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 ABXA000384Fitting · crackedAFT LOWER CARGO DOOR UPPER AFT INTERCOSTAL TEE FITTING CRACKED AT UPPER AFT DOOR STOP. REPLACED TEE-FITTING.Jul 11, 2000 · N907AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA000379Web · crackedLEFT WING TRAILING EDGE WEB, FORWARD OF AILERON, CRACKED APPROXIMATELY TWO INCHES FROM OUTBOARD EDGE.Jul 11, 2000 · N907AX · Doug DC931 · Wing Miscellaneous StructureSDR ABXA000375Pan · crackedFORWARD LOWER CARGO DOOR OUTER PAN WAS CRACKED AT DOOR STOPS NR 1, 12, 13 AND 14. REPLACED DOOR IAW DC9 SRM.Jul 11, 2000 · N907AX · Doug DC931 · Cargo/Baggage DoorsSDR USAAD00111Battery · dischargedIND - THE CEILING EMERGENCY LIGHTS IN THE FORWARD ENTRY AND 1ST CLASS PASSENGER SECTION AREA WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Jul 10, 2000 · N920VJ · Doug DC931 · Emergency LightingSDR ABXA000387Skin · crackedAFT CARGO COMPARTMENT DOOR SKIN CRACKED. REPAIRED DOOR IAW DC9 SRM 52-01.Jul 10, 2000 · N907AX · Doug DC931 · Cargo/Baggage DoorsSDR 0002459938Web · crackedA 2 INCH CRACK FWD SIDE MAIN FRAME 756 WEB CUSP LINE. REPAIRED PER EA 99-172576, L/P 1463368.Jul 10, 2000 · N1798U · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0011104Keelbeam · damagedDURING OP 15 MAINT CHECK, ON THE LOWER FUSELAGE, LT CANTED KEEL BEAM AREA WAS NECESSARY TO ACCOMPLISH KEEL BEAM WEB SPLICE REPAIR PER SSRM 53-10-110. MODIFIED CANTED KEEL BEAM PER SSRM 53-10-110.Jul 10, 2000 · N977Z · Doug DC931 · Fuselage Main, KeelSDR TWAA0011103Keelbeam · damagedDURING OP 15 MAINT CHECK, FOUND ON THE LOWER FUSELAGE, THE RT CANTED KEEL BEAM AREA, NECESSARY TO ANALYZE THE CANTED KEEL BEAM WEB SPLICE REPAIR PER SSRM 53-10-110. INSTALLED CANTED KEEL BEAM WEB SPLICE REPAIR PER SSRM 53-10-110.Jul 10, 2000 · N977Z · Doug DC931 · Fuselage Main, KeelSDR USAAD00110Power Supply · failedIND - THE CEILING EMERGENCY LIGHTS BETWEEN SEAT ROWS 5 AND 9 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)Jul 9, 2000 · N927VJ · Doug DC931 · Emergency LightingSDR 0002439938Floorbeam · corrodedCORROSION ON FLOORBOARD AT STA 160 ABOUT 10 INCHES I/B OF RT SIDE. FABRICATED REPAIR PER EA 99-172574 L/P 1462596.Jul 8, 2000 · N1798U · Doug DC931 · Fuselage Main, Floor BeamSDR 0002449938Skin · corrodedSTA 800 - 825 FUSELAGE SKIN AT L26RT UP TO L25 HAS CORROSION. REPAIRED PER EA 99-172573 L/P 1462297.Jul 7, 2000 · N1798U · Doug DC931 · Fuselage Main, Plate/SkinSDR 0002469938Angle · crackedCRACK .5 INCH LONG OMITTING FROM FASTENER HOLE. REPAIRED PER EA 99-172550 L/P 1462156.Jul 6, 2000 · N1798U · Doug DC931 · Vertical StabilizerSDR TWAA0010704Valve · wornLOST CABIN PRESSURIZATION AND PSU OXYGEN MASKS DEPLOYED. REPLACED THE RT FLOW CONTROL VALVE. CHECK-C 10-4-99 MCI. ---CLOSED---Jul 6, 2000 · N979Z · Doug DC931 · Pressure Regulator/Outflow ValveSDR USAAD00107Outflow Valve · failedPIT-CLT - FLT 375 - AFTER TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE. MAINTENANCE REPLACED THE PRESSURIZATION OUTFLOW VALVE ACTUATOR. (M)Jul 4, 2000 · N963VJ · Doug DC931 · Pressure Regulator/Outflow ValveSDR TWAA0010701Cable · brokenTHE RT SIDE FWD ESCAPE SLIDE LANYARD WAS FOUND BROKEN. REPLACED THE LANYARD. CHECK-C 11-25-99 STL.Jul 3, 2000 · N992Z · Doug DC931 · Escape SlideSDR USAA000975Door Frame · crackedPIT - FOUND FRAME CRACKED 2 INCHES, VENTRAL DOOR FRAME RIGHT SIDE ABV TOP LIGHTENING HOLE. INSTALLED ANGLE DOUBLERS AND Z DOUBLERS PER SRM 53-05 FIG 27. (M)Jun 28, 2000 · N997VJ · Doug DC931 · Passenger/Crew DoorsSDR 0002289998Stop · wornDURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH ROLL TO THE LEFT ON SLAT EXTENSION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND STOPS ON LEFT TELESCOPING DUCT WORN. REPLACED STOPS. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED Jun 27, 2000 · N8934E · Doug DC931 · Leading Edge Slat Control SystemSDR USAAD00098Light · inoperativeDTW - THE FORWARD SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERATIVE. MAINTENANCE REPLACED A SHORTED WIRE AND POWER PACK FUSE AS REQUIRED. OPS CHECKED OK. (M)Jun 22, 2000 · N960VJ · Doug DC931 · Emergency LightingSDR USAAD00097Light · failedIND- THE EMERGENCY LIGHT AT THE SERVICE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M)Jun 22, 2000 · N936VJ · Doug DC931 · Emergency LightingSDR GTIA000227Wire · exposedACY - FLT 208 - EMERGENCY TRACK FLOOR LIGHTING IN GALLEY AREA WIRES SHOWING. RE-SECURED TRACK LIGHT WIRES AND STRIP, OK TO CONTINUE. (M)Jun 19, 2000 · N969ML · Doug DC931 · Light System WiringSDR 20001005AP001Battery · dischargedIND - THE SERVICE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS DIM AND THE AFT ACCESSORY EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE SERVICE DOOR SLIDE ACTIVATED EMERGENCY LIGHT ASSEMBLY AND THE AFT ACCESSORY EMERGENCY LIGHT BATTERIES. REF USAAD0Jun 19, 2000 · N923VJ · Doug DC931 · Emergency LightingSDR USAAD00095Light · failedIND - THE SERVICE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS DIM AND THE AFT ACCESSORY EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE SERVICE DOOR SLIDE ACTIVATED EMERGENCY LIGHT ASSEMBLY AND THE AFT ACCESSORY EMERGENCY LIGHT BATTERIES. (M)Jun 19, 2000 · N923VJ · Doug DC931 · Emergency LightingSDR USAA000855Skin · crackedPIT - FOUND SKIN CRACKED 1 INCH, SVC DOOR JAMB LOWER AFT CORNER. DOUBLERS INSTALLED AFTER CRACK CUT OUT, FILLER AND TAPER SHIMS INSTALLED PER SRM 53-05 FIG 112. (M)Jun 16, 2000 · N974VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA000319Skin · delaminatedDURING C-CHECK, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR DELAMINATED 40 SQ INCHES ON INTERIOR SIDE AND 36 SQ INCHES ON EXTERIOR SIDE. REPLACED DOOR IAW DC9 OHM 32-10-6 AND DC9 MM 32-12-01.Jun 16, 2000 · N906AX · Doug DC931 · Landing Gear DoorsSDR ABXA000318Skin · corrodedDURING C-CHECK, FOUND THE FUSELAGE INTERIOR SKIN AT THE LEFT ALTERNATE STATIC PORT CORRODED BEYOND LIMITS AT FS 342. REPAIRED SKIN IAW DC9 SRM 53-04.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA000317Frame · corrodedDURING C CHECK FOUND FRAME AT STATION 218 AND LONGERON 23 LEFT CORRODED ON LOWER LEG. REMOVED CORROSION IAW DC9 SRM 51-10-3 AND REPAIRED IAW ABX SSRM DWG. K05159.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, FrameSDR ABXA000316Longeron · crackedDURING C-CHECK, FOUND LONGERON 24 LEFT CRACKED AT STATION 180. REPLACED LONGERON IAW DC9 SRM 51-30-5.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA000315Longeron · crackedDURING C-CHECK, FOUND LONGERON 24 LEFT AT STATION 200 CRACKED. REPLACED LONGERON IAW DC9 SRM 51-30-2.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA000314Bracket · crackedDURING C-CHECK, FOUND THE AFT LOWER CARGO COMPARTMENT DOOR JAMB ON LOCKING PIN BRACKET CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-5.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000313Support Fitting · crackedDURING C-CHECK, FOUND THE RT WING OUTBOARD SPOILER OUTBOARD TORSION BAR SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1.Jun 16, 2000 · N906AX · Doug DC931 · SpoilersSDR ABXA000312Longeron · crackedDURING C-CHECK, FOUND LONGERON 16 LT CRACKED AT STATION 965 FUSELAGE FRAME ATTACH POINT. REPLACED LONGERON IAW DC9 SRM 53-02.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA000306Longeron · crackedDURING -C- CHECK FOUND LONGERON 16 RT CRACKED AT STATION 965 FRAME ATTACH POINT. REPAIRED LONGERON IAW DC9 SRM 53-02.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA000305Longeron · crackedDURING C-CHECK, FOUND LONGERON 23 LEFT CRACKED AT STATION 200. REPLACED LONGERON IAW DC9 SRM 51-30-2.Jun 16, 2000 · N906AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA000311Attach Angle · crackedDURING C-CHECK, FOUND RT PYLON UPPER ATTACH ANGLE CRACKED AT STATION 996. REPAIRED IAW DC9 SRM 54-04.Jun 13, 2000 · N906AX · Doug DC931 · Nacelle/Pylon, Attach FittingsSDR ABXA000310Fitting · crackedDURING C-CHECK, FOUND THE LT INBOARD LEFT SPOILER OUTBOARD ATTACH FITTING AT TRAILING EDGE OF WING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2.Jun 13, 2000 · N906AX · Doug DC931 · SpoilersSDR USAAD00092Charger · failedIND - THE EMERGENCY LIGHT CIRCUIT BREAKER POPPED WHEN SELECTING THE EMERGENCY LIGHT SWITCH TO THE OFF POSITION. MAINTENANCE REPLACED THE BATTERY PACK CHARGER IN THE LAVATORY CEILING. (M)Jun 12, 2000 · N935VJ · Doug DC931 · Emergency LightingSDR ABXA000304Fitting · crackedDURING C-CHECK, FOUND THE RIGHT WING INBOARD SPOILER OUTBOARD TORSION BAR SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-01.Jun 12, 2000 · N906AX · Doug DC931 · SpoilersSDR ABXA000303Angle · crackedDURING C-CHECK, FOUND AFT LOWER CARGO BULKHEAD ATTACH ANGLE CRACKED AT STATION 756 AND LONGERON 28 RIGHT. REPLACED ANGLE IAW DC9 SRM 51-30-5.Jun 12, 2000 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000302Angle · crackedDURING C-CHECK, FOUND BULKHEAD ATTACH ANGLE CRACKED AT STATION 756 AND LONGERON 26 LEFT. REPLACED ANGLE IAW DC9 SRM 51-30-5.Jun 12, 2000 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000301Retainer · crackedDURING C-CHECK, FOUND RETAINER FOR WINDOW NR 28 LEFT HAND, STATION 756 CRACKED. REPAIREDRETAINER IAW ABX REA D953-37307.Jun 12, 2000 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000300Web · crackedDURING C-CHECK, FOUND CUSP WEB CRACKED FORWARD OF STATION 870, LEFT SIDE. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.Jun 12, 2000 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA0009301Afcs · malfunctionedCREW REPORTED UNCOMMANDED PITCH CHANGES IN FLIGHT WITH AUTOPILOT NOT ENGAGED. CHECK-C 12-23-99 MCI.Jun 12, 2000 · N985Z · Doug DC931 · Auto Flight SystemSDR 0002129909Tire · failedSEVERE VIBRATION DEVELOPED ABOUT THE NOSE WHEEL AREA. ABORTED TAKEOFF. THE AIRCRAFT REACHED 120 KNOTS BUT STOPPED SAFELY AND TAXIED BACK TO THE GATE. MAINTENANCE FOUND THE NOSE WHEEL TIRE CHINE SEPARATED FROM THE TIRE SIDEWALL. REPLACED THE NR 4 MAIN AND BJun 10, 2000 · N959N · Doug DC931 · TireSDR ABXA000294Power Supply · defectiveEMERGENCY EXIT LIGHTS REMAINED ON AFTER POWER WAS REMOVED AND THE SWITCH WAS OFF. REPLACED EMERGENCY LIGHT POWER SUPPLY.Jun 8, 2000 · N947AX · Doug DC931 · Emergency LightingSDR USAAD00096Battery · dischargedDAY - THE LEFT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)Jun 7, 2000 · N966VJ · Doug DC931 · Emergency LightingSDR ABXA000299Uplock Roller · out of adjON APPROACH TO ILN, THE GEAR DOOR OPEN LIGHT ILLUMINATED. ACCOMPLISHED ABNORMALPROCEDURES AND LANDED WITH EMERGENCY GEAR LEVER UP. STOPPED AIRCRAFT ON RUNWAY. ADJUSTED THE AFT UPLATCH ROLLER CLEARANCE.Jun 7, 2000 · N943AX · Doug DC931 · Landing Gear Position and WarningSDR USAAD00091Battery · dischargedIND - THE MAIN ENTRY DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Jun 6, 2000 · N959US · Doug DC931 · Emergency LightingSDR USAA000842Bulkhead · crackedPIT - FOUND BULKHEAD WEB CRACKED 3 INCHES, STATION 965 BULKHEAD (LEFT) 8 INCHES FROM FLOOR. REPLACED SECTION OF WEB PER EA 55292. (M)Jun 3, 2000 · N934VJ · Doug DC931 · Fuselage Main, BulkheadSDR USAA000840Pan · crackedPIT - FOUND DOOR PAN CRACKED 1 INCH, FORWARD CARGO DOOR, LOWER FORWARD STOP. INSTALLED DOUBLER PER SRM 52-03 FIG 8. (M)Jun 3, 2000 · N934VJ · Doug DC931 · Cargo/Baggage DoorsSDR USAA000838Tab · delaminatedPIT - FOUND 3 INCH BY 4 INCH DELAMINATION, LEFT AILERON TAB BOTTOM JB END. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER MM 27-10-5. (M)Jun 3, 2000 · N934VJ · Doug DC931 · Aileron Tabs
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