Douglas DC-9-32

Service difficulty reports · 12,755

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Query with SQL
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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 97ZZZM261Autopilot · malfunctionedFLT 640 - DTW - AUTOPILOT VIOLENTLY PITCHES UP AND DOWN DURING CRUISE FLIGHT. AUTOPILOT CONTINUED TO AUTOMATICALLY DISCONNECT. BOTH PILOTS HAD TO OVERRIDE THE AUTOPILOT TO MAINTAIN ALTITUDE AND CONTROL. TRANSFERRED TO DMI NR 00151 MEL 22-1 CATEGORY 'C'. (MFeb 4, 1997 · N942ML · Doug DC932 · Autopilot SystemSDR 9702439950Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN LAVATORIES INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Feb 4, 1997 · N9346 · Doug DC932 · Emergency LightingSDR 9702379618Compressor · stalledDURING TAKEOFF ROLL AT 60 KNOTS, THE LEFT ENGINE STALLED WITH ASSOCIATED DROP IN EPR INDICATION. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REPLACED THE LEFT ENGINE, OPERATIONAL CHECK OK.Feb 4, 1997 · N616NW · Doug DC932 · Turbine Engine Compressor SectionSDR MWEA97100Wire · brokenDURING TAKEOFF, ENGINE EPR DROPPED FROM 1.86 TO 1.4 PRIOR TO REACHING 60 KTS. ABORTED TAKEOFF AND RETURNED TO GATE. MAINT FOUND BROKEN WIRE BEHIND EPR INDICATOR. REMOVED AND REPLACED WIRE.Feb 3, 1997 · N206ME · Doug DC932 · Engine Indicating System WiringSDR 97ZZZM249Breaker · trippedFLT 195 - BOS - AT BOSTON AFTER ENGINE STARTS, LEFT ENGINE GENERATOR DROPPED OFF LINE. CAPTAIN RESET IT ON AND CROSS TIE LOCK OUT CAME ON. WENT BACK TO GATE AND RESET CROSS TIE. RESET LOCK OUT TIE BREAKER. OPS CHECK OK IAW 24-50. (M)Feb 3, 1997 · N12505 · Doug DC932 · AC Power Distribution SystemSDR 97ZZZM248Wheels · looseFLT 301 - ACY - NOSE GEAR VIBRATES BADLY ON TAKEOFF, FEELS OUT OF BALANCE. SNUBBER DOES NOT SEEM TO STOP IT ON GEAR UP. RE-TORQUED BOTH NOSE TIRES IAW MM CHAPTER 32-40-2. NO TIRE DEFECTS NOTED. (M)Feb 3, 1997 · N12505 · Doug DC932 · Wheel/Ski/FloatSDR 9702599916Frame · crackedDURING H-CHECK, FOUND CRACK IN CANTED FRAME AT FS 1143 BELOW VENTRAL STAIRS. REPAIRED PER EA 99-112048.Feb 3, 1997 · N949N · Doug DC932 · Fuselage Main, FrameSDR VJ970043Connector · failedCONNECTOR TO PORTABLE EMERGENCY LIGHT BROKE AT FORWARD FLIGHT ATTENDANT STATION. REPLACED PORTABLE LIGHT ASSEMBLY CONNECTOR. SYSTEM OPERATIONALLY CHECKED GOOD PER MM 33-50. (X)Feb 2, 1997 · N946VV · Doug DC932 · Emergency LightingSDR 9703069983Skin · crackedDURING A CHECK, FOUND CRACK IN SKIN 4 INCHES AFT OF E/E DOOR AND 1.5 INCHES RIGHT OF CENTER LINE. REPAIRED PER EA 99-120654.Feb 2, 1997 · N983US · Doug DC932 · Fuselage Main, Plate/SkinSDR 9702459603Connector · looseDURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 1CD INOPERATIVE. FOUND CONNECTOR UNDER SEAT TOO LOOSE, OPERATIONAL CHECK NORMAL.Feb 2, 1997 · N603NW · Doug DC932 · Emergency LightingSDR 9702429602Slide · low pressureDURING LINE MAINTENANCE INSPECTION, FOUND AFT TAILCONE EMERGENCY EVACUATION SLIDE PRESSURE LOW. REPLACED SLIDE.Feb 2, 1997 · N602NW · Doug DC932 · Escape SlideSDR 9702119919Lock Switch · out of adjustDURING APPROACH ON GEAR EXTENSION, THE NOSE GEAR SAFE GREEN LIGHT DID NOT ILLUMINATE. PERFORMED COCKPIT OPERATING MANUAL PROCEDURE AND RECYCLED GEAR, ALL INDICATIONS WERE NORMAL. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE NOSE GEAR LOCK SWITCHFeb 2, 1997 · N940N · Doug DC932 · Landing Gear Position and WarningSDR ABXA9700804Bushing · crackedDURING COMPLIANCE OF AD 91-22-07; ASB 32-244 R2 FOUND BUSHING, CRACKED ON RT SIDE OF AIRCRAFT, ON WING MOUNTED SECTION OF HINGE, MAIN LANDING GEAR DOOR. REPLACED BUSHING PER DC-9 OVERHAUL MANUAL 20-10-7.Feb 1, 1997 · N902AX · Doug DC932 · Landing Gear DoorsSDR 9702409942Slide Battery · dischargedDURING PERIODIC CHECK, FOUND FORWARD SERVICE DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE.Feb 1, 1997 · N3991C · Doug DC932 · Escape SlideSDR VJ970042Light · inoperativeSUBMITTER STATES, SUSPECT REMOVABLE HAND-HELD EMERGENCY LIGHT ASSEMBLY HAS AN INTERNAL SHORT. REPLACED EMERGENCY LIGHT ASSEMBLY PER MM 33-50. OPS CHECKED NORMAL. (M)Jan 31, 1997 · N909VJ · Doug DC932 · Emergency LightingSDR MWEA97097Augmentation Vlv · inoperativeLEFT ICE PROTECTION TEMP HIGH ANNUN ILLUMINATED, FOLLOWED SHORTLY BY LEFT AIR CONDITIONING SUPPLY TEMP HIGH ANNUN. DIVERTED TO MKE FROM OMA. MAINT REMOVED AND REPLACED LEFT AUGMENTATOR VALVE.Jan 31, 1997 · N206ME · Doug DC932 · Pneumatic Distribution SystemSDR MWEA97095Power Supply · inoperativeDURING SERVICE CHECK, FOUND RT EMERG NACELLE LIGHT INOPERATIVE -- MAINT REMOVED AND REPLACED RT NACELLE LIGHT BATTERY POWER SUPPLY. RETURNED A/C TO SERVICE.Jan 31, 1997 · N501ME · Doug DC932 · Emergency LightingSDR CA970218001Bolt · loose(CAN) UNABLE TO RETRACT FLAPS TO LESS THAN 15 DEGREES DUE TO FLAP LEVER JAMMING. TROUBLESHOOTING REVEALED FLAP CONTROL LEVER INTERFERENCE CAUSED BY LOOSE BOLT. BOLT TIGHTENED AND LEVER MECHANISM OPERATED NORMALLY CHECKED SERVICEABLE.Jan 31, 1997 · Doug DC932 · Trailing Edge Flap Control SystemSDR 9702209925Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL.Jan 31, 1997 · N925US · Doug DC932 · Emergency LightingSDR 9703569919Frame · corrodedDURING H-CHECK, FOUND CORROSION ON FRAME AT FS 408 BETWEEN LONGERONS 29L AND 29R. REPAIRED PER EA 99-112036.Jan 30, 1997 · N991N · Doug DC932 · Fuselage Main, FrameSDR 9703559919Frame · corrodedDURING H-CHECK, FOUND CORROSION ON FRAME AT LONGERON 30, FS 332. REPAIRED PER EA 99-112036.Jan 30, 1997 · N991N · Doug DC932 · Fuselage Main, FrameSDR 9701909613Strut · reqd serviceLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. PRESSURIZATION WAS ALSO INOPERATIVE. FLIGHT RETURNED TO MCI AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE LANDING GEAR STRUT LOW WHICH CAUSED AIRCRAFT TO REMAIN IN GROUND MODE. SERVICED NOSE STRUT AND REPJan 30, 1997 · N613NW · Doug DC932 · Nose/Tail Landing Gear Strut/AxleSDR CALA9700140Megaphone · inoperativeINSPECTION FOUND FORWARD CABIN MEGAPHONE INOPERATIVE. THE FORWARD CABIN MEGAPHONE WAS REPLACED.Jan 29, 1997 · N12510 · Doug DC932 · Emergency EquipmentSDR CALA9700139Megaphone · inoperativeINSPECTION FOUND AFT CABIN MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REPLACED.Jan 29, 1997 · N12510 · Doug DC932 · Emergency EquipmentSDR CALA9700111Hyd Line · leakingTHE RT HYDRAULIC SYSTEM LOST ALL QUANTITY DURING FLIGHT. ABNORMAL PROCEDURES WERE ACCOMPLISHED AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE ON RIGHT THRUST REVERSER VALVE LEAKING. THE LINE WAS REMOVED AND REPLACED. Jan 29, 1997 · N14524 · Doug DC932 · Hydraulic System, MainSDR CALA9700110Compressor · failedTHE NR 2 ENGINE INDICATIONS WENT TO ZERO DURING CLIMBOUT. THE ENGINE WAS SHUTDOWN AND CLE TOWER REPORTED THAT ENGINE WAS SMOKING. BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED SAFELY. MAINTENANCE IS IN PROCESS OF REMJan 29, 1997 · N12507 · Doug DC932 · Turbine Engine Compressor SectionSDR ABXA9700022Connector · looseON APPROACH WITH GEAR DOWN SELECTED, DID NOT GET THE RIGHT LANDING GEAR DOWN GREEN LIGHT OR THE RED GEAR UNSAFE LIGHT. RECYCLED THE LANDING GEAR 2 TIMES WITH NO RESULTS. PERFORMED ABNORMAL PROCEDURES IAW DC-9 OPS MANUAL. REPLACED PIN NR 5 ON CONNECTOR P1-129Jan 29, 1997 · N900AX · Doug DC932 · Landing Gear Position and WarningSDR CALA9700224Web · crackedINSPECTION FOUND A 1.5 INCH CRACK IN NR 1 PYLON WEB AT STA 1021. THE CRACK WAS LOCATED AT INTERSECTION WITH UPPER SKIN. THE CRACKED AREA WAS REMOVED. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 2.Jan 28, 1997 · N12532 · Doug DC932 · Nacelle/Pylon StructureSDR CALA9700223Strip · crackedINSPECTION FOUND NR 1 ENGINE PYLON STRIP ON LOWER STRUCTURE CRACKED FORWARD OF STA 1039.5. THE CRACK WAS 2 INCHES LONG. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-20-0.Jan 28, 1997 · N12532 · Doug DC932 · Nacelle/Pylon StructureSDR ABXA9700720Panel · delaminatedDURING C-CHECK, FOUND RIGHT WING INBOARD SPOILER DELAMINATED, (AD 92-22-08). REPLACED RIGHT INBOARD SPOILER PANEL IAW DC-9 MAINTENANCE MANUAL CHAPTER 27-61-01.Jan 28, 1997 · N903AX · Doug DC932 · SpoilersSDR 97ZZZM253Switch · failedDTW - FLT 626 - ON DESCENT WITH AIRFOIL ANTI-ICE ON, THE SUPPLY PRESSURE HIGH LIGHT CAME ON SEVERAL TIMES AND DUCT PRESSURE WAS 60 PSI. EACH TIME IT CORRECTED ON ITS OWN. REMOVED AND REPLACED AIRFOIL ICE PROTECTION HIGH PRESSURE SWITCH. SYSTEM OPS CHECK GOODJan 28, 1997 · N947ML · Doug DC932 · Airfoil Anti/De-ice SystemSDR 97ZZZM252Mach Trim Act · malfunctionedBUF - ACY - FLT 869 - AUTO-PILOT SEVERE PITCH UP DURING CRUISE. REMOVED AND REPLACED MACH TRIM ACTUATOR. OPS CHECK NORMAL IAW MM 22-20-1. AUTO-PILOT SYSTEM OPS CHECK NORMAL IAW MM 22-10, CLEARS DMI NR 0134, PLACARDS REMOVED. (M)Jan 28, 1997 · N942ML · Doug DC932 · Speed-Attitude Correction SystemSDR 9702359919Pressure Web · crackedDURING H-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 83 LEFT SIDE. REPAIRED PER EA 99-112018.Jan 28, 1997 · N991N · Doug DC932 · Fuselage Miscellaneous StructureSDR 9702009916Fitting · crackedDURING H-CHECK, FOUND CRACK IN LEFT SIDE OF TAIL SKID FITTING AT FS 1042. REPLACED FITTING PER SRM 51-30-5.Jan 28, 1997 · N949N · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9700740Skin · corrodedDURING C-CHECK, FOUND CORROSION ON FUSELAGE SKIN INTERIOR AT LONGERON 30, BETWEEN FS 986 AND FS 992 AND ON FITTING UNDER LONGERON 30 AT AFT PRESSURE BULKHEAD. REPLACED AFT LOWER SKIN PANEL FROM STATION FS 804 TO FS 996 AND BETWEEN LONGERON 26 LEFT TO LONGERONJan 27, 1997 · N903AX · Doug DC932 · Fuselage Main, Plate/SkinSDR 9702369919Frame · crackedDURING H-CHECK, FOUND A CRACK IN MAIN FRAME AT FS 718 IN LEFT WHEEL WELL. REPAIRED PER EA 99-112020.Jan 27, 1997 · N991N · Doug DC932 · Fuselage Main, FrameSDR 9701759982Evac Slide · low pressureDURING LINE MAINTENANCE INSPECTION, FOUND TAIL EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE.Jan 27, 1997 · N982US · Doug DC932 · Escape SlideSDR VJ970011Slide · low pressureL1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED L1 DOOR SLIDE IAW MM 25-60. (M)Jan 26, 1997 · N931VV · Doug DC932 · Escape SlideSDR MWEA97092Battery · dischargedDURING C-CHECK, FOUND LT NACELLE LIGHT INOP. MAINT REMOVED AND REPLACED BATTERY POWER SUPPLY.Jan 26, 1997 · N302ME · Doug DC932 · Emergency LightingSDR MWEA97090Power Supply · inoperativeDURING TRANSIT CHECK, FOUND FWD OVERWING EMERGENCY LIGHT INOP ON LT AND RT SIDES. MAINT REMOVED AND REPLACED BATTERY PWR SUPPLY, OPS CHECK GOOD.Jan 26, 1997 · N204ME · Doug DC932 · Emergency LightingSDR 97ZZZM231Auto-Pilot · malfunctionedFLT 174 - DTW - AUTO-PILOT PORPOISES IN ALL FLIGHT MODES. CREW DISCONTINUED USE OF AUTO-PILOT. DEFERRED PITCH ACCESS COMPUTER IAW MEL 22-1 CATEGORY C, CONTROL NR 00127. (M)Jan 26, 1997 · N947ML · Doug DC932 · Autopilot SystemSDR 9701469986Power Supply · malfunctionedDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT LIGHT AT ENTRY DOOR INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.Jan 26, 1997 · N986US · Doug DC932 · Emergency LightingSDR MWEA97093Release Mech · lack of lubeDURING C-CHECK, TAIL CONE DID NOT DROP OFF PROPERLY DURING TEST. MAINT RIGGED TAILCONE CABLES AND LUBED LATCHES IAW DOUGLAS MM 53-50-3.Jan 25, 1997 · N302ME · Doug DC932 · Aerodynamic FairingsSDR MWEA97088Floorbeam · crackedCREW REPORTS, BOTTOM PIN FWD ENTRANCE DOOR EVACUATION SLIDE CAME LOOSE. MAINT SECURED FWD ENTRANCE DOOR SLIDE.Jan 25, 1997 · N501ME · Doug DC932 · Fuselage Main, Floor BeamSDR 9702349919Pressure Web · crackedDURING H-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 83 RIGHT SIDE. REPAIRED PER EA 99-112018.Jan 25, 1997 · N991N · Doug DC932 · Fuselage Miscellaneous StructureSDR 9701659919Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON END FITTING FOR LONGERON 30 AT FS 604.5. INSTALLED NEW FITTING (P/N 3920329-502) PER SRM 51-30-2.Jan 25, 1997 · N991N · Doug DC932 · Fuselage Miscellaneous StructureSDR 9701649919Frame · crackedDURING H-CHECK, FOUND CRACK IN FRAME AT FS 465 BETWEEN LONGERON 27L AND 28L. REPAIRED PER EA 99-112040.Jan 25, 1997 · N991N · Doug DC932 · Fuselage Main, FrameSDR ABXA9700778Bulkhead Jamb · crackedDURING C-CHECK, FOUND VENTRAL DOOR JAMB CRACKED AT UPPER RIGHT CORNER. REPAIRED IAW ABX REA D953-17620-MR, D953-17964-MR.Jan 24, 1997 · N939AX · Doug DC932 · Fuselage Main, BulkheadSDR ABXA9700739Floorbeam · corrodedDURING C-CHECK, FOUND A FLOORBEAM AT FS 965 LOWER FLANGE AND STIFFENER ANGLE CORRODED NEAR LBL 50. REPAIRED IAW ABX REA D953-17930-MR.Jan 24, 1997 · N903AX · Doug DC932 · Fuselage Main, Floor BeamSDR ABXA9700738Bulkhead Jamb · crackedDURING C-CHECK, FOUND AFT PRESSURE BULKHEAD VENTRAL DOOR JAMB UPPER RIGHT CORNER HAS ONE RADIAL AND ONE BEND RADIUS CRACK. REPAIRED APB JAMB IAW ABX REA NR D953-17636-MR.Jan 24, 1997 · N903AX · Doug DC932 · Fuselage Main, Bulkhead
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