Douglas DC-9-31
Service difficulty reports · 7,433
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 = '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.
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
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 0401499915Frame · crackedDURING L-CHECK, FOUND CRACK IN FUSELAGE FRAME AT BS 1019 BELOW L14L. REPAIRED IAW EA 99-200165.SDR 0401579915Skin · crackedDURING L-CHECK FOUND CRACK IN FUSELAGE NOSE SKIN AT BS 69.5 RBL 20. REPAIRED PER EA 99-200164.SDR 0401489969Stiffener · crackedDURING H-CHECK FOUND CRACKS IN VERTICAL STIFFENER AT BS 756 RBL 24. REPAIRED IAW EA 99-199103.SDR ABXA040267Frame · crackedLEFT FORWARD MAIN FRAME AT FUSELAGE STA 699 WAS CRACKED BEYOND LIMITS OF DC-9 S/B 53-131. CRACK RAN BETWEEN POINTS G - J. REPLACED FRAME IAW ABX EA 53400321-001-4, WO 600204273.SDR ABXA040268Frame · crackedRIGHT FORWARD MAIN FRAME AT FUSELAGE STA 699 WAS CRACKED BEYOND LIMITS OF DC-9 S/B 53-131. CRACK RAN BETWEEN POINTS H - I. REPLACED FRAME IAW ABX EA 53400322-001-4, WO 600204273.SDR ABXA040269Switch · failedON FINAL, COCKPIT SMELLED LIKE ELECTRICAL BURNING. TURNED RADAR OFF, HELPED SOMEWHAT. VERIFIED ELECTRICAL BURNING SMELL CAME FROM NOSE TAXI LIGHT SWITCH. REPLACED SWITCH IAW DC-9 WDM 33-41-01, FOR PRECAUTIONARY. CHECKED TRANSFORMER RECTIFIERS, WINDOW HEAT, SDR ABXA040279Cusp Web · corrodedLEFT CUSP CRACKED AT STA 880. REPLACED LEFT CUSP BETWEEN FS 832 TO 899 IAW DC-9 SRM 51-30-2 AND 51-30-1.SDR ABXA040278Cusp Web · crackedNUMEROUS CRACKS IN LEFT CUSP WEB, FS 945 TO 965. REPLACED LEFT CUSP WEB IAW DC-9 SRM 51-30-1 AND 51-30-2.SDR ABXA040277Skin · corrodedEXTERIOR FUSELGAE SKIN AT STA 180, LONGERON 30 CORRODED. REPAIRED FUSELAGE SKIN AT STA 180, LONGERON 30.SDR ABXA040276Floorbeam · corrodedFLOORBEAM CORRODED AT STA 937, RIGHT BUTTLINE 18. REPAIRED FLOORBEAM IAW DC-9 SRM 53-05.SDR ABXA040275Frame · crackedLEFT MAIN FRAME STA 718 WAS CRACKED BEYOND LIMITS. REPLACED MAIN FRAME IAW JOB CARD EA 53400323-001-2.SDR ABXA040273Longeron · crackedLONGERON 17 RIGHT CRACKED AT FRAME STA 560. REPLACED DAMAGED SECTION OF LONGERON IAW DC-9 SRM 53-02.SDR ABXA040274Longeron · crackedLONGERON 12 RIGHT CRACKED AT FRAME STA 944. REPAIRED LONGERON 12 RIGHT, FS FRAME 944 IAW DC-9 SRM 53-02.SDR ABXA040272Skin · crackedSKIN WAS CRACKED AT MAIN ENTRY DOOR CUTOUT, UPPER AFT STOP. REPAIRED MAIN ENTRY DOOR CORNER IAW DC-9 SRM 53-05.SDR ABXA040247Downlock Switch · defectiveDURING GEAR EXTENSION, THE NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE WHILE THE NOSE GEAR UNSAFE LIGHT STAYED LIT. THE GEAR WAS RECYCLED. AFTER ONE MINUTE, THE NOSE GEAR CAME DOWN AND LOCKED. REMOVED AND REPLACED THE NOSE LANDING GEAR DOWNLOCK SWITCH IAW DCSDR 0401189953Controller · intermittentFLIGHT CREW WAS NOT ABLE TO CONTROL THE PRESSURIZATION WITH AUTOMATIC CONTROL AFTER TAKEOFF, UTILIZED MANUAL CONTROL. MANUAL CONTROL FAILED AND THE OUTFLOW VALVE WENT FULL OPEN AT FL230. EMERGENCY DESCENT TO 10,000 FT AND THEN NORMAL DESCENT TO 6,000 FT. CASDR ABXA040253Drive Link · crackedWHILE ACCOMPLISHING NEA7800001-001, THE LOWER RIGHT THRUST REVERSER LINK WAS FOUND CRACKED AROUND CENTER PIVOT FLANGE AND BOSS. LINK REPLACED ON J/C NEA78300001-001.SDR ABXA040255Bracket · crackedATTACH ANGLE CRACKED FORWARD SIDE FLOORBEAM STA 639, RBL 54. REPLACED ANGLE IAW DC-9 SRM 51-30-2.SDR ABXA040254Cap · crackedTRAILING EDGE FITTING CRACKED AT INBOARD SPOILER INBOARD END STOP PAD. REPLACED FITTING IAW DC-9 MM.SDR ABXA040243Warning Light · malfunctionedRT GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER TAKE OFF. LIGHT EXTINGUISHED AFTER APPROXIMATELY 2 MINUTES FOLLOWING RECYCLING OF GEAR. UNABLE TO DUPLICATE. INSPECTED UPLOCK AND DOWNLOCK LIMIT SWITCHES AND VISIBLE WIRING IAW WIRING MANUAL. OPERATIONAL CHECKSDR ABXA040252Shear Tie · crackedSHEAR TIE CRACKED FS 1019 JUST ABOVE LONGERON 17 LEFT. REPAIRED IAW DC-9 SSRM K05159.SDR ABXA040256Frame · crackedFRAME CRACKED AT LOWER END, STA 639 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03.SDR 0400979959Duct · disconnectedWHILE CRUISING AT FL330, THE CABIN ALTITUDE CLIMBED TO 11,000 FT. CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FEET AND DIVERTED TO BNA. CABIN STOPPED CLIMBING AND MAINTAINED 11,000 FEET UNTIL AIRCRAFT PASSED 15,000 FEET THEN CABIN STARTED DESCENDING AND OPSDR ABXA040218Skin · crackedAFT LOWER CARGO DOOR SKIN WAS CRACKED AT THE DOOR HANDLE CUTOUT. REMOVED CRACKS, INSTALLED SCUFF PLATE IAW DC-9 SRM 52-05.SDR ABXA040217Skin · crackedSKIN CRACKED ABOVE RIGHT PYLON AT RIVET, STA 1038, LONGERON 12 RIGHT. REPAIRED CRACK IAW DC-9 SRM 53-31-0.SDR ABXA040216Skin · crackedSKIN CRACKED ABOVE LEFT PYLON AT RIVET, STA 1038, LONGERON 12 LEFT. REPAIRED CRACK IAW DC-9 SRM 53-31-0.SDR ABXA040215Cusp Web · crackedCUSP WEB CRACKED IN TWO AREAS FS 237 TO FS 254, RIGHT BUTTLINE 45 TO RIGHT BUTTLINE 54. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.SDR ABXA040214Skin · crackedA .5 INCH CRACK COMING OUT OF FASTENER HOLE AT FORWARD LOWER CARGO DOOR UPPER CORNER FUSELAGE SKIN. INSTALLED REPAIR IAW EA 53100110-001.SDR 0400959989Pump · leakingRIGHT HYDRAULIC SYSTEM QUANTITY DROPPED TO LESS THAN 3 QUARTS DURING DESCENT. COM PROCEDURES COMPLIED WITH AND PRESSURE WAS NORMAL. FLIGHT LANDED WITHOUT INCIDENT AT IAH AND THEN HYDRAULIC QUANTITY DROPPED TO ZERO AFTER TOUCHDOWN. MAINTENANCE FOUND A LEAK ASDR ABXA040201Windshield · crackedFIRST OFFICER'S WINDSHIELD STARTED TO ARC AT THE LOWER RIGHT CORNER, THEN CRACKED SHORTLY THEREAFTER. AIRCRAFT MADE A DIVERSION TO STL AND MADE AN EMERGENCY LANDING. REPLACED RIGHT WINDSHIELD IAW DC-9 MM 56-10-02-2-0004. REPLACED TEMP CONTROLLER IAW DC-9 MMSDR 0401119929Frame · crackedDURING M-CHECK FOUND CRACK IN FRAME AT BS 598 L24L. REPAIRED PER EA 99-199088.SDR ABXA040179Longeron · corrodedBULGE AT STA 889 - 1005 LONGERON 17 LEFT - 18 LEFT. REPLACED CORRODED SECTION OF LONGERON IAW DC-9 SRM 53-02.SDR 0400839996Support Angle · crackedDURING M-CHECK FOUND CRACK IN SLANTED PRESSURE PANEL SUPPORT ANGLE AT BS 699. REPAIRED PER EA 99-198726.SDR 0400649969Pump · leakingON BASE LEG DURING APPROACH FOR LANDING, THE RIGHT HYDRAULIC SYSTEM LOST ALL FLUID AND FAILED. COMPLIED WITH COM PROCEDURES AND LANDING GEAR WAS EXTENDED MANUALLY. LANDING WAS NORMAL AT BNA ALTHOUGH THE GEAR DOORS DID HIT. GROUND CREW PINNED THE GEAR AND DOORSSDR 0400849996Longeron · crackedDURING M-CHECK FOUND CRACKS IN LONGERON 28R BS 756. REPAIRED PER EA 96-198627.SDR 0400679954Screw · shearedDUIRING DESCENT FOR LANDING, THE CREW NOTICED THE LOSS OF ALL OF THE LEFT HYDRAULIC SYSTEM FLUID. COMPLIED WITH COM PROCEDURES AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HOUSING SCREWS SHEARED ON THE ALTERNATE GEAR PUMP AND REPLACED THE PUSDR ABXA040156Proximity Switch · malfunctionedGO AROUND-MISSED APPROACH-GEAR RECYCLE. UPON PLACING MLG HANDLE IN THE DOWN POSITION FOR LANDING, MLG DOWN LIGHT FAILED TO ILLUMINATE. AFTER RUNNING ABNORMALS, DISCOVERED THE MLG WARNING CIRCUIT BREAKER WAS OUT. RESET CIRCUIT BREAKER AND EXTENDED MLG. AFTER SESDR ABXA040169Fitting · crackedLEFT FLAP HAD CRACKED FITTING AT SPLICE BETWEEN NR 4 AND 5 REMOVEABLE TRAILING EDGE SEGMENTS. REPLACED 2 EACH NEW FITTINGS IAW DC-9 SRM 51-30-2 AND 51-30-1. P/N: 9955813-509 AND -507.SDR ABXA040168Panel · crackedLT AND RT ANGLES INSIDE WRAP PANEL FORWARD OF RAM AIR SCOOP WERE CRACKED. REPLACED ANGLES IAW DC-9 SRM 51-30-2 AND 51-30-5. P/N: 5912188-49 AND -50.SDR ABXA040167Door Frame · crackedAFT PRESSURE BULKHEAD DOOR JAMB LEFT UPPER STOP FITTING CRACKED ON HORIZONTAL LEG. REPLACED FITTING IAW DC-9 SRM 51-30-2.SDR ABXA040166Longeron · crackedLONGERON 29 LT CRACKED AT STA. 588. REPAIRED LONGERON 29 LT IAW DC-9 SRM 53-02 AND REA D953-49676MR.SDR ABXA040165Longeron · crackedLONGERON 30 CRACKED, STA. 588. REPAIRED LONGERON 30 IAW REA D953-49676MR. REPAIRED FRAME AT FS 579 IAW DC-9 SRM 53-03.SDR ABXA040164Skin · corrodedLEFT ELEVATOR LOWER SKIN WAS BULGED AND CORRODED AROUND FASTENERS AND DOUBLER. REPAIRED ELEVATOR IAW DC-9 SRM.SDR ABXA040163Door Frame · crackedANGLE CRACKED ON FORWARD SIDE OF LEFT FORWARD OVERWING EXIT DOOR JAMB AT FS 617, LONGERON 15 LT. REPLACED ANGLE IAW DC-9 SRM 51-30-2.SDR ABXA040162Panel · corrodedLEFT FLAP LOWER OUTBOARD SURFACE HAD NUMEROUS PLACES WITH SURFACE CORROSION AND EVIDENCE OF INNER CORROSION. SKIN BULGED AROUND RIVET HEADS. REPAIRED TRAILING EDGE SEGMENT IAW DC-9 SRM.SDR ABXA040142Latch · jammedCOCKPIT DOOR LATCH JAMMED. DISASSEMBLED COCKPIT DOOR LATCH ASSEMBLY, FOUND HANDLE JAMMED. FREED JAM AND REASSEMBLED. OPS CHECKED GOOD IAW DC-9 MM.SDR ABXA040139Keelbeam · crackedLEFT KEELBEAM TO VERTICAL WEB ATTACH FITTING CRACKED AT BOTTOM OF WING ATTACH POINT APPROXIMATELY STA 693 FORWARD OF GEAR DOOR ACTUATOR. REPLACED FITTING IAW DC-9 SRM.SDR 0400519933Splice · crackedDURING "M" CHECK FOUND CRACK IN LONGERON 30 SPLICE FITTING FROM BS 580 TO BS 604. REPAIRED PER EA 99-198614.SDR 0400469960Control Panel · shortedCOCKPIT CREW REPORTED HEAVY SMOKE AND SPARKS COMING FROM THE CENTER CONSOLE WHILE AT CRUISE. FLIGHT DIVERTED TO AN UNEVENTFUL SAFE LANDING AT GRR. NO FIRE EXTINGUISHER WAS USED AND SOURCE OF THE SMOKE STAYED RESTRICTED TO THE AUTOPILOT CONTROL PANEL LIGHTINGSDR 0400369911Striker · out of adjustTHE AFT CARGO DOOR OPEN WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. THE TAKEOFF WAS SAFELY ABORTED AT ABOUT 130 KTS AND THE AIRCRAFT EXITED THE RUNWAY WITHOUT INCIDENT. THE WARNING INDICATION EXTINGUISHED AS THE AIRCRAFT TURNED ONTO THE TAXIWAY. MAINTENA
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