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 ABXA020114Switch · defectiveWITH ANTI-FOG CIRCUIT BREAKERS PULLED, NO BURNING SMELL NOTED. WITH ANTI-FOG CIRCUIT BREAKERS IN, A BURNING SMELL WAS NOTED. REPLACED THE WINDSHIELD HEAT SWITCH. OPS CHECKED GOOD IAW DC-9 MM.SDR ABXA020113Switch · defectiveAFTER TURNING ON WINDSHIELD HEAT, A BURNING SMELL WAS NOTED IN THE COCKPIT. THE SMELL WENT AWAY AFTER TURNING OFF WINDSHIELD HEAT. REPLACED THE WINDSHIELD HEAT SWITCH. OPS CHECKED GOOD IAW DC-9 MM.SDR ABXA020080Odor · detectedSTRONG ELECTRICAL BURNING SMELL IN COCKPIT. VERIFIED SMELL. INSPECTED EPC, RELAY PANEL, E&E COMPARTMENT AND THE GYRO COMPARTMENT. OPERATED PACK ONE AT A TIME. NO SMELL NOTED.SDR MWEA020514Bellows · lowCREW REPORTED LEFT ENGINE EPR, N1, N2, AND FUEL FLOW ALL FLUCTUATING. PERFORMED VISUAL INSPECTION OF ENGINE. NO DEFECTS NOTED. DRAINED EXCESS MOISTURE FROM MOISTURE TRAP AND SERVICED FCU BELLOWS. RAN ENGINE TO TAKEOFF POWER. ALL ENGINE PARAMETERS STABLE MSDR MEX2002270Proximity Switch · failedAIRCRAFT RETURNED, DUE TO NOSE LANDING GEAR RED LIGHT AND LANDING GEAR DOORS WERE OPEN. O-RINGS FOR THE NOSE LANDING GEAR WERE REPLACED. IAW MM SENSOR T2-61 WAS REPLACED IAW WD AND THE PROXIMITY SWITCH WAS REPLACED IAW MM. AFTER THAT, DURING THE TOWING TURNSDR AT0200074Web · corrodedHEAVY CORRODED SUBFLOOR PANEL AND INCLUDING AREA BELOW SEAT TRACK AT STA 230 TO 305 RBL 44. CUT OUT CORROSION ON SUBFLOOR, AND INSTALLED REPAIR IAW DC-9 SRM 53-01.SDR AT0200073Floor Panel · corrodedHEAVY CORRODED FLOOR PANEL STA 230 TO 305, RBL 44 TO RBL 56. REMOVED AND REPLACED SKIN ON FLOOR PANEL IAW DC-9 SRM 51-30-2.SDR 0202669942Door · out of rigRIGHT FORWARD OVERWING EXIT DOOR FELL OPEN DURING LANDING. NO PASSENGERS WERE ON THE AIRCRAFT. THE PLASTIC TRIM PANEL ON THE DOOR CRACKED WHEN THE DOOR FELL OUT. MAINTENANCE FOUND THE DOOR DAMAGED AND OUT OF RIG. REPLACED THE DOOR AND PLASTIC INNER LINER. SDR MWEA020475Spoiler · chafedINBOARD FLIGHT SPOILER OUTBOARD HINGE SUPPORT IS CHAFED. TAG #1 RIGHT WING. -- SUPPORT IS CHAFED TO LIMITS. LOCATED AND DRILLED NEW FITTINGS.SDR MWEA020474Wing · delaminatedLEFT WING AFT SIDE OF WING FLAP TRAILING EDGE PANEL IS DELAMINATED AT FORWARD OUTBOARD CORNER DOT.18. -- FABRICATED AND INSTALLED SKIN.SDR 0203069951Door · crackedDuring HCK in DHN, crack damage was found on the lower forward cargo door inner and outer flange. Repaired per EA 99-191322.SDR ABXA020076Duct · disconnectedAT FL 350, CABIN ALTITUDE INCREASED TO 9,500 ALONG WITH THE RIGHT GENERATOR TRIPPING OFF LINE. RESET GENERATOR. PERFORMED DESCENT TO 14,000 CABIN ALTITUDE WAS REGAINED AT APPROXIMATELY 17,000 TO 18,000. PACK PRESSURE NORMAL AS WELL AS ELECTRICAL PARAMETERS SDR 0203059951Bulkhead · crackedDuring HCK in DHN, the aft pressure bulkhead web was found cracked under Z=63.5 stiffener approx. 10" outboard of the ventral door jamb. Repaired per EA 99-191325.SDR AT0200072Battery · not seatedEMERGENCY LIGHTING OVERWING EXIT MARKERS INOPERATIVE (LEFT FORWARD AND AFT AND RIGHT FORWARD). SEATED EMERGENCY LIGHTING BATTERIES IN PACK B5-33, AND RESERVICED GROUND AT AFT RIGHT HAND OVERWING EXIT MARKER ASSY. OPS CHECK GOOD PER DC9 MM 33-50.SDR 0202469609Pump · malfunctionedDURING DESCENT FOR LANDING INTO MSP, THE RIGHT HYDRAULIC SYSTEM PRESSURE WENT TO ZERO PSI AND THE QUANTITY WENT TO MAX HIGH SCALE. THE RUDDER CONTROL MANUAL ANNUNCIATOR LIGHT ILLUMINATED. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT SDR GTIA020843Light · inoperativeFLT 276 - TPA - FOUND RIGHT LANDING GEAR BUTTON INDICATOR LIGHT INOPERATIVE, GREEN LENS. REMOVED AND REPLACED GEAR DOWNLOCK SWITCH ON RIGHT MAIN GEAR AND OPS CHECKED IAW MM 32-60-01. OPS CHECK NORMAL. CLOSED AS OF 8/28/02. (M)SDR MEX2002241Wheel · damagedDURING TOWING PROCEDURE IT WAS OBSERVED THE MISSING OF ONE NUT IN A WHEEL OF THE NLG. AIRCRAFT RETURNED TO PLATFORM TO REPLACE THE WHEEL 1 OF THE NLG IAW MM 32-21.SDR MWEA020459Bracket · crackedCRACKED ANGLE BRACKET FORWARD END UNDER #1 BEAM OF GALLEY DOOR (DOT JH 36). -- FABRICATED AND INSTALLED BRACKET.SDR ABXA020068Odor · detectedDURING FLIGHT, SMELLED A SULFUR ODOR TWICE. EACH LASTED FOR ABOUT 30 SECONDS, THEN WENT AWAY. VERY MUCH LIKE A MATCH BEING LIT AND THEN SNUFFED OUT. CHECKED ALL CIRCUIT BREAKERS, NONE TRIPPED. CHECKED ELECTRICAL COMPONENTS. OPS CHECKED NORMAL. RAN BOTH A/C PACSDR 0202369982Tire · separatedLEFT MAIN INBOARD TIRE FAILED DURING ROTATION ROLL ON TAKEOFF. OBJECTS DEPARTING THE FAILED TIRE DAMAGED THE LEFT FLAP TRAILING EDGE, THE LEFT ENGINE COWL, AND A PORTION OF THE SEPARATED TIRE TREAD WAS INGESTED INTO THE LEFT ENGINE. FLIGHT RETURNED TO A SAFESDR MWEA020452Switch · faultyCABIN EMERGENCY LIGHTS, NO SMOKING LIGHTS AND FASTEN SEATBELT LIGHTS FLASHING ON AND OFF RAPIDLY. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT SWITCH AND B5-23 BATTERY PACK FOR PRECAUTION.SDR GTIA020831Structure · damagedDTW - FOUND RIGHT FLAP TRAILING EDGE SPLICE APPROX 1.5 INCHES INBOARD END OF FLAP AT FIRST EXPANSION JOINT. SANDED AND INSTALLED FIBERGLASS LAYUP REPAIR ON RIGHT FLAP TRAILING EDGE. (M)SDR MWEA020463Skin · dentedFUSELAGE SKIN DENTED AT STATION 999 AFT OF LONGERON 27 RIGHT. -- CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER.SDR MWEA020462Frame · crackedLOWER FRAME ASSY STATION 1000 IS CRACKED, INLINE WITH LONGERON 28 RIGHT. -- INSTALLED REPAIR ANGLE.SDR 0202319919AcmFLIGHT ATTENDANT REPORTED SLIGHT HAZE, FUMES, AND THE AFT LAV SMOKE DETECTOR SOUNDED DURING TAKEOFF. SYMPTOMS LASTED A COUPLE OF MINUTES THEN CLEARED AND THE ALARM STOPPED. FLIGHT RETURNED TO AN UNEVENTFUL LANDING AT MSP. MAINTENANCE REPLACED THE RIGHT ACM ANDSDR MWEA020449Stringer · corrodedRIGHT WING STRINGER 21 HAS LIGHT CORROSION ON UPPER AND LOWER AFT LEG BETWEEN XRS 91&111. BLENDED CORROSION OUT OF STRINGER.SDR MWEA020458Tee Fitting · dentedAFT PRESSURE BULKHEAD TEE WAS DENTED BETWEEN LONGERONS 29 RIGHT AND 28 RIGHT. REMOVED TEE SECTION FROM LONGERON AND INSTALLED NEW TEE SECTION AND REPAIR SPLICES.SDR 0202379921Duct · damagedAT FL280 WITH ENGINE AND WING ANTI-ICE ON, THE CABIN ALTITUDE STARTED TO CLIMB AT ABOUT 700 FPM. ACCOMPLISHED COM PER RED BORDER CHECKLIST AND WENT TO FULL CLOSED MANUALLY. AIRCRAFT PERFORMED AN EMERGENCY DESCENT AND CABIN PRESSURE CONTROL WAS REGAINED AT 13SDR MWEA020448Gyro · failedCAPTAIN'S ATTITUDE INDICATOR FAILED. REMOVED AND REPLACED NR 1 VERTICAL GYRO. OPS CHECK OK REF MM 34-27-0.SDR MWEA020445Stiffener · corrodedRIGHT WING LIGHT CORROSION ON UPPER SURFACE OF HORIZONTAL STIFFENER ON INBOARD SIDE OF XRS 91 RIB ABOVE STRINGERS 17 TO 19. REMOVED AND INSTALLED STIFFENER AND FLAPPER VALVE.SDR ABXA020034Cushion · defectiveFIRST OFFICER'S SEAT CUSHION DID NOT FIT OR ATTACH TO SEAT FRAME PROPERLY. SOMETIMES RESTRICTED AFT MOVEMENT OF CONTROL COLUMN. REPLACED FIRST OFFICER'S SEAT CUSHION AS REQUIRED IAW DC-9 MM.SDR AT0200069Wire · brokenNR 1 LEFT HAND AFT ACCESSORY EMERGENCY LIGHT WILL NOT ILLUMINATE. REPAIRED BROKEN WIRE L795W18 AT VENTRAL STAIR EMERGENCY LIGHTS PER WDM-31-51, OPS CHECK NORMAL.SDR MWEA020443Controller · out of adjustAT 31,000 FEET THE AIRCRAFT LOST PRESSURE AND COULD NOT CONTROL IN AUTO OR MANUAL. MASKS AUTOMATICALLY DEPLOYED. PERFORMED ADJUSTMENT / TEST CABIN PRESSURE CONTROL REFERENCE 21-32-0-201. NO DISCREPANCY NOTED.SDR 0202059919Smoke · detectedTHE FORWARD LAV SMOKE DETECTOR ACTIVATED IMMEDIATELY AFTER TAKEOFF AND THE LEAD FLIGHT ATTENDANT OBSERVED SMOKE IN THE CABIN. FLIGHT RETURNED TO MSP AND LANDED SAFELY. MAINTENANCE REMOVED, INSPECTED AND REINSTALLED THE LAV SMOKE DETECTOR. THERE WAS NO EVIDESDR MWEA020433Skin · dentedFUSELAGE DENT AT STATION 353 1.5 INCH BELOW LONGERON 29 LEFT. FABRICATED AND INSTALLED DOUBLER.SDR MWEA020432Gusset · corrodedAFT PIT STRAP ON DOOR THRESHOLD CORRODED BETWEEN STATION 904 AND STATION 885 LONGERON 29 LEFT. REMOVED AND INSTALLED GUSSET.SDR MWEA020431Splice · crackedLONGERON SPLICE CRACKED AT FS415 AND 29 LEFT. FABRICATED AND INSTALLED SPLICE AND SHIMS.SDR MWEA020430Fitting · crackedFORWARD CARGO BAY HAS A CRACKED FITTING ON FRAME 503 AT LONGERON 28 RIGHT. REMOVED AND INSTALLED FITTING.SDR MWEA020429Stop Fitting · strippedPAX JAMB DOOR STOP FITTING (THIRD FROM BOTTOM AFT JAMB) HAS STRIPPED OUT THREADS. REMOVED AND INSTALLED FITTING.SDR AT0200066Slide · out of positionSLIDE PACK FELL OFF DOOR L1. REINSTALLED SLIDE PACK IAW MM 25-62.SDR MWEA020427Circuit Breaker · failedCREW NOTED PRIMARY TRIM WAS INOP. ALTERNATE TRIM WORKED NORMALLY. ALL SWITCHES AND CIRCUIT BREAKERS WERE IN NORMAL POSITIONS. PERFORMED TROUBLESHOOTING PROCEDURES IAW MM 27-40-0. VERIFIED BAD PRIMARY LONGITUDINAL TRIM CONTROL CIRCUIT BREAKER. REMOVED AND SDR MWEA020444Frame · corrodedFORWARD CARGO BAY FRAME AT STATION 446 LONGERON 30 IS EXFOLIATED. INSTALLED FRAME SECTION AND SPLICE.SDR AT0200067Slide · out of positionR1 DOOR SLIDE PACK FELL OUT OF POSITION. REINSTALLED R1 SLIDE.SDR MWEA020425Circuit Breaker · trippedON CLIMBOUT ALL LEFT MAIN FUEL TANK PUMP CIRCUIT BREAKERS POPPED. VISUALLY INSPECTED THE EXTERNAL POWER, GENERATOR AND CROSS TIE RELAYS. CHECKED CIRCUIT BREAKERS INSIDE EPC AND FOUND THE AIRPHONE CIRCUIT BREAKER HAD SIGNS OF ARCHING. AIRPHONES DEFERRED, PLASDR MWEA020411Longeron · crackedAFT ACCESSORY COMPARTMENT LONGERON 2 RIGHT HAS A CRACK AT STATION 1076. FABRICATED AND INSTALLED LONGERON SPLICE REPAIR.SDR MWEA020410Attach Angle · crackedA .5 INCH CRACK IN RIGHT SIDE VERTICAL TO FUSELAGE ATTACH ANGLE AT STATION 1130, APPROXIMATELY 1 FOOT FORWARD OF RUDDER TORQUE TUBE. FABRICATED AND INSTALLED SPLICE, STRAP AND FILTER.SDR MWEA020409Frame · corrodedFORWARD PIT MODERATE CORROSION AT LONGERON 30 ON LOWER FLANGE OF FRAME 446. FABRICATED, INSTALLED NEW FRAME SECTION AND SPLICES.SDR MWEA020406Shear Tie · crackedAFT ACCESSORY COMPARTMENT BULKHEAD FRAME STATION 1038 SHEAR TIE IS CRACKED JUST ABOVE LONGERON 18 LEFT. -- REMOVED SHEAR TIE SEGMENT. FABRICATED AND INSTALLED SHEAR TIE SEGMENT AND CLIPS.SDR MWEA020405FrameCANTED FRAME STATION 1132 FRAME IS CRACKED AND CORRODED APPROXAMITLY 8 INCHES RIGHT OF UPPER FUSELAGE CENTERLINE. -- REMOVED DAMAGE FRAME SECTION. FABRICATED FILLERS AND STACKED ANGLES.SDR MWEA020413Shear Tie · damagedFORWARD CARGO COMPARTMENT FRAME STATION 446 SHEAR TIE HAS NUMEROUS ELONGATED FASTENER HOLES LOCATED BETWEEN LONGERON 28 LEFT AND 26 RIGHT. FABRICATED AND INSTALLED FORMERS.
Back to Douglas DC-9-32