Douglas 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 ASAA0280232Wire · disconnectedPDX - DURING LINE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE FROM ROW 6 TO 9. RECONNECTED WIRING TO LIGHT MODULE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)SDR ZW0A0208005Tee Chord · damagedDURING CHECK-C BULKHEAD CHORD DAMAGED FUSELAGE STATION 110 LONGERON 27R AND 28R AND TEE CHANNEL AFT SIDE OF BULKHEAD. COLD WORKED TEE CHORD NDT INSPECTED PER ARA 18213 ITEM 3 SHOT PEENED, NO CRACK FOUND PER 6-51-00-03.SDR ZW0A0208004Channel · damagedDURING CHECK-C TEE CHANNEL BELOW LONGERON 28R FUSELAGE STATION 110 TO APPROX FUSELAGE STATION 129 DAMAGED. REPLACED TEE CHANNEL 9911597-502 AND SEAL PER ARA18213.SDR ZW0A0208003Longeron · damagedDURING CHECK-C LONGERON 28R DAMAGED AT FUSELAGE STATION 110 TO FUSELAGE STATION 129. REPAIRED LONGERON 28A FUSELAGE STATION 110 TO FUSELAGE STATION 129 PER SRM 53-02 FIG 18. NO CRACKS FOUND PART 6-51-00-03.SDR ZW0A0208002Skin · damagedDURING CHECK-C, SKIN DAMAGED FUSELAGE STATION 110 TO APPROX FUSELAGE STATION 129 LONGERON 28 RIGHT TO LONGERON 27 RIGHT. REPAIRED SKIN DAMAGE FS 110 TO APPROX FS 129 L28R-L27R PER ARA18213 AND SRM 53-02. NO CRACKS FOUND PER PART 6-51-00-03.SDR ZW0A0207701PanelTHE MID CARGO COMPARTMENT SHOWED FIRE INDICATION. ONE FIRE BOTTLE WAS DISCHARGED AND THE FLIGHT MADE AN UNSCHEDULED LANDING AT DFW. THERE WAS NO INDICATION OF FIRE. CORRECTIONS TO THE INDICATION PROBLEM WAS DEFERRED PER MEL. THE COCKPIT CONTROL PANEL WAS LASDR AALA20021077Wire · looseDURING OVERNIGHT MAINTENANCE TAIL CONE EMERGENCY EXIT BATTERY WIRE LOOSE. TIGHTENED SCREW ON TAIL CONE EMERGENCY EXIT BATTERY FOR WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR ASAA0280229Module · disconnectedSFO - DURING PREFLIGHT CHECK, FIRST FOUR EMERGENCY TRACK LIGHTS WERE FOUND INOPERATIVE. RECONNECTED FIRST MODULE. LIGHTS THEN OPERATED PROPERLY. (M)SDR ASAA0280231Smoke Detector · false activationSEA - DURING FLIGHT 660, SMOKE DETECTOR IN LEFT AFT LAVATORY FALSELY ALARMED DESPITE NO AMBIENT SMOKE. RESET DETECTOR. SUBSEQUENT OPERATION CHECK WAS SATISFACTORY. (M)SDR ASAA0280226Connector · loosePDX - DURING PREFLIGHT CHECK, FORWARD 1ST CLASS EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. RECONNECTED LOOSE CONNECTOR. LIGHTS THEN OPERATED PROPERLY. (M)SDR ASAA0280225Module · inoperativeSEA - DURING LINE CHECK, EMERGENCY TRACK LIGHTING WAS INOPERATIVE FROM ROW 22 TO 30. REPLACED FOUR LIGHT MODULES. LIGHTS THEN OPERATED PROPERLY. (M)SDR ASAA0280223Lanyard · disconnectedPHX - DURING PRE-FLIGHT CHECK, THE AFT SERVICE DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M)SDR AALA20021028Fuel Control · malfunctionedIAD - FLT 1395 - EN ROUTE PHL-ORD, LEFT ENGINE THROTTLE RETARDED AT 10,000 FEET AND THEN REGAINED POWER UNCOMMANDED. DIVERTED AIRCRAFT TO IAD LANDING WITHOUT INCIDENT. AIRCRAFT NOT OVERWEIGHT. REPLACED LEFT ENGINE FUEL CONTROL AND FUEL PUMP. TRIMMED ENGINESDR AALA20021017Wire · looseDFW - DURING OVERNIGHT MAINTENANCE, AFT OVERHEAD EMERGENCY EXIT LIGHT BY L2 FLIGHT ATTENDANT SEAT INOPERATIVE. TIGHTENED AFT OVERHEAD EMERGENCY EXIT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR ASAA0280221Lanyard · disconnectedBUR - DURING PREFLIGHT CHECK, THE L1 DOOR EMERGENCY SLIDE LANYARD WAS FOUND TO BE DETACHED. REATTACHED LANYARD. (M)SDR GTIA020789Warning System · false activationDTW - FLT 777 - FOUND DOOR LIGHT MASTER CAUTION ON TAKEOFF ROLL REJECTED TAKEOFF AT 70 KTS. SELF-TESTED PROXIMITY UNIT AS REQUIRED OPS CHECK GOOD. NO FAULTS DETECTED. INSPECTED DOORS EXTERIOR DOORS, FOR SECURITY, NO DEFECTS NOTED. (M)SDR ASAA0280220Fairing · damagedOAK - RIGHT HORIZONTAL STABILIZER UPPER FAIRING WAS DAMAGED DURING LINE MAINTENANCE. TEMP REPAIRED FAIRING WITH CUT OUT PIECE FROM ANOTHER FAIRING AND SPEED TAPE PER EA 5510-01157. (M)SDR GTIA020784Rheostat · failedLAX - FLT 709 - FOUND AUTO PILOT NR 1 AND NR 2 DISCONNECTS DURING RIGHT TURNS. ALSO PULSES IN ROLL. OK STRAIGHT AND LEVEL AND LEFT TURNS. TROUBLESHOT AUTOPILOT SYSTEM. FOUND AILERON SERVO RHEOSTAT BAD. CHECKED WITH METER LEFT SIDE GOOD RIGHT SIDE BAD. RESDR ZWOA0207101Wire · damagedRIGHT OVERWING FLOOR EGRESS LIGHTS INOP. REPLACED WIRE SECTION AND REPLACED MISSING COVERS. LENS MFG PN 0105607 3015MI-932831/ COVER MFG PN 0105601003 PA57-932841/ WIRE SECTION MFG PN 0105606 0055MI-93289 LAST CHECK C PERFORMED IN STL 11/16/2001. --CLOSED--SDR ZW0A0207205Bulb · burned outTHE OVERHEAD CENTER EMERGENCY LIGHT IN THE TAIL CONE AREA, AND THE EGRESS LIGHT AT ROWS 7 AND 31, WERE INOPERATIVE. REPLACED THE BULB PN 1315 IN TAIL CONE AREA, AND REPLACED THE BULB PN 7732 AT BOTH ROWS 7 AND 31. CHECK-C 3-23-01 STL. --CLOSED--SDR ZW0A0207204Battery · dischargedTHE RT AND LT SIDE EMERGENCY OVERWING EXIT LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 3-23-01 STL. --CLOSED--SDR ZW0A0207203Battery Pack · dischargedTHE EMERGENCY OVERHEAD LIGHTS WERE INOPERATIVE AT ROW 19 AND 22. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 3-23-01 STL. --CLOSED--SDR ZW0A0207104Lamp · unsecureEGRESS LIGHTING AT ROW 28 INOP. RESEATED LAMP IN SOCKET. LAST CHECK C PERFORMED IN STL 03/23/2001. --CLOSED--SDR ZW0A0207103Battery Pack · dischargedEMERGENCY OVERHEAD LIGHTS AT ROW 19 INOP. REPLACED BATTERIES IN BATTERY PACK. LAST CHECK C PERFORMED IN STL 03/23/2001 --CLOSED--SDR ZW0A0207102Lamp · burned outLOWER TAILCONE EMERGENCY LIGHTING INOP. RELAMPED LIGHT ASSEMBLY. LAST CHECK C PERFORMED IN STL 03/23/2001 --CLOSED--SDR ZW0A0207003Coalescer Bag · contaminatedSMOKE WAS PRESENT IN CABIN AFTER STARTING APU. CHECKED WATER SEPARATORS AND PERFORMED MD9-49-06 MAINTENANCE SHEET. LAST CHECK C PERFORMED 10/25/2001 AT MCI. --CLOSED--SDR GTIA020780Rheostat · failedDEN - FLT 980 - IN TURN YOKE VERY JERKY, AUTO PILOT DISENGAGES. OK IN LEVEL FLIGHT, NR 2 AUTO PILOT. TROUBLESHOT AUTOPILOT SYSTEM. FOUND AILERON SERVO RHEOSTAT BAD. CHECKED WITH METER LEFT SIDE GOOD RIGHT SIDE BAD. REMOVED AND REPLACED RHEOSTAT AND AILEROSDR ZW0A0206904CellTHE FIRST CLASS CABIN EGRESS LIGHTS WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY. CHECK-C 6-2-01 STL. --CLOSED--SDR GTIA020779Servo · noisyACY - RIGHT TURN WHEN AUTO PILOT ENGAGED AILERON SERVO MAKES GROUND NOISE FROM 0-25. REMOVED AND REPLACED AILERON SERVO DRIVE IAW MM 22-10-01. OPS CHECK NORMAL RTS CHECK PERFORMED IAW MM 22-01-05, OPS CHECK NORMAL. (M)SDR GTIA020771Indicator · malfunctionedDTW - DURING TAKEOFF, CAPTAINS AIRSPEED READ 75 KNOTS WHEN F/O'S READ 80 KTS WHEN F/O'S AIRSPEED READ 115KTS, CAPTAINS READ 100KTS, TAKEOFF ABORTED. MAX BRAKE TEMPS 20 DEGREES. REMOVED AND REPLACED F/O'S AIRSPEED INDICATOR, SYSTEM GROUND CHECKED GOOD. (M)SDR GTIA020777Drive Unit · chatteringFLT 594 - MCO - WITH AUTO PILOT ENGAGED, THE YOLK CHATTERS IN RIGHT TURNS. REMOVED AND REPLACED AILERON SERVO DRIVE. PERFORMED SYSTEM CHECK SYSTEM GROUND CHECKED GOOD. ALL IAW MD80 MM SECTIONS 22-11-01 AND 22-01-05. (M)SDR ZW0A0207605Support · damagedTHE FWD BULKHEAD SUPPORT ANGLE WAS DAMAGED AT STA 110, LBL 2. REPAIRED PER ARA 18260.SDR ZW0A0207604Support · damagedTHE FORWARD BULKHEAD SUPPORT ANGLE WAS DAMAGED AT STA 110, RBL 2. REPAIRED PER ARA 18260.SDR ZW0A0207603Structure · bentTHE Y-CHORD WAS BENT AT STA 110, LONGERON 28L TO 28R. INSTALLED NEW Y-CHORD PER ARA 18257, BETWEEN LONGERON 26L AND 26R.SDR ZW0A0207602Skin · damagedTHE FUSELAGE SKIN WAS DAMAGED UNDER THE FWD DRAIN MAST. REPAIRED DAMAGED SKIN UNDER THE FWD DRAIN MAST PER ARA 18254 AND SRM 53-04, FIG 12B.SDR ZW0A0207601Skin · damagedTHE FUSELAGE SKIN WAS DAMAGED AT 6 O'CLOCK, STATION 110 TO 113. TRIMMED OUT DAMAGED SKIN AND REPAIRED PER SRM 53-04, FIG 12B, SHEET 22.SDR ASAA0280217Module · inoperativeSEA - DURING LINE MAINTENANCE CHECK, FOUND EMERGENCY TRACK LIGHTING WAS FOUND INOPERATIVE AT ROW 30. REPLACED EMERGENCY TRACK LIGHT MODULE AT ROW 30. LIGHTS THEN OPERATED PROPERLY. (M)SDR GTIA020739Sensor · looseLGA - FLT 1865 - IMMEDIATELY INTO TAKEOFF ROLL, AFT CARGO DOOR LIGHT ILLUMINATED IT WENT OUT, THEN FLICKERED WHILE TAXIING. TRANSFERRED TO DIM, AFT CARGO DOOR INDICATION INOP. DOOR FOUND CLOSED AND LOCKED, CREW STATED AIRCRAFT WAS ROLLING AT 40 KNOTS NORMALSDR GTIA020729Computer · malfunctionedLGA - FLT 706 - WITH DFGC SELECTED TO POSITION 2 WHEN MACH VERTICAL SPEED SELECTED WILL NOT ENGAGE MACH BUT REMAINS IN IAS WHEN DFGC NR 1 SELECTED WORKS FINE. REMOVED AND REPLACED DFGC PER MD80 MM 22-01-01, SYSTEM OPS CHECK GOOD. (M)SDR ASAA0280216Wire · disconnectedSEA - DURING PREFLIGHT CHECK, EMERGENCY TRACK LIGHTING WAS FOUND DISCONNECTED AT ROW 28. RECONNECTED WIRING AT 28. LIGHTS THEN OPERATED PROPERLY. (M)SDR GTIA020728Control Panel · failedFLT 706 - LGA - IAS/MACH BUTTON WILL NOT SWITCH TO MACH ON DFGS NR 2, OK ON NR 1. REMOVED AND REPLACED FLIGHT GUIDANCE CONTROL PANEL. PERFORMED OPS HECK IAW MM 22-01-05. OPS CHECKS NORMAL. (M)SDR GTIA020726Computer · malfunctionedFLL - FLT 258 - AUTOPILOT DISCONNECTS IN RIGHT TURNS DFGS NR 2 POSITION. REMOVED AND REPLACED NR 2 DFGC IAW MD80 MM 22-01-01, OPS CHECK GOOD. (M)SDR P2EA2002M045Control Unit · malfunctionedDURING FLIGHT TO LGA SMOKE EMANATED FROM CENTER CONSOLE. AIRCRAFT DECLARED EMERGENCY, DESCENDED AND MADE UNSCHEDULED LANDING IN STL WITH NO INCIDENT. FOUND PMS MODULE OVERHEATED. DEFERRED PMS SYSTEM IAW MEL 34-37-01. PMS CIRCUIT BREAKER COLLARED. REMOVED SDR GTIA020719Inlet Screen · delaminatedFLL - NR 1 ENGINE INLET SCREEN DELAMINATING INSIDE NOSE COWL. AREA OF LINER DELAMINATED REMOVED. ENTERED ON C/O PER FAA BULLETIN FSAW 00-05 REPLACE IN 90 DAYS. REMOVED AND REPLACED LEFT ENGINE NOSE COWL PER MD80 MM 71-10-01. (M)SDR GTIA020725Slide · dislodgedFLL - FLT 258 - SLIDE PACK SEPARATED FROM HOUSING. INSTALLED SLIDE PACK IAW MD80 MM 25-62-00. NO DEFECTS NOTED AT THIS TIME. (M)SDR AALA20020906Sensor · defectiveLAS - FLT 1598 - EN ROUTE LAS-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF FROM LAS. RETURNED LAS AND LAND WITHOUT INCIDENT. REPLACED BOTH LEFT AND RIGHT TAIL COMPARTMENT TEMPERATURE SENSORS. SYSTEM GROUND CHECKED NORMAL OPSDR CA020702009Proximity Sensor · failed(CAN) NOSE LANDING GEAR UNSAFE (RED LIGHT) INDICATION IN FLIGHT WITH GEAR HANDLE UP. MECHANICAL INDICATOR SHOWED GEAR UP AND GEAR DOOR WAS CLOSED. ON EXTENSION, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON MECHANICAL INDICATOR SHOWED NOSE GEAR DOWN. UP/DOWN LOCKSDR GTIA020687Slide · out of positionDTW - FOUND L2 DOOR SLIDE PACK FELL OFF DOOR AND GOT DAMAGED. REMOVED AND REPLACED L2 DOOR SLIDE PACK IAW MD80 MM 25-62-00. (M)SDR GTIA020683Control Handle · lack of lubeDTW - FLT 249 - SLATS WOULD NOT RETRACT AFTER LANDING. LUBRICATED FLAP HANDLE SECTOR QUADRANT. OPS OK IAW MM 12-21-02. (M)SDR ASAA0280214Power Supply · dischargedSEA - DURING LINE CHECK, EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND TO REMAIN ON WITH SWITCH TURNED OFF. REPLACED POWER SUPPLY. EMERGENCY LIGHTS THEN OPERATED PROPERLY. (M)
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