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 97ZZZM25Floor Beam · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CORROSION ON THE UPPER CAP OF THE FLOOR BEAM STA 965, LBL 48. RECEIVED FROM AERO SUPPLY L-ANGLE NR 635060. FIT, TRIMMED, DRILLED UP, DEBURRED ANGLE IAW DC9 SRM 53-11-3 FIG 11A, SRM 51-10-4. TRDec 2, 1996 · N921VV · Doug DC932 · Fuselage Main, Floor BeamSDR 97ZZZM145Fitting · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND CORROSION AT LONGERON 30 END FITTING AT STATION 750. (M)Dec 2, 1996 · N922VV · Doug DC932 · Fuselage Miscellaneous StructureSDR 97ZZZM144Longeron · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD PIT FRAME AT FS 389 AND LONGERON 30 FRAME CRACKED AT BOTTOM, CRACK LENGTH 3, 1 INCH. (M)Dec 2, 1996 · N922VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR 97ZZZM143Longeron · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND THE FORWARD PIT FRAME AT FS 408 AND LONGERON 30 FRAME WAS CRACKED AT THE BOTTOM, THREE 1 INCH CRACKS. (M)Dec 2, 1996 · N922VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9625869602Connector · damagedDURING CLIMBOUT FROM MSN, NOSE LANDING GEAR GREEN LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR AND LIGHT EXTINGUISHED AFTER APPROXIMATELY FIVE MINUTES. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR LOCDec 2, 1996 · N602NW · Doug DC932 · Landing Gear Position and WarningSDR 9625839987Battery Packs · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACKS. OPERATIONAL CHECK NORMAL.Dec 2, 1996 · N987US · Doug DC932 · Emergency LightingSDR 9625819942Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND MID-CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL.Dec 2, 1996 · N3991C · Doug DC932 · Emergency LightingSDR 9625559917Fuel Pump · failedDURING TAKEOFF ROLL, A/C EXPERIENCED A UNDETERMINED ENGINE STALL. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED ENGINE INLETS, OUTLETS AND PS3 SCREENS ON BOTH ENGINES. THE NUMBER ONE ENGINE FUEL PUMP ASSEMBLY WAS REPLACED, OPS AND LEAK CHDec 1, 1996 · N967N · Doug DC932 · Engine Fuel PumpSDR CA970129010Compressor · damaged(CAN) SHORTLY AFTER TAKEOFF AT APPROXIMATELY 500 FEET THE CREW HEARD A LOUD BANG COMPRESSOR STALL, THEN A SECOND ONE. THE RIGHT ENGINE EGT WENT TO THE HIGH ZONE. THE #2 ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. POST FLIGHT INSPECTIONNov 30, 1996 · Doug DC932 · Turbine Engine Compressor SectionSDR 9625719604Latch Assembly · out of adjustDURING CLIMB, RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED RIGHT MAIN GEAR DOOR LATCH MECHANSIM.Nov 30, 1996 · N604NW · Doug DC932 · Landing Gear Door Retract SectionSDR 9625699916Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 16 AND 20 INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Nov 30, 1996 · N949N · Doug DC932 · Emergency LightingSDR 9625689942Battery · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND LEFT AND RIGHT AFT OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL.Nov 30, 1996 · N3991C · Doug DC932 · Emergency LightingSDR CA970129012Tire · blown(CAN) DURING TAKEOFF ROLL, AIRCRAFT MADE A LURCH TO THE RIGHT ACCOMPANIED BY COMPRESSOR POP AND BLIP IN RIGHT ENGINE PRESSURE RATIO AND FOLLOWED BY A BURNING RUBBER SMELL. ALL INDICATIONS SUBSEQUENTLY RETURNED TO NORMAL. MAINTENANCE INVESTIGATION REVEALED #4 TNov 29, 1996 · Doug DC932 · TireSDR 96ZZZX6047Seat Track · corrosionDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE RIGHT OUTBOARD SEAT TRACK FROM STA 930 TO STA 935. DRILL OUT SEATED TRACK, BUT SEAT TRACK OUT. FAB NEW SEAT TRACK DRILL UP NEW, DEBURRED HOLES, INSTALLED SEAT TRACK AND SPLICE PART, IAW DNov 29, 1996 · N921VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR 96643Skin · crackedDURING C-CHECK, FOUND SKIN CRACKED ON LOWER SIDE OF LEADING EDGE NEAR INBD END OF FUELING PANEL AT STA XFS 247. INSTALLED DOUBLER REPAIR IAW DAC TELEX MISC/K5L.Nov 29, 1996 · N401ME · Doug DC932 · Wing, Plate/SkinSDR 9625669604Uplock Switch · malfunctionedRIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. REPLACED RIGHT MAIN GEAR UPLOCK SWITCH AND CONNECTOR, OPERATIONAL CHECK NORMAL ON GEAR SWING.Nov 29, 1996 · N604NW · Doug DC932 · Landing Gear Position and WarningSDR 961128001Oil Cap · looseDTW - FLT 423 - IN CLIMB CONFIGURATION, FLIGHT CREW OBSERVED NR 1 ENGINE OIL QUANTITY DECREASE FROM 16 QUARTS TO 6 QUARTS. RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENGINE OIL TANK SERVICE CAP NOT SECURED. SERVICED ENGINE WITH OIL, SECURED OINov 28, 1996 · N12505 · Doug DC932 · Turbine Engine Oil SystemSDR CALA9601888Spar Web · crackedINSPECTION FOUND A 2 INCH CRACK IN OUTBOARD RADIUS OF RT WING TRAILING EDGE REAR SPAR WEB AT STA XCW 58. THE AREA WAS REPAIRED IAW DOUGLAS DRAWING 593528.Nov 27, 1996 · N17531 · Doug DC932 · Wing SparSDR 97ZZZX1765Seat Track · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL,THE LT SEAT TRACK INBOARD, STA 200 - STA 240, WAS FOUND CORRODED BEYOND LIMITS. REMOVED CORRODED SECTION OF TRACK, FABBED AND INSTALLED NEW SECTION AND SPLICE IAW DC9 SRM'S 51-30-1, 51-30-2, 51-10-3,Nov 27, 1996 · N921VV · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR 97ZZZM4Switch · out of adjustDTW - FLT 927 - TAIL CONE WARNING LIGHT FLICKERED ON LANDING ROLL. CHECKED SECURITY OF TAILCONE AND TAILCONE ATTACH HANDLES, ALL CHECKED NORMAL. FOUND TAIL CONE MICROSWITCH TO BE OUT OF ADJUSTMENT, ADJUSTED MICROSWITCH AND ACCOMPLISHED TAIL CONE DROP CHECK, Nov 27, 1996 · N942ML · Doug DC932 · Door Warning SystemSDR 96642Hydraulic Line · loosePILOT REPORTS, POSSIBLE SMOKE OR MIST IN CABIN WHILE OPERATING RT PACK WITH APU. FOUND LEAKING HYDRAULIC LINE IN AFT ACCESSORY COMPARTMENT NEAR APU INTAKE. TIGHTENED LINE, CLEANED AIRBOX AND APU DOORS, RAN APU AND RT PACK AND NO SMOKE OR MIST PRESENT.Nov 27, 1996 · N207ME · Doug DC932 · Hydraulic System, MainSDR 9627769609Thermostat · malfunctionedLEFT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED AS TAKEOFF THRUST WAS APPLIED. ABORTED TAKEOFF AT 50 KNOTS AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT ANTICIPATOR AND THERMOSTAT, OPERATIONAL CHECK NORMAL.Nov 27, 1996 · N609NW · Doug DC932 · Airfoil Anti/De-ice SystemSDR CALA9601895Longeron · crackedINSPECTION FOUND A 1 INCH CRACK IN LONGERON 16L AT STA 965. THE LONGERON WAS REPLACED IAW SRM 53-02.Nov 26, 1996 · N17531 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9601894Longeron · crackedINSPECTION FOUND A .75 INCH CRACK IN LONGERON 12L, 12R, AND 13R AT STA 965. SPLICE REPAIRS WERE INSTALLED IAW SRM 53-02, FIGURE 2A.Nov 26, 1996 · N17531 · Doug DC932 · Fuselage Main, Longeron/StringerSDR CALA9601879Angle · crackedINSPECTION FOUND A 1.75 INCH CRACK IN FORWARD E AND E COMPARTMENT ATTACH ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-02.Nov 26, 1996 · N17531 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9601778Longeron · crackedINSPECTION FOUND A 1 INCH CRACK IN LONGERON 17L AT STA 965. A LONGERON REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 2A.Nov 26, 1996 · N17531 · Doug DC932 · Fuselage Main, Longeron/StringerSDR 97ZZZM294Longeron · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND A 2 INCH CRACK IN THE FORWARD PIT AT FS 389 LONGERON 30. REMOVED CORROSION MATERIAL LOSS .001 TO .002 WITHIN LIMITS TREATED AND PRIMED IAW DC-9 SRM 51-10-3, 51-30-3. (M)Nov 26, 1996 · N922VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR 97ZZZM281Longeron · corrosionDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND CORROSION IN THE E/E COMP AT L30 FROM STATION 160 TO 218. LONGERON 30 CORRODED BEYOND LIMITS IAW DC-9 SRM 53-01. LONGERON REMOVED BETWEEN STATION 160 AND STATION 229. NEW LONGERON FABRICATED IANov 26, 1996 · N922VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR 97ZZZM277Frame · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND A CRACK IN THE FORWARD PIT FRAME AT FS 408 AND LONGERON 30, FRAME CRACKED AT BOTTOM. CUT OUT CRACKED SEGMENT OF FRAME AND FORWARD NEW SEGMENT AND SPLICE IAW DC-9 SRM 53-03 FIG 2A HEAT TREATED SEGNov 26, 1996 · N922VV · Doug DC932 · Fuselage Main, FrameSDR 97ZZZM24Frame · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND CORROSION TO BE BEYOND LIMITS AT THE FORWARD CARGO PIT FRAME STATION 522 FROM STRINGER 28R TO STRINGER 29L. (M)Nov 26, 1996 · N921VV · Doug DC932 · Fuselage Main, FrameSDR 97ZZZM141Frame · crackedDURING A SCHEDULED INSPECTION AT AERO CORP, A CRACK WAS FOUND IN THE FORWARD PIT FRAME AT FS 408 AND LONGERON 30.Nov 26, 1996 · N922VV · Doug DC932 · Fuselage Main, FrameSDR 97ZZZM135Longeron · crackedDURNING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND A CRACK IN THE FORWARD PIT FRAME AT FS 408 AND LONGERON 30. (M)Nov 26, 1996 · N922VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR 96641Power Supply · inoperativeDURING SERVICE CHECK, FOUND AFT EMERGENCY LIGHTS WOULD NOT TEST. REMOVED AND REPLACED BATTERY PWR SUPPLY, OPS CHECK GOOD.Nov 26, 1996 · N206ME · Doug DC932 · Emergency LightingSDR 96640Power Supply · inoperativeDURING A CHECK, FOUND BOTH OVERWING EMERGENCY EXIT FWD SIGNS WOULD NOT ILLUMINATE. REMOVED AND REPLACED OVERWING EXIT SIGN BATTERY POWER SUPPLY, OPS CHK GOOD.Nov 26, 1996 · N502ME · Doug DC932 · Emergency LightingSDR 9625369604Downlock Switch · malfunctionedRIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED DOWNLOCK SWITCH, CLEANED AND LUBED UPLOCK MECHANISM AND REPLACED LOOSE RIVETS FOR SEQUENCE MECHANISM ON DOOR, Nov 25, 1996 · N604NW · Doug DC932 · Landing Gear Position and WarningSDR MWEA96639Skin · crackedDURING C-CHECK, FOUND SKIN CRACKED AT STA 1132 ON LEFT SIDE NEAR RAIN GUTTER. INSTALLED SKIN SPLICE REPAIR IAW SRM 53-01 FIG 2 SHEET 3.Nov 24, 1996 · N401ME · Doug DC932 · Fuselage Main, Plate/SkinSDR CALA9601881Fittings · crackedINSPECTION FOUND A .5 INCH CRACK IN EACH OF THREE END FITTINGS AT AFT CARGO DOOR BEAM NR 1, NR 2 AND NR 4. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-00.Nov 24, 1996 · N17531 · Doug DC932 · Cargo/Baggage DoorsSDR CALA9601880Angle · crackedINSPECTION FOUND A .25 INCH CRACK IN RADIUS OF ANGLE IN FORWARD BAGGAGE BIN AT DOOR UPPER AFT CORNER. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-3.Nov 24, 1996 · N17531 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9601777Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR BEAM NR 3 FORWARD END FITTING. A NEW FITTING WAS INSTALLED IAW SRM 51-30-0.Nov 24, 1996 · N17531 · Doug DC932 · Cargo/Baggage DoorsSDR CA970129011Slat · damaged(CAN) NO SLAT EXTEND LIGHT ON AND SLAT DISAGREE LIGHT ON. LOUD BANG HEARD AT FLAPS 40 DEGREES. TROUBLESHOOTING FOUND SLAT L/H #1 IDLER EXTEND BRACKET BROKEN. MAINTENANCE REPLACED #2 L/H SLAT AND NEW L/H #1 IDLER BRACKET INSTALLED. OPERATIONAL CHECK CARRIED OUTNov 24, 1996 · Doug DC932 · Leading Edge Slat Control SystemSDR CA970129009Duct · damaged(CAN) AT FLIGHT LEVEL 350 PRESSURIZATION UNCONTROLLABLE FLOW LIGHT CAME ON. EMERGENCY DESCENT CARRIED OUT. MAINTENANCE TROUBLESHOOTING FOUND DUCTING ON LEFT HAND AIR CYCLING MACHINE DETACHED AND DUCTING ON RH PACK CRACKED AND FLEX CONNECTOR BROKEN. DUCTING ON Nov 24, 1996 · Doug DC932 · Air Distribution SystemSDR 9625269986Power Supply · inoperativeDURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 5 AND 9 INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL.Nov 24, 1996 · N986US · Doug DC932 · Emergency LightingSDR VJ960003R1Wire · failedMCO-ATL - FLT 116 - A/C RETURNED TO MCO ON CLIMB-OUT, AS PRECAUTION DUE TO BURNING ODOR IN CABIN, REPORTED BY PAX. A F/A REPORTED TO MX REP THAT A SMALL AMOUNT OF SMOKE WAS SEEN DURING LANDING. PRELIMINARY FINDINGS INDICATED LEFT GROUND POWER WIRE AT FLOOR LNov 23, 1996 · N933VV · Doug DC932 · Light System WiringSDR CA970129008Hydraulic Line · leaking(CAN) DURING TEST FLIGHT, RIGHT HYDRAULIC FLUID LOST. HYDRAULIC BRAKE PRESSURE READ 3400 P.S.I. PRIOR TO PRESSURE LOSS. NEW HYDRAULIC LINE FABRICATED AND INSTALLED AND LEAK CHECKED SERVICEABLE.Nov 23, 1996 · Doug DC932 · Hydraulic System, MainSDR MWEA96638Skin · crackedDURING INSPECTION, FOUND CRACK IN FUSELAGE SKIN AT LOWER AFT CORNER OF FWD AIRSTAIR DOOR CUTOUT. INSTALLED TEMPORARY REPAIR IAW SRM 53-05 FIG 57A SHEET 2. WILL INSTALL PERMANENT REPAIR AT D-CHECK.Nov 22, 1996 · N204ME · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA96637Longeron · crackedDURING INSPECTION, FOUND LONGERON 2R CRACKED AT STA 756. MAINTENANCE INSTALLED SPLICE REPAIR IAW DOUGLAS SERVICE REWORK DRAWING NUMBER SR09530128.Nov 22, 1996 · N204ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR 97ZZZX1767Longeron · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND .75 INCH CRACK AT FASTENER HOLE LONGERON 12R STA 645. REMOVED CRACKED AREA. FABBED AND INSTALLED 2 EACH STACKED ANGLE REPAIRS IAW DC9 SRM'S 53-01 FIG 2 AND 51-10-3.Nov 22, 1996 · N921VV · Doug DC932 · Fuselage Main, Longeron/StringerSDR 97ZZZX1766Floor Beam · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, STA 997 FL6OR BEAM CHAFED AND CORRODED FROM RBL 48 TO LBL 48. REMOVED FLOOR BEAM ANGLE, INSTALLED NEW ANGLE IAW DC9 SRM'S 53-11-3 FIG 11, 51-10-4, 51-10-3, AND 51-30-2.Nov 22, 1996 · N921VV · Doug DC932 · Fuselage Main, Floor BeamSDR 9625359604Connector · looseRIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. ON APPROACH, SPOILERS WOULD NOT ARM. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT MAIN GEAR UPLOCK SWITCH CANNON PLUG Nov 22, 1996 · N604NW · Doug DC932 · Landing Gear Position and WarningSDR 9625209924Slide · low batteryDURING PERIODIC CHECK, FOUND FORWARD GALLEY SERVICE DOOR EVACUATION SLIDE BATTERY PACK INOPERATIVE. REPLACED SLIDE.Nov 22, 1996 · N926RC · Doug DC932 · Escape Slide
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