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 GTIA9800125Light · inoperativeDTW - EMERGENCY FLOOR TRACK LIGHTING HAS AN INOPERATIVE BULB (RED AT OVERWING EXIT). REINSTALLED LOOSE BULB IN RECEPTACLE. OPERATION CHECKS GOOD. (M)SDR 9810469953Angle · crackedDURING M-CHECK, FOUND CRACK AT FORWARD ENTRY DOOR JAMB LOWER DEPRESSOR ANGLES FS 180. REPAIRED PER EA 99-160834 (P/N 5957094-1).SDR TWAA9817901Skin · crackedDURING CHECK-C, MAINT FOUND FUSELAGE SKIN CRACKED AT AFT HINGE CUTOUT FOR THE NOSE GEAR RT STRUT DOOR. INSTALLED DOUBLER OF 0.063 7075T6 WITH AD-5 RIVETS. AREA PRIMED AND PAINTED.SDR ABXA9801112Skin · corrodedWHILE COMPLYING WITH D-INSPECTION, FOUND THE LEFT WING OUTBOARD TRAILING EDGE SECTION HAD EXTENSIVE CORROSION ON INNER SURFACE OF UPPER SKIN AROUND FINGER DOUBLERS. REPLACED SKIN IAW DC9 SRM 51-30-2.SDR ABXA9801110Shear Tie · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT STATION 980 LEFT, BEHIND LONGERON 17L. REPLACED SHEAR TIE IAW DC9 SRM 53-03.SDR ABXA9801109Intercostal · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND INTERCOSTAL CRACKED AT STATION 507 AT RBL 50. REPAIRED IAW ABX REA D938-25412.SDR USAAD98198Lanyard · brokenLEX - THE MAIN ENTRANCE DOOR EMERGENCY SLIDE LANYARD WAS BROKEN. MAINTENANCE REPLACED THE MAIN ENTRANCE DOOR EMERGENCY SLIDE LANYARD. (M)SDR ABXA9801114Longeron · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND LONGERON 17 LEFT CRACKED AT STATION 965 AND 980. REPLACED LONGERON SECTION IAW DC9 SUPPLEMENTAL SRM DWG K05864.SDR USAAD98197Cylinder · malfunctionedBWI-BDL - FLT 1074 - THERE WAS A NOSE GEAR UNSAFE INDICATION WHEN THE LANDING GEAR WAS EXTENDED FOR LANDING. AFTER CYCLING THE GEAR, ALL INDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE NOSE LANDING GEAR BUNGEE CYLINDER. (M)SDR USAAD98196Retract Mech · failedDAY-PHL - FLT 648 - AFTER TAKEOFF AND GEAR RETRACTION THERE WAS EXCESSIVE VIBRATION FROM THE NOSE GEAR AREA. THE LANDING GEAR WAS CYCLED BUT DID NOT HELP. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SECURED THE RIGHT NOSE LANSDR ABXA9801115Longeron · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND LONGERON 17 RIGHT CRACKED AT STATION 965 AND 980. REPLACED LONGERON SECTION IAW DC9 SUPPLEMENTAL SRM DWG K05864.SDR USAAD98201Battery · dischargedCLT - THE FIRST CLASS SECTION CEILING EMERGNCY LGIHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE FIRST CLASS SECTION CEILING EMERGENCY LIGHTS. (M)SDR ABXA9801116Web · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE LEFT CUSP MEMBRANE CRACKED AT STATION 960. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2.SDR USAAD98192Cylinder · failedDCA-SYR - FLT 366 - DURING APPROACH WITH THE GEAR HANDLE DOWN THE GREEN NOSE GEAR LIGHT WOULD NOT ILLUMINATE. AFTER OPERATING THE LANDING GEAR FREE FALL HANDLE THE NOSE GEAR EXTENDED. MAINTENANCE REPLACED THE NOSE GEAR BUNGEE CYLINDER AND LUBED THE NOSE GEARSDR USAAD98191Power Supply · inoperativeDTW - THE GALLEY AREA EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE GALLEY AREA EMERGENCY LIGHT POWER SUPPLY. (M)SDR TWAA9817302Angle · crackedDURING OP 16 MAINT CHECK, FOUND CABIN FLOORBEAM SUPPORT ANGLE CRACKED AT STA 680 LBL 43 IN. INSTALLED NEW FITTING (P/N 3916209-501N), USING TENSION HEAD HI-LOKS AND LIKE FASTENERS.SDR TWAA9817301Membrane · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON MEMBRANE AT STA 208 TO 217, LONGERON 18L. REPLACED MEMBRANE PER SRM 53-05 FIG 55 SHEET 2 AND FASTENER SUB PER SRM 51-60-0 AND ARA 15704.SDR ABXA9801118Fitting · corrodedWHILE COMPLYING WITH D-INSPECTION, FOUND LONGERON 29 RIGHT END FITTING CORRODED AT STATION 579 TO 598. REPLACED LONGERON END FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.SDR ABXA9801117Longeron · corrodedWHILE COMPLYING WITH D-INSPECTION, FOUND CORROSION ON THE PRESSURE PANEL LONGERON TEE CAP AT STATION 604, BETWEEN LONGERONS 29 LEFT AND 29 RIGHT. REPLACED TEE CAP IAW DC9 SRM 51-30-1 AND 51-30-2.SDR ABXA9801065Longeron · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND LONGERON 30 CRACKED BETWEEN STATION 579 AND 585. REPLACED LONGERON SECTION IAW DC9 SRM CHAPTER 53-02.SDR ABXA9801063Fitting · corrodedWHILE COMPLYING WITH D-INSPECTION, FOUND LONGERON 30 END FITTING CORRODED BETWEEN STATION 579 AND 598. REPLACED LONGERON END FITTING IAW DC9 SRM 51-30-2 AND 51-30-5.SDR GTIA9800122Battery Pack · dischargedDTW - FLT 558 - DURING DAILY, FOUND AFT TAIL CONE EMERGENCY LIGHTS INOPERATIVE. FOUND BATTERY PACK AT R-27 IN AFT LAVATORY INOPERATIVE. REMOVED AND INSTALLED SERVICEABLE BATTERY PACK IAW MM 33-53-0. OPERATIONAL CHECKS GOOD. (M)SDR EISA98250Slide · lowGALLEY DOOR SLIDE PRESSURE BELOW LIMITS. GENERATED FROM MAINTENANCE REPORT. REPLACED GALLEY DOOR SLIDE PER MM 25-62-0. (M)SDR ABXA9801111Pylon · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND NR 2 PYLON CRACKED INTERNALLY, JUST AFT OF THE AFT SPAR. REPAIRED CRACK IAW ABX REA D954-25253 AND ABX DWG K05159.SDR ABXA9801064Web · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE RIGHT CUSP WEB CRACKED AT STATION 601. REPLACED RIGHT CUSP WEB BETWEEN STATION 598 AND 646 IAW DC9 SRM 51-10-3B AND 51-30-2.SDR USAAD98190Unknown · odorGSO - FLT 990 - AFTER TAKEOFF, PASSENGERS NOTED A BURNING SMELL IN THE CABIN. FLIGHT RETURNED TO GSO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED FULL POWER RUN-UPS ON BOTH ENGINES AND COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAFT WAS RELEASEDSDR ABXA9801066Bulkhead Clip · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD 2ND RADIAL CRACKED AT END CLIP. REPLACED CLIP IAW DC9 SRM 51-30-5.SDR USAAD98188Bulb · failedBNA-PHL - FLT 1952 - DURING APPROACH, THE LANDING GEAR WAS LOWERED BUT THE CREW DID NOT GET A POSITIVE NOSE GEAR INDICATION. A GO-AROUND WAS INITIATED. THE CREW CHANGED THE LIGHT BULB AND RECYCLED THE GEAR AND ALL INDICATIONS WERE NORMAL. THE AIRCRAFT LANDESDR ABXA9801070Panel · delaminatedWHILE COMPLYING WITH D-INSPECTION, FOUND RIGHT WING LOWER INBOARD TRAILING EDGE PANEL AT XRS 101 DELAMINATED. REPLACED PANEL IAW DC9 SRM CHAPTERS 51-30-1, 51-30-2, AND 51-30-5.SDR ABXA9801067Doubler · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE LEFT WING REAR SPAR DOUBLER CRACKED OUTBOARD OF TRAPEZOIDAL PANEL. REPAIRED IAW ABX REA D957-25131MR.SDR ABXA9801057Jamb · corrodedWHILE COMPLYING WITH D-INSPECTION, FOUND THE VENTRAL STAIR RIGHT JAMB STRUCTURE CORRODED BETWEEN STATION 1059 AND 1076. REPLACED RIGHT JAMB FITTING IAW DC9 SRM 51-30-1, 51-30-2, AND 51-30-5.SDR 9810309956Prox Sensor · brokenDURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR EXTENSION. CREW CYCLED GEAR WITH SAME RESULTS. GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED THROUGH PEEP HOLE. EMERGENCY EQUIPMENT WAS CALLED OUT ON STANDBY AS A PRECAUTION. AIRCRAFT LANDSDR ABXA9801068Tab · delaminatedWHILE COMPLYING WITH D-INSPECTION, FOUND THE RIGHT AILERON CONTROL TAB HAD INTERNAL WATER INTRUSION. REPLACED RIGHT AILERON CONTROL TAB IAW DC9 MM CHAPTER 27-10-2.SDR ABXA9800918Link · crackedWHILE COMPLYING WITH AD 75-14-06, FOUND LOWER LEFT THRUST REVERSER DRIVER LINK CRACKED ON NR 2 ENGINE. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-05.SDR ABXA9800917Link · crackedWHILE COMPLYING WITH AD 75-14-06, FOUND UPPER LEFT THRUST REVERSER DRIVER LINK CRACKED ON NR 2 ENGINE. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-05.SDR ABXA9800916Latch · looseCOCKPIT DOOR WAS JAMMED. SECURED HARDWARE ON DOOR LATCH ASSY.SDR USAA980531Frame · crackedPIT - DURING C-4 CHECK, FOUND .5 INCH TO .75 INCH CRACKS AT STATION 1104 AT FRAME LONGERON 13R. REPLACED FROM STA 1104 FROM 11R-22R FLOOR, FACTORY SPLICE PER SRM 53-03 FIG 30. (M)SDR USAA980530Frame · crackedPIT - DURING C-4 CHECK, FOUND .5 INCH CRACKS AT LONGERON 14L, STATION 1104 CANTED FRAME. REPLACED FRAME FROM 11L TO 22L FLOOR FACTORY SPLICE PER SRM 53-03 FIG 30. (M)SDR USAA980529Frame · crackedPIT - DURING C-4 CHECK, FOUND .5 INCH CRACKS AT 3 LONGERONS AT STATION 1104 LONGERONS 3R, 4R, AND 6R. REPLACED FRAME ASSEMBLY PER SRM 53-03 FIG 30. (M)SDR GTIA9800116Bulb · failedDTW - OVERHEAD EMERGENCY LIGHT SYSTEM LEFT AND RIGHT LIGHTS INOPERATIVE AT ROW 2, LEFT AT ROW 4, AND RIGHT AT ROW 6. REMOVED AND REPLACED LAMPS, OPERATIONAL CHECK NORMAL IAW DC-9 MM CHAPTER 33-53-0. (M)SDR GTIA9800115Bulb · failedEMERGENCY LIGHT SYSTEM IN VENTRAL STAIRWAY UPPER LEFT INOPERATIVE. REPLACED BULBS, STILL INOPERATIVE. REPLACED BULBS IAW DC-9 MM 33-50-1. CHECKS GOOD. (M)SDR TWAA9816804Angle · crackedDURING OP 16 MAINT CHECK, FOUND RT WING OTBD SPOILER, OTBD DOWN STOP ANGLE WAS CRACKED ON THE INBD SIDE. INSTALLED NEW TEE ANGLE, MFG 5918134-1, PER SRM 51-01, PG 1 ITEM C. INSTALLED RIVETS PER SRM 51-30-02. INSTALLED FASTENERS PER SRM 51-30-0.SDR TWAA9816405Former · corrodedDURING OP 16 MAINT CHECK, FOUND LIGHT CORROSION ON THE FORMER CAP AT STA 897, LONGERON 27L TO 29L. REPLACED FORMER CAP PER STANDARD PROCESSES MANUAL 6-70-1.SDR USAAD98186Control Panel · failedBWI/BOS - FLT 728 - AFTER DEPARTURE, THE LEFT ENGINE GENERATOR TRIPPED OFF-LINE. ATTEMPTS TO RESET WERE UNSUCCESSFUL. THE APU WAS ON MEL LEAVING ONLY THE RIGHT ENGINE GENERATOR TO POWER THE AIRCRAFT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCISDR GTIA9800117Slide · looseMYR - FLT 381 - SLIDE PACK CAME LOOSE FROM GALLEY DOOR. REINSTALLED SLIDE PACK COVER AND SLIDE ON GALLEY DOOR RIGHT SIDE OF AIRCRAFT. (M)SDR ABXA9801054Bulkhead Channel · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR HAD A CRACK ON BOTTOM CHANNEL. REPLACED LOWER CHANNEL IAW DC9 SRM CHAPTERS 51-10-2, 51-30-1 AND 51-30-5.SDR ABXA9801053Panel · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND THE NOSE LANDING GEAR WHEEL WELL PRESSURE PANEL CRACKED AT STATION 83 NEAR RIGHT CUSP ANGLE. INSTALLED DOUBLER REPAIR IAW DC9 SB 53-187.SDR 98ZZZX3973Control Panel · failedBWI/BOS - FLT 728 - AFTER DEPARTURE, THE LEFT ENGINE GENERATOR TRIPPED OFF-LINE. ATTEMPTS TO RESET WERE UNSUCCESSFUL. THE APU WAS ON MEL LEAVING ONLY THE RIGHT ENGINE GENERATOR TO POWER THE AIRCRAFT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCISDR USAAD98183Sensor · malfunctionedGSO-LGA - FLT 990 - UPON GEAR EXTENSION DURING APPROACH, THE GREEN NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE, ALL NOSE GEAR UNSAFE LIGHTS WERE OUT. THE GEAR WAS RECYCLED AND ALL INDICATIONS WERE NORMAL. MAINTENANCE CHECKED THE NOSE GEAR INDICATING SYSTEM, ASDR ABXA9801056Jamb · corrodedWHILE COMPLYING WITH D-INSPECTION, FOUND THE VENTRAL STAIR LEFT JAMB CORRODED ON OUTBOARD SIDE BETWEEN STATION 1059 AND 1076. REPLACED LEFT STAIR JAMB CHANNEL IAW DC9 SRM 51-30-2 AND 51-30-5.
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