Douglas DC-9-31

Service difficulty reports · 7,433

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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"

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SDR GTIA9900946Slide · detachedDTW - FLT 546 - SLIDE PACK FELL OFF GALLEY SERVICE DOOR (TWICE) R1. RE-INSTALLED ESCAPE SLIDE ON R1 DOOR IAW DC-9 MM 25-61. (X)Jul 1, 1999 · N132NK · Doug DC931 · Emergency EquipmentSDR GTIA9900937Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERIES POWER PACK ASSEMBLY. OPERATION CHECKS GOOD. (X)Jul 1, 1999 · N928ML · Doug DC931 · Emergency LightingSDR USAAD99087Engine · failedATL/PIT - FLT 7880 - AFTER ROTATION, THE LEFT ENGINE EGT CONTINUED TO CLIMB TO 600 DEGREES CELSIUS BEFORE ROLLING BACK. THE CREW REDUCED POWER WHEN THE ENGINE EXPERIENCED A COMPRESSOR STALL. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAJun 30, 1999 · N958VJ · Doug DC931 · Engine (Turbine/Turboprop)SDR ABXA990559Tab · delaminatedDURING C-CHECK, FOUND RUDDER TRIM TAB DELAMINATED. REPLACED RUDDER TRIM TAB IAW DC9 MM 27-20-2.Jun 30, 1999 · N941AX · Doug DC931 · Rudder, Tab StructureSDR TWAA9909605Skin · crackedDURING OP 16 MAINT CHECK, FOUND CRACK APPROXIMATELY 1 INCH AT TOP OF WING LEADING EDGE AT APPROXIMATELY 18 IN OTBD OF NR 7 LEADING EDGE SLAT TRACK. REPAIRED PER SRM 57-06A.Jun 29, 1999 · N979Z · Doug DC931 · Wing, Plate/SkinSDR 9902319947Sensor · malfunctionedDURING APPROACH INTO DTW, THE LEFT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR EXTENSION. CREW EXECUTED GO-AROUND PROCEDURES AND TOWER VERIFIED GEAR TO BE DOWN. EMERGENCY WAS DECLARED AND ALTERNATE GEAR EXTENSION PROCEDURES WERE UTILIZED AS A PRECAJun 29, 1999 · N8938E · Doug DC931 · Landing Gear Position and WarningSDR 9902349928Bolt · looseNOSE LANDING GEAR WOULD NOT EXTEND ON LANDING INTO MSP. CREW UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RETIGHTENED BOLT IN OVERCENTER ARM. OPERATIONAL CHECK NORMAL ON GEAR SWING. AIRCRAFT RETURNED TO SERJun 27, 1999 · N8921E · Doug DC931 · Landing Gear Retraction/Extension SystemSDR TWAA9908901Wire · wornTHE FORWARD SECTION OF THE COACH CABIN FLOOR EGRESS LIGHTS WAS INOPERATIVE. FOUND A HOLE IN THE FEEDER CABLE. REPLACED THE FEEDER CABLE FROM THE POWER SUPPLY TO THE LIGHT STRIP AT ROW 14. CHECK-C 11-13-98 STL.Jun 26, 1999 · N977Z · Doug DC931 · Light System WiringSDR TWAA9908902Battyery Pack · dischargedTHE EGRESS FLOOR LIGHTS WERE INOPERATIVE FROM ROW 21 TO ROW 24, AND THE LEFT AND RIGHT OVERWING EXIT SIGNS WERE INOPERATIVE AT ROW 15. REPLACED THE BATTERY PACK (P/N 5822-2) FOR THE EGRESS LIGHTS, AND THE BATTERIES (P/N 41B004AD07G3) FOR THE EXIT SIGNS. CHECJun 25, 1999 · N984Z · Doug DC931 · Emergency LightingSDR 9902339928Spring · brokenDURING APPROACH INTO MSP, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR BUNGEE SPRINGS. OPERATIONAL CHECK NORMAL ON GEAJun 25, 1999 · N8921E · Doug DC931 · Landing Gear Retraction/Extension SystemSDR USAAD99086Controller · failedLGA-GSO - FLT 1621 - AFTER TAKEOFF, THE RIGHT AIR CONDITIONING PACK DUCT TEMP INCREASED TO AVOVE 150 DEGREES, CAUSING THE LAVATORY SMOKE DETECTORS TO ACTIVATE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE RIGHT AIR CJun 24, 1999 · N977VJ · Doug DC931 · Cabin Temperature ControllerSDR ABXA9900558Panel · corrodedDURING C-CHECK, FOUND LEFT WING UPPER TRAILING EDGE PANEL AT STATION XRS 111.500. REPLACED PANEL IAW DC9 SRM 51-30-1 AND 51-10-4.Jun 24, 1999 · N941AX · Doug DC931 · Wing, Plate/SkinSDR 9902329928Spring · brokenNOSE LANDING GEAR WOULD NOT EXTEND ON LANDING. FLIGHT CREW PERFORMED EMERGENCY GEAR EXTENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT NOSE GEAR DOOR CABLE SPRING BROKEN. REPLACED SPRING. OPERATIONAL CHECK NORMAL ON GEAR SWINJun 24, 1999 · N8921E · Doug DC931 · Landing Gear Door Retract SectionSDR TWAA9908905Angle · crackedDURING OP 16 MAINT CHECK, FOUND COCKPIT CENTER FRAME ANGLE 9911505-7 WAS CRACKED APPROXIMATELY 1.5 INCH IN RADIUS AT I/B END STA 83.55, X=10.00, Z=42, ON LT SIDE. INSTALLED NEW FRAME PER ITEM 30 OF EMLR 69590.Jun 23, 1999 · N981Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9908904Bulkhead Brace · crackedDURING OP 16 MAINT CHECK, FOUND AFT PRESSURE BULKHEAD, FORWARD SIDE DIAGIONAL BRACE ON PRESSURE BULKHEAD AT STA 996, CRACKED AT UPPER END BETWEEN LONGERON 3L AND 4L. REMOVED, FABRICATED AND REINSTALLED ANGLE AT UPPER DIAGONAL BRACE, STA 996 BETWEEN L3L ANG L4Jun 23, 1999 · N979Z · Doug DC931 · Fuselage Main, BulkheadSDR TWAA9908903Stiffener · crackedDURING OP 16 MAINT CHECK, FOUND COCKPIT VERTICAL STIFFENER NUMBER 9911503-167 WAS CRACKED IN THE RADIUS APPROXIMATELY 1.5 INCH LONG, APPROX 2 INCHES BELOW TOP OF STIFFENER AT STA 69.5, AFT SIDE OF BULKHEAD ON X=-12 ON RT SIDE. MADE UP DOUBLER AND INSTALLED PEJun 23, 1999 · N979Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9908909Frame · crackedDURING OP 16 MAINT CHECK, FOUND COCKPIT FRAME 5 ON LT SIDE WAS CRACKED IN RADIUS AT X=+10 CONFIRMED WITH EDDY CURRENT. CRACK WAS APPROXIMATELY .75 INCH LONG AT STA 83.55. REPAIRED PER SRM 53-03 FIG 34, SHEETS 1 TO 7.Jun 22, 1999 · N981Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9908908Frame · crackedDURING OP 16 MAINT CHECK, FOUND COCKPIT FRAME CRACKED AT STA 83.55, X=-11 INCHES, APPROXIMATELY 1.5 INCHES LONG ON RT SIDE. REPAIRED PER SRM 53-03, FIG 34 SHEET 1 TO 7.Jun 22, 1999 · N981Z · Doug DC931 · Fuselage Main, FrameSDR TWAA9908601Longeron · crackedDURING OP 16 MAINT CHECK, FOUND CRACK AT LONGERON TO FRAME FASTENERS AT STA 200, LONGERON 2L. SPLICED IN NEW LONGERON PER SRM 53-02, PAGES 48 TO 53, FROM STA 190 TO 228.Jun 22, 1999 · N981Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA9900524Pan · crackedDURING C-CHECK, FOUND SERVICE DOOR PAN CRACKED. REPAIRED IAW DC9 SRM 52-03-00 AND 51-30-1.Jun 22, 1999 · N941AX · Doug DC931 · Service DoorsSDR ABXA9900523Longeron · crackedDURING C-CHECK, FOUND LONGERON 13 RIGHT CRACKED AT STATION 965. REPLACED LONGERON SECTION IAW DC9 SRM 53-02-0.Jun 22, 1999 · N941AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAAD99084Battery · dischargedTHE SERVICE DOOR SLIDE EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE SERVICE DOOR SLIDE EMERGENCY LIGHT BATTERY. (X)Jun 21, 1999 · N976VJ · Doug DC931 · Emergency LightingSDR USAAD99083Battery · dischargedDAY - THE LEFT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE LEFT NACELLE EMERGENCY LIGHT. (X)Jun 21, 1999 · N982VJ · Doug DC931 · Emergency LightingSDR ABXA9900526Panel · delaminatedDURING C-CHECK, FOUND RIGHT WING TRAILING EDGE UPPER HONEYCOMB PANEL DELAMINATED. REPLACED PANEL IAW DC9 SRM 51-30-1.Jun 21, 1999 · N941AX · Doug DC931 · Wing, Plate/SkinSDR ABXA9900525Frame · crackedDURING C-CHECK, FOUND MAIN FRAME CRACKED IN UPPER CARGO COMPARTMENT. REPAIRED IAW DC9 S/B 53-131 AND DWG 5935650-503.Jun 21, 1999 · N941AX · Doug DC931 · Fuselage Main, FrameSDR 9902639975Intercostal · crackedDURING PERIODIC CHECK, FOUND INTERCOSTAL 9911557-3 AT FS 154, LONGERON 14R CRACKED. REPAIRED PER EA 99-164421.Jun 21, 1999 · N9339 · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9908910Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND STA 200 FLOORBEAM CAP CORRODED JUST OUTBOARD OF NUMBER 4 CHAIR TRACK. REPAIRED FLOORBEAM PER SRM 53-05, PAGE 31.Jun 18, 1999 · N981Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA9908501Battery Pack · dischargedFOUND CABIN EGRESS LIGHTS INOPERATIVE FROM ROW 7 TO 14, AND ROW 22 TO AFT CABIN. ACCOMPLISHED A SPLICE TO A CUT FEEDER CABLE FOR ROWS 7 TO 9. REPLACED A FLEX FEEDER LINE (P/N 5853-1) FOR ROW 9 TO 14, AND REPLACED THE BATTER PACK FOR THE AFT CABIN. CHECK-C 6Jun 18, 1999 · N989Z · Doug DC931 · Emergency LightingSDR 9902089962Mechanism · not latchedVIBRATION FROM NOSE GEAR AREA OCCURRED AFTER GEAR RETRACTION ON TAKEOFF. CREW RECYCLED GEAR WITH SAME RESULTS. FLIGHT WAS RETURNED TO DFW AND LANDED WITHOUT INCIDENT. CREW DECLARED AN EMERGENCY DUE TO OVERWEIGHT LANDING CONDTIONS. MAINTENANCE FOUND RIGHT NJun 18, 1999 · N914RW · Doug DC931 · Landing Gear Door Retract SectionSDR TWAA9908907Support · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT NUMBER 2 SEAT TRACK TO CENTERLINE, STA 200. REPLACED FLOOR SUPPORT PER SPM 6-70-01, PAGE 3.Jun 17, 1999 · N981Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9908906Support · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STA 200, BETWEEN NUMBER 1 AND 2 SEAT TRACKS. REPLACED FLOOR SUPPORT PER STD PROCESSES MANUAL 6-70-01, PAGE 3.Jun 17, 1999 · N981Z · Doug DC931 · Fuselage Miscellaneous StructureSDR 9902659975Pax Door · crackedDURING PERIODIC CHECK, FOUND .375 INCH CRACK AT UPPER FORWARD CORNER OF PASSENGER DOOR JAMB, FS 160. REPAIRED PER EA 99-164408. (P/N 5911406-5).Jun 16, 1999 · N9339 · Doug DC931 · Passenger/Crew DoorsSDR USAAD99081Battery · dischargedIND - THE FORWARD ENTRY DOOR EMERGENCY LIGHT WAS DIM. MAINTENANCE REPLACED THE BATTERY FOR THE FORWARD ENTRY DOOR EMERGENCY LIGHT. (M)Jun 15, 1999 · N997VJ · Doug DC931 · Emergency LightingSDR TWAA9909601Longeron · crackedDURING OP 16 MAINT CHECK, FOUND A CRACK IN LONGERON 5R, APPROXIMATELY .75 INCH LONG THROUGH RIVET STA 679. REPAIRED PER DRAWING SR09530128.Jun 15, 1999 · N979Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 9902689975Intercostal · crackedDURING PERIODIC CHECK, FOUND .5 INCH CRACK AT INTERCOSTAL 99-15551-11. REPAIRED PER EA 99-164404.Jun 14, 1999 · N9339 · Doug DC931 · Fuselage Main, KeelSDR USAAD99080Battery Pack · dischargedIND - THE TAILCONE OVERHEAD EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND BATTERIES. (M)Jun 13, 1999 · N926VJ · Doug DC931 · Emergency LightingSDR USAAD99079Valve · leakingPIT-DAY - FLT 827 - AFTER TAKEOFF THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. THE LIGHT WENT OUT WHEN THE THROTTLE WAS REDUCED, BUT WITH INCREASE IN POWER THE LIGHT CAME BACK ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENAJun 12, 1999 · N997VJ · Doug DC931 · Pneumatic Distribution SystemSDR EISA99136Light · brokenFORWARD RED EMERGENCY LIGHT ON FLOOR LIGHTING BROKEN. REINSTALLED HOUSING ON FORWARD RED EMERGENCY LIGHT ON FLOOR IAW MM CHAPTER 33-53-0. OPS CHECKED GOOD. (M)Jun 12, 1999 · N943VJ · Doug DC931 · Emergency LightingSDR EISA99134Fuel Pump · failedRIGHT ENGINE FAILED NEAR V2 SPEED 115 KNOTS FOLLOWING NORMAL TAKEOFF. REMOVED AND REPLACED FUEL PUMP, ENGINE DRIVEN IAW MM 73-10-1 AND 73-20-1. LEAK CHECK AND TRIM PER 71-00-0. (M)Jun 12, 1999 · N945VJ · Doug DC931 · Engine Fuel PumpSDR 99ZZZM383Duct · leakingPIT-DAY - FLT 827 - AFTER TAKEOFF THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. THE LIGHT WENT OUT WHEN THE THROTTLE WAS REDUCED, BUT WITH INCREASE IN POWER THE LIGHT CAME BACK ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENAJun 12, 1999 · N997VJ · Doug DC931 · Pneumatic Distribution SystemSDR ABXA9900433Frame · crackedDURING C-CHECK, FOUND LEFT MAIN FRAME STATION 699 CRACKED. REPLACED LEFT MAIN FRAME IAW DC9 SRM 51-30-2 AND 51-30-1.Jun 9, 1999 · N936AX · Doug DC931 · Fuselage Main, FrameSDR USAAD99077Battery Charger · inoperativeIND - FOUND AFT SECTION OF EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER (INOPERATIVE) AND THE BATTERY PACK. (M)Jun 8, 1999 · N934VJ · Doug DC931 · Emergency LightingSDR ABXA9900416Pan · crackedDURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR PAN CRACKED. REPAIRED IAW DC9 SRM 52-03 AND 51-30-1.Jun 8, 1999 · N936AX · Doug DC931 · Cargo/Baggage DoorsSDR USAAD99078Battery · dischargedIND- FOUND SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)Jun 7, 1999 · N928VJ · Doug DC931 · Emergency LightingSDR TWAA9908101Pump · failedTHE RT ENGINE SHUT ITSELF DOWN DURING TAKEOFF. THE FLIGHT RETURNED TO SDF. REPLACED THE ENGINE FUEL PUMP DUE TO SHEARED SHAFT. ALSO, REPLACED THE FUEL CONTROL PRECAUTIONARY, (P/N 743602-5). CHECK-C 9-21-98 STL.Jun 7, 1999 · N990Z · Doug DC931 · Engine Fuel PumpSDR EISA99126Slide · failedFOUND TAILCONE SLIDE WILL NOT HOLD CHARGE. REPLACED TAILCONE SLIDE PER MM 25-62. (M)Jun 7, 1999 · N945VJ · Doug DC931 · Escape SlideSDR ABXA9900403Longeron · crackedDURING C-CHECK, FOUND LONGERON 26 LEFT CRACKED AT STATION 945. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2.Jun 7, 1999 · N936AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR 9902039956Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL.Jun 7, 1999 · N923RW · Doug DC931 · Emergency LightingSDR EISA99125Battery · dischargedGALLEY EMERGENCY SLIDE PACK LIGHT INOPERABLE. REMOVED AND REPLACED GALLEY DOOR EMERGENCY SLIDE PACK LIGHT BATTERY. (M)Jun 5, 1999 · N943VJ · Doug DC931 · Emergency LightingSDR USAA99089Longeron · crackedPIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK IN LONGERON 5 LT AT STATION 680. CUT OUT DAMAGED SECTION AND INSTALLED LONGERON REPAIR SECTION AND SPLICES PER SRM 53-02 FIG 18. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, Longeron/Stringer
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