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.

SDR ABXA040336Fitting · crackedEND FITTING AT LONGERON 29 RT ON AFT SIDE OF STA. 604 WAS CRACKED. REMOVED AND REPLACED END FITTING AT LONGERON 29 RT, STA. 604 IAW SRM 51-30-5.Sep 21, 2004 · N902AX · Doug DC932 · Fuselage Main, Attach FittingsSDR ABXA040337Fitting · crackedEND FITTING ANGLES ON AFT SIDE OF STA. 604, BUTT LINE 0, ARE CRACKED AND CORRODED. REMOVED AND REPLACED END FITTING ANGLES ON AFT SIDE OF STA. 604, BUTT LINE 0 IAW SRM 51-30-5. PN: 3924029-2N AND 3924029-1N.Sep 21, 2004 · N902AX · Doug DC932 · Fuselage Main, Attach FittingsSDR ABXA040335Skin · corrodedNUMEROUS AREAS OF CORROSION ON SKIN BELOW THE FORWARD LOWER CARGO DOOR. REPAIRED SKIN BELOW FORWARD LOWER CARGO DOOR IAW REA D953-50781MR.Sep 20, 2004 · N902AX · Doug DC932 · Fuselage Main, Plate/SkinSDR 0401399907Cylinder · damagedUPON CONFIGURING THE AIRCRAFT FOR LANDING, THE RIGHT SLAT DID NOT DEPLOY. THE AIRCRAFT DID ROLL UNCOMMANDED TO THE RIGHT. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AT DTW. MAINTENANCE AT DTW FOUND THAT ALL OF THE BOLTS FOAug 22, 2004 · N957N · Doug DC932 · Leading Edge Slat ActuatorSDR ABXA040318Door Frame · crackedCRACKED MAIN ENTRY DOOR FRAME WEB AT STA 207. REPAIRED WEB IAW DC-9 SRM 51-70-4.Aug 21, 2004 · N928AX · Doug DC932 · Fuselage Main, StructureSDR 0401389609Fuel Tank · leakingFLIGHT CREW NOTICED A FUEL IMBALANCE OF 1200 LBS BETWEEN LEFT AND RIGHT MAIN WING FUEL TANKS WHILE AT CRUISE. CREW HAD TO MANUALLY CROSSFEED THE FUEL AND ELECTED TO DIVERT TO ALTERNATE. THE LANDING AT GRB WAS UNEVENTFUL BUT NO MENTION OF COM PROCEDURES OR IFAug 20, 2004 · N609NW · Doug DC932 · Fuel StorageSDR 0401319919Line · rupturedFLIGHT CREW NOTICED THE LOSS OF HYDRAULIC FLUID FROM THE RT SYSTEM WHEN THE (RUDDER CONTROL MANUAL) LIGHT ILLUMINATED. COM PROCEDURES WERE COMPLIED WITH AND THE FLIGHT CONTINUED TO SCHEDULED DESTINATION. LANDING AT MSP WAS UNEVENTFUL. MAINTENANCE FOUND A RUPTUAug 10, 2004 · N941N · Doug DC932 · Hydraulic System, MainSDR ABXA040292Longeron · corrodedLONGERON 24 RT END CAP AT STA 945 WAS CORRODED. REPLACED END CAP IAW SRM 51-30-2 AND 51-30-5.Aug 5, 2004 · N988AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA040291Skin · corrodedFORWARD LOWER CARGO DOORS EXTERIOR SKIN HAD PITTING, CORROSION AT AFT LOWER CORNER. REPLACED DOOR ON NR 0399 IAW SRM.Aug 4, 2004 · N988AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA040290Pan · crackedFORWARD LOWER CARGO DOORS OUTER PAN WAS CRACKED AT HI-LOCK ALONG AFT EDGE, CENTER STOP PAD AREA. REPLACED DOOR ON NR 0399 IAW SRM.Aug 4, 2004 · N988AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA040289Pan · defectiveFORWARD LOWER CARGO DOOR HAD DEFECT INDICATION IN OUTER PAN ALONG UPPER EDGE AT FORWARD STOP PAD AREA. REPLACED DOOR ON NR 0399 IAW SRM.Aug 4, 2004 · N988AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA040288Pan · crackedFORWARD LOWER CARGO DOORS OUTER PAN HAD CRACK INDICATION IN OUTER RADIUS OF FORWARD HINGE. REPLACED DOOR ON NR 0399 IAW SRM.Aug 4, 2004 · N988AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA040287Pan · crackedFORWARD LOWER CARGO DOOR OUTER PAN CRACKED AT FASTENER HOLE AT UPPER FORWARD CORNER. REPLACED FORWARD LOWER CARGO DOOR ON N.R. 0399 IAW DC-9 SRM.Aug 4, 2004 · N988AX · Doug DC932 · Cargo/Baggage DoorsSDR ABXA040283Skin · crackedFUSELAGE SKIN CRACKED AT RIVET ON LONGERON 22 LT BETWEEN FS 180-200. REPAIRED ON EA 53300031-001.Aug 3, 2004 · N988AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA040286Beam · crackedAFT LOWER CARGO DOOR BEAM NR 1 BOTH FORWARD AND AFT END FITTINGS CRACKED. REPLACED FITTINGS S914025-501 AND 3914025-502 IAW SRM 51-30-1 AND 51-30-5.Aug 3, 2004 · N988AX · Doug DC932 · Fuselage Main, StructureSDR ABXA040285Longeron · crackedLONGERON 4 LT CRACKED AT FS 160 SPLICED SECTION OF LONGERON IAW SRM 53-02.Aug 3, 2004 · N988AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA040284Frame · crackedRT MAIN FRAME STA 699 WAS CRACKED IN FORWARD UPPER FLANGE BETWEEN Z-CLIP FASTENERS. REPAIRED MAIN FRAME RT 699 IAW EA 53400120-001-1.Aug 3, 2004 · N988AX · Doug DC932 · Fuselage Main, FrameSDR ABXA040282Skin · corrodedBULGE IN FUSELAGE SKIN AT CABIN OUTFLOW NOZZLE. REPLACED SECTION OF LONGERON FROM APPROXIMATELY STA. 955-990 IAW SRM.Aug 2, 2004 · N988AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA040246Lock Pin · out of adjustFIRST OFFICER'S CLEARVIEW WINDOW WOULD NOT GLIDE BACK TO FULL OPER POSITION. ADJUSTED CLEARVIEW WINDOW ECCENTRIC LOCK PIN. WINDOW OPENS AND CLOSES SMOOTHLY.Jul 15, 2004 · N988AX · Doug DC932 · Flight Compartment WindowsSDR ABXA040233Downlock Switch · defectiveNOSE LANDING GEAR DOWN (GREEN LIGHTS) DID NOT ILLUMINATE AFTER SELECTING LANDING GEAR DOWN. RECYCLED LANDING GEAR NOSE DOWN INDICATOR (GREEN LIGHT) INDICATED NORMAL DOWN AND LOCKED. REMOVED AND REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH IAW DC-9 MM 32-60-01-Jun 29, 2004 · N902AX · Doug DC932 · Landing Gear Position and WarningSDR ABXA040261Support · crackedLEFT SLAT DRIVE LOWER INBOARD BOLT ATTACHMENT SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.Jun 28, 2004 · N880DP · Doug DC932 · Leading Edge DevicesSDR ABXA040260Frame · crackedINTERCOSTAL FRAME CRACKED IN RADIUS FORWARD END OF FORWARD PASSENGER DOOR VIEWED FROM SECOND LIGHTENING HOLE FROM TOP. REPAIRED INTERCOSTAL IAW DC-9 SRM 52-05. REINSTALLED DOOR STOP IAW DC-9 SRM 51-30-1.Jun 28, 2004 · N880DP · Doug DC932 · Passenger/Crew DoorsSDR ABXA040258Door Frame · crackedINTERCOSTAL FRAME, INTERIOR OF FORWARD PASSENGER DOOR CRACKED IN RADIUS AFT END VIEWED FROM SECOND LIGHTENING HOLE FROM TOP. REMOVED FITTING AND STOP FOR REPLACEMENT AND REPAIR, FABRICATED PART IAW REA D952-50078. PRIMED AND PAINTED REINSTALLED IAW DC-9 SRM Jun 28, 2004 · N880DP · Doug DC932 · Passenger/Crew DoorsSDR ABXA040259Frame · crackedINTERCOSTAL FRAME, INTERIOR OF FORWARD PASSENGER DOOR CRACKED IN RADIUS AFT END VIEWED FROM THIRD LIGHTENING HOLE FROM TOP. STOP DRILLED CRACK AND REPAIRED PASSENGER DOOR NR 2 BEAM AFT END IAW DC-9 MM.Jun 28, 2004 · N880DP · Doug DC932 · Passenger/Crew DoorsSDR ABXA040257Attach Angle · crackedPYLON LEADING EDGE LOWER ATTACH ANGLE ON FUSELAGE CRACKED. INSTALLED NEW ANGLE IAW DC-9 SRM 51-30-2.Jun 26, 2004 · N880DP · Doug DC932 · Nacelle/Pylon Miscellaneous StructureSDR ABXA040241Attach Angle · crackedNR 2 PYLON UPPER ATTACH ANGLE CRACKED STA 980 LONGERON 14. REPAIRED NR 2 PYLON UPPER ATTACH ANGLE STA 930 LONGERON 14 IAW DC-9 SRM 54-04-10. INSTALLED FASTENERS IAW DC-9 SRM 51-30-5 AND PROTECTED AREA AGAINST CORROSION IAW DC-9 SRM 51-30-3.Jun 23, 2004 · N981AX · Doug DC932 · Nacelle/Pylon Miscellaneous StructureSDR ABXA040240Skin · crackedSKIN CRACKED STA 980 BETWEEN LONGERON 13 LEFT AND 14 LEFT. REPAIRED SKIN IAW DC-9 SRM 53-04.Jun 21, 2004 · N981AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA040212Downlock Switch · maladjustmentNOSE GEAR RED UNSAFE INDICATOR WOULD NOT ILLUMINATE WITH THROTTLES AT IDLE. PRESS TO TEST OK, HAD TO RECYCLE GEAR TO OBTAIN NOSE GEAR GREEN SAFE LIGHT. TESTED NOSE GEAR DOWNLOCK SWITCH. COULD NOT DUPLICATE. REPLACED THE NOSE GEAR DOWNLOCK SWITCH AS A PRECAJun 19, 2004 · N988AX · Doug DC932 · Landing Gear Position and WarningSDR ABXA040239Longeron · crackedLONGERON 29 LEFT CRACKED AT STA 579 THROUGH KIDNEY PANELS. INSTALLED NEW SECTION OF LONGERON 29 FS 579 TO 600 IAW REA D953-50039, DC-9 SRM 51-30-2 AND 51-30-5.Jun 18, 2004 · N981AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA040238Tee Fitting · crackedCRACKED AND CORRODED TEE ANGLE, AFT OF LT KIDNEY PANEL AT STA 606. REPLACED ANGLE IAW SRM 51-30-2.Jun 18, 2004 · N981AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA040237Shear Tie · crackedCRACKED SHEAR TIE AT FS 945 LONGERON 15 RT. REPLACED SHEAR TIE ON EA 53110008-202.Jun 18, 2004 · N981AX · Doug DC932 · Fuselage Main, StructureSDR ABXA040236Shear Tie · crackedCRACKED SHEAR TIE AT FS 945 LONGERON 14 RIGHT. REPLACED SHEAR TIE ON EA 53110008-202. REPLACED SHEAR TIE ON E.A. 53110008-202.Jun 18, 2004 · N981AX · Doug DC932 · Fuselage Main, StructureSDR ABXA040202Skin · crackedDURING LINE MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AND BULGED AT STA 759, LONGERON 29 RIGHT. REPAIRED SKIN IAW DC-9 SRM 53-04, FIG 12B.Jun 7, 2004 · N939AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA040203Skin · crackedDURING LINE MAINTENANCE, FOUND FUSELAGE SKIN CRACKED AND CORRODED AT STA 917 AND LONGERON 28 RIGHT. REPAIRED SKIN IAW REA D953-49934MR.Jun 7, 2004 · N939AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA040206Panel · damagedCOMPLY WITH COI 42381-001. REMOVED AND REPLACED WINDOW BELT RIGHT FUSELAGE EMERGENCY EXIT AREA. COMPLIED WITH COI 42381-001.Jun 4, 2004 · N984AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA040205Fitting · crackedFITTING CRACKED AFT SIDE FS 1038, LONGERON 15 RIGHT. REPLACED FITTING AT AFT SIDE OF FRAME FS 1038, LONGERON 15 RIGHT IAW DC-9 SRM 51-30-5 AND 51-30-1.May 27, 2004 · N984AX · Doug DC932 · Fuselage Main, Attach FittingsSDR ABXA040174Battery · dischargedEMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW AMM 33-00-00.May 10, 2004 · N980AX · Doug DC932 · Emergency LightingSDR 0400659620Valve · crackedWHEN THE HYDRAULIC PUMPS WERE TURNED ON DURING DESCENT, THE RIGHT HYDRAULIC SYSTEM FAILED COMPLETELY LOSING PRESSURE AND QUANTITY. CREW COMPLIED WITH COM PROCEDURES: LOSS OF RIGHT HYDRAULIC SYSTEM AND EMERGENCY GEAR EXTENSION. LANDING WAS NORMAL AND UNEVENTFULMay 1, 2004 · N620NW · Doug DC932 · Rudder Control SystemSDR 0400559605Controller · failedDURING CRUISE AT FL350 THE CABIN BEGAN AN UNCONTROLLED CLIMB. MANUAL CONTROL HAD NO EFFECT SO THE FLIGHT CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FEET. IT IS NOTED THE CREW WAS ABLE TO REGAIN MANUAL CONTROL DURING THE DESCENT. FLIGHT DIVERTED TO DTW AND LApr 17, 2004 · N605NW · Doug DC932 · Cabin Pressure ControllerSDR ABXA040141Window · stuckFIRST OFFICER'S SIDE WINDOW WAS STUCK SHUT. INSTALLED A MISSING NUT AT ROD END AT TOP OF WINDOW AND SECURED LOOSE LOCK BAR TRIM. WINDOW OPERATES NORMALLY.Apr 16, 2004 · N988AX · Doug DC932 · Flight Compartment WindowsSDR ABXA040154Angle · corrodedSPLICE ANGLE CORRODED AT STA 229, LONGERON 18 RIGHT. REPLACED SPLICE ANGLE IAW REA D953-49615.Apr 14, 2004 · N987AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA040153Web · crackedLT CUSP WEB CRACKED AT FS 965. REPAIRED LT CUSP WEB AT FS 965.Apr 12, 2004 · N987AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA040150Frame · crackedANGLE FORWARD OF CENTER WINDSHIELD AT LOWER RT OUTBOARD CORNER CRACKED. APPROXIMATE LENGTH 1.5 INCHES. REPAIRED ON REA D953-49620MR.Apr 9, 2004 · N987AX · Doug DC932 · Fuselage Main, FrameSDR ABXA040152Frame · crackedRIGHT AFT MAIN FRAME AT STA. 737 WAS CRACKED AT POINTS E TO D AND G TO J. REPAIRED MAIN FRAME STA. 737 RIGHT IAW EA 30686.Apr 9, 2004 · N987AX · Doug DC932 · Fuselage Main, FrameSDR ABXA040151Floorbeam · corrodedFLOORBEAM CORRODED AT RIGHT BUTT LINE 44 STA. 965. REPAIRED FLOORBEAM IAW DC-9 SRM 53-05.Apr 9, 2004 · N987AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA040145Floorbeam · corrodedSTA 965 FLOORBEAM STRAP CORRODED. REMOVED DAMAGED FLOORBEAM AT STA. 965 FROM LBL 54 - RBL 54. FABRICATED NEW FLOORBEAM IAW DACO DWG. 9912243.Apr 8, 2004 · N987AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA040144Beam · crackedCRACK INDICATION FOUND ON FORWARD LOWER CARGO DOOR NR 2 BEAM TEE FORWARD END AT SKIN RIVET. REPAIRED AREA IAW DC-9 SRM K05159 AND DC-9 SRM 51-30-5.Apr 8, 2004 · N987AX · Doug DC932 · Fuselage Main, StructureSDR ABXA040143Pan · crackedMAIN ENTRY DOOR PAN CRACKED AT FORWARD LOWER STOP. REPAIRED DOOR IAW DC-9 SRM.Apr 8, 2004 · N987AX · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA040149Shear Tie · corrodedCORROSION ON SHEAR TIE STA 851 ABOUT 6 INCHES ABOVE LONGERON 15 RIGHT. REPLACED SHEAR TIE IAW DC-9 SRM.Apr 8, 2004 · N987AX · Doug DC932 · Fuselage Main, StructureSDR ABXA040148Doubler · corrodedCORROSION AT STA. 226, LONGERON 18 RIGHT ON ANGLE DOUBLER. REPLACED FITTING IAW DC-9 SRM.Apr 8, 2004 · N987AX · Doug DC932 · Fuselage Main, Plate/Skin
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