Douglas DC-9-41
Service difficulty reports · 2,671
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 = 'DC941' 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 = 'DC941' 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 ABXA020265Door Frame · crackedCRACKED IN BEND RADIUS AT LEFT UPPER VENTRAL DOOR CORNER. CRACK LENGTH APPROXIMATELY 1.25 INCH IN LENGTH. REPAIRED CRACK IAW DC-9 SRM 51-10-02.SDR ABXA020264Panel · crackedNOSE WHEEL WELL UPPER PRESSURE PANEL HAD CRACK AT STA. 110 RIGHT TUNNEL, APPROXIMATELY 14 INCHES INBOARD. REPAIRED PANEL IAW DC-9 SRM 51-30-2, 51-30-1 AND 51-30-5.SDR ABXA020263Panel · crackedNOSE WHEEL WELL UPPER PRESSURE PANEL HAD CRACK AT STA. 110 LEFT TUNNEL, APPROXIMATELY 24 INCHES INBOARD. REPAIRED PANEL IAW DC-9 SRM 53-01, 51-30-2, 51-30-1 AND 51-30-5.SDR ABXA020262Panel · crackedNOSE WHEEL WELL UPPER PRESSURE PANEL STA. 89 LEFT, APPROXIMATELY 3 INCHES INBOARD, HAD CRACK. REPAIRED CRACK IAW REA D953-45373.SDR ABXA020261Splice · corrodedLEVEL II CORROSION AT F.S. 1013, LONGERON 27 LEFT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPLACED FRAME SPLICE IAW DC-9 SRM.SDR ABXA020260Fitting · crackedANGLE CRACKED AT LONGEON 30 JUST AFT OF FORWARD 'P' DOME, KEEL AREA. REPLACED ANGLE IAW DC-9 SRM 51-30-5.SDR ABXA020259Support · crackedRIGHT WING OUTBOARD SPOILER TORSION BAR SUPPORT FITTING CRACKED AT UPPER END. REPLACED FITTING IAW DC-9 SRM 51-30-1.SDR ABXA020231Battery · dischargedEMERGENCY LIGHTING WAS DIM. REPLACED EMERGENCY POWER SUPPLY BATTERIES IAW DC-9 MM 33-53-02-4.SDR ABXA020228Door Frame · crackedCRACK IN UPPER LEFT CORNER OF THE VENTRAL DOOR JAMB. REPAIRED AREA IAW REA D953-45345-MR.SDR GTIA021037Isolator · defectiveDTW - FOUND LOWER NR 1 ENGINE ISOLATOR DOES NOT HAVE ANTI-ROTATION MARK. REMOVED AND REPLACED NR 1 ENGINE LOWER ISOLATOR, CLOSED 10/10/02. (M)SDR GTIA021036Isolator · defectiveDTW - FOUND UPPER NR 1 ENGINE ISOLATOR DOES NOT HAVE ANTI-ROTATION MARK. REMOVED AND REPLACED NR 1 ENGINE UPPER ISOLATOR, CLOSED 10/10/02. (M)SDR GTIA021071Combust Chamber · wornBOROSCOPE RECORD, FOUND IGNITER GUIDE NR 4 COMBUSTION CHAMBER WORN AND OUT OF CHAMBER RESTING IN OUTER COMBUSTION CASE IGNITER PORT NR 4. BURNER CANS HAVE BEEN REPACED DURING SHOP VISIT.SDR GTIA021033Clip · missingFORWARD EMERGENCY FLASHLIGHT LOCK CLIP MISSING AND LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY.SDR ABXA020220Controller · malfunctionedON CLIMBOUT, AIRCRAFT DID NOT PRESSURIZE. PERFORMED ABNORMAL, AUTO CONTROLLER WAS INOPERATIVE. UNABLE TO CONTROL PRESSURE. INSPECTED ALL ACCESS DOORS, ALL CLOSED. INSPECTED AND LUBRICATED OUTFLOW BUTTERFLY VALVE LINKAGE AND OUTFLOW NOZZLE, NO DEFECTS FOUNDSDR ABXA020219Web · crackedFOUND NUMEROUS CRACKS IN AFT CUSP WEB, LEFT HAND SIDE APPROXIMATELY AT FS 1002. REPAIRED CUSP WEB IAW DC-9 SRM 53-01.SDR ABXA020245Web · crackedCUSP WEB AT F.S. 636 - 696, RIGHT SIDE CRACKED. REPLACED WEB IAW DC-9 SRM 51-30-1 AND 51-30-2.SDR ABXA020244Web · crackedCUSP WEB CRACKED AT STA. 1019, RIGHT BUTT LINE 54. FOUND CRACK TO BE MINOR. TRIMMED OUT CRACK IAW DC-9 SRM 53-01. (WITHIN LIMITS)SDR ABXA020243Web · crackedCUSP WEB CRACKED IN 2 PLACES AT STA. 1040, RIGHT BUTT LINE 54. REPAIRED FLOOR PANEL IAW DC-9 SRM 53-01.SDR ABXA020242Angle · crackedDOOR PAN ANGLE WAS CRACKED. REMOVED, WELDED AND REINSTALLED DOOR PAN IAW DC-9 SRM 51-30-1 AND 51-30-2, DRAWING K05818.SDR ABXA020241Splice · crackedLONGERON SPLICE AT LONGERON 30, STA. 870 - 880 WAS CRACKED. REPLACED SPLICE IAW DC-9 SRM 53-02 AND 51-30-5.SDR ABXA020240Shim · crackedEXFOLIATION IN 2 PLACES, LONGERON 23 LEFT BETWEEN F.S. 973 AND 993. REPLACED LONGERON STIFFENER STRIP IAW DC-9 SRM 51-30-2.SDR ABXA020239Web · crackedNUMEROUS CRACKS IN CUSP WEB BETWEEN FS 1021 AND 1041 AT LEFT BUTT LINE 54. REPAIRED AREA IAW DC-9 SRM 53-01.SDR ABXA020238Intercostal · crackedCRACKED INTERCOSTAL F.S. 1072 AND LONGERON 28 LEFT. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA020237Angle · crackedLEFT PYLON BULKHEAD ANGLE CRACKED IN RADIUS ADJACENT TO LOWER SPAR CRACK. REPLACED LEFT BULKHEAD ANGLE IAW REA D953-45305-MR.SDR ABXA020236Support · crackedINBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING WAS CRACKED. REPLACED SUPPORT IAW DC-9 SRM 51-10-4 AND 51-30-5.SDR ABXA020235Eyebolt · brokenSLAT DRIVE MECHANISM WAS BROKEN AT THE INBOARD ACTUATOR ON THE LEFT WING. REPLACED EYEBOLT IAW DC-9 MM 27-80-05-2-0101.SDR ABXA020234Angle · crackedSKIN CRACKED ON F.S. 37 BULKHEAD, RIGHT SIDE AT UPPER RADOME ALIGNMENT PIN. REPAIRED AREA IAW ABX DRAWING 05159 AND DC-9 SRM.SDR ABXA020216Battery Pack · dischargedCOCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK. OPS CHECKED GOOD IAW DC9 AMM 33-53-00.SDR GTIA020979Wire · looseACY - FOUND EMERGENCY FLOOR PATH LIGHTING ROW 8DEF INOPERATIVE. RESECURED FLOOR PATH LIGHTING WIRE. (M)SDR GTIA020974Dome Nut · brokenRIGHT TANK FUEL QUANTITY WENT DOWN FASTER THAN LEFT WHILE IN FLIGHT. LANDED WITH 5600 IN LEFT AND 4300 IN RIGHT. CONFIRMED QUANTITY WITH DRIP STICKS. FOUND MISSING BOLT ON FORWARD PANEL ON RIGHT WING. FOUND 2 DOME NUTS FOR RIGHT WING FQ PROBE NR 2 ACCESS PSDR 0203209756Skin · crackedWhile in DHN for Hck, a .44 inch crack was found in the skin at a fastener hole 5" above Longeron 18 right. Repaired per EA 97-191331.SDR ABXA020154Coalescer Bag · defectiveSTRONG SMELL WHILE AT TAKE-OFF POWER. PERFORMED ENGINE RUN, OPERATED BOTH PACKS FROM APU AND ENGINES. NO SMELL NOTED. VISUALLY INSPECTED PNEUMATIC DUCTING, NO DEFECTS NOTED. CHECKED ACM OILS AND REPLACED COALESCER BAGS IAW DC-9 MM PROCEDURES.SDR ABXA020203Clip · cracked#1 PYLON ATTACH ANGLE INSIDE PANEL 8111 AT UPPER AFT ENGINE MOUNT STRAP HAD CRACK NEXT TO BOLT. REPLACED ANGLE IAW DC-9 DWG 9915500 AND DC-9 SRM 51-30-5.SDR ABXA020148Sensor · defectiveAFTER GEAR RETRACTION, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON. RIGHT HYDRAULIC PUMPS ON HIGH. AT GEAR UPLATCH CHECK, THE LIGHT WENT OUT. GEAR RECYCLED ONE TIME BEFORE UPLATCH CHECK WITH THE LIGHT STILL ON. REPLACED THE LEFT GEAR DOWN SENSOR IAW DC-9 MM 32SDR ABXA020202Intercostal · crackedCRACKED INTERCOSTAL AT STA 794, RBL 22. REPAIRED INTERCOSTAL IAW DC-9 SSRM K05159.SDR ABXA020201Intercostal · crackedCRACKED INTERCOSTAL AT STA. 794, LEFT BUTT LINE 22. REPAIRED INTERCOSTAL IAW DC-9 SSRM K05159.SDR 0202759759Control Cable · out of rigON TAKEOFF, THE CREW HAD A STALL INDICATOR ACCOMPANIED WITH A STICK SHAKER. ONCE IN THE AIR, A LOUD POP WAS HEARD AND THE AIRCRAFT ROLLED TO THE RIGHT. AFTER ROLL CORRECTION, THE STALL INDICATION CLEARED BUT THE CREW ELECTED TO RETURN TO MSP. LANDING WAS UNSDR ABXA020211Web · crackedCUSP WEB WAS CRACKED AT STA 1041, LONGERON 18 LEFT. REPLACED CUSP WEB STRINGER IAW DC-9 SRM 53-01.SDR ABXA020177Web · crackedCUSP WEB WAS CRACKED AT STATION 1041, LONGERON 18 LEFT. REPLACED CUSP WEB IAW DC-9 SRM 53-01.SDR ABXA020210Intercostal · crackedINTERCOSTAL JUST BELOW RIGHT RADOME HINGE WAS CRACKED AT CUTOUT. REPLACED INTERCOSTAL AND INSTALLED FASTENERS IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA020209Angle · corrodedEXFOLIATED ANGLE ON OUTBOARD END OF SLANT PANEL. REPLACED ANGLE IAW DC-9 SRM.SDR ABXA020208Hinge · crackedRIGHT MAIN LANDING GEAR INBOARD DOOR HINGE WAS CRACKED. REMOVED AND REINSTALLED THE RIGHT MAIN LANDING GEAR DOOR FOR HINGE CHANGE IAW DC-9 MM 32-12-01-2-02-01, SRM 51-30-1, 51-30-5 AND 52-05.SDR ABXA020176Intercostal · crackedINTERCOSTAL JUST BELOW RIGHT RADOME HINGE WAS CRACKED AT CUTOUT. REPLACED INTERCOSTAL AND INSTALLED FASTENERS IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA020175Angle · corrodedEXFOLIATED ANGLE ON OUTBOARD END OF SLANT PANEL. REPLACED ANGLE IAW DC-9 SRM.SDR ABXA020174Hinge · crackedRIGHT MAIN LANDING GEAR INBOARD DOOR HINGE WAS CRACKED. REMOVED AND REINSTALLED RIGHT MAIN LANDING GEAR DOOR FOR HINGE CHANGE IAW DC-9 MM 32-12-01-2-02-01 AND SRM 51-30-1, 51-30-5, AND 52-05.SDR ABXA020200Former · crackedFORWARD LOWER CARGO DOOR, LOWER FORWARD STOP INTERCOSTAL FORMER WAS CRACKED. REPLACED BRACKET IAW DC-9 SRM 51-30-1 AND 51-30-2.SDR ABXA020199Fitting · crackedFORWARD LOWER CARGO DOOR AFT STOP FITTING AT END OF INTERCOSTAL CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR ABXA020198Pan · crackedAFT LOWER CARGO DOOR INNER PAN WAS CRACKED NEAR FORWARD LATCH HOOK AT ROLLER CUTOUT. REPLACED AFT LOWER CARGO DOOR ON N.R. #0350 AND IAW DC-9 MM.SDR ABXA020197Pan · crackedOUTER PAN WAS CRACKED AT BEAM 3 ON AFT END OF AFT LOWER CARGO DOOR. REPLACED DOOR IAW DC-9 MM.SDR ABXA020196Pan · crackedFORWARD END OF AFT LOWER CARGO DOOR HAD CRACKED PANES AT DOORSTOP CUTOUT AT BEAMS 1, 2, AND 3. REPLACED DOOR ON N.R. #0350 AND IAW DC-9 MM.
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