Douglas DC-9-32

Service difficulty reports · 12,755

Newest first. General aviation reporting is voluntary.

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 MWEA001252Thermostat · inoperativeDURING CLIMBOUT WITH CLIMB POWER, FULL ANTI-ICE "ON" RIGHT ICE PROTECT TEMP HIGH ANNUNCIATOR ILLUMINATED. QRH PROCEDURE TURNED OFF LIGHT IN ABOUT 1 MINUTE. -- PERFORMED RESISTANCE CHECK ON ELECTRONIC THERMO SWITCH NO DEFECTS NOTED. FOUND RIGHT ICE PROTECTIODec 20, 2000 · N202ME · Doug DC932 · Pneumatic Indicating SystemSDR AT0100083Rib · crackedFOUND LEFT FLAP INNER SUPPORT RIBS CRACKED. INSTALLED 2 ANGLE REPAIRS IAW DC9 SRM 51-10, 57-01, AND 51-10-02.Dec 19, 2000 · N846AT · Doug DC932 · Trailing Edge FlapsSDR CA010321010Turbine Blades · failed(CAN) AIRCRAFT REJECTED TAKEOFF ON ROLL DUE TO THE EPR INDICATION THAT WENT FROM 2.01 DOWN TO 1.6 (ENGINE PRESSURE RATIO). FLIGHT ATTENDANT REPORTED HEARING A LOUD BANG. ENGINE CONTAINED. MECHANIC FOUND EVIDENCE OF DAMAGE TO THE TURBINE SECTION. REPLACED LT ENDec 18, 2000 · Doug DC932 · Turbine SectionSDR CA010201004Turbine · damaged(CAN) AIRCRAFT REJECTED TAKEOFF ON ROLL DUE TO THE EPR INDICATION THAT WENT FROM 2.01 DOWN TO 1.6 (ENGINE PRESSURE RATIO). FLIGHT ATTENDANT REPORTED HEARING A LOUD BANG. ENGINE CONTAINED.MECHANIC FOUND EVIDENCE OF DAMAGE TO THE TURBINE SECTION. REPLACED LT ENGDec 18, 2000 · Doug DC932 · Turbine SectionSDR AT0000506Stringer · corrodedFOUND STRINGER 20R AND 21R BS 230 - 360 CORRODED BEYOND LIMITS. REMOVED AND REPLACED STRINGER 20R AND 21R BS 230 - 360 IAW DC9 SRM 51-10-03.Dec 18, 2000 · N846AT · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA001244Shear Tie · crackedSHEAR CLIP CRACKED AT FUSELAGE STATION 945 BETWEEN LONGERON 15 RIGHT. -- REMOVED AND REPLACED SHEAR CLIP.Dec 18, 2000 · N401ME · Doug DC932 · Fuselage Main, StructureSDR MWEA001254Fitting · crackedLEFT LAV AREA, AFT VENTRAL DOOR JAMB LEFT SIDE TWENTY INCHES ABOVE FLOOR, FOUND CRACKED FITTING. -- REMOVED, FABRICATED, AND INSTALLED FITTING.Dec 18, 2000 · N401ME · Doug DC932 · Fuselage Main, Attach FittingsSDR MWEA001253Intercostal · damagedE&E BAY DOOR HAD TOOLING MARKS IN RADIUS OF STIFFNER(INTERCOSTAL) AND MISDRILLED HOLE. -- REMOVED, FABRICATED, AND INSTALLED INTERCOSTAL.Dec 18, 2000 · N401ME · Doug DC932 · Service DoorsSDR MWEA001243Post · damagedFO'S CLEARVIEW WINDOW POST HOLE ELONGATED TO .358. -- REMOVED AND REPLACED WINDOW POST.Dec 18, 2000 · N401ME · Doug DC932 · Fuselage Main, StructureSDR MWEA001242Seat Track · damagedCABIN FLOORBOARD B6 AT STATION 617 TO 639 LT, BETWEEN NR 1 & 2 SEAT TRACKS HAS HOLES CRACKED OUT. -- REMOVED AND REPLACED FLOORBOARD.Dec 18, 2000 · N401ME · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA001251Acm · inoperativeAFTER TAKE OFF, CABIN CREW ADVISED OF STRONG BURNING ODOR, 3 LOUD THUDS FROM RIGHT AFT AREA WERE HEARD. -- REMOVED AND REPLACED WATER SEPERATOR SOCK, AIR CYCLE MACHINE, AND 35 DEGREE LEE VALVE.Dec 18, 2000 · N215ME · Doug DC932 · Cabin Cooling SystemSDR AT0000504Smoke Detector · damagedFOUND JUST AFTER TAKE OFF 'A' LOOP SMOKE DETECTOR IN FORWARD CARGO COMPARTMENT LIGHT ILLUMINATED. RETURNED TO CAK AIRPORT LIGHT EXTINGUISHED AFTER LANDING. CORRECTIVE ACTION: MAINTENANCE CHECKED DETECTION SYSTEM, FOUND DETECTORS DAMAGED FODec 15, 2000 · N866AT · Doug DC932 · Smoke DetectionSDR ABXA000530Bracket · bentAT FL 230, CABIN PRESSURE LIGHT ILLUMINATED. THE CREW PERFORMED EMERGENCY CHECKLIST AND DESCENDED TO 22,000 FT. AT 22,000 FT, CABIN PRESSURIZATION WAS MAINTAINED. MAINTENANCE INSPECTED AND FOUND THE FORWARD MAIN ENTRY DOOR LEAKING DURING PRESSURIZATION CHECKDec 15, 2000 · N903AX · Doug DC932 · Passenger/Crew DoorsSDR MWEA001248Apu · contaminatedDURING PUSH-BACK, AFT RIGHT AND LEFT LAV SMOKE DETECTORS SOUNDED. -- SUSPECT EXTERNAL OIL LEAK FROM APU. RAN APU FOR 30 MINUTES. NO OIL LEAKS NOTED.Dec 14, 2000 · N207ME · Doug DC932 · APU Oil SystemSDR MWEA001245Fairing · crackedRH VERTICAL STAB SKIN UNDER AFT LOWER HORIZONTAL STAB FAIRING IS CRACKED. -- REPLACED SKIN.Dec 13, 2000 · N202ME · Doug DC932 · Vertical StabilizerSDR AT0000513Fitting · crackedFOUND RIGHT AFT KEEL BEAM FITTING CRACKED AT BS 738 - 756. REMOVED AND REPLACED FITTING ON RIGHT MLG WHEEL WELL, REMOVED AND REINSTALLED HYDRAULIC RESERVIOR AND HYDRAULIC LINES IAW DC9 MM 29-00-01 AND SRM 51-10-6, 51-30-1.Dec 11, 2000 · N835AT · Doug DC932 · Fuselage Main, KeelSDR MWEA001238Pump · inoperativeDURING TAKE-OFF RIGHT HYDRAULIC TEMP HIGH LIGHT CAME ON. TAKE-OFF ABORTED. -- REPLACED ELECTRIC HYDRAULIC PUMP.Dec 11, 2000 · N215ME · Doug DC932 · Hydraulic Pump (Electric/Engine), MainSDR AT0000486Controller · inoperativeAUTO PRESSURIZATION FAILED IN FLIGHT. CABIN PRESSURE WAS CONTROLLED IN MANUAL. STOWED ALL MASK, PERFORMED OPERATIONAL CHECK OF MASK DROP SYSTEM. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER. IAW DC9 MM 21-32.Dec 9, 2000 · N867AT · Doug DC932 · Cabin Pressure ControllerSDR AT0000508Floor Support · crackedFOUND AFT CRAGO COMPARTMENT FRAME 813 LONGERON 29R CARGO FLOOR SUPPORT CRACKED. REMOVED FLOOR SUPPORT, WELD REPAIR FLOOR SUPPORT, REINSTALLED FLOOR SUPPORT IAW DC9 SRM 51-10-4, 51-30-2, EA 12-5321-29-C1362, 51-30-2, 51-30-5.Dec 7, 2000 · N835AT · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA001231Longeron · crackedLONGERON 17 LEFT CRACKED AT STATION 980. -- FABRICATED AND INSTALLED SPLICE HAT SECTION.Dec 7, 2000 · N401ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA001230Longeron · crackedLONGERON 16 RIGHT CRACKED AT STATION 965. -- FABRICATED AND INSTALLED LONGERON REPAIR.Dec 7, 2000 · N401ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA001234Seat Track · corrodedNR 4 SEAT TRACK AT STATION 376 HAS CORROSION IN UPPER CHANNEL AND LUGS. -- FABRICATED AND INSTALLED SEAT TRACK REPAIR.Dec 7, 2000 · N401ME · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA001233Shear Tie · crackedSHEAR TIE JUST UNDER LONGERON 14 LEFT CRACKED AT STATION 980. -- REMOVED AND REPLACED SHEAR TIE.Dec 7, 2000 · N401ME · Doug DC932 · Fuselage Main, StructureSDR MWEA001232Shear Tie · crackedSHEAR TIE JUST UNDER LONGERON 14 RIGHT CRACKED AT STATION 980. -- REMOVED AND REPLACED SHEAR TIE.Dec 7, 2000 · N401ME · Doug DC932 · Fuselage Main, StructureSDR AT0000511Pylon · crackedFOUND NR 2 ENGINE PYLON LOWER AND UPPER TRAILING EDGE PANEL HAS LOOSE AND MISSING FASTENERS. REMOVED AND REPLACED NR 2 ENGINE TRAILING EDGE PANEL UPPER AND LOWER SKINS. REMOVED AND REPLACED WEDGE, REMOVED AND REINSTALLED NR 2 ENGINE PYLON TRAILING EDGE ASSEMDec 6, 2000 · N835AT · Doug DC932 · Nacelle/Pylon, Plate/SkinSDR AT0000507Spar Cap · corrodedFOUND CORROSION ON FORWARD FLANGE OF LEFT HORIZONTAL UPPER REAR SPAR. REMOVED UPPER LEFT HAND HORIZONTAL SPAR CAP FROM SPAR CAP AT XRS 100. FORMED REPAIR ANGLE AND SPLICES, HEAT TREATED, DRILLED, PRIMED AND INSTALLED IAW DC9 SRM 55-02 FIGURE 21, 51-30-2, 51-Dec 6, 2000 · N835AT · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR AT0000485Regulator · inoperativePASSING THROUGH 260FL, FIRST OFFICER HEARD SURGE FROM PAX O2 SYSTEM. ALL MASKS DEPLOYED. CABIN ALTITUDE WAS AT 7000FT. REMOVED AND REPLACED PAX O2 CYLINDER REGULATOR. IAW DC9 MM35-20Dec 6, 2000 · N825AT · Doug DC932 · Passenger Oxygen SystemSDR AT0000484Door · disengagedNOSE GEAR DOOR NOT CLOSED, DID NOT CLOSE AT GEAR RETRACTION. RESECURED DOOR ON NOSE GEAR. IAW DC9 MM32-20Dec 6, 2000 · N801AT · Doug DC932 · Landing Gear DoorsSDR MWEA001235A/C Pack · failedAFTER DEPARTURE FROM MCI AT 6800 FT THE LEFT PACK SHUTDOWN. JUST PRIOR TO SHUTDOWN CREW NOTED EXTREMELY WARM AIR IN COCKPIT. RETURNED TO MCI. -- DEFERRED LEFT PACK PER DMI 12-29, MEL 21-1A CH C.Dec 6, 2000 · N203ME · Doug DC932 · Humidity Control SystemSDR AT0000512Skin · damagedFOUND AT BS 498R ONE STATIC DISCHARGE SPOT ON AFT SIDE OF WINDOW CUTOUT. REPAIRED STATIC DISCHARGE SPOT ON WINDOW CUTOUT IAW REO L00335.Dec 5, 2000 · N835AT · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0000509Tail Cone · corrodedFOUND VERTICAL STAB TAIL CONE HAS SURFACE CORROSION ON THE RIGHT AFT SIDE AND UNDER AFT SIDE. REMOVED CORROSION ON VERTICAL STAB. FABRICATED, TREATED AND INSTALLED DOUBLER IAW DC9 51-10-3, 51-30-1, 51-10-4.Dec 5, 2000 · N835AT · Doug DC932 · Aerodynamic FairingsSDR AT0000510Skin · corrodedFOUND FUSELAGE SKIN BULGING AROUND FASTENERS AT BS 889 LONGERON 29R. REMOVED CORRODED SKIN, REMOVED AND REPLACED AFT CARGO DOOR FRAME INTERNAL DOUBLER, TREATED AND INSTALLED REPLACEMENT SKIN IAW REO L00337, DC9 SRM 53-04 FIGURE C12, 51-10-4, 51-10-3, 51-30-2,Dec 4, 2000 · N835AT · Doug DC932 · Fuselage Main, Plate/SkinSDR MWEA001229Engine · lack of lubeRIGHT ENGINE OIL QUANTITY DROPPED TO 6 QUARTS IN CRUISE. -- MCI MAINTENANCE FOUND RIGHT ENGINE OIL CAP OFF. REINSTALLED CAP AND SERVICED OIL QUANTITY TO "FULL".Dec 4, 2000 · N301ME · Doug DC932 · Engine Oil Storage (Airframe Furnished)SDR ABXA000519Separator · contaminatedDURING TAKEOFF ROLL BETWEEN V1 AND VR THE COCKPIT FILLED WITH A STRONG BURNING ODER. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCK. MAINTENANCE INSPECTED THE NUMBER ONE AND NUMBER TWO ENGINE INLETS, OUTLETS AND PNEUMATIC DUCTS FOR RESIDUES. MAINTENANCE INSPECDec 4, 2000 · N901AX · Doug DC932 · Humidity Control SystemSDR TWAA0018803Power Supply · defectiveTHE EGRESS LIGHTS WERE INTERMITTENTLY GOING ON AND OFF DURING FLIGHT. REPLACED THE EGRESS LIGHT POWER SUPPLY. CHECK-C 7-4-00 MCI.Dec 3, 2000 · N931L · Doug DC932 · Emergency LightingSDR TWAA0018802Connector · looseTHE LAST 4 ROWS OF EGRESS LIGHTS FLICKERED IN CLIMB. RESEATED THE CONNECTION OF THE EGRESS LIGHTING. CHECK-C 7-4-00 MCI.Dec 2, 2000 · N931L · Doug DC932 · Emergency LightingSDR AT0000483Wire · brokenFOUND EMERGENCY LIGHT AT AFT DOOR TO VERTICAL STAIRS WILL NOT ILLUMINATE. REPAIRED BROKEN WIRE ON BATTERY PACK R88. IAW DC9 MM 20-50Dec 1, 2000 · N832AT · Doug DC932 · Light System WiringSDR MWEA001216Light · inoperativeAFT ACCESSORY EMERGENCY LIGHTS INOP. -- REPLACED LIGHT ASSEMBLY ABOVE TAILCONE RELEASE HANDLE.Nov 30, 2000 · N212ME · Doug DC932 · Emergency LightingSDR AT0000482Circuit Breaker · trippedDURING CLIMB, CIRCUIT BREAKERS POPPED AND EMERGENCY LANDING WAS PERFORMED FOLLOWED BY AN EMERGENCY EVACUATION. TROUBLE SHOOTING IN PROGRESS.Nov 29, 2000 · N826AT · Doug DC932 · AC Power Distribution SystemSDR L1GA200000552Release System · wornCOMPLY WITH SB DC9-53-257 TAIL CONE EMERGENCY RELEASE MOD ON LEGEND AIRLINES EO DC9-53-00-025 & 026-COMPLIED WITH AS REQUIRED-REF AD97-22-05Nov 28, 2000 · N12507 · Doug DC932 · Tail Cone DoorsSDR L1GA200000551Release System · wornCOMPLY WITH SB DC9-53-257 TAIL CONE EMERGENCY RELEASE MOD ON LEGEND AIRLINES EO DC9-53-00-025 & 026-COMPLIED WITH AS REQUIRED-REF AD97-22-05Nov 26, 2000 · N12510 · Doug DC932 · Tail Cone DoorsSDR AT0100027Spar · corrodedFOUND RIGHT HORIZONTAL STABILIZER FORWARD SPAR XFS 161-163 EXFOLIATED CORROSION. FABRICATED AND INSTALLED FILLER AND NUT PLATE STRIP IAW REO-L00320.Nov 22, 2000 · N839AT · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR AT0100022Floor Panel · corrodedFOUND COCKPIT FLOORPANEL 4416 CORRODED BEYOND LIMITS. REPLACED SKIN ON FLOOR PANEL 4416 IAW DC9 SRM 53-01, 53-21, AND 51-10-03.Nov 22, 2000 · N839AT · Doug DC932 · Fuselage Floor PanelSDR TWAA0018301Socket · crackedAIRCRAFT RETURNED FROM TAXI DUE TO ELECTRICAL SMELL IN AREA OF CABIN ROW 20 AND 21, LEFT SIDE. REPLACED BURNED LIGHT BULB SOCKET AT ROW 20ABC FOR LOWER SIDEWALL LIGHTS. CHECK-C 3-29-00 MCI.Nov 22, 2000 · N925L · Doug DC932 · Passenger Compartment LightingSDR ABXA000513Lock · jammedFLIGHT DECK DOOR LOCK JAMMED IN THE LOCKED AND CLOSED POSITION. MAINTENANCE INSPECTED TIGHTENED, AND LUBRICATED THE DOOR LOCK, IAW DC9 MM 52-00-00. OPS CHECKED GOOD.Nov 20, 2000 · N901AX · Doug DC932 · Fixed Inner DoorsSDR ABXA000512Battery · dischargedEMERGENCY LIGHTS FAILED TO OPERATE DURING PREFLIGHT INSPECTION. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY IAW DC9 MM 33-53-00. OPS CHECKED GOOD.Nov 20, 2000 · N981AX · Doug DC932 · Emergency LightingSDR MWEA001194Battery Pack · inoperativeAFTER ENGINE START FLIGHT ATTENDENT COMPLAINED OF STRONG ELECTRICAL SMOKE SMELL AROUND OVERWING EXITS. EMERGENCY AND FORWARD EXIT LIGHTS WOULD NOT STAY ON. FOUND BATTERY PACK HAD BURNT SMELL. REMOVED AND REPLACED EMERGENCY CEILING BATTERY PACK.Nov 19, 2000 · N206ME · Doug DC932 · Emergency LightingSDR L1GA200000550Release System · wornCOMPLY WITH SB DC9-53-257 TAIL CONE EMERGENCY RELEASE MOD ON LEGEND AIRLINES EO DC9-53-00-025 & 026-COMPLIED WITH AS REQUIRED-REF AD97-22-05,Nov 18, 2000 · N17533 · Doug DC932 · Tail Cone DoorsSDR AT0100031Skin · chafedFOUND CHAFE MARKS OUT OF LIMITS IN VERTICAL STABILIZER LEADING EDGE. REPLACED LEADING EDGE OF VERTICAL STABILIZER IAW DC9 SRM 55-01 FIG 1.Nov 17, 2000 · N839AT · Doug DC932 · Vertical Stabilizer, Plate/SkinSDR MWEA001195Starter · inoperativeSTARTED RIGHT ENGINE ON DELAYED ENGINE START, N2 ACCELERATED TO 19 PERCENT THEN BEGAN TO DECREASE RAPIDLY AT WHICH TIME START WAS TERMINATED. REPLACED STARTER.Nov 17, 2000 · N207ME · Doug DC932 · Engine Cranking
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