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 AT0200037Duct · damagedOIL SMELL AND SMOKE DETECTOR GOING OFF. FOUND RIGHT PACK ACM DUCT BLOWN. REPAIRED HOLE IN DUCT.Mar 20, 2002 · N837AT · Doug DC932 · Air Distribution SystemSDR ABXA010782Wire · brokenON LANDING AT BDL, NO GREEN GEAR LIGHT. RECYCLED LANDING GEAR, THE GREEN LIGHT ILLUMINATED. REPAIRED BROKEN WIRES TO THE NOSE GEAR UP LIMIT SWITCH CONNECTOR (P1-134) AND REPLACED THE UP LIMIT SWITCH AS A PRECAUTION. OPS CHECKED GOOD IAW DC9 MM 32-60-01-02.Mar 20, 2002 · N982AX · Doug DC932 · Landing Gear System WiringSDR MWEA020185Longeron · corrodedFORWARD PIT, CORROSION ON LONGERON AT STATION 570 LONGERON 30. REMOVED AND REPLACED LONGERON. FABRICATED AND INSTALLED RADIUS STRAP.Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020184Frame · corrodedSTATION 980 FRAME UPPER -J- CHANNEL HAS AREAS OF LIGHT CORROSION BETWEEN LONGERON 29 LEFT THROUGH LONGERON 28 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLES, SPLICES AND FRAME SECTION.Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020183Longeron · crackedFORWARD PIT LONGERON 28 LEFT IS CRACKED UNDER SPLICE AT STATION 552 THROUGH 560. -- REMOVED LONGERON, POSITIONED AND DRILLED, REINSTALLED LONGERON.Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020182Clip · corrodedAFT CARGO COMPARTMENT UNDERSIDE OF SHOVEL CLIP CORRODED AT STATION 945 LONGERON 26 RIGHT. -- REMOVED AND REPLACED SHOVEL CLIP.Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020181Frame · corrodedSTATION 832 FRAME AFT SIDE HAS CORROSION BETWEEN LONGERONS 29 RIGHT TO 28 RIGHT. FABRICATED AND INSTALLED FRAME REPAIR SECTIONS.Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020180Frame · corrodedSTATION 917 FRAME FORWARD SIDE HAS CORROSION FROM LONGERON 28 LEFT TO 29 RIGHT UNDER THE FLOOR SUPPORT. FABRICATED AND INSTALLED FRAME SECTION, REPAIR DOUBLERS, AND SUPPORT FITTING.Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020179Frame · corrodedSTATION 965 FRAME HAS LIGHT CORROSION FROM LONGERON 25 LEFT TO 27 RIGHT AFT SIDE. REMOVED AND REPLACED SPLICE.Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020177Frame · corrodedFORMER AT STATION 980 HAS AREA OF LIGHT CORROSION BETWEEN LONGERON 25 THROUGH LONGERON 26 LEFT. FABRICATED AND INSTALLED FORMER AND SPLICES.Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020178Fitting · corrodedCUSP SPLICE FITTING AT STATION 229 LEFT SIDE HAS CORROSION. REMOVED AND REPLACED FITTING.Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020176Support · crackedSTATION 897 BETWEEN LONGERONS 27 LEFT AND 28 LEFT SUPPORT HAS CORROSION BY A FASTENER. WHILE REMOVING CORROSION, FOUND SUPPORT CRACK. REMOVED AND REPLACED SUPPORT.Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020175Fitting · corrodedSTATION 945 BETWEEN LONGERONS 28 LEFT AND 27 LEFT HAS A CORRODED SUPPORT FITTING. -- REMOVED AND REPLACED SUPPORT FITTING.Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020174Support · crackedSTATION 980 BY LONGERON 27 RIGHT HAS A CRACKED SUPPORT. -- REMOVED AND REPLACED FLOOR SUPPORT.Mar 19, 2002 · N206ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020172Angle · brokenLEFT WING OUTBOARD FLAP HINGE FITTING INBOARD ATTACH ANGLE IS BROKEN. -- LOCATED, DRILLED & DEBURRED INBOARD ATTACH ANGLE AND INBOARD RIB ANGLE AND INSTALLED.Mar 19, 2002 · N205ME · Doug DC932 · Wing, Control SurfacesSDR ABXA010810Skin · corrodedFUSELAGE SKIN FLUSH REPAIR BULGING OUTWARD AND HAD RIVETS INSTALLED INTO RIVETS, STATION 379, BETWEEN LONGERON 2 - 3 RIGHT. REPAIRED AREA IAW DC-9 SRM 53-04.Mar 18, 2002 · N986AX · Doug DC932 · Fuselage Main, Plate/SkinSDR AT0200036Fuse · blownFORWARD EMERGENCY PATH LIGHTING WILL NOT ILLUMINATE ON THE FLOOR. INSTALLED FUSE ON FORWARD POWER SUPPLY FOR EMERGENCY PATH LIGHTING REF DC-9 MM 33-53 AND 33-00, OPS CHECK GOOD.Mar 18, 2002 · N819AT · Doug DC932 · Emergency LightingSDR MWEA020170Frame · corrodedSTATION 897 FRAME AT LONGERON 29 RIGHT TO 30 HAS CORROSION ON THE LOWER SURFACE. FABRICATED AND INSTALLED CLIP, REPAIR DOUBLERS, AND SHIMS.Mar 15, 2002 · N206ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020168Longeron · dentedLONGERON 20 LEFT STATION 214 HAS DENT AND HAS CARRY OVER 5735. FABRICATED AND INSTALLED LONGERON SECTION.Mar 15, 2002 · N206ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA020167Longeron · crackedLONGERON 2 RIGHT AT FUSELAGE STATION 1076 CRACKED AT END. -- REMOVED AND REPLACED WITH REPAIR, NEW LONGERON SPLICE.Mar 15, 2002 · N206ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020166Engine · leakingLEFT ENGINE OIL PRESSURE DECREASING, LEFT TEMPERATURE RISING INTO YELLOW ARCH 120 DEGREES CELSIUS. REDUCED POWER TO IDLE, OIL QUANTITY WENT TO ZERO, OIL PRESSURE LOW LIGHT CAME ON, OIL PRESSURE INDICATED 30 PSI. PERFORMED ENGINE SHUT DOWN PER QRH. MAINTENANMar 13, 2002 · N216ME · Doug DC932 · Engine (Turbine/Turboprop)SDR 0200939610Skin · crackedDuring Hck in DHN, crack damage was found at the fwd service door skin at the lower left corner area. Repaired per EA 96-189244,Mar 12, 2002 · N610NW · Doug DC932 · Fuselage Main, Plate/SkinSDR GTIA020220Computer · malfunctionedFLT 8011 - ACY - ON STABILIZED DESCENT AUTOPILOT SUDDENLY PITCHED DOWN THEN PITCHED UP. REMOVED AND REPLACED PITCH AXIS COMPUTER IAW MM 27-13-1, OPS CHECK NORMAL. (M)Mar 8, 2002 · N12536 · Doug DC932 · Flight ControllerSDR AT0200054Bulkhead · corrodedAFT PRESSURE BULKHEAD CORROSION FORWARD SIDE ABOVE 27L TO 27R. INSTALLED AFT PRESSURE BULKHEAD WEB REPAIR FROM LONG 28LT TO LONG 27RT IAW DC-9 SRM 53-03 FIG 33.Mar 7, 2002 · N835AT · Doug DC932 · Fuselage Main, BulkheadSDR MWEA020164Shutoff Valve · faultyRIGHT HAND ENGINE ANTI-ICE VALVE CAUTION LIGHT ON, WITH RIGHT HAND ENGINE ANTI-ICE SELECTED ON. REMOVED AND REPLACED RIGHT HAND ENGINE COWL VALVE. THE BAD VALVE REMOVED HAD TRIPPED THE CIRCUIT BREAKER.Mar 7, 2002 · N302ME · Doug DC932 · Engine Anti-Icing SystemSDR 0200809923Drain Valve · blownON TOUCHDOWN AT LANDING, THE RIGHT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED AND THE RIGHT HYDRAULIC QUANTITY DROPPED TO ZERO. FLIGHT CLEARED THE RUNWAY AND TURNED OFF THE RIGHT ENGINE DRIVEN AND AUXILIARY HYDRAULIC PUMPS. DURING TAXI TO GATE, SOME SMOKE ENTEMar 6, 2002 · N927RC · Doug DC932 · Hydraulic Pump (Electric/Engine), MainSDR MWEA020163FormerINBOARD FIXED VANE OUTBOARD STRUT L/E NOSE FORMER CRACKED. -- REMOVED AND REPLACED DOUBLER.Mar 6, 2002 · N205ME · Doug DC932 · Wing, Control SurfacesSDR MWEA020162Angle · crackedLEFT WING OUTBOARD FLAP HINGE FITTING OUTBOARD ATTACH ANGLE IS CRACKED. -- LOCATED, DRILLED AND DEBURRED RIB ANGLE.Mar 6, 2002 · N205ME · Doug DC932 · Wing, Control SurfacesSDR MWEA020161Web · crackedLEFT CUSP MEMBRANE STATION 579 THROUGH 598 IS CRACKED IN SEVERAL LOCATIONS AND IS PUNCTURED. FABRICATED AND INSTALLED REPAIR DOUBLER.Mar 6, 2002 · N205ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020160Web · canningSTATION 302 SUBFLOOR WEB LEFT SIDE IS OIL CANNING. -- FABRICATED AND INSTALLED SUBFLOOR WEB REPAIR.Mar 6, 2002 · N205ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020159Web · crackedCABIN SUBFLOOR HAS A CRACK IN THE WEB AT STATION 598 LEFT SIDE. FABRICATED AND INSTALLED DOUBLER.Mar 6, 2002 · N205ME · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0200028Wire · brokenDURING EMERGENCY LIGHTING CHECK OUT FOUND TAIL CONE EMERGENCY RELEASE HANDLE LIGHT INOP. FURTHER INVESTIGATION REVEALED POSITIVE WIRE CUT IN HALF 2 FEET FROM LIGHT.Mar 3, 2002 · N866AT · Doug DC932 · Light System WiringSDR 0200609617Compressor · stalledDURING TAKEOFF ROLL AT 105 KTS, THE AIRCRAFT EXPERIENCED A COMPRESSOR STALL. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED PS3 FILTERS AND SADDLE DUCTS ON BOTH ENGINES. NO DEBRIS WAS FOUND. BOTH ENGINES WERE OPERATED TO TAKEOFF POWERMar 2, 2002 · N617NW · Doug DC932 · Turbine Engine Compressor SectionSDR MWEA020157Clip · crackedRIGHT PYLON SUPPORT CLIP AT UPPER REAR SPAR CAP IS CRACKED. -- FABRICATED AND INSTALLED CLIP.Mar 1, 2002 · N205ME · Doug DC932 · Nacelle/Pylon, Attach FittingsSDR MWEA020156Clip · elongatedFRAME TO SKIN ATTACH CLIP AT STATION 598 LEFT, UPPER FORWARD CORNER OF WINDOW RETAINER HAS ELONGATED HOLE. -- FABRICATED AND INSTALLED ATTACH CLIP.Mar 1, 2002 · N205ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020155Clip · elongatedFRAME TO INTERCOSTAL ATTACH CLIP AT STATION 598 LEFT HAS ELONGATED HOLES. -- FABRICATED AND INSTALLED CLIP.Mar 1, 2002 · N205ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020154Intercostal · bentAFT ACCESSORY, INTERCOSTAL BENT AND HAS AREAS OF BARE METAL BETWEEN CANTED FRAMES 1168 AND 1155. -- FABRICATED AND INSTALLED INTERCOSTAL.Mar 1, 2002 · N205ME · Doug DC932 · Fuselage Main, StructureSDR MWEA020153Longeron · corrodedAFT ACCESSORY, LONGERON 22 LEFT HAS AREAS OF BARE METAL AND LIGHT CORROSION FROM CANTED FRAME 1121 TO SKIN SPLICE JUST FWD OF FUSELAGE STATION 1076. REMOVED AND REPLACED LONGERON SECTION.Mar 1, 2002 · N205ME · Doug DC932 · Fuselage Main, Longeron/StringerSDR ABXA010755Switch · defectiveON INITIAL GEAR EXTENSION AT ILN, NOSE GEAR DID NOT INDICATE DOWN/LOCKED. SUBSEQUENT RETRACTION/EXTENSION CYCLE YIELDED NORMAL INDICATION. REPLACED THE NOSE GEAR DOWN LOCK SWITCH IAW DC-9 MM 32-60-02.Mar 1, 2002 · N982AX · Doug DC932 · Landing Gear Position and WarningSDR MWEA020151Hinge Fitting · crackedAFT VENTRAL DOOR JAMB, LOWER JAMB DOOR HINGE IS CRACKED. REMOVED AND REPLACED WITH FITTING.Mar 1, 2002 · N215ME · Doug DC932 · Fuselage, Door HingeSDR MWEA020150Floorboard · puncturedFLOORBOARD AT FUSELAGE STATION 288 BETWEEN NR 1 AND 2 SEAT TRACK HAS A SMALL PUNCTURE. FABRICATED AND INSTALLED FLOORBOARD REPAIR.Mar 1, 2002 · N215ME · Doug DC932 · Fuselage Floor PanelSDR MWEA020149Clip · crackedKEEL BEAM AREA LEFT SIDE FRAME STATION 658 HAS A CRACKED END CLIP LOCATED AT LONGERON 27 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE.Mar 1, 2002 · N215ME · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA020148Skin · dentedLEFT ELEVATOR LOWER SKIN DENTED AT APPROXIMATELY XE 184, APPROXIMATELY 2 INCHES BY 3/8 INCH .035 DEEP. -- FABRICATED AND INSTALLED SKIN.Mar 1, 2002 · N215ME · Doug DC932 · Elevator StructureSDR MWEA020147Frame · crackedLEFT LAV AREA HAS CRACK IN FRAME AT STATION 981 BETWEEN LONGERON 16 LEFT AND 15 LEFT. REMOVED AND REPLACED FRAME.Mar 1, 2002 · N215ME · Doug DC932 · Fuselage Main, FrameSDR MWEA020146Floorbeam · chafedSTATION 617 FLOORBEAM IS LOOSE JUST INBOARD OF THE NR 2 SEAT TRACK, SHOWS SIGNS OF CHAFING. REMOVED AND REPLACED FLOORBEAM.Mar 1, 2002 · N215ME · Doug DC932 · Fuselage Main, Floor BeamSDR MWEA020145Floorboard · corrodedCORROSION ON CABIN FLOOR BOARD 31 AT STATION 237. FABRICATED AND INSTALLED SLICE REPAIR.Mar 1, 2002 · N215ME · Doug DC932 · Fuselage Floor PanelSDR MWEA020144Seat Track · corrodedCORROSION ON NR 3 SEAT TRACK AT FROM 200 TO STATION 237. FABRICATED AND INSTALLED SEAT TRACK SECTION.Mar 1, 2002 · N215ME · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR MWEA020143Mount Bracket · gougedSTATION 351 FLOORBEAM STRUT SIDEWALL MOUNT RIGHT SIDE IS GOUGED. FABRICATED AND INSTALLED MOUNT.Mar 1, 2002 · N215ME · Doug DC932 · Fuselage Miscellaneous StructureSDR AT0200029Slide · out of positionFORWARD L1 DOOR CHUTE FELL OUT OF CONTAINER. REINSTALLED SLIDE REF 25-62.Feb 28, 2002 · N847AT · Doug DC932 · Escape SlideSDR ABXA010754Warning System · malfunctionedON INITIAL GEAR EXTENSION AT ILN, NOSE LANDING GEAR DID NOT INDICATE DOWN/LOCKED. SUBSEQUENTIAL RETRACT/EXTENSION CYCLE YIELDED NORMAL INDICATION. PERFORMED FUNCTIONAL CHECK IAW DC-9 MM 32-60-00-2-0101, NORMAL INDICATION AT THIS TIME.Feb 28, 2002 · N982AX · Doug DC932 · Landing Gear Position and Warning
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