Douglas DC-9-31

Service difficulty reports · 7,433

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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 = 'DC931'
  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 9627249905Skin · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON BELLY OF AIRCRAFT, ELEVEN INCHES AFT OF E/E COMPARTMENT OPENING BETWEEN LONGERONS 29L AND 30L. INSTALLED TEMPORARY REPAIR PER EA 99-110796, L/P 6377247.Dec 28, 1996 · N955N · Doug DC931 · Fuselage Main, Plate/SkinSDR 9627239933Downlock · malfunctionedDURING APPROACH, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RED UNSAFE LIGHT WAS OUT. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED BROKEN WIRE G200LDec 28, 1996 · N1334U · Doug DC931 · Landing Gear Position and WarningSDR 9627169989Fuel Control · out of trimAS TAKEOFF POWER WAS APPLIED THE NUMBER ONE ENGINE EPR INDICATION WOULD NOT REACH TARGET EPR SETTING. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TRIMMED THE NUMBER ONE ENGINE FUEL CONTROL AND DRAINED THE MOISTURE TRAP, OPERATIONAL CHECK WAS OK.Dec 28, 1996 · N8945E · Doug DC931 · Fuel Controlling SystemSDR 9627159992Batteries · dischargedDURING PERIODIC CHECK, OVERWING EXIT EMERGENCY LIGHTS AT ROW 11 FAILED TEN MINUTE TEST. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL.Dec 28, 1996 · N8960E · Doug DC931 · Emergency LightingSDR 9627139992Battery Pack · dischargedDURING PERIODIC CHECK, TAIL COMPARTMENT OVERHEAD AND BOTH NACELLE EMERGENCY LIGHTS FAILED TEN MINUTE TEST. REPLACED BATTERIES IN TAIL COMPARTMENT PACKS AND REPLACED BATTERY PACKS FOR NACELLE LIGHTS, OPERATIONAL CHECK NORMAL.Dec 28, 1996 · N8960E · Doug DC931 · Emergency LightingSDR 9627099911Connector · damagedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, NO HELP. REPAIRED BAD CONNECTOR BEHIND SIDEWALL, OPERATIONAL CHECK NORMAL.Dec 28, 1996 · N961N · Doug DC931 · Emergency LightingSDR GTIA9700092Seat Track · corrodedMHV - FORWARD CABIN SEAT TRACK AT RBL 22 FS 200 THROUGH 230 AT STATION 200 HAS CRACKS, DRILL START AND CORROSION. REMOVED OLD SENT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK IAW 51-10-3, 51-10-2 AND 53-05. (M)Dec 27, 1996 · N928ML · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR 9627229935Clamps · looseTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED APPROXIMATELY TEN MINUTES AFTER TAKEOFF. LIGHT EXTINGUISHED AFTER BLEEDS WERE TURNED OFF. FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED CLAMPS TO LEFT AUGMENTATION VALVE AND REPDec 27, 1996 · N1332U · Doug DC931 · Pneumatic Distribution SystemSDR 9627039981Skin · corrodedDURING PERIODIC CHECK, FOUND DOUBLER AT FORWARD BAG BIN DOOR JAMB WITH SEVERAL AREAS OF CORROSION FROM FS 362 TO FS 435, INSIDE AND OUTSIDE SKIN AT BOTTOM SIDE OF DOOR OPENING. CUT LOWER SECTION OF DOOR DOUBLER AT FORWARD AND AFT SIDE. INSTALLED REPAIR DOUBLDec 26, 1996 · N994Z · Doug DC931 · Fuselage Main, Plate/SkinSDR 97ZZZM193Vert Gyro · malfunctionedFLT 1421 - DTW - DURING CLIMB CONFIGURATION WITH THE AUTO PILOT ENGAGED EXPERIENCED A VIOLENT PITCH DOWN CONDITION, AUTO PILOT DISENGAGED. REMOVED AND REPLACED NR 2 VERTICAL GYRO. SYSTEM OP CHECK GOOD ON GROUND IAW DC-9 MM 34-27-0 AND 22-10-0. (M)Dec 25, 1996 · N969ML · Doug DC931 · Attitude Gyro and Indicating SystemSDR 9626969969Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL.Dec 25, 1996 · N9333 · Doug DC931 · Emergency LightingSDR 9626959995Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL.Dec 25, 1996 · N8978E · Doug DC931 · Emergency LightingSDR 9626929952Control Cable · brokenLEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER RETRACTION. FLIGHT RETURNED TO MSP, LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED SHEARED RIVETS ON LEFT MAIN GEAR DOOR LATCH MECHANISM AND BROKEN DOOR SEQUENCE CABLE, OPERATIONAL CHECK NORMAL.Dec 25, 1996 · N916RW · Doug DC931 · Landing Gear Door Retract SectionSDR GTIA9700090Skin · mis installedMHV - STATION 600 LONGERON 30 SKIN REPAIR NOT PER SRM 53-04 FIG 12B. FINGER DOUBLERS NOT INSTALLED. INSTALLED FINGER DOUBLERS AS PER SRM 53-04 PAGE 35 FIG 12B. (M)Dec 24, 1996 · N928ML · Doug DC931 · Fuselage Main, Plate/SkinSDR 9626989938Power Supply · malfunctionedDURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL.Dec 24, 1996 · N1798U · Doug DC931 · Emergency LightingSDR 9626979968Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 5, 7 AND 9 INOPERATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL.Dec 24, 1996 · N9332 · Doug DC931 · Emergency LightingSDR 9626899964Epr Line · frozenAS TAKEOFF POWER WAS APPLIED, THE RIGHT ENGINE EPR INDICATION DID NOT RESPOND. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REPLACED THE RIGHT ENGINE EPR INDICATOR, EPR TRANSMITTER AND THE PROBLEM CONTINUED. MAINTENANCE THEN APPLIED HEAT TO PT7 LIDec 24, 1996 · N912RW · Doug DC931 · Engine Pressure Ratio (EPR)SDR GTIA9700132Fitting · corrodedMHV - AFT CARGO DOOR AFT EDGE GUIDE FITTINGS AND FASTENERS CORRODED. AFT DOOR EDGE SPACER CORRODED. BEAM 5 UPPER FORWARD ATTACH ANGLE, 1 FASTENER CORRODED. REMOVED AND REPLACED GUIDE FITTINGS PER SRM'S 52-30-4 AND 20-31. REMOVED CORROSION WITHIN LIMITS PERDec 23, 1996 · N928ML · Doug DC931 · Cargo/Baggage DoorsSDR 9626849937Battery Pack · malfunctionedDURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK.Dec 23, 1996 · N908H · Doug DC931 · Emergency LightingSDR USAAD96184Latch · wornFLT 1035 - CLT-SAV - ON GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ON. RETURNED TO CLT. FOUND LEFT MAIN STRIKER WORN ON DOOR LATCH MECHANISM. REPLACED DOOR LATCH ASSEMBLY. (M)Dec 22, 1996 · N912VJ · Doug DC931 · Landing Gear Door Retract SectionSDR 9626839911Evac Slide · low batteryDURING PERIODIC CHECK, MAIN CABIN DOOR EVACUATION SLIDE FAILED EMERGENCY BATTERY TEST. REPLACED SLIDE.Dec 22, 1996 · N961N · Doug DC931 · Escape SlideSDR 9626799990Epr Lines · frozenAS THROTTLES WERE ADVANCED FOR TAKEOFF, THE RIGHT ENGINE EPR INDICATION WAS INOPERATIVE. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE APPLIED HEAT TO ASSOCIATED EPR LINES AND RAN ENGINE. INDICATIONS WERE OK, SUSPECT ICING OF EPR RELATED LINES.Dec 22, 1996 · N8950E · Doug DC931 · Engine Pressure Ratio (EPR)SDR 97ZZZM73Light · brokenDTW - FLT 1130 - RIGHT FORWARD EMERGNCY LIGHT TRACK BROKEN (LIGHTS WILL NOT STAY IN TRACK). MAINTENANCE REMOVED AND REPLACED PLASTIC RETAINER FOR FORWARD EMERGENCY PATH LIGHTING, OPS CHECK GOOD. (M)Dec 21, 1996 · N934ML · Doug DC931 · Emergency LightingSDR USAAD96183Airspeed Ind · stuckFLT 528 - LGA-ROC - ON ROTATION, CAPTAINS AIRSPEED INDICATION FROZE. RETURNED TO FIELD. REPLACED CAPTAINS AIRSPEED INDICATOR. (M)Dec 20, 1996 · N980VJ · Doug DC931 · Airspeed/Mach IndicatorSDR GTIA9700089Door Beam · crackedMHV - AFT CARGO DOOR BEAM NR 1 AFT ATTACH ANGLE CRACKED. REPAIR PER SRM 51-10-4, 51-30-5, 51-30-1 (NEW PART INSTALLED). (M)Dec 20, 1996 · N928ML · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9700088Angle · crackedMHV - COCKPIT OVERHEAD, FORWARD TOP MOUNT OF EPC LBL 12.5 ANGLE IS CRACKED FS 150. REPLACED NEW BRACKET IAW 53-01-0, 20-16-0. (M)Dec 20, 1996 · N928ML · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9700087Rib · crackedMHV - VERTICAL STABILIZER LE PANEL RT SIDE HAS 5 RIBS CRACKED THROUGH FASTENER HOLES AT EDGE OF PANEL. LEFT SIDE HAS 3 RIBS CRACKED THROUGH FASTENER HOLES AT EDGE OF PANEL. FABRICATED AND INSTALLED PARTS IAW 55-02 FIG 14, 51-10-3, 51-20-0, 51-30-0. ALL CRADec 20, 1996 · N928ML · Doug DC931 · Vertical Stabilizer, Spar/RibSDR GTIA9700086Panel · crackedMHV - LEFT WING LOWER FLAP AREA NR L-2 BUTTE PANEL HAS A LARGE CRACK. REPAIRED HONEY COMB PANEL PER SRM 57-04, DOUBLER INSTALLED PER SRM 57-04 AND 57-30. (M)Dec 20, 1996 · N928ML · Doug DC931 · Trailing Edge FlapsSDR GTIA9700085Mount · corrodedMHV - NR 1 ENGINE AFT MOUNT FILLING HAS SURFACE CORROSION. REMOVED AND REPLACED NR 1 AFT VIBRATION ISOLATOR IAW 71-20-2. (M)Dec 20, 1996 · N928ML · Doug DC931 · Engine Mount SectionSDR GTIA9700084Support · corrodedFLOOR SUPPORT ANGLE RT SIDE STATION 148-168 HAS EXFOLIATION CORROSION OUT OF LIMITS. REMOVED DAMAGED AREA FLOOR SUPPORT ANGLES, FABRICATE DOUBLERS AND FILLERS IAW SRM 53-01 FIG 2. INSTALLED IAW 51-30-2. (M)Dec 20, 1996 · N928ML · Doug DC931 · Fuselage Miscellaneous StructureSDR 9626829912Wire · brokenFORWARD CABIN EMERGENCY FLOOR PROXIMITY LIGHTS ILLUMINATED DURING FLIGHT. MAINTENANCE REPAIRED BROKEN WIRE UNDER SEATS 2C AND 2D. OPERATIONAL CHECK NORMAL.Dec 20, 1996 · N962N · Doug DC931 · Light System WiringSDR GTIA9700083Floor Panel · peelingMHV - FLOOR PANEL NR 5 MYLAR PEEING, DOUBLER MISSING ON BOTH SIDES AND HAS SOME AREA DELAMINATING. FABRICATED AND INSTALLED (3) NEW DOUBLERS. REBOND DOUBLERS PER MM 20-20-0. (M)Dec 19, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9700082Support · crackedMHV - FORWARD CARGO UPPER FLOORBEAM TO SKIN FORWARD SUPPORT IS CRACKED AT STATION 389 RBL 60 2F-6. INSTALLED NEW BRACKET PER SRM 51-30-3. (M)Dec 19, 1996 · N928ML · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9700081Angle · crackedMHV - FORWARD ACCESSORY COMP AT STATION 180 AT CENTER LINE ABOVE LONGERON 30 ATTACH ANGLE FOR FLOOR SUPPORT IS CRACKED, ALSO ATTACH ANGLE ABOVE 29L IS ALSO CRACKED. FABRICATED ANGLES. REMOVED AND REPLACED ANGLES PER SRM 51-10-02, 51-10-3, AND 51-30-02. (M)Dec 19, 1996 · N928ML · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9700080Frame · corrodedMHV - FRAME HAS CORROSION AT STATION 929 RBL 62 ZF 6-15. REMOVED CORRODED AREA, FABRICATED NEW SUPPORT BRACKET PER SRM 53-11-3. INSTALLED IAW 51-30-1. (M)Dec 19, 1996 · N928ML · Doug DC931 · Fuselage Main, FrameSDR GTIA9700079Skin · crackedMHV - DURING NDT INSPECTION OF AIRCRAFT PER SID 53.09.029 CRACKS WERE INDICATED IN THE FUSELAGE SKIN AT 5 RIVETS AT FS 69.550 APPROXIMATELY 15 INCH LEFT OF CENTERLINE OF THE AIRCRAFT. INSPECTED FOUND INITIAL REPAIR PER DRAWING SR09530239 WAS IMPROPERLY INSTALDec 19, 1996 · N928ML · Doug DC931 · Fuselage Main, Plate/SkinSDR 9627919981Release Mech · malfunctionedDURING H-CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE. ADJUSTED TAILCONE RELEASE MECHANISM, FUNCTIONAL TEST OK.Dec 19, 1996 · N994Z · Doug DC931 · Aerodynamic FairingsSDR 9626689968Batteries · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 10 THROUGH 12 INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY. OPERATIONAL CHECK NORMAL.Dec 19, 1996 · N9332 · Doug DC931 · Emergency LightingSDR TWAA9615801Wire · brokenSTL - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, RIGHT MAIN LANDING GEAR DID NOT INDICATE UP AND LOCKED. CYCLED LANDING GEAR. FOUND WIRE 2G204E24 AND 2G206E24, BROKEN. REPAIRED WIRES AND REPLACED SWITCH, MFG P/N H14-6. LANDING GEAR INDICATION AND OPERADec 18, 1996 · N977Z · Doug DC931 · Landing Gear System WiringSDR GTIA9700078Floor Panel · delaminatedMHV - AFT FLOOR PANEL S/N 2686 AND END DELAMINATED ALONG EDGE AND CRACKED IN LOWER ANGLE ALONG DELAMINATION. REPAIRED DELAMINATION PER SRM 53-05. STOP DRILLED CRACK PER SRM 53-01 AND REPAIRED PER SRM 53-05. FABRICATED REPAIR DOUBLERS PER SRM 53-05. ALODINEDec 18, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9700077Floor Panel · crackedMHV - FLOOR PANEL NR 21 HAS 6 CRACKS IN HAT CHANNELS. REMOVED DAMAGED AREAS, FABRICATED DOUBLERS AND INSTALLED IAW SRM 53-05, 51-10-3, 51-10-4, 53-30-2. (M)Dec 18, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9700076Floorboard · crackedMHV - FLOORBOARD NR 21 HAT SECTIONS CHAFED, CRACKED AND BROKEN OUT. REPAIRED FLOORBOARD IAW 53-05, INSTALLED IAW 51-30-2. (M)Dec 18, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR 97ZZZM75Downlock Sw · failedDTW - FLT 626 - DURING LANDING GEAR EXTENSION EXPERIENCED A UNSAFE INDICATION ON RIGHT MAIN LANDING GEAR. RECYCLED LANDING GEAR, RIGHT MAIN GEAR REMAINED UNSAFE. LANDED DTW WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN GEAR DOWN LOCK POSDec 18, 1996 · N934ML · Doug DC931 · Landing Gear Position and WarningSDR 9626679994Downlock Switch · failedDURING APPROACH INTO MSO, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR LOCK SWITCH. OPERATIONAL CHECK NORMAL ON GDec 18, 1996 · N8979E · Doug DC931 · Landing Gear Position and WarningSDR 9626619912Batteries · dischargedEMERGENCY LIGHTS IN FORWARD CABIN AND AT GALLEY SERVICE DOOR EXIT REMAINED ON DURING FLIGHT. REPLACED BATTERIES IN MODULE AT GALLEY SERVICE DOOR, OPERATIONAL CHECK NORMAL.Dec 18, 1996 · N962N · Doug DC931 · Emergency LightingSDR GTIA9700075Structure · damagedMHV - FLOOR BOARD, WINGS BOX AREA, UPPER AREA HAS SEVERAL CRACKS AND TORN OUT HOLES. HAT CHANNELS HAVE CRACKS AT THE FORWARD ENDS, INSULATION TAPE IS LOOSE. FLOOR SKIN DAMAGED BEYOND REPAIR. REMOVED FLOORBOARD PANEL SKIN AND FABRICATED NEW PANEL SKIN. REMODec 17, 1996 · N928ML · Doug DC931 · Fuselage Main, StructureSDR GTIA9700074Floor Panel · crackedMHV - FLOOR PANEL HAS BREAK OUT FROM ONE FASTENER HOLE ALONG EDGE AND TWO EACH EDGE STRIPS MISSING. FABRICATED PATCH IAW SRM 55-01. TREATED AND PRIMED PATCH IAW SRM 51-10-03. INSTALLED PATCH WITH RIVETS IAW SRM 51-30-2. FABRICATED EDGE STRIPS IAW MM 53-20-Dec 17, 1996 · N928ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9700073Pan · crackedMHV - PASSENGER ENTRY DOOR PAN FORWARD LOWER CORNER ON FORWARD SIDE IN CRACK JUST BELOW LOWER HINGE. REMOVED AND REPLACED DOOR PAN SEGMENT PER SRM 52-05, 51-10-3, 51-10-4, 51-30-2, 51-30-5, 51-30-7. (M)Dec 17, 1996 · N928ML · Doug DC931 · Passenger/Crew DoorsSDR 97ZZZM74Connector · looseACY - FLT 511 - DURING CLIMB CONFIGURATION RIGHT ENGINE OIL PRESSURE DECREASE TO 42 PSI, AND BEGAN FLUCTUATING BETWEEN 42 AND 40 PSI. OIL TEMPERATURE AND QUANTITY NORMAL. MAINTENANCE FOUND OIL PRESSURE TRANSMITTER CANNON PLUG LOOSE AND SOAKED WITH OIL. CLEADec 17, 1996 · N934ML · Doug DC931 · Engine Oil PressureSDR 9626659962Downlock Ind · malfunctionedDURING APPROACH, LEFT MAIN LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW RECYCLED GEAR AND VERIFIED VISUALLY THROUGH PERISCOPE THAT GEAR WAS DOWN AND LOCKED. GREEN LIGHT ILLUMINATED AFTER BULB REPLACEMENT. AIRCRAFT LANDED WDec 17, 1996 · N914RW · Doug DC931 · Landing Gear Position and Warning
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