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 0203969914Door Frame · corrodedDuring HCK in DHN, corrosion was found just forward and below the aft cargo door forward lower corner. The existing repair was removed and a new repair was installed per EA 99-191383.SDR 0203959914Door · crackedDuring Hck in DHN, two cracks were found, on in the pan and one in the support of the aft ventral door. Repaired per EA 99-191379.SDR ABXA020340Doubler · crackedLEFT MAIN FRAME AT F.S. 699 WAS CRACKED IN FORWARD POCKET AT/BETWEEN "Z" CLIP ATTACH BOLTS. REPAIRED MAIN FRAME ON E.A. 53400110-001-1 AND DC-9 SRM.SDR ABXA020339Fitting · crackedFORWARD SIDE OF AFT PRESSURE BULKHEAD RIGHT VENTRAL DOOR WEB SUPPORT ANGLE WAS CRACKED. REPLACED SUPPORT ANGLE IAW DC-9 SRM 51-10-4, 51-30-2 AND 51-30-5.SDR ABXA020338Floorbeam · corrodedFLOORBEAM AT STA 995 WAS CORRODED ON THE TOP FLANGE AT LEFT BUTT LINE 46. REPAIRED FLOOR BEAM IAW DC-9 SRM.SDR ABXA020337Fitting · crackedAFT LOWER CARGO DOOR, #3 BEAM AFT END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.SDR ABXA020336Clip · crackedAFT LOWER CARGO DOOR, INNER ANGLE AT #2 BEAM FITTING AREA WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.SDR ABXA020335Fitting · crackedAFT LOWER CARGO DOOR, #4 BEAM AFT END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.SDR ABXA020334Fitting · crackedAFT LOWER CARGO DOOR, #2 BEAM FORWARD END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.SDR ABXA020333Clip · crackedAFT LOWER CARGO DOOR, #5 BEAM FORWARD END FITTING WAS CRACKED. REPLACED AFT LOWER CARGO DOOR IAW DC-9 MM AND NON ROUTINE #0345.SDR ABXA020332Panel · crackedAFT LOWER CARGO DOOR, OUTER PAN CRACKED AT BLIND NUT AND BULGED OUT AT SAME LOCATION LOWER AFT CORNER. REPLACED AFT LOWER CORNER DOOR IAW DC-9 MM AND NON ROUTINE #0345.SDR ABXA020331Frame · corrodedLEVEL II CORROSION ON FRAME AT STA. 446, AFT SIDE, BETWEEN LONGERON 28 LEFT AND 28 RIGHT. REPAIRED FRAME IAW DC-9 SRM 53-03.SDR ABXA020330Splice · crackedLONGERON 30 END FITTING BETWEEN F.S. 579 AND 596 CRACKED ON BOTH VERTICAL FLANGES. REPLACED END FITTINGS IAW DC-9 SRM.SDR ABXA020329Longeron · crackedLONGERON 29 LEFT CRACKED BETWEEN F.S. 579 AND 596. CRACKED ON BOTH VERTICAL FLANGES. REPAIRED LONGERON IAW REA D553-45780MR.SDR ABXA020299Door Frame · crackedWHILE COMPLYING WITH AD 80-02-16, FOUND CRACK IN OUTER PLUG DOOR FRAME. REPAIRED AREA IAW REA D952-45160-MR.SDR ABXA020328Skin · crackedRUDDER TOP RIGHT SIDE HAD LARGE CRACK. REPLACED RUDDER IAW DC-9 SRM.SDR 2003F00128Flashlight · inoperativeNO LED ON FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AND LOW VOLTAGE. REMOVED AND REPLACED PORTABLE EMERGENCY LIGHT IAW DC-9 MM 33-53-0. OPERATIONAL CHECK GOOD. (M)SDR 2003F00127Battery Pack · dischargedR-1 AND L-1 DOOR SLIDE DOOR LIGHTS INOPERATIVE. PROBLEM DETERMINED TO BE LOW VOLTAGE. REMOVED AND REPLACED BOTH BATTERY PACKS IAW DC-9 MM 33-50-1. OPERATIONAL CHECK GOOD. (M)SDR 2003F00050Power Supply · dischargedAFT OVERWING EMERGENCY DOOR LIGHTS INOPERATIVE. PROBLEM WAS DETERMINED TO BE THE BATTERY POWER SUPPLY. REMOVED AND REPLACED THE BATTERY POWER SUPPLY IAW DC9 MM 33-53-O, OPERATIONAL CHECK GOOD. (M)SDR 0203709981Stiffener · corrodedDURING H CHECK, CORROSION WAS FOUND ON THE UPPER SURFACE OF STATION 756 BULKHEAD TEE BETWEEN LONGERONS 29R AND 30. REPAIRED PER EA.SDR 0203639993ComputerOn takeoff at 1000 feet the flight crew experienced rapid yaw movements to both left and right. Required full yoke deflection to maintain control of the aircraft. COM complied with and both yaw damper and rudder servo were turned off. Flight returned to an uneSDR 0203699981Floorbeam · corrodedDURING HCK IN ATL, CORROSION WAS FOUND IN THE VERTICLE FLANGE OF THE STATION 200 FLOORBEAM LOWER CAP. THE CORROSION EXTENDED TO THE LEFT OF STATION X=0 ALL THE WAY TO THE END OF THE PART. REPAIRED PER EA 99-190813.SDR ABXA020258Battery · dischargedEMERGENCY LIGHTS NOT ARMED WAS NOT ILLUMINATED ON OVERHEAD PANEL. REPLACED 2 EACH, 1.2 VDC BATTERIES IAW DC-9 MM 33-53-00-8. OPS CHECKED GOOD.SDR 0203479938Actuator · leakingDURING APPROACH FOR LANDING WHEN CREW SELECTED SLAT DEPLOYMENT, THE AIRCRAFT HAD AN UNCOMMANDED ROLL TO THE LEFT ACCOMPANIED BY SLAT DISAGREEMENT LIGHT. COMPLIED WITH COM PROCEDURES, THE SLATS WERE RETRACTED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THE RIGHSDR ABXA020257Switch · defectiveNOSE LANDING GEAR DOWN SAFE LIGHT DID NOT ILLUMINATE WITH GEAR HANDLE DOWN AND NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED HANDLE, SAME INDICATION. DURING ABNORMAL CHECKLIST, NORMAL GEAR DOWN INDICATION OCCURED. REPLACED THE NOSE LANDING GEAR DOWN LOSDR 0203679947Door Frame · crackedWHILE IN FOR A L CHECK. A CRACK WAS FOUND IN THE LOWER FORWARD CORNER OF THE R1 SERVICE DOOR JAMB. REPAIRED PER EA.SDR 0203689947Frame · crackedDURING L CHECK, A CRACK WAS FOUND IN THE UPPER AFT CORNER OF THE R1 SERVICE DOOR JAMB. REPAIRED PER EA.SDR ABXA020254Longeron · crackedLONGERON 7 RIGHT WAS CRACKED AT FS 597. REPLACED LONGERON SECTION IAW DC-9 SRM 53-02.SDR ABXA020253Longeron · crackedLONGERON 6 LEFT WAS CRACKED AT FS 718. REPLACED LONGERON SECTION IAW DC-9 SRM 53-02.SDR ABXA020252Longeron · crackedLONGERON 17 LEFT CRACKED AT STA 966. REPAIRED AREA IAW DC-9 SRM 53-02.SDR ABXA020251Longeron · crackedLONGERON 14 LEFT CRACKED AT STA 980. REPAIRED AREA IAW DC-9 SRM 53-02.SDR ABXA020250Splice · crackedINBOARD AFT FITTING, FLOOR BEAM STA. 965 LEFT, WAS CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR ABXA020249Fitting · crackedSLAT TRACK X0S 429.1, INBOARD SUPPORT FITTING TO FRONT SPAR ATTACH ANGLE CRACKED. REPLACED AREA IAW REA D957-45321 AND DC-9 SRM.SDR ABXA020248Fitting · crackedFITTING CRACKED, FORWARD OF INBOARD GEAR DOOR ACTUATOR. REPLACED FITTING IAW DC-9 SRM 51-30-5.SDR ABXA020247Pan · crackedFORWARD ENTRANCE DOOR PAN CRACKED AT LOWER SIDE OF LOWER HINGE CUT OUT. REPLACED PAN SECTION IAW DC-9 SRM 51-30-1, 51-30-2, 51-30-5, 51-10-3, 51-20-0 AND 51-10-4.SDR ABXA020224Attach Angle · corrodedFORWARD CARGO DOOR AFT HINGE FORWARD ATTACH ANGLE ON HINGE HAD CORROSION. REPLACED ATTACH ANGLE IAW DC-9 SRM.SDR ABXA020222Attach Angle · crackedPYLON LOWER ATTACH ANGLE FORWARD END WAS CRACKED. REPAIRED PYLON LOWER ATTACH ANGLE FORWARD END IAW DC-9 SRM 54-04 AND SSRM DWG #K07439.SDR ABXA020223Longeron · crackedLONGERON 4 LEFT, CRACKED AT F.S. 200. REPLACED LONGERON IAW DC-9 SRM.SDR 0203339910Pressure Panel · crackedDuirng Hck in ATL, a crack was found in the flight compartment horizontal pressure panel at station 105. The crack is located at x=+35. Repaired per EA 99-190723.SDR 0203329910Pressure Panel · crackedDuring HCK in ATL, a crack was found in the flight compartment horizontal pressure panel at station 105, X=-35. Repaired per EA 99-190722.SDR 0202859956Controller · malfunctionedA FAINT ELECTRICAL SMELL WAS OBSERVED NEAR ROW 4 AND DURING TAXI THE SMELL PROGRESSED TO THE MIDDLE OF THE MAIN CABIN. AIRCRAFT RETURNED TO THE GATE WITHOUT INCIDENT. REPLACED SEAT 3AB PSU LIGHT CONTROLLER. OPERATIONAL CHECK OK.SDR ABXA020169Skin · corrodedDURING ROUTINE LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED CORROSION ON THE FUSELAGE SKIN, LOCATED AT THE LOWER CARGO DOOR JAMB, FORWARD LOWER CORNER. THE DAMAGE TO THE SKIN WAS TRIMMED OUT AND A NEW SECTION OF SKIN WAS SPLICED IN, IAW DC-9 SRM 53-04, FIG. SDR ABXA020168Doubler · corrodedDURING ROUTINE LINE OPERATIONS AT ILN, MAINTENANCE DISCOVERED CORROSION ON THE FUSELAGE SKIN RESULTING IN THE DISCOVERY OF CORROSION ON THE INTERNAL DOUBLER P/N 5910158-24. THE DAMAGE TO THE INTERNAL DOUBLER WAS TRIMMED OUT AND A NEW SECTION SPLICED IN IAW DC-SDR 0203089912Door Frame · crackedWhile stationed in MSP during pressurization checks for squealing, the aft ventral door upper left hand corner jamb was found cracked. Repaired per EA. 99-187509.SDR ABXA020152Latch · out of adjustRIGHT GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. UPLATCH CHECK FAILED (GEAR DOOR OPEN LIGHT CAME ON AND GEAR EXTENDED). WHEN THE GEAR HANDLE WAS PLACED IN UP POSITION, RIGHT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT WENT OUT. RIGHT GEAR RETRACTEDSDR ABXA020146Bracket · out of adjustAFTER TAKEOFF WITH GEAR HANDLE UP, THE RIGHT GEAR RED UNSAFE LIGHT ILLUMINATED. RECYCLED THE GEAR WITH NO CHANGE. THE GEAR UPLATCH CHECK ALSO FAILED. ADJUSTED THE TENSION ON THE RIGHT MAIN GEAR DOOR ROLLER BRACKET AND SPRING ASSEMBLY IAW DC-9 MM 32-31-04-2-SDR ABXA020145Switch · faultyON FINAL APPROACH, GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH. RECYCLED GEAR AND LIGHT STILL DID NOT GO OUT. EXTENDED GEAR LIGHT ON AT FLAPS 15 DEGREES. WHEN FLAPS 25 DEGREES SELECTED, LIGHT WENT OUT. EXECUTED MISSED APPROACH. CONFIGURED TO EXT/15 DEGREES SDR ABXA020206Longeron · crackedLONGERON 29 LEFT FORE AND AFT OF SPLICE CRACKED AT FS 408. REPLACED SECTION OF LONGERON IAW DC-9 SRM 53-02.SDR 0202749937Powerpack · faultyDURING CLIMB THROUGH 8000 FEET, THE AIRCRAFT WOULD YAW LEFT AND RIGHT. COMPLIED WITH COM PROCEDURES AND YAW ACTION STOPPED WHEN MANUAL RUDDER WAS SELECTED. AIRCRAFT RETURNED TO A NORMAL LANDING AT CLT. MAINTENANCE REPLACED THE RUDDER POWER PACKAGE. AIRCRAFSDR 0202699975Relief Valve · leakingDURING GEAR UPLATCH CHECK AFTER TAKEOFF, THE RIGHT HYDRAULIC SYSTEM FLUID QUANTITY WENT TO ZERO. GEAR DOOR OPENED AND MAIN LANDING GEAR EXTENDED AS THE HYDRAULIC SYSTEM FAILED. CREW ENSURED GEAR WAS PROPERLY EXTENDED PER COM. FLIGHT RETURNED TO MDT AND LAND
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