Douglas DC-9-31

Service difficulty reports · 7,433

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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 0501169996Outflow Valve · leakingAT FL310, WITH POWER AT CRUISE SETTING AND AIRFOIL ANTI-ICE ON, THE RED "CABIN PRESS" WARNING LIGHT ILLUMINATED. CABIN WAS JUST ABOVE 10,000 FEET AND CLIMBING AT 800-900 FPM. CREW COMPLIED WITH COM AND THE RED BORDERED CHECKLIST BUT COULD NOT REGAIN CONTROL OJul 27, 2005 · N8932E · Doug DC931 · Pressure Regulator/Outflow ValveSDR 050116996Outflow Valve · leakingAT FL310, WITH POWER AT CRUISE SETTING AND AIRFOIL ANTI-ICE ON, THE RED "CABIN PRESS" WARNING LIGHT ILLUMINATED. CABIN WAS JUST ABOVE 10,000 FEET AND CLIMBING AT 800-900 FPM. CREW COMPLIED WITH COM AND THE RED BORDERED CHECKLIST BUT COULD NOT REGAIN CONTROL Jul 27, 2005 · N8932E · Doug DC931 · Pressure Regulator/Outflow ValveSDR ABXA050224Frame · crackedSHEAR TIE CRACKED FS 1087, LONGERON 2 RIGHT. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5.Jul 26, 2005 · N907AX · Doug DC931 · Fuselage Main, FrameSDR ABXA050181Fitting · crackedAFT LOWER BAG BIN DOOR NR 1 BEAM FORWARD END FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1.Jul 26, 2005 · N907AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA050180Frame · crackedLONGERON 23 LEFT CRACKED AT FRAME, FS 200. REPAIRED AREA IAW DC-9 SRM 53-02.Jul 25, 2005 · N907AX · Doug DC931 · Fuselage Main, FrameSDR 0501129981Clamp · leakingDURING CRUISE FLIGHT AT FL290 WITH AIRFOIL ANTI-ICE SYSTEM ON, THE CABIN STARTED CLIMBING AT 300 FT/MIN. INITIATED DESCENT AND COMPLIED WITH THE RED BORDERED CHECK LIST. WHEN THE ANTI-ICE SYSTEM WAS SWITCHED OFF THE CREW WAS ABLE TO CONTROL CABIN PRESSURE BUT Jul 25, 2005 · N994Z · Doug DC931 · Air Distribution SystemSDR ABXA050223Skin · corrodedSKIN LONGERON 30, FS 680 TO FS 737 WAS CORRODED. BLENDED CORROSION AND REPAIRED DAMAGED AREAS IAW DC-9 SRM.Jul 24, 2005 · N907AX · Doug DC931 · Fuselage Main, Plate/SkinSDR 0501059996Coalescer Bag · dirtyDURING INITIAL DESCENT AT ABOUT 1000 FPM, THE CABIN BEGAN A RAPID CLIMB OF OVER 1500 FPM. COM PROCEDURES WERE COMPLIED WITH BUT DID NOT HELP. WITH CABIN ALTITUDE CLIMBING ABOVE 10,000, CREW DONNED OXYGEN MASKS, DECLARED AN EMERGENCY, AND PERFORMED A RAPID DEJul 16, 2005 · N8932E · Doug DC931 · Humidity Control SystemSDR 0501029959Slide · malfunctionedDUE TO WEATHER EN ROUTE, AIRCRAFT DIVERTED. WHILE ON GROUND, PERSONNEL ATTEMPTED TO LOWER AFT STAIRWAY, INSTEAD THEY INADVERTENTLY RELEASED TAIL CONE. EMERGENCY ESCAPE SLIDE FOR TAIL DID NOT DEPLOY WHEN TAIL CONE SEPARATED FROM AIRCRAFT. VELCRO CLOSURE AND LJul 15, 2005 · N919RW · Doug DC931 · Escape SlideSDR ABXA050166Angle · crackedLEFT DORSAL FIN ATTACH ANGLE CRACKED DURING ROUTINE LINE MAINTENANCE. REPAIRED IAW EA53420010-103 FOR ANGLE REPLACEMENT.Jul 8, 2005 · N943AX · Doug DC931 · Vertical Stabilizer, Attach FittingsSDR 0500959996Tube · failedDURING THE TAKEOFF ROLL, THE NR 1 ENGINE EPR INDICATION ROLLED BACK. THE TAKEOFF WAS ABORTED AT 120KTS. MAINTENANCE FOUND A FAILED TUBE IN THE PT7 MANIFOLD. THE TUBE WAS REPLACED AND THE LEAK CHECK WAS GOOD.Jun 23, 2005 · N8932E · Doug DC931 · Engine Pressure Ratio (EPR)SDR ABXA050158Relay · malfunctionedNOSE LANDING GEAR LIGHTS DID NOT ILLUMINATE. UNSAFE LIGHT WAS OUT. CYCLED GEAR WITH THE SAME RESULT. WIGGLED GEAR HANDLE AND NOSE LIGHT ILLUMINATED NORMAL. REMOVED AND REPLACED RELAY R2-28. SWUNG GEAR IAW DC-9 ADJ/TEST 32-60-00-2-0201. OPS CHECKED GOOD.Jun 23, 2005 · N929AX · Doug DC931 · Landing Gear Position and WarningSDR 0500929915Pressure System · malfunctionedLEVEL AT FL 340, FLIGHT WAS DIVERTED DUE TO WEATHER. RED MASTER WARNING AND CABIN PRESS LIGHTS ILLUMINATED AS CABIN ALTITUDE CLIMBING THROUGH 10,000 FT. COM PROCEDURES COMPLIED WITH BUT DID NOT HELP. CREW INITIATED RAPID DESCENT AND DECLARED EMERGENCY. CABJun 20, 2005 · N965N · Doug DC931 · Cabin Pressure Control SystemSDR ABXA050151Wire · brokenRT MAIN GEAR DOWN INDICATION "GREEN LIGHT" INTERMITTENT. CHECKED WITH ALT MAIN GEAR INDICATION. SHOWED GEAR DOWN. DID A MISSED APPROACH AND DECLARED AN EMERGENCY. VERIFIED NO RIGHT GEAR INDICATION, ALT SYS GOOD, FOUND CORROSION ON SWITCH S1-184 AND CONNECTJun 10, 2005 · N908AX · Doug DC931 · Landing Gear System WiringSDR ABXA050145Bulb · failedGEAR DOOR OPEN LIGHT DID NOT ILLUMINATE BEFORE EXTENSION OF LANDING GEAR. NORMAL OPERATION OF LANDING GEAR SYSTEM OCCURRED (3 GREEN, GOOD HYDRAULICS). EMERGENCY CALLED, CREW DID FLY BY TOWER TO VERIFY GEAR DOWN AND DOORS UP. INSPECTED GEAR DOOR SWITCHES ANDJun 8, 2005 · N946AX · Doug DC931 · Landing Gear Position and WarningSDR ABXA050144Annunciator · malfunctionedAFTER EMERGENCY POWER CHECK, LOWER CARGO FIRE, TAIL COMP TEMP HIGH, APU FIRE, AND DC EMERGENCY BUSS OFF LIGHTS ILLUMINATED. REMOVED AND REPLACED ANNUNCIATOR PANEL. OPS CHECKED GOOD IAW DC-9 AMM 31-03-00-2-0002.Jun 6, 2005 · N907AX · Doug DC931 · Central WarningSDR 0500869952Flap System · out of rigACFT BEING CONFIGURED FOR LANDING AND ONCE FLAPS EXTENDED PAST 25 DEGREES ACFT ROLLED TO RIGHT. CREW DID NOT NOTICE ANY UNCOMMANDED AIRCRAFT MOVEMENTS WHEN FLAPS WERE INITIALLY LOWERED, ONLY AFTER THE 25 DEGREE DOWN SETTING. FLIGHT CREW STABILIZED ACFT FOR REJun 5, 2005 · N916RW · Doug DC931 · Trailing Edge Flap Control SystemSDR ABXA050143Controller · defectiveAT 5000 FT. LOST CABIN PRESSURE. BOTH BLUE LIGHTS ON PRESSURE CONTROLLER ON. DID ABNORMAL, COULD NOT REGAIN CABIN CONTROL. REMOVED AND REPLACED NR 2 CABIN PRESSURE CONTROLLER AND PERFORMED OPS CHECK IAW DC-9 AMM 21-32-00. OPS CHECKED GOOD.Jun 3, 2005 · N943AX · Doug DC931 · Cabin Pressure ControllerSDR ABXA050149Bulkhead · crackedLEFT BULKHEAD SPAR STUB (HORIZONTAL WEB) AT FS 1039 APPROX LONGERON 15 LEFT CRACKED ON BOTTOM COMING FROM INBOARD FORWARD BOLT HOLE. STOP DRILLED/REPAIRED IAW DC-9 SRM 53-01.Jun 1, 2005 · N947AX · Doug DC931 · Fuselage Main, BulkheadSDR ABXA050153Pan · crackedPASSENGER ENTRY DOOR PAN CRACKED IN 3 LOCATIONS ON FORWARD SIDE, 2 EACH 5 INCH CRACKS, 1 EACH 2 INCH CRACK. REMOVED AND REPLACED MAIN ENTRY DOOR IAW DC-9 MM 52-11-00-5-001.May 31, 2005 · N947AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA050150Pan · crackedPASSENGER ENTRY DOOR PAN CRACKED IN 3 LOCATIONS ON FORWARD SIDE. REMOVED AND REPLACED MAIN ENTRY DOOR IAW DC-9 MM 52-11-00-5-001. WORK ACCOMPLISHED ON NON ROUTINE 0311. (2 EACH - 5 INCH CRACKS, 1 EACH - 2 INCH CRACKS).May 31, 2005 · N947AX · Doug DC931 · Passenger/Crew DoorsSDR ABXA050148Pan · crackedPASSENGER ENTRY DOOR PAN CRACKED ABOVE UPPER DOOR HINGE MOUNT APPROX 3 INCHES EMANATING FROM PREVIOUS REPAIR. REPLACED DOOR ON NON ROUTINE 0311 AND IAW DC-9 MM.May 31, 2005 · N947AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA050147Floor Support · corrodedSTA 218 FLOOR SUPPORT HAD INTERGRANULAR CORROSION ON LOWER SIDE. REMOVED AND REPLACED FLOOR SUPPORT IAW DC-9 SRM 51-30-5.May 27, 2005 · N947AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA050146Door · crackedLT MAIN ENTRY DOOR FORWARD UPPER CORNER APPEARED TO BE CRACKED. DOOR REPLACED ON NON ROUTINE 0311, IAW DC-9 MM.May 27, 2005 · N947AX · Doug DC931 · Passenger/Crew DoorsSDR 0500799977Clamp · separatedDURING CRUISE AT FL330, THE AIRCRAFT LOST CABIN AUTO PRESSURIZATION AND CREW COULD NOT MAINTAIN IT IN MANUAL EITHER. FLIGHT PERFORMED AN EMERGENCY DESCENT TO 10,000 FEET AND DIVERTED TO A NORMAL SAFE LANDING AT ATL. CABIN ALTITUDE MADE IT TO 12,000 FT DURINGMay 25, 2005 · N9341 · Doug DC931 · Humidity Control SystemSDR ABXA050134Angle · crackedCRACKED VERTICAL ANGLE BELOW RIGHT BUTT LINE 44 TRACK AT STA 617 FLOORBEAM. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-5.May 18, 2005 · N906AX · Doug DC931 · Fuselage Main, Attach FittingsSDR ABXA050133Frame · crackedRIGHT CENTER MAIN FRAME AT STA 718 REQUIRES REPLACEMENT PER DC-9 SERVICE BULLETIN 53-100, PAGE 11, ITEM 1E. REMOVED AND REPLACED MAIN FRAME AT STA 718 IAW EA 53400324-001-2.May 17, 2005 · N906AX · Doug DC931 · Fuselage Main, FrameSDR ABXA050131Support · brokenFLOOR TRACK SUPPORT BROKE OFF BETWEEN LONGERON 28 RIGHT, LONGERON 27 RIGHT, AFT OF CARGO DOOR. FABRICATED NEW SUPPORT AND REPAIRED AREA IAW DC-9 SRM 51-30-2.May 16, 2005 · N906AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA050132Web · crackedCRACK INSIDE PYLON UNDER PANEL 8206. REPAIRED CRACK IAW DC-9 SRM 54-01.May 16, 2005 · N906AX · Doug DC931 · Nacelle/Pylon Miscellaneous StructureSDR ABXA050107Fuel Cap · defectiveAFTER TAKEOFF, TOWER ADVISED FUEL VENTING FROM LEFT WING. AIR TURNBACK, MADE RETURN TO ILN. LOST 1000 LBS OF FUEL IN FLIGHT. EMERGENCY DECLARED BY TOWER. FOUND LEFT OVER THE WING FILL CAP POPPED. CAP FOUND TO BE NOT LOCKING. REMOVED AND REPLACED LEFT OVEMay 12, 2005 · N946AX · Doug DC931 · Fuel StorageSDR ABXA050119Stop Fitting · crackedSTOP FITTING CRACKED FOR FORWARD LOWER CARGO DOOR JAMB TOP FORWARD FITTING. REPLACED FORWARD LOWER CARGO DOOR JAMB STOP FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.May 10, 2005 · N946AX · Doug DC931 · Fuselage Main, StructureSDR 0500709989Water Separator · damagedDURING CLIMBOUT AT ABOUT 600 FEET THE FLIGHT ATTENDANT NOTIFIED THE COCKPIT THAT THE CABIN HAD SMOKE COMING OUT OF ALL VENTS AND ITS ACCOMPANIED BY AN ACRID SMELL. THE FLIGHT RETURNED TO AN UNEVENTFULL LANDING BACK AT MSP. NO MENTION OF COM PROCEDURE COMPLIAMay 7, 2005 · N8945E · Doug DC931 · Humidity Control SystemSDR ABXA050118Pan · crackedFORWARD LOWER CARGO DOOR PAN FLANGE CRACKED AFT LATCH POSITION. REPAIRED AREA IAW DC-9 SRM 52-05.May 4, 2005 · N946AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA050117Seat Track · corrodedHEAVILY CORRODED CENTER SEAT TRACK STA 214. CENTER SEAT TRACK REMOVED AND REPLACED ON JC 0281 IAW DC-9 SRM.May 4, 2005 · N946AX · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA050115Skin · crackedVERTICAL STAB JUST ABOVE AFT TIP OF RUDDER, LEFT SIDE, CRACKED AND MISSING FASTENERS. REPAIRED AREA IAW DC-9 SRM 55-01.May 3, 2005 · N946AX · Doug DC931 · Vertical Stabilizer, Plate/SkinSDR ABXA050116Bracket · crackedFRAME BRACKET CRACKED AND CORRODED AT STA 389, LONGERON 29 - 28 LEFT. REMOVED AND REPLACED BRACKET IAW DC-9 SRM 51-30-5.May 3, 2005 · N946AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA050114Structure · corrodedRIGHT FLAP NR 2 TRAILING EDGE SECTION HAD BULGING RIVETS ON THE LOWER SURFACE AT THE OUTBOARD AFT CORNER. REPAIRED AREA IAW DC-9 SRM.May 2, 2005 · N946AX · Doug DC931 · Trailing Edge FlapsSDR 0500609944Control Cable · out of rigUPON SLAT EXTENSION FOR LANDING AT MBS, THE AIRCRAFT ROLLED SLIGHTLY AND THE "SLAT DISAGREEMENT" LIGHT ILLUMINATED. PER VISUAL CHECK, BOTH WINGS SLATS DID EXTEND BUT THE RIGHT WING WAS NOT AS FAR AS THE LEFT SIDE. COMPLIED WITH COM PROCEDURES, AN EMERGENCY WASApr 22, 2005 · N1309T · Doug DC931 · Leading Edge Slat Control SystemSDR 0500769968Cusp Web · crackedDURING "M" CHECK, FOUND CRACK IN RT CUSP WEB AT BS 834. REPAIRED PER EA 99-203527.Apr 14, 2005 · N9332 · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA050091Switch · defectiveON APPROACH, NOSE GEAR SAFE FAILED TO ILLUMINATE. RAN ABNORMAL, GEAR RECYCLE, LANDED WITHOUT PROBLEM. VERIFIED WORN PADDLE ON NOSE LANDING GEAR DOWN SWITCH. REMOVED AND REPLACED GEAR DOWN SWITCH IAW DC-9 MM 32-60-01-2-0101. OPS CHECKED GOOD.Apr 14, 2005 · N924AX · Doug DC931 · Landing Gear Position and WarningSDR 0500449943Boot · blownWHILE CRUISING AT FL330, THE RED CABIN PRESS ANNUNCIATOR LIGHT ILLUMINATED AS THE CABIN WAS CLIMBING THROUGH 11,000 FEET. AN EMERGENCY DESCENT WAS EXECUTED AND COMPLIED WITH COM PROCEDURES. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENApr 2, 2005 · N1308T · Doug DC931 · Humidity Control SystemSDR 0500439943Line · looseDURING CRUISE AT FL350, THE RED CABIN PRESS ANNUNCIATOR LIGHT ILLUMINATED. CREW COMPLIED WITH COM AND PERFORMED AN EMERGENCY DESCENT AND DIVERTED TO A NORMAL SAFE LANDING AT DFW. MASKS DID NOT DEPLOY. MAINTENANCE BITE OF THE SYSTEM SHOWED NR 2 CONTROLLER FAApr 2, 2005 · N1308T · Doug DC931 · Cabin Pressure Control SystemSDR 0500469954Frame · corrodedDURING M-CHECK FOUND CORROSION ON FRAME AT BS 996. REPAIRED PER EA 99-203328.Mar 29, 2005 · N921RW · Doug DC931 · Fuselage Main, FrameSDR 0500379954Longeron · corrodedDURING M-CHECK FOUND CORROSION FROM BS 737-756 ON LONGERON 29L. REPAIRED PER EA 99-203145.Mar 8, 2005 · N921RW · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA050073Web · crackedSTA 1038 BULKHEAD AT LONGERON 13 LEFT WAS CRACKED AT LIGHTENING HOLE. REPAIRED IAW DC-9 SRM 53-01.Mar 8, 2005 · N949AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA050069Longeron · corrodedLONGERON 30 AT STA 945 WAS CORRODED BEYOND LIMITS. REPLACED LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2.Mar 8, 2005 · N945AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA050070Skin · crackedDURING ROUTINE LINE MAINTENANCE AT ILN, FOUND THE FUSELAGE SKIN CRACKED 1 INCH LONG AT STA 897 AND LONGERON 29 RT. SKIN WAS FOUND TO BE CORRODED BEYOND LIMITS ON THE INTERIOR SURFACE UNDER LONGERON 30. INSTALLED SKIN SPLICE, REPAIRED IAW DC-9 SRM 53-04 FIG 1Mar 8, 2005 · N945AX · Doug DC931 · Fuselage Main, Plate/SkinSDR ABXA050072Frame · crackedFRAME CRACKED FS 889 AT LONGERON 29 LEFT. REPAIRED CRACKED FRAME FLANGE IAW DC-9 SRM DWG K05159.Mar 7, 2005 · N949AX · Doug DC931 · Fuselage Main, FrameSDR ABXA050038Warning System · malfunctionedGEAR DOOR OPEN LIGHT DID NOT GO OUT AFTER EXTENDING ON APPROACH TO ILN, WENT ON MISSED APPROACH. RECYCLED GEAR AND LIGHT WENT OUT. CYCLED GEAR DOORS SEVERAL TIMES, LIGHT OPS CHECKED GOOD IAW DC-9 MM 32-30-00.Mar 2, 2005 · N947AX · Doug DC931 · Landing Gear Position and WarningSDR ABXA050030Tube · brokenNR 1 ENGINE FLAME-OUT DURING CLIMB AT 7,000 FT. OIL PRESSURE STAYED ABOVE 10 PSI FOR APPROXIMATELY 20 MINUTES DURING WINDMILLING AFTER FLAME-OUT. AIR TURNBACK TO ILN. ACCOMPLISHED TROUBLESHOOTING PER P&W MM FOR FLAME-OUT, INSPECTED INLET AND EXHAUST AREAS. Feb 17, 2005 · N937AX · Doug DC931 · Turbine Engine Oil System
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