Douglas DC-9-32

Service difficulty reports · 12,755

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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 = 'DC932'
  ORDER BY difficulty_date DESC"

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SDR CALA9601074Longeron · crackedINSPECTION FOUND A .1250 INCH CRACK IN LONGERON 5R AT STA 699. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 2.Jul 1, 1996 · N18544 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9601073Longeron · crackedINSPECTION FOUND LONGERON 5L CRACKED AT STA 699. THE LONGERON WAS REPAIRED IAW SRM 53-02.Jul 1, 1996 · N18544 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9601072Longeron · crackedINSPECTION FOUND A .25 INCH CRACK IN LONGERON 1L AT STA 699. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 4.Jul 1, 1996 · N18544 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9601071Longeron · crackedINSPECTION FOUND A CRACK IN LONGERON 2L AT STA 756. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.Jul 1, 1996 · N18544 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9601068Flr Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD BAGGAGE BIN FLOOR SUPPORT AT STA 446, LONGERON 29R. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2.Jul 1, 1996 · N18544 · Doug DC932 · Fuselage Miscellaneous StructureSDR 9616439940Longeron · corrodedDURING M-CHECK, FOUND CORROSION ON THE LEFT WING STR 13 TO 15, 17 BETWEEN XW 58 AND XRS 112. REPAIRED STRINGER (P/N 5919239, 5919237, 5919238) PER EA 99-110827.Jul 1, 1996 · N3322L · Doug DC932 · Wing, Longeron/StringerSDR 9615339941Spar · corrodedDURING H-CHECK, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR CAP (XW 58 - XRS 91) AND SPAR CAP SPLICE T (XRS 112). REPAIRED CAP (P/N 5911305-503) AND T (P/N 5911357-1) PER EA 99-110801, 99-110805.Jul 1, 1996 · N3324L · Doug DC932 · Wing SparSDR 9614639917Wire · shortedFLIGHT ATTENDANT REPORTED FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPAIRED SHORTED WIRE AT ROW 10, OPERATIONAL CHECK NORMAL.Jul 1, 1996 · N967N · Doug DC932 · Light System WiringSDR 9614629611Battery Pack · malfunctionedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK OK.Jul 1, 1996 · N611NW · Doug DC932 · Emergency LightingSDR 9614609919Switch · malfunctionedDURING APPROACH, LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LANDING GEAR LEVER WARNING SWITCH, OPERATIONAL CHECK NORMAL.Jul 1, 1996 · N941N · Doug DC932 · Landing Gear Position and WarningSDR 9614599602Door · openVIBRATION WAS COMING FROM NOSE GEAR AREA AFTER TAKEOFF. GEAR INDICATION WAS NORMAL. RECYCLED GEAR BUT VIBRATION CONTINUED. FLIGHT RETURNED TO MDT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT FORWARD NOSE LANDING GEAR DOOR OPEN.Jul 1, 1996 · N602NW · Doug DC932 · Landing Gear Door Retract SectionSDR 96ZZZM1200Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND A CRACK IN LONGERON 1L, STATION 756. REPAIRED PER SRM 53-02, FIGURE 4, PAGE 5. (M)Jun 30, 1996 · N921L · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9615329940Splice · corrodedDURING M-CHECK, FOUND CORROSION ON THE LOWER FORWARD SPAR CAP SPLICE PLATE AT XRS 91, LEFT SIDE. REPAIRED SPLICE (P/N 3912208-1) PER EA 99-109071.Jun 30, 1996 · N3322L · Doug DC932 · Wing Miscellaneous StructureSDR 9614619986Power Supply · inoperativeDURING PERIODIC CHECK, FOUND AFT STAIRWAY AND OVERHEAD TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.Jun 30, 1996 · N986US · Doug DC932 · Emergency LightingSDR ABXA9700215Fairing · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-07, FOUND NR 1 REVERSER UPPER DOOR INBOARD FAIRING CRACKED. REPLACED IAW DC-9 SRM 51-30-2, 51-30-8.Jun 28, 1996 · N928AX · Doug DC932 · Engine Thrust ReverserSDR CALA9601062Latch · out of rigTHE TAILCONE EXTERIOR RELEASE HANDLE PULLED LOW AT 20 POUNDS. TAILCONE LATCH ADJUSTMENT WAS PERFORMED AND PULL WAS WITHIN SPECIFICATIONS PER MM 53-50-3.Jun 27, 1996 · N18544 · Doug DC932 · Aerodynamic FairingsSDR CALA9601036Latch · out of adjustTHE TAILCONE EXTERIOR RELEASE HANDLE PULLED LOW AT 20 POUNDS. TAILCONE LATCH WAS ADJUSTED AND THE EXTERIOR RELEASE HANDLE PULL TESTED WITHIN SPECIFICATIONS AT 34 POUNDS PER MM 53-50-3.Jun 27, 1996 · N18544 · Doug DC932 · Aerodynamic FairingsSDR 9614209950Lights · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT SEATS 1CD INOPERATIVE. DEFERRED PER MEL 33-24B. DAMAGED WIRE FROM FLOOR TO SEAT 1D NEEDS REPAIR.Jun 27, 1996 · N9346 · Doug DC932 · Emergency LightingSDR 9614219917Batteries · dischargedDURING PREFLIGHT CHECK, FOUND SEVERAL SECTIONS OF CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES AND BURNED OUT BULB.Jun 26, 1996 · N967N · Doug DC932 · Emergency LightingSDR ABXA9700077Fitting · misdrilledDURING C-CHECK, FOUND A .1875 INCH HOLE DRILLED THROUGH THE UPPER SURFACE OF THE WING INBOARD FLAP ATTACH FITTING. REPAIRED IAW ABX REA D957-15559-MR.Jun 25, 1996 · N928AX · Doug DC932 · Wing Miscellaneous StructureSDR 96ZZZX4188Skin · wornDURING MAINTENANCE, LT INBD FLAP T/E INBD CHAFE STRIP AND SKIN NEXT TO CHAFE STRIP HAS APPROXIMATELY 12 INCH AREA CHAFED. COMPLIED WITH LMAC E.O. 3822 BY CUTTING OUT DAMAGE SECTION OF FLAP INBD WEDGE SKIN AND SPLICED IN NEW SECTION IAW LMAC E.O. 3822, AND 811Jun 25, 1996 · N906VJ · Doug DC932 · Trailing Edge FlapsSDR 96ZZZM1075Conduit · cutDURING MAINTENANCE, WHILE VERIFYING FLAP FOLLOW-UP CABLES FOR PROPER INSTALLATION PER FLEET CAMPAIGN 2296. FOUND LT AILERON UP CABLE NR 35 IN LEFT WHEEL WELL CHAFING THROUGH ELECTRICAL CONDUIT APPROX ONE INCH LONG BY .1875 INCH DEEP.Jun 25, 1996 · N906VJ · Doug DC932 · Electrical Power SystemSDR 9615289941Chord · corrodedDURING H-CHECK, FOUND CORROSION ON THE FORWARD SPAR LOWER CAP, WS 58 - 76, LEFT SIDE. REPAIRED CAP (P/N 5911307-505) PER EA 99-110530.Jun 24, 1996 · N3324L · Doug DC932 · Wing SparSDR 9614119925Epr Indicator · malfunctionedNR 1 ENGINE EPR INDICATION FROZE AT 1.45 ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR INDICATOR WITH A SERVICEABLE UNIT. SYSTEM OPERATION RETURNED TO NORMAL.Jun 24, 1996 · N925US · Doug DC932 · Engine Pressure Ratio (EPR)SDR 9613929919Stall Warn Comp · malfunctionedSTALL WARNING SYSTEM ACTIVATED ON ROTATION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT STALL WARNING COMPUTER AND RIGHT AOA TRANSDUCER, OPERATIONAL CHECK NORMAL.Jun 24, 1996 · N941N · Doug DC932 · Stall Warning SystemSDR MWEA96252Evac Slide Cover · fell offCREW REPORTS, GALLEY DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED GALLEY DOOR SLIDE COVER.Jun 23, 1996 · N302ME · Doug DC932 · Emergency EquipmentSDR CA960723556Controller · failed(CAN) AIRCRAFT RETURNED FROM FLIGHT DUE TO ONE PRESSURE CONTROLLER ON DEVIATION AND A SECOND CONTROLLER FAILED DURING CLIMB. PASSENGER OXYGEN MASKS DEPLOYED. MAINTENANCE ACTION INVOLVED CHANGING #1 AND #2 PRESSURE CONTROLLERS AND #1 CABIN PRESSURE SELECTOR. CAJun 23, 1996 · Doug DC932 · Cabin Pressure ControllerSDR CALA9600862Cable · twistedINSPECTION FOUND TAILCONE RELEASE CABLE ON LEFT HAND SIDE AT TIMING BLOCK DAMAGED AND TWISTED. THE CABLE WAS REMOVED AND REPLACED.Jun 21, 1996 · N14534 · Doug DC932 · Aerodynamic FairingsSDR CALA9600861Clips · wornTHE TAILCONE INTERIOR RELEASE HANDLE CLIPS WERE FOUND WORN AND THE HANDLE PULLED FROM CLIPS AT 5 POUNDS. THE CLIPS WERE REMOVED AND REPLACED.Jun 21, 1996 · N14534 · Doug DC932 · Aerodynamic FairingsSDR ABXA9700212Fairing · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND NR 2 REVERSER UPPER DOOR OUTBOARD FAIRING CRACKED. REPLACED IAW DC-9 SRM 51-30-2, 51-30-8.Jun 21, 1996 · N928AX · Doug DC932 · Engine Thrust ReverserSDR 9614059918Fitting · corrodedDURING H-CHECK, FOUND CORROSION IN THE LEFT WING NR 2 FLAP FORWARD HINGE FITTING FASTENER HOLES. REPLACED HINGE (P/N 5919218-505) PER CITEXT 09-5740-1-9800.Jun 21, 1996 · N940N · Doug DC932 · Wing, Control Surface Attach FittingsSDR CALA9600951Beam · crackedINSPECTION FOUND A .5 CRACK IN FORWARD END OF MAIN CABIN DOOR NR 8 BEAM. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31.Jun 20, 1996 · N14534 · Doug DC932 · Passenger/Crew DoorsSDR CALA9600950Intercostal · crackedINSPECTION FOUND A 3.5 CRACK IN FORWARD ACCESSORY COMPARTMENT INTERCOSTAL AT STA 37. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-10-1.Jun 20, 1996 · N14534 · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96251Apu Access Door · unlatchedPILOT REPORTS, VIBRATION FELT IN RUDDER PEDALS AT 240 KTS. A/C RETURNED TO MKE. FOUND LT APU ACCESS DOOR HAD COME OPEN TO CAUSE VIBRATION. REPLACED DOOR, NO OTHER DAMAGE NOTED.Jun 19, 1996 · N301ME · Doug DC932 · Auxiliary Power Unit (APU) DoorsSDR ABXA9700214Former · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND RIGHT FLAP OUTBOARD FLAP ATTACH FITTING CRACKED. REPLACED IAW DC-9 SRM 51-30-1, 51-30-2.Jun 19, 1996 · N928AX · Doug DC932 · Trailing Edge FlapsSDR ABXA9700213Bracket · crackedDURING C-CHECK AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT FLAP ATTACH BRACKET CRACKED AT STATION 353. REPLACED IAW DC-9 SRM 51-30-4, 51-30-1, 51-30-2.Jun 19, 1996 · N928AX · Doug DC932 · Trailing Edge FlapsSDR CALA9600841Tire · cap separatedTHE RT HYDRAULIC QUANTITY WENT TO ZERO IN FLIGHT AND THE PRESSURE STARTED DROPPING. THE RIGHT ENGINE PUMP WAS TURNED OFF. THE PRESSURE STAYED AT ZERO AND RIGHT QUANTITY ROSE TO 6. THE GEAR AND FLAPS WERE LOWERED USING THE LEFT SYSTEM AND THE AIRCRAFT LANDEDJun 18, 1996 · N18544 · Doug DC932 · TireSDR CA960723550Controller · inoperative(CAN) AT FLIGHT LEVEL 350 FLOW LIGHT CAME ON. DESCENT INITIATED, LIGHT WOULD GO OFF AND ON. AT FLIGHT LEVEL 290 LIGHT CAME ON AND CABIN STARTED TO CLIMB AT MAX RATE. EMERGENCY DESCENT INITIATED AND CABIN CONTROL REGAINED JUST BELOW 20,000 FEET. MAINTENANCE CARJun 18, 1996 · Doug DC932 · Cabin Pressure ControllerSDR 9613829950Switch · malfunctionedRIGHT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE ON APPROACH. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT MAIN GEAR DOWNLOCK SWITCH. CYCLED GEAR SEVERAL TIMES, OPERATIONAL CHECK NORMAL.Jun 18, 1996 · N9346 · Doug DC932 · Landing Gear Position and WarningSDR 9613799921Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT BATTERY PACKS WITH LOW VOLTAGE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Jun 18, 1996 · N943N · Doug DC932 · Emergency LightingSDR CA960723548Controller · inoperative(CAN) AT FLIGHT LEVEL 330, FLOW LIGHT CAME ON, CABIN 1000 FT/MINUTE. COMPLETED DRILL, CABIN UNCONTROLLABLE, OXYGEN MASKS DEPLOYED WHEN CABIN THRU FLIGHT LEVEL 10,000 FT., RECOVERED CABIN PRESSURE AT FLIGHT LEVEL 220. MAINTENANCE ACTION INVOLVED CHANGING #1 CABJun 17, 1996 · Doug DC932 · Cabin Pressure ControllerSDR CA960723547Fuel Atomizer · leaking(CAN) PRIOR TO DEPARTURE AND WITH AIR CONDITIONING PACKS ON, THERE WAS A PRESENCE OF OILY SMOKE IN THE CABIN. MAINTENANCE CHECK FOUND FUEL LEAKING AT AUXILIARY POWER UNIT FUEL ATOMIZER. THE FUEL ATOMIZER ASSEMBLY AND SEAL WERE CHANGED AND LEAK CHECK CARRIED OUJun 17, 1996 · Doug DC932 · APU Engine Fuel and ControlSDR 9616429941Longeron · corrodedDURING H-CHECK, FOUND CORROSION ON THE RIGHT WING STR 17 FROM STA 69 TO 137. REPAIRED STRINGER (P/N 5919339-2) PER EA 99-110809.Jun 17, 1996 · N3324L · Doug DC932 · Wing, Longeron/StringerSDR MWEA96162Beam · crackedDURING INSP, FOUND AFT VENTRAL DOOR HAS CRACK IN LT LOWER BEAM. REPLACED BEAM IAW SRM 51-30.Jun 16, 1996 · N203ME · Doug DC932 · Passenger/Crew DoorsSDR CA960723546Elect Receptacle · malfunction(CAN) PRIOR TO DEPARTURE, BURNING SMELL DETECTED IN GALLEY AREA. OVENS AND ELECTRICAL OUTLET CHECKED.Jun 15, 1996 · Doug DC932 · Buffet/GalleysSDR 96ZZZM1137Longeron · crackedSTL - DURING SPECIAL INSPECTION, FOUND .5 INCH CRACK LONGERON 5R STATION 756, REPAIRED PER SRM 53-02 FIGURE 2.Jun 15, 1996 · N926L · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA96250Spar · corrosionDURING CERT INSP, LT WING INTERIOR AFT SPAR FOUND WITH MILD CORROSION ON REAR SPAR HORIZONTAL SURFACE AT STA XRS 69.000 AND XRS 91.000. REMOVED CORROSION IAW SRM 51-03-3, SHOT PEENED AFFECTED AREA OF SPAR, TREATED, PRIMED AND INSTALLED STRAP PER DAC TELEX SVCJun 14, 1996 · Doug DC932 · Wing SparSDR MWEA96249Bracket · crackedDURING CERT INSP, FOUND AN AFT RT BRACKET CRACKED ON RT INTERCOSTAL AT STA 996.0. FABRICATED A NEW BRACKET IAW SRM 53-01, PAGE 1 AND INSTALLED IAW SRM 53-01, PAGE 1.Jun 14, 1996 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA96172Bulkhead Angle · corrodedDURING CERT INSP, FOUND AFT CARGO COMPT BULKHEAD ANGLE HAD LIGHT CORRSION ON UNDERSIDE AT STA 996 FROM LONGERONS 25R TO 18R. SPLICED IN A NEW ANGLE IAW THE SRM 53-05, FIG 93.Jun 14, 1996 · N206ME · Doug DC932 · Fuselage Main, BulkheadSDR MWEA96171Skin · damagedDURING CERT INSP, REPAIR MOD OF VHF ANTENNA REQUIRES INSTALLATION AT STA 470, LONG 30. INSTALLED PERMANENT REPAIR ON VHF ANTENNA PER SB 53-188 AND SRO 9530005.Jun 14, 1996 · N206ME · Doug DC932 · Fuselage Main, Plate/Skin
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