Douglas DC-9-14

Service difficulty reports · 1,736

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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 = 'DC914'
  ORDER BY difficulty_date DESC"

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SDR 9519359156Retract Mech · malfunctionedDURING CLIMB, A VIBRATION WAS FELT IN THE NOSE LANDING GEAR AREA. AIRCRAFT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. FOUND THE LEFT FORWARD NOSE LANDING GEAR DOOR OPEN. REPLACED GEAR DOOR, FORWARD LINK, AND DOOR STOP CABLES. OPERATIONAL CHECK GOOD.Nov 30, 1995 · N8915E · Doug DC914 · Landing Gear Door Retract SectionSDR 9518989152Eel Wire · brokenTHE EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE IN FORWARD CABIN AREA. REPAIRED SPLICE AT ROW 1, OPERATIONAL CHECK OK.Nov 23, 1995 · N8911E · Doug DC914 · Emergency LightingSDR MWEA95431Evac Slide · low pressureDURING INSPECTION, FOUND GALLEY SERVICE DOOR EVACUATION SLIDE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED GALLEY SERVICE DOOR EVACUATION SLIDE, RETURNED A/C TO SERVICE.Nov 17, 1995 · N80ME · Doug DC914 · Escape SlideSDR 9518829152Eel Track · out of adjustDURING PREFLIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTING AT FORWARD CABIN GALLEY INOPERATIVE. FOUND FLOOR LIGHTING TRACK OUT OF ALIGNMENT, ADJUSTED TRACK AND OPERATIONAL CHECK OK.Nov 17, 1995 · N8911E · Doug DC914 · Emergency LightingSDR 9517849155Battery Pack · dischargedDURING LINE CHECK, THE RIGHT OVERWING EXIT AND RIGHT CEILING EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACKS. OPERATIONAL CHECK GOOD.Nov 12, 1995 · N8914E · Doug DC914 · Emergency LightingSDR 9517899178Door Latch · out of adjustDURING CLIMB, THE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED THE LANDING GEAR AND LIGHT EXTINGUISHED. THE AIRCRAFT CONTINUED TO CMH AND LANDED WITHOUT INCIDENT. ADJUSTED THE SPRING TENSION ON THE LEFT MAIN LANDING GEAR Nov 11, 1995 · N3310N · Doug DC914 · Landing Gear Door Retract SectionSDR 9519209162Skin · corrodedDURING H-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 332 TO 351, LONGERONS 28L TO 29R. REPAIRED SKIN (P/N5911412-3), PER EA 91-103318.Nov 10, 1995 · N8907E · Doug DC914 · Fuselage Main, Plate/SkinSDR 9518319154Prbc · malfunctionedNR 2 ENGINE EXPERIENCED A COMPRESSOR STALL ON TAKEOFF. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE PRBC AND INSPECTED THE ENGINE, NO DAMAGE NOTED. SUBSEQUENT RUNUP WAS SATISFACTORY.Nov 10, 1995 · N8913E · Doug DC914 · Compressor Bleed ValveSDR MWEA95364Eel Power Supply · malfunctionedMAINTENANCE REPORTS, DURING SERVICE CHECK THE RT OVERHEAD EMERGENCY ESCAPE LIGHT WOULD NOT EXTINGUISH. MAINTENANCE REPLACED BATTERY POWER SUPPLY. OPS CHECK GOOD, RETURNED A/C TO SERVICE.Nov 8, 1995 · N500ME · Doug DC914 · Emergency LightingSDR MWEA95366Battery Pack · low chargeDURING SERVICE CHECK, FOUND FWD GALLEY AND COCKPIT OVERHEAD EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. RETURNED A/C TO SERVICE.Nov 6, 1995 · N700ME · Doug DC914 · Emergency LightingSDR MWEA95363Fuel Control · leakingCREW REPORTS, WHILE TAXIING TO GATE, STRONG FUEL ODOR PERMEATED THE CABIN AFTER STARTING APU. MAINTENANCE FOUND FUEL LEAKING FROM APU FUEL CONTROL DRAIN. REPLACED APU FUEL CONTROL, OPS AND LEAK CHECK GOOD. RETURNED A/C TO SERVICE.Nov 5, 1995 · N80ME · Doug DC914 · APU Engine Fuel and ControlSDR MWEA95362Skin · dentedCREW REPORTS BIRD STRIKE ON LEFT WING AT DCA. DURING BIRD STRIKE INSPECTION AT DCA, FOUND LEFT WING LEADING EDGE DENTED BEYOND LIMITS STA XRS 80. AIRCRAFT FERRIED TO MKE. MAINTENANCE IN MKE INSTALLED DOUBLER REPAIR IAW SRM 57-06, FIG 2 AS A TEMPORARY REPAIROct 29, 1995 · N500ME · Doug DC914 · Wing, Plate/SkinSDR MWEA95361Door Latch · out of adjustDURING INSPECTION, THE RIGHT OVERWING EMERGENCY EXIT DOOR HANDLE WAS DIFFICULT TO OPERATE. MAINTENANCE ADJUSTED DOOR LATCH IAW DAC MM 52-21-0. OPS CHECK GOOD, RETURNED A/C TO SERVICE.Oct 26, 1995 · N400ME · Doug DC914 · Emergency ExitsSDR 9518409152Connector · corrodedDURING APPROACH AT 5,000 FEET, 160 KNOTS, AND FLAPS AT 20 DEGREES, STALL WARNING STICK SHAKER ACTIVATED. EXECUTED GO-AROUND PROCEDURES AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED ON SECOND ATTEMPT. FOUND CORROSION AT THE LEFT FLAP TRANSMITTER CANNON PLUG. CLOct 19, 1995 · N8911E · Doug DC914 · Trailing Edge Flap Control SystemSDR 9516729150Fence · separatedAFTER FLIGHT ARRIVAL, MAINTENANCE DISCOVERED THAT THE LEFT WING LEADING EDGE FENCE WAS MISSING. REPLACED THE FENCE.Oct 17, 1995 · N8908E · Doug DC914 · Wing Miscellaneous StructureSDR MWEA95351Eel Batteries · dischargedCREW REPORTS, FWD EMERGENCY FLASHLIGHT AT FLT ATTENDANT STA HAS WEAK CHARGE. MAINTENANCE REMOVED AND REPLACED BATTERIES. OPS CHECK GOOD AND RETURNED A/C TO SERVICE.Oct 13, 1995 · N400ME · Doug DC914 · Emergency LightingSDR 9515339156Relay · malfunctionedAFTER TAKEOFF, AUTO PRESSURIZATION SYSTEM FAILED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED RELAY R2-55 AND OUTFLOW VALVE LINKAGE. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE.Oct 11, 1995 · N8915E · Doug DC914 · Cabin Pressure Control SystemSDR 9516029153Fitting · crackedDURING MAINTENANCE INSPECTION, FOUND A CRACK IN THE LOWER FOOT FITTING FS 69 BETWEEN CENTER WING STRINGERS 11 AND 12. REPLACED FITTING PER SRM 51-30-5.Oct 3, 1995 · N8912E · Doug DC914 · Wing Miscellaneous StructureSDR MWEA95341Girt Bar Mount · looseDURING INSPECTION, THE TAIL EVACUATION SLIDE GIRT BAR WAS FOUND LOOSE ON RIGHT MOUNT. MAINTENANCE TIGHTENED RIGHT SIDE GIRT BAR MOUNT AND RETURNED A/C TO SERVICE.Oct 1, 1995 · N400ME · Doug DC914 · Emergency EquipmentSDR MWEA95340Intercostal · crackedDURING INSPECTION, THE AFT CARGO COMPARTMENT FLOOR SUPPORT INTERCOSTAL WAS FOUND CRACKED AT STA 810 LONGERON 286 AND 28R. MAINTENANCE FABRICATED AND INSTALLED NEW INTERCOSTAL FROM 2024-T2 .050 MATERIAL IAW SRM 53-10-3 FIG 3 AND 53-01, PG 1, RETURNED A/C TO SEOct 1, 1995 · N400ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA95339Intercostal · crackedDURING INSPECTION, FOUND INTERCOSTAL CRACKED AT STA 150 RT SIDES, JUST FWD OF GALLEY SERVICE DOOR 54 ABOVE CUSP LINE. MAINTENANCE FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 53-01 FIG 2 SHT 4, RETURNED A/C TO SERVICE.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA95338Frame · crackedDURING INSPECTION, 3 FRAMES WERE FOUND CRACKED IN KEEL BEAM AREA AT STA 503, 525, 544, ALL ON OUTBD AND RT SIDE. MAINTENANCE FABRICATED AND INSTALLED ANGLE REPAIRS IAW SRM 53-03 FIG 12.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage Main, FrameSDR MWEA95337Frame · corrodedDURING INSPECTION, FOUND FRAME AT STA 566 IN KEEL AREA CORRODED BEYOND LIMITS. MAINTENANCE BLENDED CORROSION AND INSTALLED ANGLE REPAIR IAW SRM 53-03 FIG 12.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage Main, FrameSDR MWEA95336Frame · crackedDURING INSPECTION, FOUND FRAMES AT STA 525 AND 544 CRACKED ON OUTBD END LT SIDE OF KEEL AREA. MAINTENANCE FABRICATED AND INSTALLED ANGLE REPAIRS IAW SRM 53-02 FIG 12, RETURNED A/C TO SERVICE.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage Main, FrameSDR MWEA95335Fitting · crackedDURING INSPECTION, IN THE KEEL BEAM AREA AN ATTACH FITTING WAS FOUND CORRODED AT STA 562. MAINTENANCE INSTALLED ANGLE REPAIR IAW SRM 53-01 FIG 2 SHT 4, RETURNED A/C TO SERVICE.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA95334Longeron · corrodedDURING INSPECTION, LONGERON 30 AT STA 661 WAS FOUND CORRODED BEYOND LIMITS UNDER FLANGE AT FRAME ATTACH POINT. MAINTENANCE REMOVED AND REPLACED LONGERON IAW SRM 53-01 PG 1, RETURNED A/C TO SERVICE.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA95333Angle · corrodedDURING INSPECTION, FOUND MODERATE CORROSION IN GALLEY SERVICE DOOR JAMB FORWARD LOWER POCKET, HORIZONTAL BEAM. MAINTENANCE BLENDED CORROSION AND FOUND TO BE BEYOND LIMITS. INSTALLED ANGLE REPAIR IAW SRM 53-05 FIG 55, RETURNED A/C TO SERVICE.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA95332Floorbeam · chafedDURING INSPECTION, FOUND FLOORBEAM AT STA 256, 275, 408, AND 465 CHAFED FROM FLOOR CENTER PANELS. MAINTENANCE FABRICATED AND INSTALLED WEAR STRIP REPAIR IAW SRM 53-05 FIG 20A, RETURNED A/C TO SERVICE.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage Main, Floor BeamSDR MWEA95331Frame · corrodedDURING INSPECTION, THE FRAME AT STA 661 LONGERON 30 IN AFT CARGO COMPT, WAS FOUND CORRODED. MAINTENANCE BLENDED CORROSION AND INSTALLED DOUBLER REPAIR IAW SRM 53-03 FIG 2A SHT 1, RETURNED A/C TO SERVICE.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage Main, FrameSDR MWEA95330Frame · corrodedDURING INSPECTION, THE FRAME AT STA 680 LONGERON 30 IN AFT CARGO COMPT, WAS FOUND CORRODED. MAINTENANCE BLENDED CORROSION AND INSTALLED DOUBLER REPAIR IAW SRM 53-03 FIG 2A, RETURNED A/C TO SERVICE.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage Main, FrameSDR MWEA95329Frame · corrodedDURING INSPECTION, FOUND FRAME IN AFT CARGO COMPT STA 786 LONGERON 30, WAS CORRODED.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage Main, FrameSDR MWEA95328Seat Track · corrodedDURING INSPECTION, FOUND MODERATE CORROSION ON NR 2 SEAT TRACK AT STA 217. CORROSION REMOVAL WAS BEYOND LIMITS. INSTALLED NEW SECTION OF SEAT TRACK IAW SRM 51-30-5, RETURNED A/C TO SERVICE.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA95327Door Jamb · corrodedDURING INSPECTION, FOUND AFT CARGO DOOR JAMB CORRODED UNDER DOOR CUTOUT PAN. REMOVED CORROSION AND INSTALLED SECTION OF DOOR PAN IAW 53-05 FIG HH SHT 4, RETURNED A/C TO SERVICE.Oct 1, 1995 · N400ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA95323Slide Cover · fell offGALLEY DOOR SLIDE COVER CAME OFF WHEN OPENED FOR CATERING TRUCK. REPOSITIONED SLIDE IN HOLDER AND REINSTALLED THE DOOR SLIDE COVER.Sep 26, 1995 · N80ME · Doug DC914 · Emergency EquipmentSDR 9514429162Brake Switch · malfunctionedAFTER TAKEOFF, PRIMARY TRIM SWITCH ON CAPTAIN'S YOKE WAS INOPERATIVE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED STABILIZER BRAKE SWITCH AT AFT PEDESTAL. OPERATIONAL CHECK OK AND AIRCRAFT RETURNED TO SERVICE.Sep 22, 1995 · N8907E · Doug DC914 · Stabilizer Control SystemSDR MWEA95307Skin · crackedDURING INSPECTION, THE FWD CARGO DOOR SKIN WAS FOUND CRACKED ON FWD LOWER CORNER APPROX .75 INCH LENGTH. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 52-05 FIG 4 PG 5, RETURNED A/C TO SERVICE.Sep 17, 1995 · N80ME · Doug DC914 · Cargo/Baggage DoorsSDR MWEA95306Evac Slide · deployedDURING INSPECTION, TAIL EVACUATION SLIDE INADVERTENTLY DEPLOYED WHILE INSTALLING. MAINTENANCE INSTALLED NEW TAIL EVACUATION SLIDE AND RETURNED A/C TO SERVICE.Sep 15, 1995 · N700ME · Doug DC914 · Escape SlideSDR MWEA95309Intercostal · crackedDURING INSPECTION, FOUND CRACKED INTERCOSTAL AT STA 642, 6 INCHES LEFT OF CENTERLINE AT FLOORBEAM LEVEL. MAINTENANCE FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 53-01 PG 9 AND 53-01 FIG 2 SHEET 4.Sep 13, 1995 · N700ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA95305Rib · crackedDURING INSPECTION, THE RT FWD ADF ANTENNA ATTACH RIB STRUCTURE WAS FOUND CRACKED, APPROX 2 INCHES LENGTH AT STA 474 LONGERON 20R. MAINTENANCE INSTALLED ANGLE REPAIR IAW SRM 53-01 FIG 2 SHEET 2, RETURNED A/C TO SERVICE.Sep 13, 1995 · N700ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA95303Inlet Bullet · crackedDURING INSPECTION, THE LEFT ENGINE NOSE INLET BULLET WAS FOUND CRACKED AT MOUNT BOLTS. MAINTENANCE REMOVED AND REPLACED NOSE INLET BULLET. OPS CHECK GOOD AND RETURNED A/C TO SERVICE.Sep 13, 1995 · N600ME · Doug DC914 · Turbine Engine Air Inlet SectionSDR MWEA95286Eel Power Supply · failedDURING SERVICE CHECK, THE GALLEY AREA EMERGENCY LIGHTS WOULD NOT COME ON WHEN AC BUSES ARE TURNED OFF. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY. OPS CHECK GOOD AND RETURNED A/C TO SERVICE.Sep 7, 1995 · N500ME · Doug DC914 · Emergency LightingSDR MWEA95295Skin · errodedDURING INSPECTION, VERTICAL STABILIZER SKIN WAS FOUND CHAFED BEYOND LIMITS UNDER LEFT AFT HORIZONTAL STAB FAIRING. MAINTENANCE FABRICATED AND INSTALLED NEW SKIN IAW SRM 55-30-0 FIG 7, 55-01 FIG 4 SHT 2. RETURNED A/C TO SERVICE.Sep 5, 1995 · N600ME · Doug DC914 · Vertical Stabilizer, Plate/SkinSDR MWEA95294Splice · crackedDURING INSPECTION, FOUND LONGERON SPLICE 13R AT STA 897 CRACKED IN TWO PLACES. MAINTENANCE REMOVED AND REPLACED LONGERON SPLICE 39164311, IAW SRM 53-10.Sep 5, 1995 · N600ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA95293Press Panel · crackedDURING INSPECTION, FOUND CRACK STA 83 IN NOSE GEAR WELL PRESSURE PANEL RUNNING UNDER CUSP ANGLE ON BOTH LEFT AND RIGHT SIDES OF GEARWELL. MAINTENANCE INSTALLED REPAIR DOUBLER, .020 CRES MATERIAL IAW SB 53-187 AND RETURNED A/C TO SERVICE.Sep 5, 1995 · N600ME · Doug DC914 · Fuselage Miscellaneous StructureSDR MWEA95292Fitting · crackedDURING INSPECTION, FOUND FITTING FOR AFT UPPER ENGINE MOUNT CRACKED AT STA 859. MAINTENANCE FABRICATED NEW FITTING IAW DAC DRAWING 5917717 AND INSTALLED IAW SRM 53-01 PG 1. RETURNED A/C TO SERVICE.Sep 5, 1995 · N600ME · Doug DC914 · Fuselage, Powerplant Attach FittingsSDR MWEA95291Floorbeam · corrodedDURING INSPECTION, THE FLOORBEAM AT STA 817 WAS FOUND MODERATELY CORRODED IN 3 AREAS. MAINTENANCE REPLACED UPPER BEAM CAP IAW SRM 53-30 AND RETURNED A/C TO SERVICE.Sep 5, 1995 · N600ME · Doug DC914 · Fuselage Main, Floor BeamSDR MWEA95290Longeron · crackedDURING INSPECTION, FOUND LONGERON 16L CRACKED AT STA 908 AFT ACCESSORY COMPARTMENT. MAINTENANCE REMOVED AND REPLACED LONGERON SECTION AT STA 908 WITH (P/N 27779225) IAW SRM 53-10-4 FIG 8 AND RETURNED A/C TO SERVICE.Sep 5, 1995 · N600ME · Doug DC914 · Fuselage Main, Longeron/StringerSDR MWEA95289Former · crackDURING INSPECTION, FOUND FORMER AT STA 880 AND L17R HAS A CRACK EMANATING FROM HOLE TO EDGE OF FORMER. MAINTENANCE INSTALLED DOUBLE ANGLE REPAIR IAW SRM 53-01 FIG 2 SHT 4 AND RETURNED A/C TO SERVICE.Sep 5, 1995 · N600ME · Doug DC914 · Fuselage Main, FrameSDR MWEA95288Frame · crackedDURING INSPECTION, FOUND FORMER AT STA 897 AND L16R CRACKED AT UPPER AND LOWER EDGES. MAINTENANCE REMOVED AND REPLACED FORMER IAW SRM 53-01 PG 1. ALSO, FABRICATED AND INSTALLED NEW FITTING IAW DAC DRWG 3959083. RETURNED A/C TO SERVICE.Sep 5, 1995 · N45725 · Doug DC914 · Fuselage Main, FrameSDR MWEA95287Skin · errodedDURING INSPECTION, THE VERTICAL STABILIZER SKIN WAS FOUND CHAFED BEYOND LIMITS UNDER THE LEFT FWD HORIZONTAL STAB FAIRING. MAINTENANCE FABRICATED AND INSTALLED NEW SKIN IAW SRM 51-10-2A, 51-30-2, 51-30-5, 55-30-0. RETURNED A/C TO SERVICE.Sep 5, 1995 · N600ME · Doug DC914 · Vertical Stabilizer, Plate/Skin
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