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 CALA9801093Longeron · crackedINSPECTION FOUND LONGERON 17R AT FS 955.091 AND FS 945. THE CRACKED SECTIONS OF LONGERON WERE REMOVED IAW SRM 51-30-2. NEW SECTIONS OF LONGERON WERE FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18, 51-10-3, 51-30-1, 51-30-2 AND 51-30-5.May 30, 1998 · N12538 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9800917Longeron · crackedINSPECTION FOUND A CRACK OUT OF UPPER FASTENER HOLE BEHIND ANGLE BRACKET IN LONGERON 17L AT FS 955. THE ANGLE BRACKET WAS ALSO CRACKED. THE LONGERON AND ANGLE BRACKET WERE REMOVED. A NEW LONGERON AND BRACKET WERE FABRICATED AND INSTALLED IAW SRM 53-02, FIGUMay 30, 1998 · N12538 · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800180Skin · dentedREMOVED AND REPLACED LT UPPER CROWN SKIN NOSE SECTION IAW DC9 SRM 5103902. ORDERED, FIT, TRIMMED, LOCATED AND DRILLED NEW SKIN IAW DC9 SRM 51-10-4. INSTALLED NEW SKIN LT UPPER NOSE IAW DC9 SRM 51-30-2, 51-30-5 AND EO 9-53-003.May 29, 1998 · N948VV · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9809117Rib · crackedMCI - DURING OP 15 MAINTENANCE CHECK, THE LEFT WING OUTBOARD FLAP HINGE CASTING ATTACH RIBS WERE CRACKED ON INBOARD AND OUTBOARD SIDES INSIDE FLAP STRUCTURE. RIBS REMOVED AND NEW RIBS INSTALLED PER SRM 51-01, AND FASTENERS INSTALLED PER STANDARD PRACTICES ANDMay 29, 1998 · N920L · Doug DC932 · Trailing Edge FlapsSDR MWEA98636Cover · fell offTHE FORWARD PASSENGER DOOR SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED SLIDE COVER.May 29, 1998 · N401ME · Doug DC932 · Emergency EquipmentSDR MWEA98634Shear Tie · corrosionFOUND CORROSION ON SHEAR TIE AT STATION 305 BETWEEN LONGERON 29L AND 29R. MAINTENANCE FABRICATED AND INSTALLED SHEAR TIE.May 29, 1998 · N204ME · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800916Angle · crackedINSPECTION FOUND A .5 CRACK IN FLOOR PANEL ATTACH ANGLE AT FS 680, LBL 4. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-10-3.May 29, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9800477Valve · failedAFTER TAKEOFF, GEAR HANDLE SELECTED UP, THE NOSE LANDING GEAR AND MAIN LANDING GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. GEAR WAS RECYCLED THREE TIMES WITH THE SAME RESULT. REPLACED LANDING GEAR CONTROL VALVE IAW DC9 MM 32-32-0.May 29, 1998 · N980AX · Doug DC932 · Landing Gear Retraction/Extension SystemSDR VJ9800264Web · crackedLT FWD CARGO PIT WEB CRACKED AND CORRODED BEYOND LIMIT AT STA 218 TO 228, LBL 40 TO 58, IAW DC9 SRM 53-01 FIG 1. REMOVED LT O/B FLOOR PANEL AFT OF FWD ENTRY DOOR, REMOVED WEB AND FABRICATED WEB PANEL FROM 7075T6, .020, IAW DC9 SRM 53-10-2, FIG 5. TREATED ANDMay 28, 1998 · N935VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800157Cover · fell offDOOR SLIDE (GALLEY) ACCIDENTALLY CAME OUT OF THE COVER. SLIDE DID NOT DEPLOY. INSTALLED SLIDE COVER IAW 25-61 / SP 8100.May 28, 1998 · N915VV · Doug DC932 · Emergency EquipmentSDR TWAA9808703Bulkhead · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND LOWER ANGLE CRACKED ONE INCH AT 3 O'CLOCK POSITION ON FORWARD SIDE OF AFT PRESSURE BULKHEAD. REPAIRED ANGLE WITH DOUBLER PER SRM 53-01, PAGE 10. (M)May 28, 1998 · N920L · Doug DC932 · Fuselage Main, BulkheadSDR CALA9801092Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN VERTICAL ATTACH ANGLE AT FS 658, BL 45R. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-3, AND 51-30-5.May 28, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9800910Frame · crackedINSPECTION FOUND CRACKS IN FORWARD PIT FRAME AT FS 466, STRINGER 29L. THE CRACKS WERE STOP DRILLED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263.May 28, 1998 · N12538 · Doug DC932 · Fuselage Main, FrameSDR CALA9800909Floor · crackedINSPECTION FOUND SEVERAL CRACKS IN RT NR 61 FLOORBOARD. A FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-10-3.May 28, 1998 · N12538 · Doug DC932 · Fuselage Floor PanelSDR CALA9800908Skin · crackedINSPECTION FOUND INTERIOR CRACKS ON VERTICAL FIN LEADING EDGE FORWARD OF PITOT TUBE AROUND COUNTER SINK. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2.May 28, 1998 · N12538 · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR CALA9800907Doubler · crackedINSPECTION FOUND A 1.5 CRACK IN RT WING LEADING EDGE FRAME UPPER DOUBLER AT WS 444.5. THE DOUBLER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2.May 28, 1998 · N12538 · Doug DC932 · Wing Miscellaneous StructureSDR CALA9800906Doubler · crackedINSPECTION FOUND A 3.75 CRACK COMING FROM SCREW HOLE IN RT WING UPPER WING TO BODY FAIRING BONDED DOUBLER. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3.May 28, 1998 · N12538 · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800263Support · corrodedFWD CARGO PIT UPPER AND LOWER FLOOR SUPPORT L-ANGLE HAS CORROSION BEYOND LIMIT AT FS 820, L28L TO L28R. REMOVED CORROSION AND FABRICATED L-ANGLE FLOOR SUPPORT IAW DC9 SRM 53-20, 51-10-2 AND 51-10-2A. HEAT TREATED, PRIMED AND INSTALLED L-ANGLE.May 27, 1998 · N935VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800262Support · corrodedRT FLOOR SUPPORT CORRODED BEYOND LIMIT AT STA 996 TO 965. REMOVED CORROSION AND FOUND SKIN CORRODED OUT OF LIMIT IN Z-ANGLE. FABRICATED SKIN FROM 7075T6, .032, AND Z-ANGLE FROM 7075T6, .032. DRILLED AND DEBURRED SKIN AND Z-ANGLE IAW DC9 SRM 51-10-2, 51-10-4.May 27, 1998 · N935VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800261Skin · corrodedFWD CARGO PIT, RH REPAIR DOUBLER AND SKIN CORRODED BEYOND LIMIT AT FS 360, L30-27R. REMOVED CORROSION, FABRICATED REPLACEMENT DOUBLER FROM 2024T3 .025 INCH, IAW DC9 SRM 53-04, TREATED, PRIMED AND INSTALLED PLUS APPLIED SEALANT.May 26, 1998 · N935VV · Doug DC932 · Fuselage Main, Plate/SkinSDR 9809399918Acm · failedBOTH AFT LAVATORY SMOKE ALARMS ACTIVATED AFTER TAKEOFF. FLIGHT ATTENDANT REPORTED AN ELECTRICAL TYPE SMELL IN AFT CABIN. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH HEAT EXCHANGERS AND RIGHT AIR CYCLE MACHINE, OPERATIONMay 26, 1998 · N940N · Doug DC932 · Cabin Cooling SystemSDR VJ9800260Longeron · corrodedCORROSION IN FORWARD PIT AT FS 231, L29R BEYOND LIMITS. REMOVED CORROSION, RT LONGERON 29, FS 231 TO 246. DRILLED NEW SECTION OF LONGERON AND LONGERON SPLICES IAW DC9 SRM 53-02, FIG 18. DEBURRED, TREATED AND INSTALLED LONGERON AND SPLICES AND SHIMS IAW DC9 May 25, 1998 · N935VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA98625Pan · crackedFOUND CRACK ON AFT ENTRANCE DOOR PAN AT UPPER RIGHT STOP FITTING. MTC FABRICATED AND INSTALLED NEW UPPER DOOR PAN.May 25, 1998 · N206ME · Doug DC932 · Passenger/Crew DoorsSDR MWEA98624Rib · corrosionFOUND CORROSION ON RIGHT WING LEADING EDGE RIB AT NUMBER 3 SLAT DRIVE TRACK. MTC FABRICATED AND INSTALLED NEW FITTING.May 25, 1998 · N206ME · Doug DC932 · Wing, Rib/BulkheadSDR MWEA98623Intercostal · crackedFOUND CRACK ON PASSENGER DOOR INTERCOSTAL AFT OF INTERIOR HANDLE MECHANISM. MTC REMOVED AND REPLACED INTERCOSTAL.May 25, 1998 · N206ME · Doug DC932 · Passenger/Crew DoorsSDR MWEA98622Adi · inoperativeON CLIMBOUT, FIRST OFFICER ADI DID NOT INDICATE MORE THAN 3 DEGREE NOSE UP WHEN IN 15 DEGREE CLIMB. MTC REMOVED AND REPLACED FIRST OFFICERS ADI.May 25, 1998 · N207ME · Doug DC932 · Integrated Flight SystemSDR CALA9800899Relay · inoperativeWHEN GEAR WAS EXTENDED ON APPROACH, ONLY UPPER HALF OF GREEN DOWN AND LOCKED LIGHTS ILLUMINATED. THE GEAR WAS RECYCLED AND CIRCUIT BREAKERS WERE CHECKED. A GO-AROUND WAS PERFORMED AND THE GEAR WAS CONFIRMED DOWN AND LOCKED THROUGH VIEW PORT. THE AIRCRAFT LAMay 25, 1998 · N12532 · Doug DC932 · Landing Gear Position and WarningSDR ABXA9800465Shear Tie · crackedDURING C-CHECK, FOUND FRAME SHEAR TIE AT STATION 1019 CRACKED BETWEEN LONGERON 14L AND 15L. REPLACED SHEAR TIE IAW DC9 SRM 51-30-5.May 25, 1998 · N980AX · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800156Batteries · dischargedEMERGENCY LIGHTS OUT, AFT OVERWING EXITS. REMOVED AND REINSTALLED SAME BATTERIES AND THE SYSTEM OPS CHECKED NORMAL.May 23, 1998 · N914VV · Doug DC932 · Emergency LightingSDR MWEA98621Battery Pack · dischargedTHE AFT COMPARTMENT AND CABIN FLOOR EMERGENCY LIGHT FOUND INOP. MTC REMOVED AND REPLACED BATTERY PACK IN RIGHT LAVATORY.May 23, 1998 · N602ME · Doug DC932 · Emergency LightingSDR 9809599605Engine · failedDURING CLIMB AT 1500 FEET, THE LEFT ENGINE EXPERIENCED A CONTAINED FAILURE. AIRCRAFT RETURNED TO MKE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE, OPERATIONAL CHECK OK.May 23, 1998 · N605NW · Doug DC932 · Engine (Turbine/Turboprop)SDR VJ9800259Support · corrodedAFT CARGO COMPARTMENT CORRODED AT STA 832, L28R. REMOVED SUPPORT, NUT PLATE AND COROSION ON UPPER FLANGE. CORROSION LOSS OF .028 BEYOND LIMIT. INSTALLED SUPPORT IAW DC9 SRM 51-30-2, AT STA 832, L28R, AFTER ALODINING AND PRIMING IAW DC9 SRM 51-10-3, 51-30-2.May 22, 1998 · N935VV · Doug DC932 · Fuselage Miscellaneous StructureSDR VJ9800174Rib · crackedLT WING NR 1 SLAT, STA 58.768. VERTICAL ATTACH WEB CRACKED APPROXIMATELY 1 INCH. REMOVED EXISTING REPAIR AND REPAIRED SLAT WEB IAW EO 9-27-003.May 22, 1998 · N966VV · Doug DC932 · Wing, Rib/BulkheadSDR TWAA9808702Bulkhead · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND AFT PRESSURE BULKHEAD, UPPER ANGLE CRACKED ONE INCH AT 9 O'CLOCK POSITION, FORWARD SIDE OF AFT PRESSURE BULKHEAD. REPLACED ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M)May 22, 1998 · N920L · Doug DC932 · Fuselage Main, BulkheadSDR TWAA9808701Skin · damagedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND AFT CARGO DOOR CUTOUT SKIN DAMAGED ON LOWER FORWARD SIDE. REPAIRED SKIN AND INSTALLED DOUBLER PER SRM 53-05, PAGE 261. (M)May 22, 1998 · N920L · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA98620Latch · lack of lubeTHE GIRT BAR LATCH FOR MAIN CABIN DOOR SLIDE NEEDS TO BE LUBRICATED. MTC LUBRICATED GIRT BAR LATCHES.May 22, 1998 · N501ME · Doug DC932 · Emergency EquipmentSDR VJ9800155Actuator · failedAIRCRAFT AIR RETURNED, NOSE GEAR UNSAFE LIGHT ON AFTER RETRACTION. CYCLED THE GEAR WITH THE SAME INDICATION. REPLACED NOSE GEAR RETRACT CYLINDER AND OPS CHECKED GOOD PER MM32-32-06. PAGES 201-205 AIRCRAFT OK FOR SERVICE.May 21, 1998 · N915VV · Doug DC932 · Landing Gear ActuatorSDR VJ9800154Battery Pack · dischargedFWD CABIN EMERGENCY TRACK LIGHT INOP. REPLACED THE FWD CABIN EPL BATTERY PACK PER MM 33-50. SYSTEM OPS CHECKED GOOD.May 19, 1998 · N910VJ · Doug DC932 · Emergency LightingSDR CA980608021Apu · leaking(CAN) DURING CLIMB OUT, AN OILY SMELL WAS DETECTED IN BUSINESS CLASS SECTION OF PASSENGER COMPARTMENT. SMELL DISSIPATED AFTER LEFT HAND AIR CONDTIONER PACK TURNED OFF. MAINTENANCE CHECK REVEALED AUXILIARY POWER UNIT WAS CONTAMINATING LEFT AIR CONDITIONER PACMay 19, 1998 · Doug DC932 · Airborne Auxiliary Power Unit (APU) SystemSDR VJ9800153Pressurization · malfunctionedAIRCRAFT LOST CABIN PRESSURIZATION AT FL 32.6 CABIN ALTITUDE INCREASED TO 12500 FEET, O2 MASK DROPPED, SYSTEM WAS FUNCTIONING PROPERLY UNTIL THIS POINT. CREW AND PAX O2 USED.May 18, 1998 · N931VV · Doug DC932 · Cabin Pressure Control SystemSDR TWAA9809211Frame · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND NOSE GEAR WHEEL WELL CHORD ANGLE CRACKED THROUGH A RIVET IN LT TUNNEL, .5 INCH BELOW PRESSURE DECK AT STATION 79 LBL 17. STOP DRILLED AND INSTALLED DOUBLER PER SRM 53-01, PAGE 10. (M)May 15, 1998 · N995Z · Doug DC932 · Fuselage Main, FrameSDR CALA9800952Door · crackedINSPECTION FOUND A 7 INCH CRACK IN FORWARD CARGO DOOR AFT EDGE ADJACENT TO LATCHING MECHANISM, 15 INCHES ABOVE LOWER EDGE. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-03, FIGURE 1, 51-30-2, AND 51-30-5.May 15, 1998 · N27509 · Doug DC932 · Cargo/Baggage DoorsSDR 9809309612Harness · failedDURING APPROACH INTO FAR, NOSE LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR PROXIMITY HARNESS. OPERATIONAL CHECK NORMAL ON GEAR SWIMay 15, 1998 · N612NW · Doug DC932 · Landing Gear Position and WarningSDR 9809279613Relay · failedAUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF. FLIGHT RETURNED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED R2-4 GROUND CONTROL RELAY. OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE.May 15, 1998 · N613NW · Doug DC932 · Cabin Pressure Control SystemSDR 9809269613Amplifier · failedAUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF, FLIGHT WAS RETURNED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CABIN PRESSURE AMPLIFIER. OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE.May 15, 1998 · N613NW · Doug DC932 · Cabin Pressure Control SystemSDR VJ9800173Longeron · corrodedCORROSION AT FS 294, LONGERON 30. REMOVED CORRODED SECTION OF LONGERON AND REPAIRED PER RES-1-05422.May 14, 1998 · N966VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR VJ9800152Coalescer · dirtyAFTER TAKEOFF, FLIGHT ATTENDANT EXPERIENCED AN UNUSUAL SMELL IN FWD CABIN. AS A PRECAUTIONARY MEASURE, FLIGHT CREW ELECTED TO RETURN TO MAIN MAINTENANCE BASE. INSPECTED AIRCRAFT, OPERATED BOTH ENGINES, INSPECTED APU, AIR CONDITIONING DUCTING IN GALLEYS. NO May 14, 1998 · N907VJ · Doug DC932 · Humidity Control SystemSDR MWEA98597Slide Cover · fell offMKE - FLT 207 - THE GALLEY DOOR EMERGENCY SLIDE COVER DISLODGED. MAINTENANCE INSTALLED GALLEY DOOR SLIDE COVER. (M)May 14, 1998 · N502ME · Doug DC932 · Emergency EquipmentSDR CALA9800865Longeron · crackedCRACK (1.3) AT FRAME STA 756 L3L. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED AND INSTALLED REPAIR SPLICES PER SRM 53-02 AND 51-10-3.May 14, 1998 · N27509 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9800864Floorbeam · corrodedFLOORBEAM IS CORRODED AT FS 980 LBL 15 TO LBL 50. REMOVED DAMAGED AREA. FABRICATED, PRIMED, AND INSTALLED REPAIR PER SRM 51-10-3, 53-01, 53-05, AND 51-30-5.May 14, 1998 · N27509 · Doug DC932 · Fuselage Main, Floor Beam
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