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 0201329981Controller · malfunctionedAIRCRAFT WAS CRUISING AT FL330 WHEN THE CABIN PRESSURE ANNUNCIATOR LIGHT ILLUMINATED AND CABIN ALTITUDE WAS APPROACHING 10,000 FEET. WING ANTI-ICE AND ENGINE ANTI-ICE WERE BOTH ON AT THE TIME AND TURNING THEM OFF DID NOT HELP TO REGAIN CABIN PRESSURE. CREW DSDR 0201329961Controller · malfunctionedAIRCRAFT WAS CRUISING AT FL330 WHEN THE CABIN PRESSURE ANNUNCIATOR LIGHT ILLUMINATED AND CABIN ALTITUDE WAS APPROACHING 10,000 FEET. WING ANTI-ICE AND ENGINE ANTI-ICE WERE BOTH ON AT THE TIME AND TURNING THEM OFF DID NOT HELP TO REGAIN CABIN PRESSURE. CREW DSDR 0201199995Duct · ratchetingDURING APPROACH FOR LANDING INTO GRR, THE SLAT DISAGREEMENT LIGHT REMAINED ILLUMINATED AND THE AIRCRAFT ROLLED TO THE LEFT. FLIGHT CREW COMPLIED WITH COM PROCEDURES AND ACCOMPLISHED AN UNEVENTFUL NO SLAT LANDING AT GRR. CONTRACT MAINTENANCE COULD NOT FIND ANSDR 0201139981Slide · failedGROUND SERVICE AGENT DROPPED THE TAIL CONE WHILE TRYING TO GAIN ENTRY INTO THE AIRCRAFT. THE EVACUATION SLIDE DID NOT DEPLOY WHEN THE TAIL CONE DROPPED. MAINTENANCE REPLACED THE TAIL CONE. DROPPED CHECK TESTED THE TAIL CONE AND SLIDE ASSEMBLY AND THE SLIDE SDR ABXA010872Wire · damagedNO IGNITION ON EITHER ENGINE. FOUND WIRES 1J6H24 AND 2J4D24 BURNT THROUGH THREE FEET LEFT OF PEDESTAL IN THE CAPTAIN'S CONSOLE. REPLACED THE DAMAGED SECTION OF WIRES AND OPS CHECKED BOTH ENGINE IGNITION SYSTEMS IAW DC-9 MM. NO DEFECTS NOTED.SDR ABXA010814Fitting · crackedNR 6 TEE CRACKED APPROXIMATELY 1 INCH LONG AT LONGERON 14. REPLACED THE NR 6 TEE IAW DC-9 SRM.SDR ABXA010815Control Column · crackedCAPTAIN'S CONTROL COLUMN SHOWED CRACK INDICATIOIN AND WAS BLENDED BEYOND LIMITS. REPLACED CAPTAIN'S CONTROL COLUMN IAW DC-9 SRM 51-30-1 AND 51-30-2.SDR ABXA010805Track · lack of lubeCOULD NOT OPEN CAPTAIN'S SLIDING WINDOW. LUBED TRACK AND LOCKING MECHANISM. CAPTAIN'S CLEARVIEW WINDOW OPS CHECKED GOOD.SDR 0200929970Rib · crackedDuring Overnight CK. in MSP the #5 leading edge rib was found cracked common to the lower most aft fastener hole . The crack was .5" long. Repaired per EA 99-189349.SDR ABXA010783Power Supply · dischargedDURING PREFLIGHT CHECK, FOUND THE EMERGENCY CABIN LIGHTS INOPERATIVE. REPLACED THE BATTERY POWER SUPPLY IAW DC-9 MM. OPS CHECKED GOOD.SDR 0201069997Duct · lack of lubeUPON SLAT EXTENSION, THE AIRCRAFT ROLLED TO THE RIGHT AND THE BLUE SLAT EXTEND LIGHT DID NOT ILLUMINATE. CREW CYCLED SLATS ONCE MORE WITH SAME RESULTS. FOLLOWED COM PROCEDURES AND LANDED UNEVENTFULLY WITHOUT SLATS AT FSD. MAINTENANCE INSPECTED AND CHECKED THE SDR 0201019937Skin · crackedAircraft inspection in STL revealed 2 cracks in the airstair door cut out. One crack was .25" and the other was .5". Repaired per EA 99-185358.SDR 0200649937Skin · crackedDuring stop over in STL while inspecting the fwd airstair door cutout, 2 cracks were found in the fuselage skin at the lower aft corner. One crack is approx. .025" long and extends FWD from fastener hole. The second crack is .050" long and extends aft from theSDR 0200589938Wire · shortedAFTER LANDING AT IND, SIGNIFICANT SMOKE WAS COMING FROM GLARESHIELD ON EITHER SIDE OF THE ALTITUDE ALERTER. SMOKE STOPPED AFTER THE PARKING CHECK WAS DONE AT THE GATE. MAINTENANCE INSPECTED BUT FOUND NO EVIDENCE OF SMOKE OR FIRE. THEN TWO FLIGHTS LATER ON NSDR 0201009903Frame · crackedDuring Mck in ATL, Sta 1076 frame was found cracked at longeron 15L. Repaired per EA 99-185571.SDR 0200639903Frame · crackedDuring M ckin ATL, Sta 1076 frame was found cracked at longeron 15L. EA 99-185571 allows for repair for the frame.SDR 0200569996Terminal · damagedCREW REPORTED SMOKE IN COCKPIT. COMPLIED WITH COM PROCEDURES AND DONNED OXYGEN MASK. SMOKE ORIGINATED BEHIND OVERHEAD PANEL AND DISSIPATED SHORTLY AFTER THE WINDSHIELD HEAT WAS TURNED OFF SO IT LASTED ONLY 15 SECONDS. LANDING WAS UNEVENTFUL AND THE EMERGENCSDR 0201049954Pressure Panel · corrodedDuring HCK in DHN, corrosion damage was found to the RH slant panel lower attach angle. Repaired per EA 99-188363.SDR 02010399003Longeron · crackedDuring MCK in ATL, Longeron 23R was found cracked at sta 758. Repaired per EA 99-185561.SDR 0201029903Pressure Panel · crackedDuring Hck in ATL 2 cracks were found on the station 105 pressure panel, X=35rh (1.0") and x=25rh (1.0"). repaired per EA 99-185564.SDR 0200629903Pressure Panel · crackedDuring M-ck in ATL, cracks were found in the flight compartment horizontal pressure panel at sta 105. The cracks are located at RH x=35 1.0" and RH X=25 1.0". Repaired per EA 99-185564.SDR 0200469903Pressure Panel · crackedduring Mck in ATL, cracks were found int the flight compartment horizontal pressure panel at station 105. RH x=35 1"long, RH X=25 1"long. Repaired per EA 99-185564.SDR ABXA010735Door Frame · corrodedAFT VENTRAL DOOR JAMB AT RBL 0 TO RBL 6, LOWER SECTION, CORRODED AND TWO POPPED RIVETS. REPAIRED AREA IAW DC-9 SRM 51-70-5.SDR ABXA010734Spar · crackedLEFT UPPER FORWARD SPAR WAS CRACKED AT THE INBOARD LEADING EDGE ATTACH HOLE. REPAIRED SPAR IAW DC-9 REA D957-43288MR.SDR 0200279971Duct · bindingFLIGHT DIVERTED TO AN AIRPORT WITH A LONGER RUNWAY WHEN THE CREW DETERMINED THAT THE LEFT WING SLATS WOULD NOT EXTEND. THE AIRCRAFT DID ROLL TO THE LEFT AND THE SLAT DISAGREEMENT LIGHT DID ILLUMINATE. FOLLOWED COM PROCEDURES AND MADE AN UNEVENTFUL LANDING ATSDR ABXA010733Longeron · crackedLONGERON 4 LEFT AT F.S. 200 WAS CRACKED. REPLACED LONGERON IAW DC-9 SRM 53-02.SDR ABXA010732Fitting · crackedAFT LOWER CARGO DOOR, NR 3 INTERCOSTAL BEAM FORWARD END FITTING ANGLE CRACKED. REPLACED ANGLE IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR ABXA010731Fitting · crackedAFT LOWER CARGO DOOR, #4 INTERCOSTAL BEAM, AFT END FITTING CRACKED. REPLACED END FITTING IAW DC-9 SRM 51-30-5 AND 51-30-1.SDR ABXA010730Intercostal · crackedAFT LOWER CARGO DOOR, TEMPORARY REPAIR (STOP DRILL) ON INTERCOSTAL ON AFT SIDE OF LOWER DOOR STOP FITTING. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-1.SDR ABXA010729Pan · crackedAFT LOWER CARGO DOOR, OUTER PAN BULGED AND CRACKED AROUND BLIND NUT ON LEADING EDGE. REPAIRED AREA IAW DC-9 SERVICE REWORK DWG 5934142.SDR ABXA010728Tab · delaminatedRIGHT SIDE OF RUDDER TAB DELAMINATED. REPLACED RUDDER CONTROL TAB IAW DC-9 AMM 27-20-02-4-0001.SDR ABXA010727Vane · delaminatedINBOARD FIXED VANE WAS DELAMINATED ON LOWER SKIN AT XRS 170. REPLACED FIXED VANE IAW DC-9 SRM 27-51-02-2-0002.SDR ABXA010726Panel · delaminatedLEFT WING, LOWER INBOARD BONDED PANEL HAD AREA OF DELAMINATION. REPLACED PANEL IAW DC-9 SRM 51-30-2 AND 51-30-1. SEAM SEALED PANEL IAW DC-9 SRM 51-20-6.SDR ABXA010725Support Fitting · crackedTWO VERTICAL SUPPORTS CRACKED, EACH SIDE OF THE RUDDER TORQUE TUBE AREA. REPLACED THE VERTICAL SUPPORT BRACKETS, RIGHT AND LEFT SIDE IAW DC-9 SRM 51-30-5.SDR 0200459981Stabilizer · crackedDuring overnight in MSP, a crack was found on the verticle stabilizer front spar left lower chord.Repaired per EA 99-187946SDR 0200449960Bulkhead · crackedDuring RON in CMH, a crack was found on the Apb radial stiffener at l 6 rhs. The crack runs from the outbrd edge of the stiffener to the outer most fastener hole. Repaired per EA 99-185524.SDR ABXA010723Web · crackedCUSP WEB CRACKED BETWEEN FS 945 - 965, LONGERON 18 LEFT. REPAIRED AREA, DOUBLER INSTALLED ON CUSP WEB IAW DC-9 SRM 53-01.SDR 0200439944Spoiler · crackedDuring RON at ORD, a 1/2" crack was found in the lower skin of the L/H inbrd flight spoiler at station 206 hinge drive fitting. The crack emenated from the edge of the skin cutout to an adjacent fastener. Repaired per EA 99-85357.SDR ABXA010722Skin · crackedCRACK INDICATION IN SKIN BETWEEN 2 FASTENERS, BETWEEN LONGERON 5 RIGHT AND LONGERON 6 RIGHT AT FS 996. INSTALLED PERMANENT REPAIR IAW DC-9 EA 53110005.SDR ABXA010700Skin · corrodedCORROSION ON SKIN UNDER LONGERON 30 AT FUSELAGE 870. REMOVED CORROSION IAW DC-9 SRM 53-01. CUT-OUT PORTION OF SKIN PLATING THAT WAS CORRODED BEYOND LIMITS AND REPAIRED IAW DC-9 SRM 53-04.SDR ABXA010699Longeron · crackedLONGERON 30 AT F.S. 870 WAS CORRODED AND CRACKED UNDERNEATH FLANGES. REPLACED LONGERON 30 STATION 862 - 879 IAW DC-9 SRM 53-02. INSTALLED FORWARD AND AFT SPLICES AT STATION 862 - 879 IAW DC-9 SRM 51-30-5.SDR ABXA010682Skin · crackedDURING LINE MAINTENANCE VISIT, FUSELAGE SKIN WAS CRACKED AT THE FORWARD ENTRY DOOR, UPPER AFT CORNER, STATION 218, LONGERON 7 LEFT. REPAIRED FUSELAGE SKIN IAW DC-9 SRM.SDR ABXA010698Splice · crackedLONGERON SPLICE CRACKED F.S. 945 TO F.S. 965, LONGERON 22 LEFT. REPLACED SPLICE IAW DC-9 SRM.SDR ABXA010697Longeron · crackedLONGERON 29 LEFT WAS CRACKED BETWEEN STATION 313 TO STATION 332. REPLACED LONGERON 29 LEFT BETWEEN STATION 313 TO STATION 332 IAW DC-9 SRM.SDR 0200249962Warning System · false activationON TAKEOFF ROLL, THE AFT CARGO DOOR OPEN WARNING LIGHT ILLUMINATED AND FLASHED ON/OFF FOUR TIMES. CREW SAFELY ABORTED THE TAKEOFF AT 110 KTS AND RETURNED TO THE GATE. MAINTENANCE INSPECTED THE DOOR AND LIGHT ASSEMBLY AND DID NOT FIND ANY PROBLEMS. DISCREPANSDR ABXA010677Battery · dischargedCABIN EMERGENCY LIGHTS TEST VERY DIM, OVERHEAD PANEL IN COCKPIT. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC-9 MM 33-53-00-8-0001.SDR 0200159946Web · crackedDuring Hck in ATL, A crack was found in the lower outboard corner of the diagonal web in the L/H engine pylon just forward of the rear spar. Repaired per EA 99-185474.SDR 0200139946Floorbeam · crackedDURING HCK IN ATL, A CRACK WAS FOUND IN THE UPPER VERTICLE FLANGE OF THE STATION 237 FLOORBEAM AT X=6. REPAIRED PER EA 99-185447.SDR 0200149946Skin · corrodedDuring HCK in ATL, corrosion was found on the R/H wing upper skin doubler flange attachment holes for the fuel access door. Repaired per EA 99-185451.SDR 0200039960Control Valve · failedDURING TAKEOFF ROLL AT 100 KNOTS, THE RIGHT ENGINE EGT INDICATION ENTERED THE RED ARCH ZONE OF THE INDICATOR. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGINE PRESSURE RATIO BLEED CONTROL AND PERFORMED ENGINE BORESCOPE. O
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