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 95ZZZX6377Fuel Tank · overfilledATL - FLT 276 - AFTER TAKEOFF, AIRCRAFT EXPERIENCED FUEL VENTING OVERBOARD. AIRCRAFT RETURNED TO ATL. FOUND LT WING INDICATION READING LOW. WING OVER-SERVICED, BACK FLUSHED FUEL, NO TRANSFER OCCURRED.Sep 28, 1995 · N915VV · Doug DC932 · Fuel StorageSDR 95ZZZX6369Oil System · leakingPHL/ATL - FLT 219 - AT THE GATE IN PHL, THE FLIGHT CREW FOUND SMOKE IN THE CABIN. FOUND APU (PN GTCP8598D) LEAKING OIL CAUSING SMOKE IN THE CABIN; THE APU WAS PLACED ON MEL.Sep 28, 1995 · N902VJ · Doug DC932 · APU Oil SystemSDR 9515189613Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE RIGHT FLAP NR 1 WEDGE UPPER OUTBOARD FORWARD CORNER FITTING. REPLACED FITTING PER DWG 5912992 AND SRM 51-30, 51-10.Sep 28, 1995 · N613NW · Doug DC932 · Trailing Edge FlapsSDR MWEA95326Oil Press Wire · brokenTEN MINUTES INTO FLIGHT, LEFT ENGINE OIL PRESSURE BEGAN TO FLUCTUATE AND ALL OTHER INDICATIONS WERE NORMAL. TWENTY MINUTES INTO FLIGHT, LEFT ENGINE OIL PRESSURE DROPPED TO ZERO AND OIL PRESSURE LOW LIGHT AND OTHER INDICATIONS NORMAL. ACFT RETURNED TO MKE. FSep 27, 1995 · N602ME · Doug DC932 · Engine Oil PressureSDR MWEA95325Regulator · intermittentDURING TAKEOFF AT APPROXIMATELY 100 KTS, THE LEFT ENGINE OIL PRESSURE WAS SLIGHTLY ABOVE 80 PSI. ABORTED TAKEOFF, RETURNED TO BLOCK. REPLACED REGULATOR PER MM 79-32 AND ADJUSTED TO PROPER LIMITS. RUN UP, LEAK AND OPS CHECK GOOD.Sep 27, 1995 · N602ME · Doug DC932 · Engine Oil PressureSDR CAL950909Skin · crackedHOU - INSPECTION FOUND A 1 INCH CRACK AT RIVET OF FUSELAGE SKIN STATION 990, LONGERON 14L. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 41. (M)Sep 27, 1995 · N12539 · Doug DC932 · Fuselage Main, Plate/SkinSDR CAL950908Frame · corrodedHOU - INSPECTION FOUND CORROSION ON BELT FRAME IN AFT BAGGAGE BIN AT STATION 870. THE CORROSION WAS REMOVED AFTER REMOVING THE FASTENERS. THE AREA WAS ALODINED AND PRIMED AND THE FASTENERS WERE REINSTALLED. THE REPAIR WAS PERFORMED IAW SRM 51-10-3 AND 51-30Sep 27, 1995 · N12539 · Doug DC932 · Fuselage Main, FrameSDR CAL950907Window Frame · crackedHOU - INSPECTION FOUND A .25 INCH CRACK IN LEFT WINDOW NR 23 FRAME. THE FRAME WAS REPAIRED IAW SRM 53-01, FIGURE 2. (M)Sep 27, 1995 · N12539 · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL950883Blkhd Angle · crackedHOU - INSPECTION FOUND A 1 INCH CRACK IN ANGLE CLIP ON AFT PRESSURE BULKHEAD AT OUTBOARD NR 1L HORIZONTAL BEAM. THE CLIP WAS REMOVED AND A NEW CLIP INSTALLED PER DOUGLAS DRAWING 991558. (X)Sep 27, 1995 · N12539 · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9600151Keel Beam · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT CANTED KEEL OUTBOARD RAIL CORRODED. REPAIRED CANTED KEEL IAW ABX REA D953-12923-MR.Sep 27, 1995 · N989AX · Doug DC932 · Fuselage Main, KeelSDR ABXA9500953Panel · delaminatedDURING C-CHECK INSPECTION AND COMPLIANCE WITH AD 92-22-08, FOUND LEFT WING UPPER BONDED PANEL FORWARD OF AILERON DELAMINATED. REPLACED PANEL IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.Sep 27, 1995 · N982AX · Doug DC932 · Wing, Plate/SkinSDR 9515149603Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LONGERON 23R ATTACH FITTING AT FS 996. REPLACED FITTING PER SRM 51-30-2.Sep 27, 1995 · N603NW · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL950930Belt Frame · corrodedHOU - INSPECTION FOUND CORROSION ON BELTFRAME FROM LONGERON 25L TO 24R AT STATION 832. THE CORROSION WAS REMOVED. A DOUBLER AND REPAIR ANGLE WERE INSTALLED IAW SRM 53-03, FIGURE 5. (M)Sep 26, 1995 · N12539 · Doug DC932 · Fuselage Main, FrameSDR CAL950884Angle · crackedHOU - INSPECTION FOUND A 1 INCH CRACK IN LT WING L/E SPLICE ANGLE BETWEEN NR 3 AND NR 4 SLAT TRACKS. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-0. (X)Sep 25, 1995 · N12539 · Doug DC932 · Wing Miscellaneous StructureSDR CAL50885Skin · crackedHOU - INSPECTION FOUND SKIN AND DOUBLER CRACKED AND BULGED AT STA 579, LONGERONS 29L-29R. THREE CRACKS WERE FOUND AND MEASURED .25 INCH, .50 INCH, AND .75 INCH LONG. THE SKIN AND DOUBLER WERE REPAIRED IAW SRM 53-04, FIGURE 43. (X)Sep 25, 1995 · N12539 · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9600167Frame · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE LEFT FUSELAGE FRAME AT FS 718 CRACKED FROM THE FORWARD BOLT HOLE UP TO AND BEYOND A PREVIOUS REPAIR. REPLACED FUSELAGE FRAME IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-3 AND 51-30-5.Sep 25, 1995 · N989AX · Doug DC932 · Fuselage Main, FrameSDR MWEA95322Portable Fire-X · leakedFORWARD FLIGHT ATTENDANT'S PORTABLE HALON FIRE EXTINGUISHER, FOUND LEAKED DOWN TO ZERO. REPLACED THE FIRE EXTINGUISHER WITH A SERVICEABLE UNIT.Sep 24, 1995 · N203ME · Doug DC932 · Fire Bottle, PortableSDR MWEA95321Eel · dimFORWARD OVERWING EXIT EMERGENCY LIGHTS DIM ON LEFT AND RIGHT SIDES. OPS CHECKED EMERGENCY LIGHT SYSTEM AND FOUND ALL LIGHTS TO WORK.Sep 24, 1995 · N502ME · Doug DC932 · Emergency LightingSDR MWEA95320Skin · crackedSKIN AROUND LEFT AFT NOSE GEAR DOOR AFT HINGE HAS A PROGRESSING CRACK THROUGH 2 STOP DRILLS. INSTALLED DOUBLER AROUND NOSE GEAR HINGE POINT IAW SRM 53-05 FIGURE 62.Sep 23, 1995 · N202ME · Doug DC932 · Landing Gear DoorsSDR MWEA95319Door Beam · crackedGALLEY SERVICE DOOR UPPER HORIZONTAL BEAM CRACKED .6250 INCH, AT FORWARD END OF THE OUTER RADIUS. REMOVED DOOR AND REPAIRED CRACK IAW SERVICE REWORK DRAWING 5939988. REINSTALLED DOOR, OPS AND PRESSURE CHECKED.Sep 23, 1995 · N202ME · Doug DC932 · Galley DoorsSDR MWEA95318Portable Fire-X · brokenFORWARD CABIN HALON FIRE EXTINGUISHER HANDLE BROKE IN HALF, AS THE FLIGHT ATTENDANT WAS CHECKING IT OVER PRIOR TO FLIGHT. REMOVED AND REPLACED WITH A SERVICEABLE EXTINGUISHER.Sep 23, 1995 · N502ME · Doug DC932 · Fire Bottle, PortableSDR MWEA95317Evac Slide · low pressureMAIN DOOR SLIDE FOUND LOW ON PRESSURE. REMOVED AND REPLACED CABIN DOOR SLIDE WITH A SERVICEABLE UNIT.Sep 23, 1995 · N401ME · Doug DC932 · Escape SlideSDR 95ZZZM557Temp Control Vlv · failedFLT NR 238 - DFW-ATL - FLIGHT ATTENDANTS ON CLIMB-OUT REPORTED SMOKE IN THE CABIN. AIRCRAFT RETURNED TO DFW. MAINTENANCE CHECKED SYSTEMS AND FOUND RIGHT PACK TEMPERATURE CONTROL VALVE AT FAULT, PLACED ON MEL LOG, PAGE 4928.Sep 23, 1995 · N934VV · Doug DC932 · Cabin Cooling SystemSDR MWEA95316Smoke Detector · failedLEFT HAND SMOKE DETECTOR INOP UPON TESTING WARNING FUNCTION. REMOVED AND REPLACED SMOKE DETECTOR AND OPS CHECK GOOD.Sep 22, 1995 · N502ME · Doug DC932 · Smoke DetectionSDR CAL950863Skin · crackedIAH - INSPECTION FOUND A .75 INCH CRACK IN FORWARD CABIN DOOR SKIN AT HOLD OPEN HOOK CUTOUT. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5210-01235. (M)Sep 22, 1995 · N27522 · Doug DC932 · Passenger/Crew DoorsSDR CA960110501Switch · inoperative(CAN)DURING CLIMB, RIGHT ENGINE OIL STRAINER CLOGGING LIGHT CAME ON. RIGHT ENGINE SHUTDOWN. MAINTENANCE CHECK FOUND 13TH STAGE AIR ANTI-ICE DUCT UNDONE AT ENGINE LOW OIL PRESSURE AND OIL FILTER DIFFERENTIA L PRESSURE SWITCHES. THE 13TH STAGE AIR CAUSED DAMAGE Sep 21, 1995 · Doug DC932 · Engine Oil Indicating SystemSDR ABXA9600176L0ngeron · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LONGERON 20 CORRODED AT THE LEFT TRAPEZOIDAL PANEL JUST FORWARD OF FS 737. REPLACED LONGERON 20L IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.Sep 21, 1995 · N989AX · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA9600148Skin · dentedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD FUSELAGE SKIN DENTED AT FS 237 ABOVE LONGERON 17R. REPAIRED FUSELAGE SKIN IAW ABX REA D953-12906-MR.Sep 21, 1995 · N989AX · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9600126Bushing · wornDURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 91-22-07; SB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR INTERCONNECT LINK WORN. REPLACED BUSHING AND SLEEVE ON LINK IAW DC-9 OVERHAUL MANUAL 20-10-7.Sep 21, 1995 · N989AX · Doug DC932 · Landing Gear DoorsSDR ABXA9600125Rod · wornDURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 91-22-07; SB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD DOOR CONNECTING ROD FROM THE GEAR TO DOOR ROD ENDS WORN. REPLACED ROD ENDS IAW DC-9 OVERHAUL MANUAL 20-10 AND MM 32-12-1.Sep 21, 1995 · N989AX · Doug DC932 · Landing Gear Door Retract SectionSDR ABXA9600124Door · delaminatedDURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 91-22-07; SB 32-244, FOUND THE LEFT MAIN LANDING GEAR OUTBOARD FLYING DOOR DELAMINATED. REPLACED LEFT FLYING DOOR IAW DC-9 MM 32-12-1.Sep 21, 1995 · N989AX · Doug DC932 · Landing Gear DoorsSDR CAL950844Jamb Door · dentedHOU - INSPECTION FOUND A DENT IN THE FORWARD SERVICE DOOR AFT JAMB. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 42. (M)Sep 20, 1995 · N15525 · Doug DC932 · Fuselage Main, Attach FittingsSDR ABXA9600140Angle · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE CUSP WEB ANGLE CRACKED FORWARD OF FS 218. REPAIRED CUSP WEB ANGLE IAW ABX REA D-953-12721-MR.Sep 20, 1995 · N989AX · Doug DC932 · Fuselage Miscellaneous StructureSDR 95ZZZX6376Fuel Heat Valve · failedNR 1 ENGINE OIL TEMPERATURE EXCEEDED 120 DEGREES FOR 12 MINUTES, MAXIMUM TEMPERATURE, 139 DEGREES. REPLACED FUEL HEAT VALVE. DRAINED AND REPLACED ENGINE OIL. REMOVED AND REPLACED OIL SCREEN PER MM 72-00, 518C. CHECKS OK. NO LEAKS ON RUN-UP.Sep 20, 1995 · N906VJ · Doug DC932 · Engine Fuel DistributionSDR 95ZZZX6284Fuel Heat Valve · failedNR 1 ENGINE OIL TEMP EXCEEDED 120 DEGREES FOR 12 MINUTES, MAXIMUM TEMP 139 DEGREES. REPLACED FUEL HEAT VALVE. DRAINED AND REPLACED ENGINE OIL. REMOVED AND REPLACED OIL SCREEN PER MM 72-00, 518C CKS OK. NO LEAKS ON RUN-UP.Sep 20, 1995 · N906VJ · Doug DC932 · Engine Fuel DistributionSDR CAL950856Skin · crackedIAH - INSPECTION FOUND A .1250 INCH CRACK IN SKIN AT STATION 996 BETWEEN LONGERONS 9 AND 10R. A REPAIR WAS FABRICATED AND INSTALLED IN REFERENCE TO DAC DRAWING J060138 AND EA 5361-01001. (M)Sep 19, 1995 · N58545 · Doug DC932 · Fuselage Main, Plate/SkinSDR ABXA9600146Spar · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON A REPAIR ON THE RIGHT WING LOWER TEE CAP AT XRS 531. REPAIRED RIGHT WING LOWER SPAR IAW ABX REA D957-12806-MR.Sep 19, 1995 · N989AX · Doug DC932 · Wing SparSDR MWEA95315Skin · punctureDURING INSPECTION, THE RT NR 1 SLAT RECEIVED A 2 INCH DIAMETER PUNCTURE HOLE, WHEN INADVERTENTLY STRIKING WORK STAND. MAINTENANCE INSTALLED 30 DAY TEMPORARY PATCH REPAIR IAW DOUGLAS APPROVAL AND SRM 57-09 FIG 10A. RETURNED A/C TO SERVICE.Sep 18, 1995 · N204ME · Doug DC932 · Leading Edge DevicesSDR MWEA95314Frame · crackedDURING C-CHECK, FOUND FRAME CRACKED IN 2 PLACES AT FUS STA 1076, LONGERON 2 LT AND 2 RT. MAINTENANCE SPLICED IN NEW SECTION OF FRAME IAW SRM 53-02 FIG 32. RETURNED A/C TO SERVICE.Sep 18, 1995 · N602ME · Doug DC932 · Fuselage Main, FrameSDR MWEA95313Angle · crackedDURING C-CHECK, THE ATTACH ANGLE AT STA 1076 LONGERON 2L WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED ATTACH ANGLE WITH DOUGLAS PART IAW SRM 53-01. RETURNED A/C TO SERVICE.Sep 18, 1995 · N602ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA95312Angle · crackedDURING C-CHECK, FOUND FRAME ATTACH ANGLE CRACKED AT STA 1075, LONGERON 2R. MAINTENANCE REMOVED AND REPLACED ANGLE WITH DOUGLAS PART IAW SRM 53-01.Sep 18, 1995 · N602ME · Doug DC932 · Fuselage Miscellaneous StructureSDR 9514879921Skin · crackedDURING B-CHECK, FOUND A .5 INCH CRACK IN THE FORWARD AIRSTAIR DOOR JAMB SKIN, LOWER AFT CORNER. REPAIRED DOOR JAMB PER EA 99-99068.Sep 18, 1995 · N943N · Doug DC932 · Fuselage Main, Plate/SkinSDR 9514369921Unsafe Light · illuminatedRIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. CLEANED, LUBED UPLATCH MECHANISMS, ADJUSTED DOOR ROLLER AND CYCLED GEAR NUMEROUS TIMES. ALL INDICATIONS CHECKED NORMAL AND AIRCRAFT RSep 18, 1995 · N943N · Doug DC932 · Landing Gear Position and WarningSDR CAL950842Skin · crackedHOU - INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT STATION 1038 BETWEEN LONGERON 10R AND 11R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, PAGE 8. (M)Sep 17, 1995 · N15525 · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA95311Eel Power Supply · malfunctionedDURING C-CHECK, THE CABIN EMERGENCY LIGHTS OVER ROWS 1 THROUGH 14 WERE VERY DIM. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY FOR OVERHEAD EMERGENCY LIGHTS. OP CHECK GOOD AND RETURNED A/C TO SERVICE.Sep 16, 1995 · N602ME · Doug DC932 · Emergency LightingSDR MWEA95310Angle · crackedDURING C-CHECK, FOUND 3 CRACKED FITTINGS ON AFT ENTRANCE DOOR FRAME, INTERNAL STRUCTURE. MAINTENANCE REMOVED AND REPLACED FITTINGS WITH NEW DOUGLAS PARTS IAW DAC DRAWING 9915565. RETURNED A/C TO SERVICE.Sep 16, 1995 · N602ME · Doug DC932 · Fuselage Miscellaneous StructureSDR CAL950845Longeron · corrodedHOU - INSPECTION FOUND CORROSION ON LONGERON 30 IN AFT BAGGAGE BIN FROM STATION 935 TO 990. THE CORRODED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION WAS SPLICED IN PER SRM 53-02, FIG 16. (M)Sep 16, 1995 · N15525 · Doug DC932 · Fuselage Main, Longeron/StringerSDR 9515519607Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE UPPER LEFT SKIN PANELS FROM XRS 90 TO 383. REPAIRED PER EA 96-100273.Sep 16, 1995 · N607NW · Doug DC932 · Wing, Plate/SkinSDR CAL950852Blkhd Web · crackedHOU - INSPECTION FOUND A 3.5 INCH CRACK ON AFT PRESSURE BULKHEAD WEB AT RIGHT EDGE OF AFT ENTRY DOOR JAMB. THE BULKHEAD WEB WAS REPAIRED IAW ECRA 5310-03164. (M)Sep 15, 1995 · N15525 · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9600168Bracket · damagedDURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 89-14-02; ASB 27-307, FOUND A PREVIOUS WELD REPAIR ON THE LEFT RUDDER PEDAL BRACKET NOT IAW THE SERVICE BULLETIN. REPLACED THE LEFT RUDDER PEDAL BRACKET IAW DC-9 MM 27-20-12.Sep 14, 1995 · N989AX · Doug DC932 · Rudder Control System
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