Douglas DC9-15
Service difficulty reports · 926
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 = 'DC915' 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 = 'DC915' 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 MWEA030172Doubler · dentedLEFT FLAP FOUND DENT 1 X .068 INCH DEEP AT STATION XRS 320. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER.SDR MWEA030175Switch · out of adjustELEVATOR POWER ON ANNUNCIATOR DOES NOT ILLUMINATE ON ELEVATOR POWER CHECK. INSPECTED SWITCH AND PERFORMED ADJUSTMENT TEST. NO DEFECTS NOTED, TEST GOOD.SDR MWEA030170Panel · dentedRIGHT CENTER SPOILER PANEL HAS DENT 1.5 X .033 INCH DEEP AND DELAMINATED. ROUT OUT DAMAGE BONDED EXISTING DOUBLER.SDR MWEA030167Panel · dentedRIGHT CENTER SPOILER PANEL HAS A DENT 2.5 X .052 INCH DEEP AND DELAMINATED. ROUT OUT DAMAGE AND BOND EXISTING DOUBLER.SDR MWEA030173Structure · dentedLEFT AILERON TAB HAS A DENT LOCATED AFT OF THE THIRD HINGE OUTBOARD TRAILING EDGE DENT 2 X .080 INCH DEEP. REPAIRED AND BALANCED AILERON CONTROL TAB.SDR MWEA030171Skin · dentedRIGHT CENTER SPOILER PANEL HAS DENT 1.75 X .037 INCH DEEP AND DELAMINATED. ROUT OUT DAMAGE AND BOND DOUBLER.SDR MWEA030169Skin · dentedLEFT WING INBOARD FLIGHT SPOILER HAS DENT 2.375 X .059 INCH DEEP. CUT OUT DAMAGE, HOT BOND DOUBLER.SDR MWEA030168Skin · dentedLEFT WING GROUND SPOILER HAS A DENT 2 X .058 INCH DEEP. CUT OUT DAMAGE, HOT BOND ON REPAIR DOUBLER.SDR ABXA030056Warning Horn · activatedAFTER TAKE-OFF OUT OF ILN, AIRCRAFT FAILED TO PRESSURIZE AND CONFIGURATION WARNING HORN SOUNDED. CHECKED LT OLEO SWITCH, EXERCISED SWITCH SEVERAL TIMES. CLEANED AND RESEATED CONNECTOR. CREW ASSISTED IN GROUND OPS CHECK OF PRESSURIZATOIN AND CONFIG. WARNING SYSDR MWEA020768Doubler · puncturedTHERE IS A PUNCTURE IN THE SUBFLOORING JUST AFT OF STATION 160 AT RIGHT SIDE OF CENTERLINE OF FUSELAGE. -- REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER.SDR MWEA020767Doubler · crackedFORWARD FACE OF THE AFT PRESSURE BULKHEAD AT THE SEVEN O'CLOCK POSTION DOOR JAMB PIN HOLDER IS CRACKED. -- FABRICATED AND INSTALLED FINGER DOUBLER AND DOUBLER.SDR MWEA020766Doubler · crackedFORWARD FACE OF THE AFT PRESSURE BULKHEAD AT THE FIVE O'CLOCK POSITION PLUG DOOR JAMB PIN HOLDER IS CRACKED. -- FABRICATED AND INSTALLED FINGER DOUBLER AND REPAIR DOUBLER.SDR MWEA020765Nut Plate · corrodedPRESSURE SLANT PANEL CORRODED AROUND LOWER NUT PLATES ON LEFT SIDE FROM APPROXIMATELY 22 INCHES TO 44 INCHES FROM CENTERLINE. -- FABRICATED AND INSTALLED NEW SLANT PANEL AND INSTALLED NUT PLATES.SDR MWEA020751Stiffener · crackedSTIFFENER AT AFT PRESSURE BULKHEAD AFT SIDE RADIAL 20 RIGHT. -- FABRICATED AND INSTALLED STIFFENER.SDR MWEA020750Doubler · crackedFORWARD CARGO DOOR OUTER PAN RADIUS IS CRACKED INBOARD OF LOWER FORWARD DOOR STOP PAD. -- FABRICATED, DRILLED AND INSTALLED DOUBLER.SDR MWEA020749Stiffener · crackedSTIFFENER AT AFT PRESSURE BULKHEAD AFT SIDE RADIAL 20 LEFT IS CRACKED. -- FABRICATED AND INSTALLED STIFFENER.SDR MWEA020746Stiffener · corrodedSIX EACH STIFFENERS CORRODED ON LEFT PRESSURE PANEL. -- FABRICATED AND INSTALLED STIFFENERS.SDR MWEA020739Intercostal · crackedFORWARD CARGO DOOR, INTERCOSTAL IS CRACKED BETWEEN BEAM #5 AND UPPER DOOR PAN. -- LOCATED AND DRILLED AND INSTALLED NEW INTERCOSTAL.SDR MWEA020731Doubler · corrodedEXISTING REPAIR ON SUBFLOOR AT STATION 165 APPROXIMATELY 10 INCHES RIGHT SIDE FROM CENTERLINE HAS SEVERAL FASTENERS PULLING THROUGH FLOOR WEB.SDR MWEA020730Doubler · corrodedCORROSION IN SUBFLOOR AT APPROXIMATELY STATION 170 ABOUT 20 INCHES RIGHT OF FUSELAGE CENTERLINE. -- REMOVED CORROSION FABRICATED AND INSTALLED DOUBLER.SDR MWEA020729Doubler · corrodedCORROSION THROUGH SUBFLOORING JUST AFT OF STATION 160 AT LEFT SIDE OF FUSELAGE CENTERLINE.. -- REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER.SDR 0203489138Sensor · failedAT FL310, THE CABIN PRESSURE BECAME UNSTABLE AND THEN COMPLETELY FAILED. CREW FOLLOWED COM PROCEDURES AND DESCENDED TO 8000 FT. MASKS DID DEPLOY IN THE CABIN. FLIGHT RETURNED TO MSP AND LANDED UNEVENTFULLY. MAINTENANCE FOUND THE OUTFLOW VALVE OUT OF RIG ANSDR 02034191382Insulation · out of positionAT FL330, CABIN PRESSURE WAS LOST. FLIGHT DESCENDED TO 10,000 FT AND CONTINUED TO DTW. MASKS DID DEPLOY IN THE CABIN. CREW WAS NOT ABLE TO COMPLETELY CLOSE THE OUTFLOW VALVE. MAINTENANCE FOUND INSULATION MATERIAL BLOCKING THE VALVE AND RESECURED IT. OPERASDR MWEA02574Intercostal · damagedINTERCOSTAL AT FRAME STATION 340 BETWEEN LONGERON 28 AND 29 DAMAGED. REMOVED INTERCOSTAL, FIT AND DRILLED UP AND INSTALLED NEW INTERCOSTAL.SDR MWEA020573Intercostal · gougedAFT CARGO COMPARTMENT INTERCOSTAL AT LONGERON 29 RIGHT HAS GOUGES ALONG AFT END AT STATION 785. REMOVED INTERCOSTAL, DRILLED UP AND INSTALLED NEW INTERCOSTAL.SDR MWEA020571Rib · tornAFT END OF XCW 42 RIBS IS TORN ABOUT MIDWAY UPPER WEB. FABRICATED FILLER AND REPAIRED DOUBLER, LOCATED AND DRILLED FILLER AND DOUBLER, INSTALLED FILLER AND DOUBLER.SDR MWEA020570Hinge · wornLT MLG OUTBOARD FLYING DOOR. THE ARTICULATING DOOR HINGE HAS A FAIR AMOUNT OF MOVEMENT VERTICALLY. REMOVED, LOCATED AND DRILLED WORN HINGE SECTION AND INSTALLED HINGE SECTION AND FLYING DOOR.SDR MWEA020568Splice · damagedFASTENER HOLES DAMAGED IN CENTER TANK ON STRINGER 17 AFT SPLICE PLATE APPROXIMATELY 1 INCH LEFT OF STATION 0 BULKHEAD. SPOTFACED HOLE TO REMOVE DAMAGE, FABRICATED AND INSTALLED FASTENERS IN STRAP.SDR MWEA020567Frame · crackedFASTENER HOLES AT FRAME STATION 785 AND LONGERON 22 LEFT IS CRACKED. FABRICATED, LOCATED AND DRILLED AND INSTALLED FRAME SPLICE. REMOVED AND INSTALLED SHEAR TIE.SDR MWEA020566Longeron · damagedAFT CARGO LONGERON 29 RIGHT HAS ELONGATED HOLES TWO EACH STATION 785 FRAME LOCATION. FABRICATED AND INSTALLED SECTION OF LONGERON. REMOVED AND INSTALLED SHOVEL CLIP.SDR MWEA020562Fitting · corrodedRIGHT WING XCW 58 LOWER WING TEE REQUIRES REPAIR OR REPLACEMENT DUE TO CORROSION REMOVAL. REMOVED WING TEE, RECEIVED NEW WING TEE, LOCATED AND DRILLED AND INSTALLED WING TEE.SDR MWEA020561Floor Support · corrodedFORWARD CARGO COMPARTMENT FLOOR SUPPORT AT STATION 218 HAS SEVERAL AREAS LIGHT CORROSION LONGERON 30 TO 28 RIGHT DOT 469. HEAT TREATED 2 DOUBLERS, LOCATED AND DRILLED DOUBLER, INSTALLED REPAIR DOUBLER, LOCATING AND DRILLED REMAINING FLOOR LINING, INSTALLED 2 SDR MWEA020556Shear Tie · damagedREMOVED SHEAR TIE AT STATION 785 FROM LONGERON 21 LEFT TO 27 LEFT TO FACILITATE MAINTENANCE. SHEAR TIE HAS SEVERAL ELONGATED HOLES, LOCATED AND DRILLED AND INSTALLED SHEAR TIE.SDR MWEA020560Door Frame · corrodedFORWARD CARGO COMPARTMENT LOWER DOOR JAMB HAS SEVERAL AREAS OF MODERATE CORROSION STATION 312 TO 370. REMOVED DAMAGED SECTION FIT, DRILLED SECTION AND INSTALLED NEW SECTION.SDR MWEA020558Attach Angle · damagedSTATION 930 AT THE LEFT DORSAL FIN ATTACH ANGLE HAS TWO FASTENERS PULLING THROUGH. REMOVED 2 HI-LOKS, FABRICATED AND INSTALLED SLEEVE BUSHINGS.SDR MWEA020557Attach Angle · damagedSTATION 930 FRAME AT THE RIGHT DORSAL FIN ATTACH ANGLE HAS A FASTENER PULLING THROUGH. REMOVED 2 HI-LOKS FROM RIGHT SIDE, REAMED 2 HOLES, FABRICATED AND INSTALLED SLEEVE BUSHING.SDR MWEA020555Intercostal · damagedREMOVED INTERCOSTAL FROM STATION 785 TO 800 AT LONGERON 29 RIGHT TO FACILITATE MAINTENANCE. FOUND ELONGATED HOLES. LOCATED AND DRILLED INTERCOSTAL, INSTALLED INTERCOSTAL.SDR MWEA020554Intercostal · damagedAT STATION 766 LONGERON 29 RIGHT INTERCOSTAL FORWARD ATTACH CLIP HAS ELONGATED HOLE. REMOVED ATTACH CLIP, FABRICATED AND INSTALLED CLIP.SDR MWEA020553Intercostal · damagedINTERCOSTAL AT FRAME STATION 332 BETWEEN LONGERON 28 AND 29 DAMAGED. REMOVED INTERCOSTAL, FABRICATED FIT AND DRILLED CLIPS AND INTERCOSTAL, INSTALLED INTERCOSTAL AND CLIP.SDR MWEA020550Clip · crackedCENTER TANK FORWARD SPAR ACCESS WEB 8 EACH INSULATION ATTACH CLIPS REQUIRE REMOVAL TO FACILITATE OTHER MAINTENANCE. REMOVED AND INSPECTED CLIPS, FABRICATED AND INSTALLED CLIPS.SDR MWEA020549Intercostal · damagedINTERCOSTAL AT FRAME STATION BETWEEN LONGERON 28 AND 29 DAMAGED. FIT AND DRILLED INTERCOSTAL REMOVED AND INSTALLED INTERCOSTAL.SDR MWEA020548Intercostal · damagedINTERCOSTAL AT FRAME STATION 360 BETWEEN LONGERON 29 DAMAGED. FIT AND DRILLED INTERCOSTAL REMOVED AND INSTALLED INTERCOSTAL.SDR MWEA020547Shear Tie · damagedAT FRAME STATION 786 FRAME TO SKIN SHEAR TIE HAS NUMEROUS ELONGATED HOLES FROM LONGERON 30 TO 27 LEFT. LOCATED AND DRILLED SHEAR TIE, REMOVED AND INSTALLED SHEAR TIE.SDR MWEA020546Intercostal · damagedINTERCOSTAL AT FRAME STATION 320 BETWEEN LONGERON 28 AND LONGERON 29 DAMAGED. FIT AND DRILLED INTERCOSTAL, REMOVED AND INSTALLED INTERCOSTAL.SDR MWEA020545Skin · crackedNOSE SKIN HAS 4 POSSIBLE CRACKS AT STATION 76.6, 18 INCHES LEFT OF CENTER AREA NEEDS TO BE STRIPPED AND VERIFIED. VERIFIED CRACKS LOCATED AND DRILLED PILOT HOLES AND FABRICATED DOUBLER.SDR MWEA020542Intercostal · damagedINTERCOSTAL AT LONGERON 29 BETWEEN FRAME STATION 313 AND 370 HAS A LARGE HOLE ON UPPER AFT END. REMOVED AND INSTALLED INTERCOSTAL.SDR MWEA020516Intercostal · corrodedFORWARD CARGO COMPARTMENT HAS LIGHT CORROSION ON INTERCOSTAL AT STA 218-237 BETWEEN LONGERON 28R-27R. DRILLED UP NEW INTERCOSTAL, REMOVED AND INSTALLED INTERCOSTAL.SDR MWEA020515Intercostal · crackedFORWARD CARGO DOOR HAS A CRACKED INTERCOSTAL OUTBOARD OF LOWER AFT STOP FITTINGS BELOW BEAM 1. LOCATED AND DRILLED INTERCOSTAL. REMOVED AND INSTALLED INTERCOSTAL.SDR MWEA020441Connector · faultyLEFT ENGINE OIL TEMPERATURE IS PEGGED. PRESSURE AND QUANTITY IS NORMAL PER QRH. ENGINE NOT SHUT DOWN WITHIN 15 MINUTE LIMIT WHEN AIRCRAFT LANDED AT MILWAUKEE. FUEL TEMPERATURE ALSO DID NOT INCREASE. REPAIRED AND REPLACED LEFT ENGINE OIL TEMPERATURE CONNECTSDR ABXA010880Stop Fitting · shearedHORIZONTAL STABILIZER JACKSCREW, UPPER MECHANICAL STOP SHEARED OFF. REMOVED AND REPLACED THE JACKSCREW ASSEMBLY IAW DC-9 MM.
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