Douglas DC-9-41

Service difficulty reports · 2,671

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 = 'DC941'
  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 ABXA020265Door Frame · crackedCRACKED IN BEND RADIUS AT LEFT UPPER VENTRAL DOOR CORNER. CRACK LENGTH APPROXIMATELY 1.25 INCH IN LENGTH. REPAIRED CRACK IAW DC-9 SRM 51-10-02.Oct 9, 2002 · N976AX · Doug DC941 · Fuselage Main, StructureSDR ABXA020264Panel · crackedNOSE WHEEL WELL UPPER PRESSURE PANEL HAD CRACK AT STA. 110 RIGHT TUNNEL, APPROXIMATELY 14 INCHES INBOARD. REPAIRED PANEL IAW DC-9 SRM 51-30-2, 51-30-1 AND 51-30-5.Oct 9, 2002 · N976AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA020263Panel · crackedNOSE WHEEL WELL UPPER PRESSURE PANEL HAD CRACK AT STA. 110 LEFT TUNNEL, APPROXIMATELY 24 INCHES INBOARD. REPAIRED PANEL IAW DC-9 SRM 53-01, 51-30-2, 51-30-1 AND 51-30-5.Oct 9, 2002 · N976AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA020262Panel · crackedNOSE WHEEL WELL UPPER PRESSURE PANEL STA. 89 LEFT, APPROXIMATELY 3 INCHES INBOARD, HAD CRACK. REPAIRED CRACK IAW REA D953-45373.Oct 9, 2002 · N976AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA020261Splice · corrodedLEVEL II CORROSION AT F.S. 1013, LONGERON 27 LEFT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPLACED FRAME SPLICE IAW DC-9 SRM.Oct 8, 2002 · N976AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA020260Fitting · crackedANGLE CRACKED AT LONGEON 30 JUST AFT OF FORWARD 'P' DOME, KEEL AREA. REPLACED ANGLE IAW DC-9 SRM 51-30-5.Oct 8, 2002 · N976AX · Doug DC941 · Fuselage Structure (General)SDR ABXA020259Support · crackedRIGHT WING OUTBOARD SPOILER TORSION BAR SUPPORT FITTING CRACKED AT UPPER END. REPLACED FITTING IAW DC-9 SRM 51-30-1.Oct 8, 2002 · N976AX · Doug DC941 · Wing StructureSDR ABXA020231Battery · dischargedEMERGENCY LIGHTING WAS DIM. REPLACED EMERGENCY POWER SUPPLY BATTERIES IAW DC-9 MM 33-53-02-4.Oct 7, 2002 · N966AX · Doug DC941 · Emergency LightingSDR ABXA020228Door Frame · crackedCRACK IN UPPER LEFT CORNER OF THE VENTRAL DOOR JAMB. REPAIRED AREA IAW REA D953-45345-MR.Oct 6, 2002 · N990AX · Doug DC941 · Fuselage Main, StructureSDR GTIA021037Isolator · defectiveDTW - FOUND LOWER NR 1 ENGINE ISOLATOR DOES NOT HAVE ANTI-ROTATION MARK. REMOVED AND REPLACED NR 1 ENGINE LOWER ISOLATOR, CLOSED 10/10/02. (M)Oct 1, 2002 · N130NK · Doug DC941 · Engine Mount SectionSDR GTIA021036Isolator · defectiveDTW - FOUND UPPER NR 1 ENGINE ISOLATOR DOES NOT HAVE ANTI-ROTATION MARK. REMOVED AND REPLACED NR 1 ENGINE UPPER ISOLATOR, CLOSED 10/10/02. (M)Oct 1, 2002 · N130NK · Doug DC941 · Engine Mount SectionSDR GTIA021071Combust Chamber · wornBOROSCOPE RECORD, FOUND IGNITER GUIDE NR 4 COMBUSTION CHAMBER WORN AND OUT OF CHAMBER RESTING IN OUTER COMBUSTION CASE IGNITER PORT NR 4. BURNER CANS HAVE BEEN REPACED DURING SHOP VISIT.Oct 1, 2002 · N130NK · Doug DC941 · Turbine Engine Combustion SectionSDR GTIA021033Clip · missingFORWARD EMERGENCY FLASHLIGHT LOCK CLIP MISSING AND LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY.Oct 1, 2002 · N131NK · Doug DC941 · Emergency EquipmentSDR ABXA020220Controller · malfunctionedON CLIMBOUT, AIRCRAFT DID NOT PRESSURIZE. PERFORMED ABNORMAL, AUTO CONTROLLER WAS INOPERATIVE. UNABLE TO CONTROL PRESSURE. INSPECTED ALL ACCESS DOORS, ALL CLOSED. INSPECTED AND LUBRICATED OUTFLOW BUTTERFLY VALVE LINKAGE AND OUTFLOW NOZZLE, NO DEFECTS FOUNDOct 1, 2002 · N954AX · Doug DC941 · Cabin Pressure ControllerSDR ABXA020219Web · crackedFOUND NUMEROUS CRACKS IN AFT CUSP WEB, LEFT HAND SIDE APPROXIMATELY AT FS 1002. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.Sep 29, 2002 · N975AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020245Web · crackedCUSP WEB AT F.S. 636 - 696, RIGHT SIDE CRACKED. REPLACED WEB IAW DC-9 SRM 51-30-1 AND 51-30-2.Sep 28, 2002 · N973AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020244Web · crackedCUSP WEB CRACKED AT STA. 1019, RIGHT BUTT LINE 54. FOUND CRACK TO BE MINOR. TRIMMED OUT CRACK IAW DC-9 SRM 53-01. (WITHIN LIMITS)Sep 25, 2002 · N973AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020243Web · crackedCUSP WEB CRACKED IN 2 PLACES AT STA. 1040, RIGHT BUTT LINE 54. REPAIRED FLOOR PANEL IAW DC-9 SRM 53-01.Sep 25, 2002 · N973AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020242Angle · crackedDOOR PAN ANGLE WAS CRACKED. REMOVED, WELDED AND REINSTALLED DOOR PAN IAW DC-9 SRM 51-30-1 AND 51-30-2, DRAWING K05818.Sep 25, 2002 · N973AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020241Splice · crackedLONGERON SPLICE AT LONGERON 30, STA. 870 - 880 WAS CRACKED. REPLACED SPLICE IAW DC-9 SRM 53-02 AND 51-30-5.Sep 25, 2002 · N973AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA020240Shim · crackedEXFOLIATION IN 2 PLACES, LONGERON 23 LEFT BETWEEN F.S. 973 AND 993. REPLACED LONGERON STIFFENER STRIP IAW DC-9 SRM 51-30-2.Sep 25, 2002 · N973AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA020239Web · crackedNUMEROUS CRACKS IN CUSP WEB BETWEEN FS 1021 AND 1041 AT LEFT BUTT LINE 54. REPAIRED AREA IAW DC-9 SRM 53-01.Sep 25, 2002 · N973AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020238Intercostal · crackedCRACKED INTERCOSTAL F.S. 1072 AND LONGERON 28 LEFT. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5.Sep 25, 2002 · N973AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020237Angle · crackedLEFT PYLON BULKHEAD ANGLE CRACKED IN RADIUS ADJACENT TO LOWER SPAR CRACK. REPLACED LEFT BULKHEAD ANGLE IAW REA D953-45305-MR.Sep 25, 2002 · N973AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA020236Support · crackedINBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING WAS CRACKED. REPLACED SUPPORT IAW DC-9 SRM 51-10-4 AND 51-30-5.Sep 24, 2002 · N973AX · Doug DC941 · Wing StructureSDR ABXA020235Eyebolt · brokenSLAT DRIVE MECHANISM WAS BROKEN AT THE INBOARD ACTUATOR ON THE LEFT WING. REPLACED EYEBOLT IAW DC-9 MM 27-80-05-2-0101.Sep 24, 2002 · N973AX · Doug DC941 · Leading Edge Slat Control SystemSDR ABXA020234Angle · crackedSKIN CRACKED ON F.S. 37 BULKHEAD, RIGHT SIDE AT UPPER RADOME ALIGNMENT PIN. REPAIRED AREA IAW ABX DRAWING 05159 AND DC-9 SRM.Sep 24, 2002 · N973AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA020216Battery Pack · dischargedCOCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CHECKED GOOD IAW DC9 AMM 33-53-00.Sep 24, 2002 · N972AX · Doug DC941 · Emergency LightingSDR GTIA020979Wire · looseACY - FOUND EMERGENCY FLOOR PATH LIGHTING ROW 8DEF INOPERATIVE. RESECURED FLOOR PATH LIGHTING WIRE. (M)Sep 17, 2002 · N131NK · Doug DC941 · Light System WiringSDR GTIA020974Dome Nut · brokenRIGHT TANK FUEL QUANTITY WENT DOWN FASTER THAN LEFT WHILE IN FLIGHT. LANDED WITH 5600 IN LEFT AND 4300 IN RIGHT. CONFIRMED QUANTITY WITH DRIP STICKS. FOUND MISSING BOLT ON FORWARD PANEL ON RIGHT WING. FOUND 2 DOME NUTS FOR RIGHT WING FQ PROBE NR 2 ACCESS PSep 16, 2002 · N131NK · Doug DC941 · FastenersSDR 0203209756Skin · crackedWhile in DHN for Hck, a .44 inch crack was found in the skin at a fastener hole 5" above Longeron 18 right. Repaired per EA 97-191331.Sep 13, 2002 · N756NW · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA020154Coalescer Bag · defectiveSTRONG SMELL WHILE AT TAKE-OFF POWER. PERFORMED ENGINE RUN, OPERATED BOTH PACKS FROM APU AND ENGINES. NO SMELL NOTED. VISUALLY INSPECTED PNEUMATIC DUCTING, NO DEFECTS NOTED. CHECKED ACM OILS AND REPLACED COALESCER BAGS IAW DC-9 MM PROCEDURES.Sep 4, 2002 · N973AX · Doug DC941 · Air Distribution SystemSDR ABXA020203Clip · cracked#1 PYLON ATTACH ANGLE INSIDE PANEL 8111 AT UPPER AFT ENGINE MOUNT STRAP HAD CRACK NEXT TO BOLT. REPLACED ANGLE IAW DC-9 DWG 9915500 AND DC-9 SRM 51-30-5.Aug 29, 2002 · N972AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA020148Sensor · defectiveAFTER GEAR RETRACTION, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON. RIGHT HYDRAULIC PUMPS ON HIGH. AT GEAR UPLATCH CHECK, THE LIGHT WENT OUT. GEAR RECYCLED ONE TIME BEFORE UPLATCH CHECK WITH THE LIGHT STILL ON. REPLACED THE LEFT GEAR DOWN SENSOR IAW DC-9 MM 32Aug 29, 2002 · N954AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA020202Intercostal · crackedCRACKED INTERCOSTAL AT STA 794, RBL 22. REPAIRED INTERCOSTAL IAW DC-9 SSRM K05159.Aug 28, 2002 · N972AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020201Intercostal · crackedCRACKED INTERCOSTAL AT STA. 794, LEFT BUTT LINE 22. REPAIRED INTERCOSTAL IAW DC-9 SSRM K05159.Aug 28, 2002 · N972AX · Doug DC941 · Fuselage Miscellaneous StructureSDR 0202759759Control Cable · out of rigON TAKEOFF, THE CREW HAD A STALL INDICATOR ACCOMPANIED WITH A STICK SHAKER. ONCE IN THE AIR, A LOUD POP WAS HEARD AND THE AIRCRAFT ROLLED TO THE RIGHT. AFTER ROLL CORRECTION, THE STALL INDICATION CLEARED BUT THE CREW ELECTED TO RETURN TO MSP. LANDING WAS UNAug 25, 2002 · N759NW · Doug DC941 · Leading Edge Slat Control SystemSDR ABXA020211Web · crackedCUSP WEB WAS CRACKED AT STA 1041, LONGERON 18 LEFT. REPLACED CUSP WEB STRINGER IAW DC-9 SRM 53-01.Aug 16, 2002 · N954AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020177Web · crackedCUSP WEB WAS CRACKED AT STATION 1041, LONGERON 18 LEFT. REPLACED CUSP WEB IAW DC-9 SRM 53-01.Aug 16, 2002 · N954AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020210Intercostal · crackedINTERCOSTAL JUST BELOW RIGHT RADOME HINGE WAS CRACKED AT CUTOUT. REPLACED INTERCOSTAL AND INSTALLED FASTENERS IAW DC-9 SRM 51-30-2 AND 51-30-5.Aug 14, 2002 · N954AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020209Angle · corrodedEXFOLIATED ANGLE ON OUTBOARD END OF SLANT PANEL. REPLACED ANGLE IAW DC-9 SRM.Aug 14, 2002 · N954AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020208Hinge · crackedRIGHT MAIN LANDING GEAR INBOARD DOOR HINGE WAS CRACKED. REMOVED AND REINSTALLED THE RIGHT MAIN LANDING GEAR DOOR FOR HINGE CHANGE IAW DC-9 MM 32-12-01-2-02-01, SRM 51-30-1, 51-30-5 AND 52-05.Aug 14, 2002 · N954AX · Doug DC941 · Landing Gear DoorsSDR ABXA020176Intercostal · crackedINTERCOSTAL JUST BELOW RIGHT RADOME HINGE WAS CRACKED AT CUTOUT. REPLACED INTERCOSTAL AND INSTALLED FASTENERS IAW DC-9 SRM 51-30-2 AND 51-30-5.Aug 14, 2002 · N954AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020175Angle · corrodedEXFOLIATED ANGLE ON OUTBOARD END OF SLANT PANEL. REPLACED ANGLE IAW DC-9 SRM.Aug 14, 2002 · N954AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA020174Hinge · crackedRIGHT MAIN LANDING GEAR INBOARD DOOR HINGE WAS CRACKED. REMOVED AND REINSTALLED RIGHT MAIN LANDING GEAR DOOR FOR HINGE CHANGE IAW DC-9 MM 32-12-01-2-02-01 AND SRM 51-30-1, 51-30-5, AND 52-05.Aug 14, 2002 · N954AX · Doug DC941 · Landing Gear DoorsSDR ABXA020200Former · crackedFORWARD LOWER CARGO DOOR, LOWER FORWARD STOP INTERCOSTAL FORMER WAS CRACKED. REPLACED BRACKET IAW DC-9 SRM 51-30-1 AND 51-30-2.Aug 13, 2002 · N963AX · Doug DC941 · Fuselage Structure (General)SDR ABXA020199Fitting · crackedFORWARD LOWER CARGO DOOR AFT STOP FITTING AT END OF INTERCOSTAL CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.Aug 13, 2002 · N963AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA020198Pan · crackedAFT LOWER CARGO DOOR INNER PAN WAS CRACKED NEAR FORWARD LATCH HOOK AT ROLLER CUTOUT. REPLACED AFT LOWER CARGO DOOR ON N.R. #0350 AND IAW DC-9 MM.Aug 12, 2002 · N963AX · Doug DC941 · DoorsSDR ABXA020197Pan · crackedOUTER PAN WAS CRACKED AT BEAM 3 ON AFT END OF AFT LOWER CARGO DOOR. REPLACED DOOR IAW DC-9 MM.Aug 12, 2002 · N963AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA020196Pan · crackedFORWARD END OF AFT LOWER CARGO DOOR HAD CRACKED PANES AT DOORSTOP CUTOUT AT BEAMS 1, 2, AND 3. REPLACED DOOR ON N.R. #0350 AND IAW DC-9 MM.Aug 12, 2002 · N963AX · Doug DC941 · Doors
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