Douglas DC-9-31

Service difficulty reports · 7,433

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 = 'DC931'
  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.

SDR 0500189947Line · leakingDURING FLIGHT, THE AIRCRAFT LOST PRESSURE AND A TOTAL LOSS OF FLUID FROM THE RIGHT HYDRAULIC SYSTEM. COMPLIED WITH COM PROCEDURES AND AIRCRAFT CONTINUED TO ORIGINAL DESTINATION. THE LANDING AT BTR WAS UNEVENTFUL. MAINTENANCE FOUND A LINE COMING FROM THE ELEFeb 11, 2005 · N8938E · Doug DC931 · Hydraulic System, MainSDR 0500169967Angle · corrodedDURING M-CHECK FOUND CORROSION ON LT CUSP TEE ANGLE. REPAIRED PER EA 99-200923.Feb 8, 2005 · N9331 · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA050022Warning Switch · defectiveNOSE GEAR UNSAFE RED WARNING LIGHT ILLUMINATED DURING UPLATCH CHECK (APPROX 10,000 FT MSL), COMPLIED WITH ABNORMAL. RECYCLED LANDING GEAR AND GOT GOOD DOWN AND LOCK (GREEN INDICATORS) WHEN THE LANDING GEAR WAS RETRACTED, THE NOSE GEAR UNSAFE LIGHT CAME ON AGAJan 22, 2005 · N929AX · Doug DC931 · Landing Gear Position and WarningSDR ABXA050003Pressure Switch · defectiveSHORTLY AFTER T/O, FLOW LIGHT ON AUTO PRESSURE CONTROLLER ILLUMINATED. TRANSFER LOCKOUT AND STANDBY LIGHT ALSO ON. RAN ABNORMAL PER MANUAL SECTION 21, CHAPTER 3. FLOW LIGHT, TRANSFER LOCKOUT AND STANDBY LIGHTS REMAINED ON. WENT TO MANUAL. STILL UNABLE TO CONTRJan 6, 2005 · N945AX · Doug DC931 · Cabin Pressure Control SystemSDR ABXA050012Skin · crackedRIGHT NOSE SKIN CRACKED AT 2 RIVETS AT FS 76.5 FORWARD OF FIRST OFFICER'S WINDSHIELD WIPER MOTOR. REPAIRED AREA IAW DC-9 JOB CARD EA 53100074-003-1.Jan 5, 2005 · N929AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA050014Fitting · crackedFLOORBEAM SUPPORT UPPER END FITTING CRACKED AT BOTH BOLT HOLES FS 965 AT LEFT BUTTLINE 32. REMOVED AND REPLACED FLOORBEAM SUPPORT UPPER END FITTING IAW DC-9 SRM 51-30-1 AND DC-9 SRM 51-30-5.Jan 5, 2005 · N929AX · Doug DC931 · Fuselage Main, Attach FittingsSDR ABXA050013Skin · crackedLEFT NOSE SKIN AT STA 69.5 FORWARD OF CAPTAIN'S WINDSHIELD WIPER MOTOR NEEDED STRIPPED AT AREA MARKED. REPAIRED AREA IAW DC-9 JOB CARD EA 53100075-003-2.Jan 5, 2005 · N929AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA050010Pan · crackedFORWARD LOWER CARGO DOOR PAN CRACKED BETWEEN LATCH AND STOP FROM GOUGE. REPAIRED FORWARD LOWER CARGO DOOR PAN IAW DC-9 SRM 52-05.Jan 4, 2005 · N929AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA050011Support Fitting · crackedFORWARD LOWER CARGO DOOR STOP SUPPORT FITTING CRACKED AFT OF FORWARD HINGE INSIDE LIGHTING HOLE. REMOVED AND REPLACED FITTING ON FORWARD LOWER CORNER DOOR AFT OF FORWARD HINGE IAW DC-9 SRM 51-30-5.Jan 4, 2005 · N929AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA050009Support Fitting · crackedFORWARD LOWER CARGO DOOR SUPPORT FITTING CRACKED AT STOP BOLT HOLE. REMOVED AND REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.Jan 4, 2005 · N929AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA050008Pan · crackedTWO CRACKS EMINATING FROM HILOC HOLE AT AFT LOWER DOOR STOP ON FORWARD LOWER CARGO DOOR. REPAIRED AREA AND REMOVED AND REPLACED BRACKET IAW DC-9 SRM 52-03, 51-30-2, 51-20-5, AND 51-30-1.Jan 4, 2005 · N929AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA050007Pan · crackedTWO CRACKS EMINATING FROM HILOC HOLE AT UPPER FORWARD DOOR STOP ON FORWARD LOWER CARGO DOOR. REPAIRED AREA IAW DC-9 SRM 52-03.Jan 4, 2005 · N929AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA050006Fitting · corrodedCORRODED BATHTUB FITTING LONGERON 29 LEFT STA 996. REMOVED AND REPLACED FITTING AT LONGERON 29 LEFT IAW DC-9 SRM 51-30-5.Jan 4, 2005 · N929AX · Doug DC931 · Fuselage Main, Attach FittingsSDR ABXA050001Connector · looseEMERGENCY DECLARED, HAD GEAR DOOR OPEN LIGHT IN CRUISE FLIGHT. PERFORMED ABNORMALS, NO HELP. ON APPROACH, AFTER GEAR EXT, STILL HAD DOOR OPEN LIGHT. PERFORMED ABNORMALS. PULLED EMERGENCY GEAR RELEASE. MECHANICS MET THE AIRCRAFT. TIED DOORS UP AND PINNED Jan 2, 2005 · N924AX · Doug DC931 · Landing Gear Position and WarningSDR 0402159943Frame · crackedDURING "M" CHECK, FOUND CRACK IN FUSELAGE FRAME AT FS 408 L16R TO L18R. REPAIRED PER EA 99-201809.Dec 13, 2004 · N1308T · Doug DC931 · Fuselage Main, FrameSDR 0402149989Shutoff Valve · leakingTHE RIGHT HYDRAULIC SYSTEM FAILED IN FLIGHT AND EXPERIENCED A COMPLETE LOSS OF FLUID. COMPLIED WITH COM PROCEDURES AND AIRCRAFT CONTINUED TO SCHEDULED DESTINATION. LANDING AT CMH WAS UNEVENTFUL AND MAINTENANCE REPLACED A LEAKING RUDDER HYDRAULIC POWER SHUTOFDec 7, 2004 · N8945E · Doug DC931 · Hydraulic System, MainSDR A4JA12100403Smoke Detector · contaminatedAFTER LANDING IN SWF, BOTH LAV SMOKE DETECTORS SOUNDED. NO INDICATION OF SMOKE. CLEANED DEBRIS FROM LAV SMOKE DETECTOR. GROUND OPS CHECK NORMAL IAW DC9 MM 26-10-0.Nov 27, 2004 · N935DS · Doug DC931 · Smoke DetectionSDR ABXA040380Switch · arcedCREW REPORTED ELECTRICAL ODOR COMING FROM OVERHEAD PANEL. FOUND WINDSHIELD HEAT SWITCH IN OVERHEAD PANEL ARCING AND WIRE H578B16 INSULATION MELTED. REPAIRED WIRE IAW WDM 30-41-00 AND REMOVED AND REPLACED WINDSHIELD HEAT SWITCH. WINDSHIELD HEAT OPS CHECKED GNov 16, 2004 · N946AX · Doug DC931 · Windshield/Door Rain/Ice RemovalSDR 0401989911Fuel Filter · leakingPILOT REPORTED A STRONG OIL/FUEL ODOR IN THE AIRCRAFT FOR ENTIRE LENGTH OF THE FLIGHT. MAINTENANCE FOUND THE APU LOW PRESSURE FUEL FILTER LEAKING 72 DROPS PER MINUTE. MAINTENANCE REPLACED THE FUEL FILTER AND PACKING. ALSO REPLACED COALESCER BAGS. COMPLIED Nov 10, 2004 · N961N · Doug DC931 · APU Engine Fuel and ControlSDR ABXA040373Computer · defectiveAUTOPILOT DID AN UNCOMMANDED 3000 FT MIN DESCENT WITH PITCH WHEEL IN ALTITUDE DETENT. FLIGHT 158, STA ALB. COULD NOT DUPLICATE. SUSPECT PITCH COMPUTER INSTALLED FOR TRIM PROBLEM CAUSING DIFFICULTIES WITH ALT HOLD. REMOVED AND REPLACED PITCH AXIS COMPUTER. Nov 10, 2004 · N943AX · Doug DC931 · Autopilot SystemSDR ABXA040372Charger · defectiveDIVERSION FOR A BATTERY CHARGER PROBLEM WHICH OCCURRED OUT OF ICT EN ROUTE TO ILN. AIRCRAFT DIVERTED TO MCI. BATTERY CHARGER INDICATED CONSTANT CHARGE IN CLIMB GREATER THAN 40 AMPS FOR MORE THAN 2 MINUTES. REMOVED AND REPLACED BATTERY CHARGER AND BOTH BATTENov 8, 2004 · N948AX · Doug DC931 · Battery/Charger SystemSDR ABXA040368Pump · defectiveRIGHT ENGINE FLAMED OUT ON SHORT FINAL TO ILN, SPEED 135 KT, ALT 2100. REMOVED AND REPLACED NR 2 ENGINE FUEL PUMP IAW DC-9 MM 73-10-01-2. REMOVED AND REPLACED NR 2 ENGINE FCU IAW DC-9 MM 73-20-01-2.Nov 2, 2004 · N923AX · Doug DC931 · Engine Fuel PumpSDR ABXA040369Frame · crackedFORWARD LEFT MAIN FRAME, STA 699 WAS CRACKED WITHIN REPAIRABLE LIMITS. REPAIRED MAIN FRAME, STA 699 LT IAW DC-9 SERVICE REWORK DRAWING 5933650 AND JOB CARD EA 63400110-001-1.Oct 27, 2004 · N942AX · Doug DC931 · Fuselage Main, FrameSDR ABXA040371Frame · crackedAFT LEFT MAIN FRAME, STA 737, REQUIRED REPLACEMENT DUE TO CRACKS. REMOVED AND REPLACED AFT LEFT MAIN FRAME STA 737 IAW JOB CARD EA 53400325-001-4.Oct 27, 2004 · N942AX · Doug DC931 · Fuselage Main, FrameSDR ABXA040370Frame · crackedFORWARD RIGHT MAIN FRAME, STA 699, REQUIRED REPLACEMENT. CRACKED BEYOND LIMITS OF REPAIR. REMOVED AND REPLACED RIGHT MAIN FRAME, STA 699 IAW JOB CARD EA 53400322-001-4.Oct 27, 2004 · N942AX · Doug DC931 · Fuselage Main, FrameSDR SE28102004Charger · failedDURING B-CHECK MAINTENANCE FOUND THE AFT HALF OF THE EMERGENCY PATH TRACK WOULD NOT COME ON. REMOVED AND REPLACED EMERGENCY PATH LIGHTING BATTERY AND BATTERY CHARGER IAW MM 33-53-1. OPS CHECKS GOOD.Oct 20, 2004 · N933JK · Doug DC931 · Emergency LightingSDR ABXA040361Frame · crackedLEFT FORWARD MAIN FRAME STA 699 CRACKED AT FORWARD AND AFT FLANGE. REQUIRED REPLACEMENT PER NEA 53400100-002-30. REMOVED AND REPLACED LEFT MAIN FRAME IAW EA 53400321-001-2 AND DC-9 SRM.Oct 19, 2004 · N944AX · Doug DC931 · Fuselage Main, FrameSDR ABXA040360Fitting · crackedUPPER AFT STOP PAD SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC-9 SRM.Oct 19, 2004 · N944AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA040358Bracket · crackedRUDDER UPPER HINGE BRACKET CRACKED AT RIGHT MOUNT HOLE. REMOVED AND REPLACED UPPER HINGE BRACKET IAW DC-9 SRM 51-30-1.Oct 18, 2004 · N944AX · Doug DC931 · Vertical StabilizerSDR 0401789956Drain · cloggedAT CRUISE SPEED AND ALTITUDE, THE AIRCRAFT WOULD NOT TURN WITH AUTOPILOT. CREW CANCELLED AUTOPILOT AND WAS STILL UNABLE TO TURN THE CONTROL WHEEL BY HAND. COMPLIED WITH COM PROCEDURES AND AIRCRAFT DESCENDED TO A LOWER WARMER ALTITUDE. CREW FELT A SNAP AND TSep 28, 2004 · N923RW · Doug DC931 · Aileron Control SystemSDR 0401909953Stiffener · crackedDURING H-CHECK, FOUND CRACKS IN VERTICAL STIFFENERS AT BS 756 L28R, L28L AND ABOVE L26L. REPAIRED PER EA 99-200337.Sep 22, 2004 · N918RW · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA040319Pan · corrodedFORWARD LOWER CARGO DOOR PAN WAS CORRODED OUT OF LIMITS. REPLACED FORWARD LOWER CARGO DOOR PAN IAW DC-9 MM.Sep 7, 2004 · N944AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA040325Spar Cap · crackedLEFT HORIZONTAL STABILIZER LOWER AFT SPAR CAP CRACKED OUTBOARD TIP. REPAIRED AREA IAW REA D955-50434MR.Sep 3, 2004 · N923AX · Doug DC931 · Horizontal Stabilizer, Spar/RibSDR ABXA040324Spar Cap · crackedRIGHT HORIZONTAL STABILIZER FORWARD LOWER OUTBOARD SPAR CAP CRACKED APPROXIMATELY 3.25 INCHES. REPAIRED LOWER OUTBOARD SPAR CAP IAW REA D955-50424MR.Sep 3, 2004 · N923AX · Doug DC931 · Horizontal Stabilizer, Spar/RibSDR ABXA040323Cusp Web · crackedRIGHT CUSP WEB CRACKED SEVERAL PLACES FORWARD OF FS 965. REPAIRED RIGHT CUSP WEB FORWARD OF STA 965 IAW DC-9 SRM 53-01.Sep 2, 2004 · N923AX · Doug DC931 · Fuselage Miscellaneous StructureSDR 0401829911Skin · crackedDURING L-CHECK FOUND CRACK IN SKIN IN UPPER FORWARD CORNER OF FORWARD SERVICE DOOR JAMB. REPAIRED PER EA 99-199627.Sep 1, 2004 · N961N · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA040321Skin · crackedAPPROXIMATELY 1 INCH CRACK IN EXTERNAL SKIN JUST FORWARD OF RIGHT WIPER ACCESS PANEL. REPAIRED CRACK IN EXTERNAL SKIN IAW REA D953-50452MR.Sep 1, 2004 · N923AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA040322Angle · crackedMAIN ENTRY DOOR BOTTOM ANGLE OF DOOR CRACKED AT BOTH FORWARD AND AFT SIDES. REMOVED AND REPLACED LOWER ANGLES OF MAIN ENTRY DOOR IAW DC-9 SRM 51-30-1 AND 51-30-2.Sep 1, 2004 · N923AX · Doug DC931 · Passenger/Crew DoorsSDR 0401479907Control Cable · out of rigAT ROTATION SPEED DURING TAKEOFF ROLL, THE AIRCRAFT PICKED UP AND TOOK OFF WITHOUT ANY PILOT INPUT ON THE CONTROLS. CREW ALSO MENTIONED FEELING A VIBRATION THROUGH THE YOKES DURING FLIGHT. AIRCRAFT WOULD PITCH UP NOTICEABLY DURING CLIMBOUT WITH AUTOPILOT DISAug 31, 2004 · N957N · Doug DC931 · Elevator Tab Control SystemSDR 0401819911Skin · crackedDURING L-CHECK, FOUND CRACK IN FUSELAGE NOSE SKIN AROUND FASTENERS AT BS 76.5 LBL 15 TO LBL 21. REPAIRED IAW EA 99-200584.Aug 24, 2004 · N961N · Doug DC931 · Fuselage Main, Plate/SkinSDR 01082304Fire Loop · malfunctionedLT ENGINE FIRE LOOP IAI LIGHT ILLUMINATED. DEFERRED IAW MEL 26-1-1, CONTROL NR M-934-155. CAT C, DUE 09/02/04. PLACARDS INSTALLED M PROCEDURES C/W.Aug 23, 2004 · N934LK · Doug DC931 · Fire DetectionSDR 0401379961Cooling Turbine · odorDURING CLIMBOUT FROM MSP, THE FLIGHT CREW NOTICED THAT THE RIGHT AIR CONDITIONER SYSTEM IN OVERHEAT CONDITION. CABIN CREW REPORTED A HAZE OF SMOKE AND BURNING ODOR IN THE CABIN. WHEN THE RIGHT PACK WAS SHUT DOWN THE SMOKE AND SMELL DISSIPATED. FLIGHT CONTINAug 21, 2004 · N924RW · Doug DC931 · Cabin Cooling SystemSDR ABXA040311Intercostal · crackedFORWARD LOWER CARGO DOOR INTERCOSTAL ANGLE WAS CRACKED AT THE FORWARD LOWER STOP AREA. REPLACED ANGLE FORWARD LOWER STOP DOOR IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.Aug 19, 2004 · N924AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA040310Intercostal · crackedCENTER INTERCOSTAL AT LOWER EDGE OF AFT LOWER CARGO DOOR HAD CRACKED ATTACH ANGLE. REPLACED ANGLE IAW DC-9 SRM 51-30-5.Aug 19, 2004 · N924AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA040307Seat Track · crackedCENTER SEAT TRACK CRACKED AND CORRODED AT FS 996. SPLICED IN NEW SECTION OF TRACK STA 926 - 1019 IAW DC-9 SRM K05406 AND SRM 51-30-1.Aug 19, 2004 · N924AX · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA040308Seat Track · corrodedDOUBLE SEAT TRACK CORRODED AT FS 996, RIGHT BUTT LINE 6. REPLACED TRACK AT RIGHT BUTT LINE 6 AT STA 965 - 1019 IAW DC-9 SRM 51-30-1.Aug 19, 2004 · N924AX · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA040309Floor Support · crackedLEFT INBOARD FLOOR SUPPORT FITTING CRACKED AT STA 945. REPLACED FITTING AT LEFT FLOOR TRACK, AFT LOWER CARGO, STA 945 IAW DC-9 SRM 51-30-5.Aug 19, 2004 · N924AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA040305Frame · crackedCRACK IN THE MAIN FRAME AFT POCKET, EXTENDED TO THE MAIN ATTACH BOLT. CRACK LENGTH 1.625 AND 2.170. REPAIRED IAW SERVICE REWORK DRAWING 5934375-505 IAW ABX REA D953-50391. INITIATED WATCH ITEM 924-035 FOR REPETITIVE INSPECTION INTERVALS OF 1600 FLIGHT HOURSAug 18, 2004 · N924AX · Doug DC931 · Fuselage Main, FrameSDR ABXA040306Frame · crackedCRACK IN THE FORWARD POCKET EXTENDED FROM THE MAIN ATTACH HOLE TO THE FIRST REPAIR ATTACH HOLE. RIGHT MAIN FRAME REPLACED IAW EA 53400324-001-2 AND WORK ACCOMPLISHED ON NR 0271.Aug 16, 2004 · N924AX · Doug DC931 · Fuselage Main, FrameSDR 0401279997Angle · crackedDURING M-CHECK FOUND CRACK IN VERTICAL STABILIZER ATTACH ANGLE AT BS 1095. REPAIRED PER EA 99-195833.Aug 5, 2004 · N8933E · Doug DC931 · Fuselage, Stabilizer Attach Fittings
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