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 USAAD00016Charger · failedLGA - THE CEILING EMERGENCY LIGHTS IN THE FIRST CLASS PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD CEILING EMERGENCY LIGHT BATTERY CHARGER. (M)Jan 23, 2000 · N923VJ · Doug DC931 · Emergency LightingSDR 0000229906Wire · failedEMERGENCY LIGHT ARM AND CHARGE CIRCUIT BREAKER POPPED. MAINTENANCE REPAIRED SHORTED WIRING AT CLAMP IN TAIL COMPARTMENT. OPERATIONAL CHECK NORMAL.Jan 23, 2000 · N956N · Doug DC931 · Light System WiringSDR 0000549927Angle · crackedCRACK IN UPPER FASTENER OF LEFT VERTICAL ATTACH ANGLE AT BS 1095. REPAIRED PER EA 99-172131.Jan 22, 2000 · N8920E · Doug DC931 · Fuselage Main, FrameSDR USAAD00014Rod · brokenPIT-BOS - FLT 1962 - AFTER TAKEOFF AND GEAR RETRACTION, CREW RECEIVED LEFT MLG DOOR UNSAFE LIGHT. CREW FOLLOWED CHECKLIST. FLIGHT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GEAR DOOR FOLLOW-UP SYSTEM DRIVE ROD AND THE LJan 22, 2000 · N920VJ · Doug DC931 · Landing Gear Door Retract SectionSDR TWAA0001605Floor Panel · corrodedDURING OP 16 MAINT CHECK FOUND CABIN FLOOR PANEL 71 CORRODED. MADE NEW FLOOR PANEL PER SSRM 53-00-104 PAGE 201.Jan 21, 2000 · N989Z · Doug DC931 · Fuselage Floor PanelSDR TWAA0001604Door Jam · corrodedDURING OP 16 MAINT CHECK THE AFT CARGO COMPT DOOR JAM, AFT INTERIOR SURFACE HAD LIGHT CORROSION. REPAIRED DAMAGED SECTION OF WEB AT AFT DOOR JAM PER SRM 53-01 PAGE 18 FIG 4. TREATED AREA AND PARTS PER SRM 51-40-03. INSTALLED FASTENERS PER SRM 51-30, 51-10-4Jan 21, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA000094Beam · corrodedPIT - FOUND BEAM CORRODED IN 2 AREAS, 1 INCH BY 1 INCH. CORROSION LEVEL 1. CUT OUT CORRODED AREAS AND INSTALLED NESTED ANGLE. (M)Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA000096Seat Track · corrodedPIT - LEFT INBOARD SEAT TRACK STATION 237 HAS CORROSION 2 INCH BY 4 INCH. CORROSION LEVEL 1. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. (M)Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR USAA000095Floor Support · corrodedPIT - STATION 160 A/C CENTERLINE RIGHT FLOOR SUPPORT HAS 2 INCH BY 36 INCH CORROSION. LEVEL 1. MANUFACTURE NEW SUPPORT AND INSTALLED. (M)Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA000101Frame · crackedPIT - STA 109.5 CANTED BELTRAME. WEB HAD 3.50 INCH CRACK. BELT FRAME FOUND CRACKED AT BS 109.5. REPAIRED PER EA 53797. (X)Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Main, FrameSDR USAA000099Angle · crackedPIT - LEFT VERTICAL STABILIZER DRAG ANGLE, STA 1104. DRAG ANGLE HAD 2 CRACKS, .75 INCH AND .3750 INCH. DRAG ANGLE FOUND CRACKED ON VERTICAL STABILIZER. CUT OUT DAMAGED AREA AND INSTALLED STRAP PER SRM 53-05 FIG 23A (DASH 505 CONFIG). (X)Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA000098Angle · crackedPIT - REMOVED AND REPLACED VERTICAL STABILIZER DRAG ANGLE, STA 1104. DRAG ANGLE HAD 2 INCH CRACK. DRAG ANGLE FOUND CRACKED ON VERTICAL STABILIZER. STOP DRILLED CRACK ENDS AND INSTALLED REPAIR PER SRM 53-05 FIG 23 AND 23A. (X)Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA000097Bulkhead · crackedPIT - RIGHT SIDE STA 965 BULKHEAD WEB LOWER END, WEB HAD 2 INCH CRACK. BULKHEAD FOUND CRACKED AT BS 965. CUT OUT DAMAGED WEB SECTION AND INSTALLED NEW PER SRM 53-03 FIG 19. (X)Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Main, BulkheadSDR USAA000093Skin · crackedPIT - LONGERON 22L BELOW AIR STAIR, SKIN HAD .25 INCH CRACK. SKIN CRACKED AT BS 180 LONGERON 22L. PERMANENT REPAIR DOUBLER INSTALLED PER SRM 9530219 AND EO 53910467. (X)Jan 20, 2000 · N927VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA0001603Stiffener · crackedDURING OP 16 MAINT CHECK FOUND CRACK IN UPPER END OF VERTICAL STIFFENER AT STA 1019, APU ENCLOSURE LEFT SIDE. REMOVED STIFFENER AND SENT TO WELDING SHOP. STIFFENER WAS WELDED PER INTER-SHOP TICKET 799450. REPLACED STIFFENER WITH HI-LOKS HLT336 PER SRM 51-30Jan 20, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR USAAD00018Battery · dischargedIND - THE SERVICE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS DIM AND THE MAIN ENTRANCE DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE SERVICE AND MAIN ENTRANCE DOORS. (M)Jan 19, 2000 · N922VJ · Doug DC931 · Emergency LightingSDR TWAA0001205Intercostal · crackedDURING OP 16 MAINT CHECK FUSELAGE STA 40, LBL 12 IN, TOP NOSE SKIN AREA, INTERCOSTAL HAD CRACK APPROX 5 IN LONG RUNING ANGULAR. REPLACED 9957899-3 INTERCOSTAL WITH NEW PART PER SRM 51-01, PAGE 1 AND 3; 51-10-04, 51-30 2 AND 3 FOR RIVET AND HILOCK REMOVAL INSTJan 17, 2000 · N989Z · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000010Fire Detector · malfunctionedRIGHT ENGINE LOOP B LIGHT AND ANNUNCIATOR ILLUMINATED. COMPLIED WITH EMERGENCY PROCEDURES, DISCHARGED BOTH FIRE BOTTLES, DECLARED EMERGENCY AND SHUT DOWN RIGHT ENGINE. REPLACED FIRE DETECTOR ELEMENT ON LOOP B RIGHT ENGINE. OPS CHECKED GOOD.Jan 15, 2000 · N948AX · Doug DC931 · Fire DetectionSDR TWAA0001204Floor Panel · crackedDURING OP 16 MAINT CHECK, FLOOR PANEL NUMBER 61 HAD 2 EA CRACKED HAT SECTIONS AT AFT END. REMOVED 4 HAT SECTIONS AND REPLACED WITH 4 NEW HAT SECTIONS PER SSRM 53-00-104, A AND B.Jan 14, 2000 · N989Z · Doug DC931 · Fuselage Floor PanelSDR 0000139944Drag Link · lack of lubeNOSE LANDING GEAR WOULD NOT EXTEND NORMALLY ON APPROACH INTO PWM. FLIGHT WAS DIVERTED TO BOS AND LANDED WITHOUT INCIDENT. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. MAINTENANCE GREASED NOSE GEAR, DRAG LINK, RETRACT CYLINDER, AND BUNGEE. Jan 14, 2000 · N1309T · Doug DC931 · Landing Gear Retraction/Extension SystemSDR ABXA000068Support · crackedDURING C-CHECK, FOUND FLOORBEAM SUPPORT CRACKED STATION 658, RBL 22. REPLACED FLOORBEAM SUPPORT IAW DC9 SRM 51-30-2.Jan 13, 2000 · N942AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA000047Pan · crackedDURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR PAN AND SKIN CRACKED. REPAIRED IAW REA D95235065 AND SRM 52-05 FIGURE 50 SHEET 2.Jan 13, 2000 · N942AX · Doug DC931 · Cargo/Baggage DoorsSDR ABXA000046Frame · crackedDURING C-CHECK, FOUND STATION 737 RT MAIN FRAME CRACKED. REPAIRED CRACK IAW REA D95335059 MR.Jan 13, 2000 · N942AX · Doug DC931 · Fuselage Main, FrameSDR 0000149907Power Supply · failedDURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL.Jan 13, 2000 · N957N · Doug DC931 · Emergency LightingSDR 0000169949Power Supply · failedDURING LINE MAINTENANCE INSPECTION, FOUND CATWALK AND TAILCONE RELEASE HANDLE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL.Jan 12, 2000 · N8928E · Doug DC931 · Emergency LightingSDR TWAA0000915Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT RAIL AT STA 446, WAS BLENDED OUT OF LIMITS. FABRICATED 40 IN SECTION USING OLD FLOOR SUPPORT AS TEMPLATE. INSTALLED WITH RIVETS USING DOUGLAS DRAWING 5956026 FOR SPECS.Jan 11, 2000 · N989Z · Doug DC931 · Fuselage Main, Floor BeamSDR 0000159960Battery Pack · dischargedEMERGENCY LIGHTS IN FORWARD CABIN ILLUMINATED AND WOULD NOT TURN OFF. PROBLEM COULD NOT BE DUPLICATED. BATTERY PACK AND BATTERIES WERE REPLACED. OPERATIONAL CHECK NORMAL.Jan 11, 2000 · N920RW · Doug DC931 · Emergency LightingSDR GTIA000015Lens · missingTPA - EMERGENCY FLOOR PATH LIGHTING FOUND TO HAVE ONE RED LENS COVER AND BULB MISSING AFT OF AIRCRAFT. REPLACED MISSING BULB AND RES LENS COVER TO EMERGENCY EGRESS LIGHTING. OPERATIONAL CHECK PERFORMED FUNCTIONS. (M)Jan 10, 2000 · N934ML · Doug DC931 · Emergency LightingSDR TWAA0000501Actuator · wornAFTER TAKEOFF AT GEAR RETRACTION CAPTAIN NOTED SPARKS COMING FROM CENTER PEDESTAL NEAR HIS RIGHT FOOT. ALSO, NOTICED A BURNING SMELL. FLIGHT RETURNED TO ATL. FOUND THE GROUND SPOILER ACT HAD FAILED. PLACARDED THE ACT PER MEL FOR LATER REPLACEMENT. CHECK-CJan 9, 2000 · N985Z · Doug DC931 · Drag Control ActuatorSDR GTIA000014Light · malfunctionedISP - FLT 432 - EMERGENCY AISLE LIGHTING CAME ON IN FLIGHT AND WOULD NOT GO OUT. OPS CHECK SEVERAL TIMES ON GROUND NO DISCREPANCIES NOTED. (M)Jan 9, 2000 · N934ML · Doug DC931 · Emergency LightingSDR USAAD0006Manifold · rupturedATL/PHL - FLT 561 - AFTER TAKEOFF, THE RIGHT ENGINE A-LOOP ILLUMINATED FOLLOWED LATER BY THE ENGINE FIRE WARNING. AFTER PULLING THE THROTTLE BACK, THE ENGINE FIRE WARNING QUIT AND BOTH FIRE LOOP LIGHTS WENT OUT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED Jan 7, 2000 · N937VJ · Doug DC931 · Engine Bleed Air SystemSDR GTIA000011Light · looseDTW - FORWARD EMERGENCY TRACK LIGHTING STRIP TEMPORARILY SECURED WITH SPEED TAPE. REPLACED EMERGENCY LIGHTING STRIP AND INSTALLED THRESHOLD PLATE IAW DC-9 SRM 51-30-2. (M)Jan 6, 2000 · N934ML · Doug DC931 · Emergency LightingSDR USAAD00005Pump · failedIAD-LGA - FLT 6492 - AFTER TAKEOFF, THE LEFT HYDRAULIC PRESSURE DROPPED TO ZERO WITH NO LOSS OF HYDRAULIC QTY. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP. (M)Jan 5, 2000 · N935VJ · Doug DC931 · Hydraulic Pump (Electric/Engine), MainSDR TWAA0000301Power Supply · inoperativeTHE FIRST CLASS CABIN OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 9-17-99 STL.Jan 5, 2000 · N937F · Doug DC931 · Emergency LightingSDR USAAD00003Connector · loosePHL-ATL - FLT 637 - AFTER TAKEOFF, THE RIGHT ENGINE 'B' FIRE LOOP INDICATED FAILURE AND THE FIRE INDICATION LIGHT WOULD NOT EXTINGUISH. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SECURED THE ELECTRICAL CONNECTOR AT THE RIGHT Jan 2, 2000 · N937VJ · Doug DC931 · Fire DetectionSDR GTIA0000001Placard · missingDTW - FLT 91 - SOME OF THE SEATS THE PLACARDS 'LIFE VEST UNDER SEAT' ARE MISSING. REPLACED MISSING PLACARDS IAW DC9 MM 11-41-00. (M)Jan 2, 2000 · N934ML · Doug DC931 · Placards and MarkingsSDR USAAD00002Linkage · lack of lubeBOS-CLT - FLT 1659 - AFTER TAKEOFF, THE LANDING GEAR LANDING RELEASE BUTTON WAS STILL DETENTED. THE LANDING GEAR WAS RAISED USING THE ALTERNATE METHOD. THE AIRCRAFT FLEW LONG ENOUGH TO PREVENT LANDING OVERWEIGHT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDEJan 1, 2000 · N934VJ · Doug DC931 · Landing Gear Retraction/Extension SystemSDR USAAD00001Battery · dischargedIND - THE LEFT NACELLE SCAN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LEFT NACELLE SCAN EMERGENCY LIGHT BATTERY. (M)Jan 1, 2000 · N924VJ · Doug DC931 · Emergency LightingSDR USAAD99185Engine · failedMKE - FLT 359 - AT FLT LEVEL 2000 FT, SHUTDOWN RIGHT ENGINE DUE TO EXCESSIVE EGT. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO THE FIELD, MAKING A SAFE, UNEVENTFUL LANDING. FOUR MINUTES SINGLE ENGINE TIME. MAINTENANCE REPLACED THE RIGHT ENGINE. (M)Dec 29, 1999 · N929VJ · Doug DC931 · Engine (Turbine/Turboprop)SDR 2000ZZZX355Frame · crackedPIT - DURING A CHECK, FOUND 3 INCH CRACK IN TAIL CONE ATTACH FRAME RT SIDE AT RUDDER ACTUATOR ATTACH POINT. CUT OUT DAMAGE. SPLICED IN SECTION PER DOUGLAS DRAWING 9911843. (X)Dec 29, 1999 · N982VJ · Doug DC931 · Fuselage Main, FrameSDR 9905459906Ecu · failedDURING TAXI INTO IAD, FORWARD CARGO SMOKE DETECTOR LIGHT ILLUMINATED. FLIGHT CREW ACTIVATED FORWARD CARGO BAY FIRE BOTTLE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE OR SMOKE DAMAGE. REPLACED NR 1 CADec 28, 1999 · N956N · Doug DC931 · Fire DetectionSDR USAAD99184Battery · dirtyLGA - FOUND CABIN EMERGENCY FLOOR LIGHTING INOPERATIVE FORWARD OF ROW FIVE. MAINTENANCE CLEANED THE CONNECTOR ON THE BATTERY PACK. (M)Dec 27, 1999 · N920VJ · Doug DC931 · Emergency LightingSDR USAAD99183Slide · dischargedATL - FOUND FORWARD ENTRY DOOR ESCAPE SLIDE PRESSURE BELOW MINIMUMS. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLIDE. (M)Dec 26, 1999 · N963VJ · Doug DC931 · Escape SlideSDR GTIA9901234Wire · damagedMCO - FLT 92 - AFT ENTRY EMERGENCY 'EXIT' SIGN ON LEFT SIDE WALL INOPERATIVE. REPAIRED GROUND WIRE AT AFT ENTRY OVERHEAD. PANEL AND OPS CHECKED GOOD PER MM CHECK 33-50-00. (M)Dec 25, 1999 · N934ML · Doug DC931 · Light System WiringSDR TWAA9917415Door Frame · crackedDURING CHECK-C MAINT, FOUND A FORWARD LT PASSENGER DOOR STOP HOLE, FOURTH HOLE FROM THE TOP ON THE AFT SIDE AND FIFTH FROM THE BOTTOM, AFT SIDE. THE DOOR STOP HOLE HAD A .75 IN CRACK. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND INSTALLED DOUBLER PER EMLR 9Dec 24, 1999 · N988Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9917402Longeron · crackedDURING CHECK-C MAINT, THE AFT END OF LONGERON 2L WAS CRACKED AT STA 1076. COMPLETED LONGERON SPLICE PER SRM 53-02, FIG 8.Dec 24, 1999 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9917401Longeron · crackedDURING CHECK-C MAINT, LONGERON 2R WAS CRACKED AT STA 1076. REPAIRED LONGERON 2R AT STA 1076 PER SRM 53-02, FIG 8.Dec 24, 1999 · N988Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR 9905619961Battery Pack · dischargedDURING PERIODIC CHECK, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.Dec 24, 1999 · N924RW · Doug DC931 · Emergency LightingSDR TWAA9917403Angle · crackedDURING CHECK-C MAINT, THE FUSELAGE TO VERTICAL STAB ATTACH ANGLE WAS CRACKED .875 INCH LONG AT RT SIDE, STA 1121. CRACK IS BEYOND STOP DRILLED HOLES OF LOWER LEG CRACK. REPAIRED PER SRM 53-05, FIG 230. DOUBLER INSTALLED.Dec 23, 1999 · N988Z · Doug DC931 · Vertical StabilizerSDR ABXA9900857Seat · wornCAPTAIN'S SEAT VERTICAL MOVEMENT ADJUSTMENT RELEASES INADVERTENTLY. SEAT SLIDES TO FLOOR WITHOUT ACTUATION. REPLACED CAPTAIN'S SEAT.Dec 21, 1999 · N947AX · Doug DC931 · Flight Compartment Equipment
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