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.
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
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 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.SDR 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.SDR 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.SDR 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)SDR 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 ANDSDR MWEA030133Windshield · failedFIRST OFFICER'S WINDSHIELD SHATTERED AT ALTITUDE (OUTER PANE). REMOVED AND REPLACED FIRST OFFICER'S WINDSHIELD.SDR 0300799615Bracket · crackedDURING H-CHECK, FOUND CRACK IN FUSELAGE HORIZONTAL LEG BRACKET AT BS 69 RT SIDE. REPAIRED PER EA 96-190942.SDR 0300809612Skin · crackedDURING L-CHECK, FOUND CRACKS ON FUSELAGE NOSE SKIN AT BS 69.5 AND BS 76.5. REPAIRED PER EA 96-190940.SDR MWEA030132Control Box · inoperativeWHILE ARMING ANTI-SKID RIGHT OUTBOARD AND INBOARD LIGHTS REMAINED ON. REMOVED AND REPLACED ANTI-SKID CONTROL BOX.SDR MWEA030402Skin · canningEVIDENCE OF OIL CANNING ON LEFT SIDE OF FUSELAGE STATION 1025. INSTALLED DOUBLER.SDR 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)SDR 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 TSDR 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.SDR GTIA030114Fitting · leakingRIGHT WHEEL WELL AFT FUEL MANIFOLD INBOARD SIDE DRIPPING FUEL. RESECURED LOOSE FITTING AT APU FUEL LINE SHROUD CONNECTION. LEAK CHECK GOOD.SDR MWEA030120Warning Light · illuminatedRT START ENGINE VALVE ANNUNCIATOR STAYED ON. VERIFIED VALVE CLOSED, LIGHT IN COCKPIT OUT, COULD NOT DULPICATE AT THIS TIME.SDR 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.SDR 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 DISCONNSDR MWEA030112Throttle Switch · defectiveGEAR WARNING HORN SOUNDED. -- REMOVED AND REPLACED ON SWITCH UNIT AND INSTALLED LEFT THROTTLE SWITCH.SDR 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. (MSDR 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 SDR MWEA030111Flange · elongatedFIRST OFFICER AFT INBOARD SEAT TRACK FOUND ENLONGATED HOLES. -- REMOVED AND REPLACED UPPER FLANGE OF FIRST OFFICER'S INBOARD SEAT TRACK.SDR 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.SDR MWEA030105Receiver · inoperativeFIRST OFFICER NR 2 NAV FAILED, VOR, GS, AND LOC FLAGS SHOWING. REMOVED AND REPLACED VOR/ILS RECEIVER.SDR 0300329614Skin · corrodedDuring "H" check found corrosion on fuselage skin between BS 160-180 L28L-L28R. Repaired per EA 96-194258.SDR 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 REVESDR MWEA030072Drive Shaft · shearedWHEN ATTEMPTING TO START #2 ENGINE THE N2 WENT TO 10% THEN DROPPED OFF TO ZERO. -- REMOVED AND REPLACED STARTER DRIVE SHAFT.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR MWEA030053Bulkhead · crackedSTATION 965 RIGHT FORWARD PYLON BULKHEAD HAS A CRACK GOING INBOARD OF LIGHTENING HOLE AT Z = 50.0. FABRICATED AND INSTALLED DOUBLER.SDR MWEA030051Rib · crackedLEFT NR 5 SLAT OUTBOARD RIB IS CRACKED AT LOWER AFT CORNER. REMOVED CRACKED RIB AND INSTALLED NEW RIB.SDR MWEA030050Skin · crackedFUSELAGE SKIN CRACKED AT FRAME STATION 180 SHEAR TIE BETWEEN LONGERON 1&2 RIGHT. FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED DOUBLER.SDR MWEA030043Transmitter · defectiveRIGHT OIL PRESSURE WAS AT ZERO. -- REMOVED AND REPLACED TRANSMITTER AND BUTT SPLICE.SDR MWEA030039Seal · corrodedLOWER SEAL ON LEFT FORWARD OVERWING EMERGENCY EXIT DOOR IS CORRODED. -- LOCATED AND INSTALLED NEW SEAL RETAINER.SDR MWEA030038Spar · damagedLEFT WING STATION XRS 157 AFT SPAR REPAIR. -- FABRICATED AND INSTALLED REPAIR PARTS, FABRICATED AND INSTALLED NEW TEE.SDR MWEA030037Frame · crackedCANTED FRAME AT STATION 1168 AT THE 2 O'CLOCK POSITION IS CRACKED. -- LOCATED,DRILLED AND INSTALLED NEW FRAME.SDR 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.SDR MWEA030033Doubler · dentedFUSELAGE DENT AFT OF CARGO DOOR STATION 965 BETWEEN LONGERON 25-26 RIGHT. -- FABRICATED AND INSTALLED DOUBLER.SDR 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 SSDR 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. REPLACEDSDR MWEA030009Filter · defectiveRIGHT HYDRAULIC SYSTEM FLUID QUANTITY DEPLETED AND LOST PRESSURE. REMOVED AND REPLACED AUXILIARY LINE FILTER HOUSING AND FILTERS.SDR 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.SDR 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 GSDR 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.SDR MWEA020769Web · crackedFOUND TWO CRACKS IN WEB AT FUSELAGE STATION 1038 LEFT SIDE AT APPROXIMATELY LONGERON 12. -- REMOVED AND REPLACED NEW SECTION.SDR 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 DISPSDR AT0300001Battery · dischargedOVERWING EMERGENCY EXIT DOOR LIGHTS WILL NOT ILLUMINATE (SEAT ROW 18A & F). REMOVED AND REPLACED BATTERY AND POWER SUPPLY.SDR 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 FOLLOW
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