Douglas DC-9-32

Service difficulty reports · 12,755

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC932'
  ORDER BY difficulty_date DESC"

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SDR VJ9800583Structure · corrodedRT KEEL AREA AT FS 680 TO 756 CORRODED. Z ANGLE, L29R, LONGERON AND FITTING CORRODED BEYOND LIMIT. INSTALLED NEW PARTS IAW DC9 SRM 51-30-3, 51-10-4, 51-30-1, 51-30-2, 51-30-5 AND 53-01 FIG 1.Sep 30, 1998 · N924VV · Doug DC932 · Fuselage Main, StructureSDR VJ9800582Skin · crackedDENT 1.5 INCHES BY .038 D/X=35 OUT LIMIT IAW DC9 SRM 53-04 FIG 38, SHEET 10, CONDITION 1B3. CUT OUT DENT, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04, FIG 38, 51-10-4, 51-30-2 AND AIRTRAN RES 981774. REINSTALLED ALL COMPONENTS REMOVED FOR ACCESSep 30, 1998 · N924VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800581Skin · dentedDENT 1.5 INCHES BY .037 D/X=41 AT FS 410.5, L28-29R, AND FS 412.5, L28-29R, OF 1 INCH BY .018 D/X=56 OUT OF LIMIT IAW SRM 53-04, FIG 10. CUT OUT DENT, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW DC9 SRM 51-10-4, 53-01 FIG 4, 51-10-3, 51-30-2 AND -5 PLUSSep 30, 1998 · N924VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800564Skin · creasedCREASE AT FS 522, L28R, APPROXIMATELY 3 BY 5 TIMES .070 INCHES OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38. CUT OUT AREA, REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR AND FINGER DOUBLER IAW DC9 SRM 51-10-2, 53-04, FIG 12, 51-30-2, 51-30-5. 51-10-4 AND AIRTRAN Sep 30, 1998 · N924VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800563Skin · corrodedAFT CARGO SKIN AT FS 937, L28R, CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED NEW DOUBLER IAW DC9 SRM 53-01 FIG 4, 51-30-2 AND AIRTRAN RES 981737.Sep 30, 1998 · N924VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800541Floorbeam · corrodedFLOOR SUPPORT STRUCTURE LEFT OF CENTER LINE CORRODED BEYOND LIMIT IAW DC9 SRM 53-01 FIG 1 AT FS 965, LBL 30. CUT OUT CORRODED SECTION OF FLOORBEAM, FABRICATED AND INSTALLED NEW SECTION IAW DC9 SRM 53-05 FIG 20A.Sep 30, 1998 · N924VV · Doug DC932 · Fuselage Main, Floor BeamSDR VJ9800540Skin · corrodedA DENT, 11 INCHES BY 2.625 TIMES .084 WITH A DEPTH OF .098, FOUND AT FS 351 TO 362 L19 AND 20R. REMOVED AND FORMED NEW SKIN AND SPLICE. DRILLED, COUNTERSUNK, TREATED AND PRIMED. INSTALLED NEW SKIN AND SPLICE IAW DC9 SRM 51-30, 51-10-4, 51-10-3, RES 191745 ASep 30, 1998 · N924VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800539Skin · dentedA DENT, 2 INCHES BY .016 AT FS 436, L27 AND 28R OUT OF LIMIT IAW DC9 SRM 53-04 FIG 38. CUT OUT DENTED AREA, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-01 FIG 4, 51-10-3, 51-30-2 AND RES 191736.Sep 30, 1998 · N924VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800530Skin · dentedCREASED OUT OF LIMITS DENT WAS FOUND AT FS 447 L26 & 27 L 1 1.5 X .068 IAW DC-9 SRM 53-04 FIG 38. FABRICATED AND INSTALLED REPAIR IAW SRM 53-04 FIG 38, 51-10-3 AND DAC NTSPM PART 8.Sep 30, 1998 · N924VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800529Angle · corrodedFLOOR SUPPORT STRUCTURE AT FS 996 APPROX 31 LT OF THE CENTER LINE WAS FOUND WITH CORROSION AROUND FASTENER HOLE. REMOVED THE UPPER L FLOORBEAM ANGLE IAW DC-9 SRM 53-01 FIG 1, 51-10-3, 51-30-2, 51-10-1.Sep 30, 1998 · N924VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800520Skin · dentedDENT .O45 INCHES IN DEPTH AT FS 206.25, L21 AND 22R, OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38. COLD WORKED AREA, FABRICATED, INSTALLED REPAIR IAW DC9 SRM 53-04, FIG 38 VIEW P, 51-10-3 AND MM 21-00.Sep 30, 1998 · N924VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800477Cover · looseGALLEY SLIDE COVER LOOSE. RESECURED IAW MM 25-61 AND PERFORMED REQUIRED INSPECTION.Sep 30, 1998 · N923VV · Doug DC932 · Emergency EquipmentSDR VJ9800476Control Box · malfunctionedNO BRAKE PRESSURE INDICATION WHEN ANTI-SKID SELECTED ON, TAKING AIRCRAFT RUNWAY POSITION. MAINTENANCE INSPECTED ANTI-SKID AND BRAKE SYSTEM AND TROUBLE SHOT PROBLEM TO ANTI-SKID CONTROL BOX. .Sep 30, 1998 · N912VV · Doug DC932 · Brake Anti-Skid SectionSDR VJ9800447Slide · dislodgedFWD ENTRY EMERGENCY DOOR SLIDE DISLODGED FROM CASING WHEN DOOR OPENED. SECURED SLIDE IAW MM 25-00.Sep 30, 1998 · N913VV · Doug DC932 · Emergency EquipmentSDR VJ9800446Battery · dischargedEMERGENCY LIGHT AT MAIN CABIN PASSENGER DOOR INOP. REPLACED BATTERIES, OPS CHECKED NORMAL.Sep 30, 1998 · N917VV · Doug DC932 · Emergency LightingSDR VJ9800580Angle · crackedAFT ENTRANCE DOOR LT SIDE WALL SUPPORT ANGLE CRACKED AND CORRODED. FABRICATED AND INSTALLED NEW ANGLE IAW DC9 SRM 51-30-2, 51-30-4, 52-11-0, FIG 2, 51-20-2A AND AIRTRAN RES 981705.Sep 29, 1998 · N924VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800562Longeron · corrodedLT WHEEL WELL IN KEEL BEAM AREA AT FS 718-737 CORRODED BEYOND LIMIT IAW DC9 SRM 53-01 FIG 1. REMOVED AND REPLACED LONGERON IAW DC9 SRM 51-30-2, 51-30-5, 51-30-1 AND 51-30-3. KEEL BEAM DETERMINED TO BE WITHIN LIMIT IAW AIRTRAN RES 981746.Sep 29, 1998 · N924VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800533Actuator · corrodedRT MLG RETRACT ACTUATOR AND CORRODED AND SUPPORT BUSHING TRUNNION IS WORN AND CORRODED. REMOVED AND REPLACED RT MLG RETRACT ACTUATOR AND BUSHINGS TRUNNION IAW DC9 32-32-2 AND 57-40-2.Sep 28, 1998 · N924VV · Doug DC932 · Landing Gear ActuatorSDR VJ9800528Skin · corrodedLEFT HAND AFT GALLEY PAN WAS FOUND WITH CORROSION ON THE I/B EDGE. REMOVED CORRODED SKIN. FABRICATED AND INSTALLED NEW SKIN IAW DC-9 SRM 51-30-2, 51-10-4, 51-10-3 AND RES 981704.Sep 28, 1998 · N924VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800527Support · corrodedAFT CARGO COMPARTMENT FLOOR TRACK WAS FOUND WITH CORROSION ON THE INNER AND OUTER SURFACES AT FS 756 TO 851 LT. FABRICATED AND INSTALLED NEW REPAIR MEMBER IAW SRM 51-10-3 AND 53-21-0 FIG 10.Sep 28, 1998 · N924VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800526Floor · corrodedFS 218 TO 332 THE LT FWD FLOOR PANEL AND TIE DOWN TRACK WAS FOUND WITH CORROSION. REMOVED FLOOR PANEL AND TIE DOWN TRACK IAW DC-9 SRM 53-21-0 FIG 8, 51-10-3 AND RES 981748.Sep 28, 1998 · N924VV · Doug DC932 · Fuselage Floor PanelSDR VJ9800525Floor · corrodedFWD CARGO FLOOR PANEL AT FS 218 TO 351 WAS FOUND WITH CORROSION AROUND EDGES. REMOVED PANEL, FABRICATED AND INSTALLED NEW PANEL IAW DC-9 SRM 51-10-3, 53-21-0 AND 53-01 PG 6.Sep 28, 1998 · N924VV · Doug DC932 · Fuselage Floor PanelSDR VJ9800514Skin · chafedVERTICAL SKIN ON LT AND RT UPPER AND LOWER BANANA FAIRING CHAFED. RT UPPER BANANA FAIRING SKIN CHAFED OUT OF LIMIT IAW DC9 SRM 55-01. REMOVED SKIN, FABRICATED AND INSTALLED NEW SKIN IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2 AND 55-01.Sep 28, 1998 · N911VV · Doug DC932 · Vertical StabilizerSDR VJ9800434Power Supply · inoperativeIN EMERGENCY POSITION, LH NACELLE LIGHT WON'T WORK. REPLACED BATTERY POWER SUPPLY IAW MM 33-50.Sep 28, 1998 · N909VJ · Doug DC932 · Emergency LightingSDR MWEA98980Battery Pack · dischargedTHE LEFT ENGINE NACELLE LIGHT WILL NOT TEST WITH EMERGENCY LIGHTING. MTC REMOVED AND REPLACED BATTERY PACK.Sep 28, 1998 · N302ME · Doug DC932 · Emergency LightingSDR CA981019025Combustion Case · cracked(CAN) DURING ENGINE DISASSEMBLY THE COMBUSTION OUTER CASE WAS FOUND CRACKED IN THE REAR FLANGE AT THREE DIFFERENT LOCATIONS. THE CRACKS WERE FROM THE HOLES AT THE INNER DIAMETER AND CONTINUED TOWARDS THE OUTER CASE WALL. THE COMBUSTION OUTER CASE WAS REPLACESep 28, 1998 · Doug DC932 · Turbine Engine Combustion SectionSDR 9810159619Control Cable · brokenAFTER TAKEOFF, THE FLIGHT CREW NOTICED A LOUD BANG AND STRONG FLUTTER FROM THE NOSE LANDING GEAR DOOR AREA. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR STOP CABLE AND NOSE LANDING GEAR DOOR. OPERATIONAL CHESep 26, 1998 · N619NW · Doug DC932 · Landing Gear Door Retract SectionSDR VJ9800445Skin · gougedGOUGE IN FUSELAGE SKIN AT FS 967, L21-22R, BEYOND LIMIT IAW DC9 SRM 53-04, FIG 8. BLENDED AREA, FABRICATED AND INSTALLED DOUBLER REPAIR IAW DC9 SRM 51-10-3, 53-31-0 FIG 8 AND 53-04 FIG 38.Sep 25, 1998 · N911VV · Doug DC932 · Fuselage Main, Plate/SkinSDR VJ9800433Actuator · failedNOSE GEAR WOULD NOT RETRACT. FERRIED AIRCRAFT FROM IAD TO MAIN MAINTENANCE BASE IN ATL FOR CONVENIENCE. REPLACED NLG ACTUATING CYLINDER IAW MM 32-32-6, PG 204 - 206. LEAK AND OPS CHECKED GOOD.Sep 25, 1998 · N966VV · Doug DC932 · Landing Gear ActuatorSDR 9810729609Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND COCKPIT AND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL.Sep 25, 1998 · N609NW · Doug DC932 · Emergency LightingSDR 9810149606Roller · out of adjustAFTER LANDING GEAR EXTENSION, THE LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW FOLLOWED COM PROCEDURES, RECYCLED THE LANDING GEAR SYSTEM, AND LANDED AT DTW WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT LANDING GEAR DOOR LOCK ROLLER ASSep 25, 1998 · N606NW · Doug DC932 · Landing Gear Door Retract SectionSDR VJ9800420Battery · dischargedAFT STAIRS EMERGENCY LIGHTING BATTERIES WON'T HOLD A CHARGE. REPLACED NICAD BATTERIES IAW MM 33-50, OPS CHECKED GOOD.Sep 24, 1998 · N946VV · Doug DC932 · Emergency LightingSDR VJ9800419Battery Pack · dischargedAFT STAIRS EMERGENCY LIGHT INOP. REPLACED BATTERY POWER SUPPLY IAW MM 3350, OPS CHECKED GOOD.Sep 24, 1998 · N946VV · Doug DC932 · Emergency LightingSDR TWAA9815502Engine · failedTHE LT ENG FILTER CLOG LIGHT ILLUMINATED AND EGT INCREASED. RETARDED THROTTLE AND DIVERTED TO BNA. FOUND METAL IN MAIN OIL SCREEN. ENGINE WAS CHANGED. CHECK-C 11-15-97 MCI. *S/D* ANALYSIS OF MATERIAL IN OIL SCREEN FOUND EVIDENCE OF M-50 BEARING MATERIAL.Sep 24, 1998 · N922L · Doug DC932 · Engine (Turbine/Turboprop)SDR CALA9801962Battery · dischargedLEFT EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS TURNED ON. REMOVED AND REPLACED AFT BATTERY PACK IN AFT BAG BIN OVERHEAD PER MM 33-53-0.Sep 24, 1998 · N12507 · Doug DC932 · Emergency LightingSDR CA981019028Controller · failed(CAN) AIRCRAFT RETURNED TO AIRPORT WITH RIGHT PACK OVERHEAT AND SMOKE AND BURNING SMELL. RIGHT PACK TEMP CONTROL VALVE WENT TO FULL HOT, WHEN COLD SELECTED VALVE RESPONDED CORRECTLY. TEMPERATURE CONTROLLER REPLACED.Sep 24, 1998 · Doug DC932 · Cabin Temperature ControllerSDR VJ9800482Spar · magnetizedREPAIR ON AFT SIDE REAR SPAR LWR CAP XRS 525 DETERMINED TO BE MAGNETIC WITHIN 5 FEET FLUX VALVE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51-10-4 AND AIRTRAN RES 981625.Sep 23, 1998 · N911VV · Doug DC932 · Wing SparSDR VJ9800418Hub Cap · wornSMOKE ODOR IN CABIN. AIRCRAFT RETURNED TO MCO. FOUND EVIDENCE OF NR 4 TIRE SPINNING IN WHEEL WELL. REPLACED RUBBER HUB CAP.Sep 23, 1998 · N935VV · Doug DC932 · Wheel/Ski/FloatSDR 9810499942Frame · crackedDURING M-CHECK, FOUND CRACK ON FRAME WEB AT FS 1038, INBOARD OF LONGERON 14R, EMITTING FROM UNDER STIFFENER. REPAIRED PER EA 99-162759.Sep 23, 1998 · N3991C · Doug DC932 · Fuselage Main, FrameSDR VJ9800518Support · corrodedFLOOR SUPPORT AT FS 160, RBL 0-45, CORRODED BEYOND LIMIT. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-3, 51-30-2, 51-10-4, 51-10-2.Sep 22, 1998 · N936VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800417Control Box · failedNO BRAKE PRESSURE DURING TAXI WITH ANTISKID SYSTEM ON. REPLACED ANTISKID CONTROL BOX AND OPS CHECKED GOOD IAW MM 32-43.Sep 22, 1998 · N912VV · Doug DC932 · Brake Anti-Skid SectionSDR MWEA98971Cover · detachedFORWARD ENTRY DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED FORWARD ENTRY DOOR EVACUATION SLIDE COVER.Sep 22, 1998 · N302ME · Doug DC932 · Emergency EquipmentSDR MWEA98970Light · inoperativeFORWARD ENTRANCE PORTABLE EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FOWARD ENTRY EMERGENCY FLASHLIGHT.Sep 22, 1998 · N209ME · Doug DC932 · Emergency LightingSDR CALA9801853Vane · gougedINSPECTION FOUND RT WING UPPER MOVEABLE VANE LEADING EDGE GOUGED. A REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 1, 51-10-4, 51-10-3, 51-30-2, AND 51-10-2.Sep 22, 1998 · N70542 · Doug DC932 · Trailing Edge FlapsSDR CA981019029Controller · failed(CAN) ON DEPARTURE AT 2,500 FEET, THE RIGHT AIR CONDITION PACK OVERHEATED THEN FORWARD FIRE DETECTORS ANNUNCIATED, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, DECLARED EMERGENCY AND RETURNED TO BLOCKS . REPLACED AUTOMATIC CABIN TEMPERATURE CONTROLLER.Sep 22, 1998 · Doug DC932 · Cabin Temperature ControllerSDR VJ9800412Slide · looseFWD ENTRY DOOR EVAC SLIDE LOOSE FROM CASE. RESECURED SLIDE PACK LATCH AND COVER PER MM 25-51.Sep 21, 1998 · N914VV · Doug DC932 · Emergency EquipmentSDR VJ9800411R1Uplock Latch · inoperativeGEAR DOOR OPEN LIGHT ON WITH LANDING GEAR INDICATING DOWN AND LOCKED. REMOVED AND REPLACED THE LT MLG UPLOCK LATCH ASSY IAW D MM 32-31-4.Sep 21, 1998 · N918VV · Doug DC932 · Landing Gear Retraction/Extension SystemSDR VJ9800411Indication · malfunctionedGEAR DOOR OPEN LIGHT ON WITH LANDING GEAR INDICATING DOWN AND LOCKED.Sep 21, 1998 · N918VV · Doug DC932 · Landing Gear Position and WarningSDR VJ9800513Tab · corrodedRT ELEVATOR GEAR TAB HAS 1 INCH DIAMETER CORROSION SPOT. CUT OUT CORROSION, CLEANED AREA, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 51-70-2.Sep 20, 1998 · N911VV · Doug DC932 · Elevator, Tab StructureSDR VJ9800416Slide · contaminatedTAIL CONE EVAC SLIDE ASSY SATURATED WITH FOREIGN MATERIALS. REMOVED AND REPLACED TAIL CONE SLIDE ASSY.Sep 20, 1998 · N967VV · Doug DC932 · Escape Slide
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