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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AT9900064Outflow Valve · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND OUTFLOW VALVE HOUSING CORRODED AROUND NUT PLATES AND HAS SURFACE CORROSION LOWER INBOARD SIDE. REMOVED NUT PLATES AND CORROSION FOUND BEYOND LIMITS. REINSTALLED OUT FLOW VALVE IAW DC9 SRM 53-01 FIG 1, 51-10-3, ANSDR AT9900062Frame · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. E/E COMPARTMENT AT FRAME STA 180 L-29L TO L-29R WAS FOUND CORRODED AT FASTENERS LOCATION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR ANGLES AND STRAPS IAW DC9 SRM 51-10-3, 53-03 FIG 4A, 53-01 FIG 1, AND 51-30-5.SDR VJ9800660Slide · not securedMAIN CABIN ENTRY DOOR NOT SECURED. MAIN CABIN ENTRY DOOR SLIDE SECURED PER DC9 MM 25-62-0 RII COMPLIED WITH.SDR VJ9800659Slide · not securedFORWARD EMERGENCY EXIT SLIDE CAME OFF L-1 DOOR. REINSTALLED EMERGENCY EXIT SLIDE L-1 DOOR PER MM 25-60.SDR AT9900042Longeron · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION OUT OF LIMITS AND LEVEL 2 CORROSION AT THE FORWARD CARGO PIT COMPARTMENT AT STA 517 L-27R AND STA 218 L-29L. REMOVED CORROSION OUT OF LIMITS, FABRICATED AND INSTALLED NEW FLOOR CHANNEL AND LONGERON SECTISDR 9810909916Spar Cap · crackedDURING PERIODIC CHECK, FOUND RIGHT WING LOWER SPAR CAP WITH ONE INCH CRACK AT FS 353 BELOW LOWER OUTBOARD MOUNTING HOLE AT NR 4 HINGE FITTING. INSTALLED INTERIM REPAIR PER EA 99-159428.SDR 9810899920Doubler · crackedDURING PERIODIC CHECK, FOUND EXTERNAL SKIN DOUBLER CRACKED BETWEEN FRAME AND DOUBLER AT FS 83.5. FABRICATED AND INSTALLED NEW DOUBLER PER EA 99-158085.SDR VJ9800670Gusset · corrodedSCHEDULED INSPECTION, FLOOR FRAME FS 965 HAS CORROSION ON FRAME AND ATTACHING BRACKETS. REMOVED GUSSET, FOUND IT TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW GUSSET IAW DC9 SRM 51-30-2.SDR MWEA981155Slide · low pressureFORWARD ENTRY DOOR EVACUTATION SLIDE PRESSURE LOW. REMOVED AND REPLACED FORWARD ENTRY DOOR EVACUATION SLIDE.SDR CALA9802177Fitting · crackedINSPECTION FOUND A .5 INCH CRACK IN C-1 DOOR AFT LOWER STOP INTERCOSTAL TEE FITTING. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-8 AND 51-10-4.SDR AT9900099Angle · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLOOR SUPPORT ANGLE AT AFT BULKHEAD OF E/E COMPARTMENT CORRODED BEYOND LIMITS. REMOVED CORRODED FLOOR SUPPORT ANGLE, FABRICATED EXTRUSION, HEAT TREATED, DRILLED, AND INSTALLED IAW DC9 SRM 51-10-4, 51-30-1, 51-1SDR VJ9800682Skin · chafedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE VERTICAL STAB PANEL (DOG HOUSE) CHAFFING AT THE LEFT HAND AFT SECTION. FABRICATED AND INSTALLED NEW PANEL IAW DC9 SRM 51-10-3, 51-30-3, 55-31-0, AND AIRTRAN RES 982127.SDR VJ9800667Web · crackedSCHEDULED INSPECTION, FOUND A CRACK IN THE FORWARD CARGO DOOR. FABRICATED AND INSTALLED NEW REPAIRS IAW DC9 SRM 52-01 FIG 2 AND 51-10-3.SDR VJ9800666Rib · crackedSCHEDULED INSPECTION, LEFT WING LEADING EDGE RIB IS CRACKED AT STA 543 (NR 5 SLAT). REMOVED LEFT WING LEADING EDGE CRACKED RIB, DRILLED, DEBURRED, TREATED, PRIME AND INSTALLED NEW RIB IAW DC9 SRM 51-10-4, 51-10-3, AND 51-30-3.SDR VJ9800648Fuel Pump · malfunctionedAIR RETURN AFTER V1 ON THE TAKEOFF ROLL, NR 1 ENGINE THRUST DROPPED TO 1.44 EPR 79 PERCENT N1, 420 EGT 86.5 N1, 4400 FUEL FLOW STAYED THERE REGARDLESS OF THROTTLE POSITION. REMOVED AND REPLACED FUEL PUMP IAW 73-10-1, OPS CHECKED GOOD ON ENGINE RUN.SDR AT9900075Pan · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND CRACKS ON THE OUTER PAN FLANGE AFT CARGO DOOR AFT CENTER STOP AND ANOTHER ONE AT THE FORWARD CARGO DOOR AFT TOP (C-1 DOOR). FABRICATED, DEBURRED, PRIMED AND INSTALLED NEW DOUBLERS AND REPAIRS IAW DC9 SRM 52-03 FIGSDR 9810889611Actuator · failedLEFT MAIN LANDING GEAR GREEN LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW RECYCLED GEAR AND RED NOSE GEAR UNSAFE LIGHT REMAINED ON. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LENS LIGHT ASSEMBLY FOR LEFT MAIN GEAR GREEN LISDR VJ9800671Web · crackedSCHEDULED INSPECTION, CUSP WEB ANGLE AND DOUBLER CORRODED AND CRACKED AT FS 230L (CORRODED) AND STA 617 RT (CRACKED). REMOVED CORROSION AND FORMED SPLICE ANGLE FROM 7075-T6 .090 IAW DC9 SRM 53-04 AND RES 982167. REMOVED AND REPLACED CUSP WEB AT STA 617 TO 65SDR AT9900059Jamb · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. THE AFT PIT DOOR THRESHOLD PAN WAS FOUND WITH CORROSION, DENTS AND PUNCTURES. REMOVED, REPLACED, INSTALLED THE DOOR PAN AND SPLICES IAW DC9 SRM 53-05 FIG 44, 51-10-4, 51-10-3, 51-30-1, AND 51-20-0.SDR 9810929993Power Supply · inopDURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE IN FIRST CLASS SECTION AND AT GALLEY DOOR. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK NORMAL.SDR VJ9800672Longeron · crackedSCHEDULED INSPECTION, LONGERONS AT 4L STA 160 AND 22R STA 979R WERE FOUND CORRODED AND CRACKED. REMOVED LONGERON 4L FROM STA 148 TO 190. FABRICATED REPAIR LONGERON AND SPLICE FROM 277922-3 AND 7637813-3 IAW SRM DC9 53-11-1 FIG 3 AND 53-02. AT STATION 979R, SDR AT9900101Hat · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT HAT SECTION CANTED FRAME AT STA 1089 L-6R CORRODED. REMOVED HAT SECTION OUTBOARD OF L-6R, ALSO TREATED AND PRIMED CANTED FRAME AT L-10L TO L-10R. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-10-3, 53-01-SDR AT9900076Longeron · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS CRACKS AT DIFFERENT LONGERON LOCATIONS. THE LOCATIONS ARE AS FOLLOW: STA 945 L-17R, STA 965 L-13, 16, 17R, STA 965 L-14, 17L. LONGERON (P/N 7637813-3), (P/N 2777922-4), (P/N 1A-41527-1), (P/N 2777948), SSDR AT9900065Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. THE AFT PIT DRAIN BRACKET WAS FOUND CORRODED. REMOVED AND REPLACED THE DRAIN VALVE ASSEMBLY AND BRACKET IAW DC9 SRM 51-30-2, AND 51-10-3.SDR AT9900052Fitting · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION AT END TIE AT STA 996 L-27L AND L-28L. REMOVED AND REPLACED END TIE FITTINGS, DRILLED NEW PART, DEBURRED, TREATED, PRIMED AND INSTALLED NEW PARTS IAW DC9 SRM 51-30-2, 51-30-5, 51-10-3, 51-10-4, 53-01 FIGSDR VJ9800668Seat Track · corrodedSCHEDULED INSPECTION, FORWARD CARGO LEFT HAND TRACK FS 446 TO 511 HAS SURFACE CORROSION THRU OUT. REMOVED AND REPLACED WITH A NEW SECTION OF TRACK IAW DC9 SRM 51-10-4 AND 51-10-2.SDR MWEA981147Latch · out of adjustTAIL CONE DID NOT DROP DURING FUNCTIONAL CHECK. MTC ADJUSTED LATCH LEVER CABLE.SDR AT9900102Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT ACCESSORY COMPARTMENT CABLE PULLEY BRACKET HAS CORROSION AT STA 1120 LEFT SIDE LOWER AREA. REMOVED, REPLACED, AND INSTALLED NEW PULLEY BRACKET IN AFT ACCESSORY COMPARTMENT IAW DC9 MM 16-10-20. SYSTEM NOT DSDR AT9900074Skin · dentedSCHEDULED INSPECTION AT AERO CORP, FL. A DENT WAS FOUND TO BE OUT OF LIMITS AT STA 338 L-28R. COLD WORKED DENT TO ORIGINAL CONTOUR, FABRICATED DOUBLER, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-2, 51-10-2 AND 53-04 FIG 38.SDR AT9900058Floor · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CARGO CENTER FLOOR PANEL CORRODED AND WITH ELONGATED HOLES AT STA 756 TO 794. REMOVED PANEL, FABRICATED, TREATED, PRIMED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 51-10-2, 53-21-0 FIG 10, AND 51-10-4.SDR AT9900057Skin · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. CORROSION WAS FOUND UNDER THE AUXILIARY TANK JUST FORWARD OF THE RIGHT HAND KIDNEY PANEL AT STA 559. REMOVED ALL CORROSION AND DOUBLER, FABRICATED AND INSTALLED NEW REPAIR DOUBLER AND REPLACED END CAP FITTING IAW DC9 SRSDR AT9900055Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON CARGO TRACKS AT VARIOUS STATION LOCATIONS. THE LOCATIONS ARE AS FOLLOWS: STA 218 TO 362 LT, STA 351 TO 446 LT, STA 446 TO 511 LT, STA 897 TO 965 LT, STA 218 TO 362 RT, STA 351 TO 362 RT, STA 362 TO 3SDR AT9900049Bracket · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. LOWER FACE ON UPPER PRESSURE PANEL IN NOSE WHEEL WELL HAS CORROSION ON INSULATION SUPPORT MOUNT BRACKETS AT STA 71 16 LEFT TO RIGHT OF CENTER, STA 73 TO 78 16 LEFT TO CENTER, STA 80 TO 99 16 FROM LEFT TO RIGHT CENTER. SDR VJ9800684Filler · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND CORROSION ON AFT LAVATORY VANITY TO BE OUT OF LIMITS. REMOVED OLD FILLER, FABRICATED AND INSTALLED NEW FILLER IAW DC9 SRM 51-10-04, 51-10-3, AND 51-30-2.SDR AT9900097Spar · misdrilledSCHEDULED INSPECTION AT AERO CORP, FL, FOUND LEFT HAND HORIZONTAL STABILIZER UPPER SPAR CAP HAS HOLE DRILLED ON UPPER SIDE NEXT TO FASTENER HOLE AT STA 120. REMOVED NUT PLATE CLIP, REPAIRED FASTENER HOLE BY STEPPING UP HOLE AND REINTALLING NUT PLATE CLIP IAW SDR AT9900050Bulkhead Angle · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD CENTER L ANGLE AND AROUND FASTENER LOWER END STA 996 AFT PIT. THE OTHER WAS FOUND ON THE FORWARD CARGO AFT BULKHEAD CENTER PANEL HAS ELONGATED HOLES, WORN AND SURFACE CORROSISDR AT9900034Cusp Web · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND CUSP WEBS CORRODED AND CRACKED AT THE FOLLOWING LOCATIONS FS 598 RT, FS 617 RT, FS 794 TO 813 LT, FS 813 TO 832 LT, FS 869 TO 889 LT, FS 870 TO 897 RT, FS 894 LT, AND FS 897 TO FS 908 RT. REPAIRED, REMOVED ALL CORSDR ABXA9801180Indication · malfunctionedGEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. RECYCLED GEAR AT 200 KTS, LIGHT REMAINED ON. RECYCLED GEAR AT 250 KTS, LIGHT WENT OUT. VISUALLY INSPECTED GEAR AND WHEEL WELL AREA. NO DEFECTS NOTED. OPERATED GEAR. ALL INDICATIONS WERE NORMAL.SDR 99ZZZX336Chip Collector · failedCHIP COLLECTOR ON RIGHT ENGINE, NR 4 BEARING SCAVENGE LINE, CHIP COLLECTOR MAGNETIC PROBE EJECTED FROM CHIP COLLECTOR BODY. ENGINE OIL DRAINED FROM ENGINE IN-FLIGHT. ANALYSIS DETERMINED THE INTERNAL CHECK VALVE OF CHIP COLLECTOR WAS STUCK IN THE OPEN POSITIOSDR CALA9802161Skin · corrodedINSPECTION FOUND FUSELAGE SKIN BULGED AT STA 218 BETWEEN LONGERONS 17R AND 18R. THE BULGED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-04, PAGE 208, 51-10-3, AND 51-30-2.SDR AT9900100Frame · chafedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT SECTION INTERIOR TAIL CONE RELEASE HANDLE METALLIC PLACARD WAS CHAFFING AGAINST THE FRAME AT STA 1143. CLEAN UP WORN FRAME, FABRICATED STRAP TO BACK SIDE OF FRAME FLANGE, PRIMED AND INSTALLED IAW DC9 SRM 53SDR AT9900031End Cap · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND SEVERAL CORRODED LONGERON END CAPS AT THE FOLLOWING LOCATIONS FS 1164 L-3R, FS 1164 L-5R, FS 1164 L-7R, FS 1164 L-9R. REMOVED AND REPLACED ALL END CAPS IAW DC9 SRM 51-30-2 AND 51-30-5.SDR MWEA981146Windshield · defectiveBURNING SMELL IN COCKPIT. DIVERTED TO MKE. SMELL WORSENED, DECLARED EMERGENCY LANDING. CENTER WINDSHEILD HEAT BLOCK ON CENTER WINDSHEILD TERMINAL E MELTED, BURNT. REMOVED AND REPLACED CENTER WINDSHEILD TEMP CTRL BOX.SDR MWEA981138Longeron · corrodedFOUND CORROSION ON LONGERON 30 AT STATION 603 SHOVEL END. MTC REMOVED AND REPLACED LONGERON AND FITTING.SDR ABXA9801160Wire · brokenRIGHT ENGINE OIL TEMPERATURE INDICATION EXTREME HIGH END OF SCALE DURING CRUISE FLIGHT. ALL INDICATIONS NORMAL. PERFORMED ENGINE SHUTDOWN. FOUND WIRE E355A18N BROKEN AT GROUND LUG 906. REPAIRED WIRE. ALSO, FOUND FOUR GROUND TERMINAL BRACKETS AND LUG HARDSDR MWEA981139Web · corrosionFOUND CORROSION AT FUSELAGE 935 AFT PIT DOOR JAM BY LONGERON 25 AND 26 RIGHT ON WEB SECTION. MTC REMOVED AND REPLACED WEB SECTION.SDR AT9900098Panel · crackedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD PIT NR 2 AND NR 3 LOWER SIDE WALL PANEL HAS A 4 CRACK AND 8 HOLE. REMOVED, REPLACED, FABRICATED, TRIMMED, AND DRILLED NEW PANELS IAW DC9 SRM 51-30-0, 53-21-0, MM 25-52-1, AND RES NR 982221.SDR ABXA9801161Wire · brokenRIGHT ENGINE OIL TEMPERATURE INDICATION EXTREME HIGH END OF SCALE DURING CRUISE FLIGHT. CHECKED AND RESET CIRCUIT BREAKER. ALL OTHER INDICATIONS NORMAL. PERFORMED ENGINE SHUTDOWN. FOUND BROKEN WIRE AT RIGHT ENGINE GROUND BLOCK ON TOP OF ENGINE. REPAIRED ISDR MWEA981142Skin · dentedFOUND SMALL DENT ON FUSELAGE SKIN AT FUSELAGE 237 JUST BELOW L17 LEFT. MTC COLD WORKED DENT AND FOUND ON CRACKS FABRICATED AND INSTALLED DOUBLER.SDR MWEA981141Skin · dentedFOUND SMALL GOUGE IN FUSELAGE SKIN AT FS 229 JUST BELOW L17 LEFT. MTC COLD WORKED DENT AND FOUND NO CRACKS AND FABRICATED AND INSTALLED DOUBLER.
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