Boeing DC-9-83
Service difficulty reports · 16,530
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 = 'DC983' 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 = 'DC983' 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 ASAA0280120Connector · looseSEA - DURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS INOPERATIVE IN 1ST CLASS. RECONNECTED LOOSE CONNECTORS. LIGHTS THEN OPERATED PROPERLY. (M)SDR GTIA020258Isolation Mount · wornDTW - NR 2 FORWARD LOWER VIBRATION ISOLATOR REGS CHANGE DUE TO SLIP MARK OUT OF LIMITS. REMOVED AND REPLACED NR 2 ENGINE FORWARD LOWER VIBRATION ISOLATOR IAW MD80 MM 71-20-02. INSTALLATION CHECKS GOOD WITH NO FURTHER DEFECTS NOTED AT THIS TIME. (M)SDR GTIA020259Isolation Mount · wornDTW - NR 2 ENGINE FORWARD UPPER VIBRATION ISOLATOR REGS CHANGE DUE TO METAL FLAKING OFF OF INNER RACE. REMOVED AND REPLACED NR 2 ENGINE FORWARD UPPER VIBRATION ISOLATOR IAW MD80 MM 71-20-02. INSTALLATION CHECKS GOOD WITH NO FURTHER DEFECTS NOTED AT THIS TIMESDR GTIA020260Isolation Mount · wornDTW - NR 2 ENGINE AFT VIBRATION ISOLATOR REGS CHANGE DUE TO SCRATCHES ON INNER FACE. REMOVED AND REPLACED NR 2 ENGINE AFT VIBRATION ISOLATOR IAW MD80 MM 71-20-02. INSTALLATION CHECKS GOOD WITH NO FURTHER DEFECTS NOTED AT THIS TIME. (M)SDR GTIA020261Battery · dischargedMCO - AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY IAW M 33-53-00. LIGHTS CHECK OK. (M)SDR GTIA020263Wire · chafedORD - AUTOPILOT AND AUTOTHROTTLES KICKED OFF AT 240. TAIL KICKED TO ONE SIDE TURNED OFF YAW DAMPER AND HAND FLEW AIRCRAFT. PERFORMED SYSTEM TROUBLESHOOTING AND SERVO/SENSOR OPERATION IAW MD80 MM 22-01-03. NOTED 2 CHAFED WIRE ON LUG NR 2 TERMINAL S-30-5. BUSDR GTIA020264Turbine Blades · damagedDTW - NR 2 ENGINE REQUIRES BORESCOPE FOUND C-1 BLADE DAMAGED AND BORESCOPE REVEALED DAMAGED 7TH STAGE BLADES OUT OF LIMITS. REMOVED AND REPLACED ENGINE. (M)SDR GTIA020270Striker · out of adjustSJU - FLT 774 - AFT CARGO DOOR LIGHT ON AFTER TAKEOFF, RTB SJU, LIGHT OUT AFTER LANDING. ADJUSTED STRIKER PLATE FOR AFT CARGO DOOR PROX SWITCH IAW MD80 MM 52-70-02. FUNCTIONS CHECK OK. (M)SDR GTIA020257Switch · inoperativeDTW - FLT 56 - PRIMARY TRIM ON F/O SIDES STOP WORKING ON APPROACH INTO DTW HANDLES WERE USED AFTER LANDING, LEFT AND RIGHT ELECTRIC TRIM SWITCH AND HANDLES MANUAL TRIM INOPERATIVE. REMOVED AND REPLACED PRIMARY TRIM MOTOR. OPS CHECK GOOD IAW MD80 MM 27-40-01.SDR GTIA020268Actuator · failedLGA - PREFLIGHT, FOUND PRIMARY STAB TRIM WOULD NOT OPERATE NORMALLY FROM THE SUITCASE HANDLES, MOTOR THERMALLY CUTS OUT AFTER ONLY SHORT USAGE 5-10 SECONDS FROM YOLK SWITCHES. FOUND 'B' PHASE C/B BAD REMOVED AND REPLACED 'B' PHASE C/B, OPS CHECK NORMAL PER A/SDR AALA20020483Window Frame · crackedTUL - FOUND WINDOW FRAME CRACKED STATION 947 LONGERON 12L. STOP DRILLED, CRACK AND INSTALLED DOUBLER PER 53-10-00-25 PAGE 2 FIG 1. (M)SDR AALA20020482Window Frame · crackedTUL - FOUND WINDOW FRAME CRACKED STATION 1021 LONGERON 12L. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-10-25 PAGE 2 FIG 1. (M)SDR ASAA0280110Web · chafedPAE - DURING 30K-CHECK, FOUND APU COMPARTMENT CEILING CHAFED AT FS 1368. CUT OUT CHAFED AREA AND INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M)SDR ASAA0280113Window · looseSEA - DURING PREFLIGHT CHECK, IT WAS DETERMINED THAT LOOSE WINDOW FOAM MOLDING WAS STOPPING THE SLIDING CLEARVIEW WINDOW FROM OPENING. RE-GLUED FOAM MOLDING. WINDOW THEN OPERATED PROPERLY. (M)SDR GTIA020253Actuator · failedMYR - PRIMARY TRIM NOSE DOWN INTERMITTENT ON GROUND. REMOVED AND REPLACED PRIMARY TRIM MOTOR PER MD80 MM 27-40-01, OPERATIONAL TEST OF PRIMARY TRIM MOTOR. OPS CHECK GOOD. (M)SDR GTIA020254Controller · malfunctionedFLL - FLT 1083 - NR 2 AUTOPILOT VERY JERKY IN LEVEL FLIGHT, YOKE MOVES BACK AND FORTH IN SHORT CHOPPY MOVEMENTS. STP RTS CHECK SHOWED 4 FAULTS A/P, F/D, A/T, S/V, Y/D. REMOVED AND REPLACED NR 2 DFGC. OPS CHECK NORMAL IAW MM 22-01-05. RTS CHECK INDICATES 'GSDR AALA20020486Angle · crackedTUL - FOUND LEFT WINDOW FRAME ANGLE CRACKED. STOP DRILLED END OF CRACK, CONFIRMATION WITH DYE CHECK. INSTALLED ANGLE DOUBLER PER AARD 53-10-00-25. (M)SDR MEX2002087Bearing · failedFLT 574 - CUN-MEX - AIRCRAFT ARRIVED TO PLATFORM WITH HYDRAULIC FLUID LEAK IN THE RIGHT SYSTEM. IT WAS CHECKED AND THE LEAK WAS FOUND AT THE PTU SHUTOFF VALVE. BEARINGS WERE CHANGED IAW MM 29-10-08. DURING OVERNIGHT SERVICE WERE DETECTED THAT THE SEPARATOR SDR ASAA0280103Door Frame · damagedPAE - DURING 30K-CHECK, FOUND MECHANICAL DAMAGE ON RIGHT FORWARD SERVICE DOOR CUTOUT FORWARD LOWER CORNER. REPAIRED CUTOUT (JAMB PAN) PER EA 5301-02071. (M)SDR ASAA0280112Splice · damagedPAE - DURING 30K-CHECK, FOUND FRAME TO FLOORBEAM SPLICE AT FS 984 TO HAVE ELONGATED HOLES. REPLACED SPLICE PER MM 20-10-15 AND SRM 53-14-3. (M)SDR ASAA0280111Web · crackedPAE - DURING 30K-CHECK, FOUND PAX CABIN CUSP WEB CRACKED AT FS 987-999. REPLACED WEB PER SRM 51-30-2, 51-30-5, AND 51-10-4. (M)SDR ASAA0280109Angle · corrodedPAE - DURING 30K-CHECK, FOUND CORROSION ON FORWARD SERVICE DOOR CUTOUT (JAMB) AFT EDGE ANGLE AT FLOOR. REPLACED ANGLE PER SRM 51-10-4, 51-30-2, AND 51-30-1. (M)SDR ASAA0280108Angle · corrodedPAE - DURING 30K-CHECK, FOUND CORROSION ON FORWARD SERVICE DOOR CUTOUT, JAMB, FORWARD EDGE ANGLE AT FLOOR. REPLACED ANGLE PER SRM 51-10-4, 51-30-2, AND 51-30-1. (M)SDR ASAA0280107Rib · gougedPAE - DURING 30K-CHECK, FOUND LEFT WING NR 1 SLAT INBOARD RIB GOUGED IN INTERCONNECTING PIN BORE. REPLACED INBOARD RIB PER SRM 51-30-2. (M)SDR ASAA0280106Web · corrodedPAE - DURING 30K-CHECK, FOUND CORROSION ON FLOORWEB AT FS 1140. REPLACED WEB PER SRM 51-30-2. (M)SDR ASAA0280105Web · corrodedPAE - DURING 30K-CHECK, FOUND CORROSION ON WEB AT FS 1193-1231. REPLACED WEB PER SRM 51-30-2. (M)SDR ASAA0280104Web · corrodedPAE - DURING 30K-CHECK, FOUND CORROSION ON WEB AT FS 984-1003. REPLACED WEB PER SRM 51-30-2. (M)SDR ASAA0280102Frame · corrodedPAE - DURING 30K-CHECK, FOUND CORROSION IN AFT CARGO BAY ON UPPER SURFACE OF LOWER FLANGE OF FAIL/SAFE ANGLE AT FASTENER HOLES AT FS 1117. REPLACED FAIL/SAFE ANGLE PER SRM 53-01 AND 51-30-02. (M)SDR ZW0A0203502Cap · leakingFUEL SMELL IN AIRCRAFT CABIN. REMOVED AND REPLACED LEAKING RUBBER CAP ON ATOMIZER IN APU COMBUSTION CHAMBER.SDR AALA20020337Battery · dischargedDFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS AND HALF OF COACH EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR ASAA0280101Web · corrodedPAE - DURING 30K CHECK, FOUND WEB CORRODED AT FS 712-731. REPAIRED WEB PER SRM 51-30-2, 53-01 FIG 1, 51-70-4 FIG 2, 51-10-3, AND MM 53-20-01. (M)SDR GTIA020247Proximity Sensor · dirtyDTW - FOUND AFTER DEPARTURE DURING GEAR RETRACTION, GOT A RED UNSAFE LIGHT ON THE LEFT MAIN. RECYCLED THE GEAR AND HAD NORMAL INDICATIONS. CLEAN PROXIMITY SENSORS, OPS CHECKED GOOD IAW MD80 MM 32-60-05. (M)SDR GTIA020248Switch · faultyDTW - FLT 909 - ALTERNATE TRIM MOTO TRIMS WHEN RIGHT SWITCH IS MOVED. LEFT SWITCH IN CENTER POSITION, RIGHT SWITCH ALONE WILL MOVE TRIM IN BOTH DIRECTIONS. REMOVED AND REPLACED ALT TRIM BRAKE RELEASE SWITCH AND ALT TRIM SWITCH. SYSTEM OPS CHECK GOOD IAW MM SDR GTIA020252Socket · looseLGA - FLT 774 - FOUND EMERGENCY LIGHT IN FORWARD OVERHEAD INOPERATIVE. FOUND SOCKET LOOSE. RESECURED SOCKET AND RELAMPED. OPS CHECK NORMAL IAW MM 33-50-00. (M)SDR AALA20020339Battery · dischargedSEA - DURING OVERNIGHT MAINTENANCE, FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD OVERWING EMERGENCY EXIT LIGHT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA20020356Beam · corrodedTUL - FOUND CORROSION ON AFT CARGO DOOR BEAM STATION 1155-1212. REMOVED AND REPLACED AFT CARGO DOOR BEAM FROM STATION 1117 TO 1250 PER AARD 53-10-00-3. (M)SDR ASAA0280100O-Ring · leakingPDX - FOUND OIL ODOR IN CABIN DURING FLIGHT. REPLACED LEAKING O-RING FOR APU OIL CLUSTER. OP CHECKED OK. (M)SDR ASAA0280099Module · disconnectedSEA - DURING PREFLIGHT CHECK, FOUND DISCONNECTED EMERGENCY TRACK LIGHTS IN THE 1ST CLASS CABIN. RECONNECTED LIGHT MODULE. LIGHTS THEN OPERATED NORMALLY. (M)SDR GTIA020249Light · out of positionDTW - SAFETY GLOW FLOOR PATH LIGHTING HAS NO BREAKS AT LEFT OVERWING EXITS. REPOSITIONED SAFETY GLOW FLOOR PATH LIGHTING AT LEFT OVERWING EXITS IAW SPIRIT AIRLINES ENGINEERING DRAWING NR SG-DC9 REVISION F. (M)SDR GTIA020244Battery · dischargedFLL - EMERGENCY LIGHTS AT EMERGENCY EXIT AFT ON LEFT AND RIGHT SIDES ROW 22AC AND 22DEF ARE INOPERATIVE. REMOVED AND REPLACED BATTERIES IN THE CONT. UNIT FOR LT AND RIGHT AFT EMERGENCY EXIT ROW OVERHEAD LIGHTS. OPS CHECK GOOD IAW MM 33-50-00. (M)SDR GTIA020245Servo · failedFLT 386 - DTW - AUTOPILOT WILL NOT STAY ENGAGED, TRIPS OFF EVERY 2-3 MINUTES, DFGS NR 1 OR NR 2, ALT TRIM OK. FOUND ELEVATOR POWER SERVO FAIL IN FLIGHT FAULT REVIEW. REMOVED AND REPLACED ELEVATOR SERVO IAW MM 21-12-01, PERFORMED AUTO PILOT CHECK AND RTS. OPSDR AALA20020357Frame · crackedTUL - FOUND CANT FRAME AT STATION 1485 HAS CRACKS UNDER AFT STAIR ACTUATOR CASTING ATTACH POINT. CUT OFF DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-33 (CANT FRAME REPAIR). (M)SDR ASAA0280098Splice · corrodedPAE - DURING 30K-CHECK, FOUND CORROSION ON CARGO TRACK LEFT LOWER SURFACE COMMON TO TRACK SPLICE AT FS 1211-1225. REPLACED SPLICE PER SRM 51-30-5, FIG 1. (M)SDR ASAA0280097Lanyard · disconnectedSEA - FORWARD SERVICE R-1 DOOR EMERGENCY SLIDE LANYARD DISCONNECTED. REATTACHED LANYARD. (M)SDR MEX2002077Switch · failedFLT 6426 - MEX-MTY - CABIN CREW REPORTED THAT SLAT AND SIF LIGHT WAS TURN ON AT ANY SELECTION/POSITION FLAP. IT WAS DETECTED A TROUBLE WITH THE SWITCH S1-467. SUCH SWITCH WAS REPLACED IAW MM 27-81-02, TESTS OK. AT RON, MEX 21/22 SEVERAL TESTS WERE PERFORMEDSDR MEX2002075Sensor · failedFLT 429 - MIA-MEX - AIRCRAFT RETURNED TO RAMP AS CONSEQUENCE OF SLAT DISAGREE LIGHT COMES ON STEADY DURING TAXI. SLATS OPERATION WAS CHECKED, THE RIGHT AND LEFT PROXIMITY SWITCH CIRCUIT BREAKER WAS RESET AND WAS PERFORMED A BITE TO THE STALL WARNING COMPUTER SDR ASAA0280075Outflow Valve · failedEN ROUTE TO SEA FLT 748, AUTO CABIN PRESSURE CONTROL MALFUNCTIONED, WITH CREW PERFORMING EMERGENCY DESCENT FROM 28,000 FEET ALTITUDE TO 10,000. REPLACED OUTFLOW VALVE MOTOR/ACTUATOR ASSEMBLY. SYSTEM THEM OP CHECK OK. (M)SDR AALA20020347Frame · gougedTUL - FOUND FRAME AT STATION 1401 HAS DEEP GOUGE AT INSTRUMENT AIRLINE ATTACH POINT AT LONGERON 21 RT. INSTALLED REPAIR DOUBLER AT STATION 1401 PER SRM 53-03 PAGE 5. (M)SDR AALA20020344Support · corrodedTUL - FOUND CORROSION ON F/B SUPPORT STATION 1212 L29R-L30. INSTALLED NEW FLOOR SUPPORT AT STATION 1212 L29R TO L30 SRM 51-01. (M)SDR ASAA0280076Frame · corrodedPAE - DURING 30K-CHECK, FOUND CORROSION ON TOP OF FRAME IN AFT CARGO BAY. INSTALLED NEW FRAME PER SRM 53-03, FIG 2A. (M)
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