE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED INTERMITTANTLY AFTER GEAR WAS FULLY RETRACTED, AND CONTINUED TO INTERMITTANTLY ILLUMINATE FOR THE REMAINDER OF THE FLIGHT. FLIGHT CREW RECYCLED THE LANDING GEAR. MAINTENANCE INSPECTED AND REPLACED THE RIGHFeb 6, 2001 · N988AX · Doug DC932 · Landing Gear Position and WarningSDR AT0100055Light · corrodedFOUND EMERGENCY LIGHTS JUST INSIDE CABIN INOPERATIVE. CLEANED SLIGHT OXIDATION FROM BATTERIES AND HOLDER, REINSTALLED IAW DC9 MM 33-50.Feb 6, 2001 · N867AT · Doug DC932 · Emergency LightingSDR AT0100054Battery Pack · dischargedFOUND LEFT NACELLE EMERGENCY LIGHT WOULD NOT COME ON. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW DC9 MM 33-50.Feb 6, 2001 · N867AT · Doug DC932 · Emergency LightingSDR ABXA0100038Socket · intermittentTHE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED INTERMITTANTLY AFTER GEAR WAS FULLY RETRACTED, AND CONTINUED TO INTERMITTANTLY ILLUMINATE FOR THE REMAINDER OF THE FLIGHT. FLIGHT CREW RECYCLED THE LANDING GEAR. MAINTENANCE INSPECTED AND REPLACED THE RIGHFeb 6, 2001 · N988AX · Doug DC932 · Landing Gear Position and WarningSDR 0100459984Fuel Control · malfunctionedDURING TAKEOFF, THE FLIGHT CREW REPORTED A COMPRESSOR STALL BELIEVED TO BE FROM THE RIGHT ENGINE. A HIGH SPEED ABORTED TAKEOFF WAS ACCOMPLISHED AND THE FLIGHT RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE FUEL CONTROL UNITS LOCATED ON BOTH Feb 5, 2001 · N984US · Doug DC932 · Fuel Control/Turbine EnginesSDR MWEA010145Sense Line · chafedFLIGHT CREW REPORTED RIGHT ENGINE EXHAUST PRESSURE RATIO INDICATION READS HIGH. ALL OTHER INDICATIONS READ NORMAL. MAINTENANCE FOUND PRESSURE RATIO SENSE LINE CHAFED AND REPLACED THE LINE.Feb 5, 2001 · N401ME · Doug DC932 · Power Indicating SystemSDR AT0100078Tripler · crackedFOUND FORWARD AIRSTAIR CUT OUT DOUBLER CRACKED IN AFT LOWER CORNER. INSTALLED TRIPLER, FILLER, INTERCOSTAL, AND CHANNEL IAW REO L00360.Feb 2, 2001 · N802AT · Doug DC932 · Fuselage Main, Plate/SkinSDR 0100359619Battery · inoperativeDURING LINE CHECK, FOUND ALL CATWALK EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR CATWALK EMERGENCY EXIT LIGHTING. OPERATIONAL CHECK NORMAL.Feb 1, 2001 · N619NW · Doug DC932 · Emergency Lighting
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