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 9510929995Bulkhead · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 110 BULKHEAD FORWARD CAP AT APPROXIMATELY LONGERON 26R IN THE NOSE LANDING GEAR WELL. REPAIRED PER EA 99-92197.SDR 9510919995Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE SKIN DOUBLER, LONGERON 23L BETWEEN FS 895 - 915. REPAIRED PER EA 99-92183.SDR 9509249976Fitting · crackedDURING PERIODIC CHECK, FOUND CRACKS IN THE FORWARD CARGO DOOR JAMB INTERCOSTAL END FITTINGS AFT OF THE FORWARD DOOR HINGE AND FORWARD OF THE AFT DOOR HINGE. REPLACED FITTINGS PER SRM 51-30.SDR 9509179976Fitting · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN THE FS 598 INTERCOSTAL FITTING BETWEEN LONGERONS 27L - 28L. REPLACED FITTING PER SRM 51-30-0.SDR 9508969990Gear Light · malfunctionedNOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE ON APPROACH INTO MSP. RECYCLED GEAR AND NORMAL INDICATION WAS ACHIEVED. FLIGHT LANDED WITHOUT INCIDENT. LUBED NOSE LANDING GEAR. OPERATIONAL CHECK OK, AIRCRAFT RETURNED TO SERVICE.SDR 9510909995Yoke · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FASTENER HOLE FOR THE RIGHT ENGINE YOKE ISOLATOR MOUNT AT THE FORWARD SPAR. REPAIRED YOKE PER EA 99-93566.SDR 9509169976Fitting · crackedDURING PERIODIC CHECK, FOUND A CRACK IN THE GALLEY SERVICE DOOR NR 2 BEAM AFT END FITTING. REPLACED FITTING PER SRM 51-30-10.SDR USAA950722Eel Power Supply · defectiveCLE - THE FORWARD CEILING EMERGENCY LIGHTS WOULD NOT SHUT OFF. MAINTENANCE REPLACED THE POWER SUPPLY. OPERATIONS CHECKED GOOD. (X)SDR ABXA9500613Floor Beam · damagedDURING C-CHECK INSPECTION, FOUND AN EXISTING REPAIR TO THE FLOOR BEAM AT STA. 917 TO BE DAMAGED. REPAIRED IAW ABX REA D953-11698-MR.SDR ABXA9500612Floor Beam · damagedDURING C-CHECK INSPECTION, FOUND TWO HOLES INCORRECTLY LOCATED AND ONE HOLE DOUBLE DRILLED AT STA. 897. REPAIRED IAW ABX REA D953-11716-MR.SDR ABXA9500540Skin · holes elongatedDURING C-CHECK INSPECTION, FOUND LOOSE SCREWS ON THE VERTICAL STABILIZER, LEFT SIDE FORWARD BOTTOM ATTACH ANGLE. REPAIRED IAW ABX REA D953-11728-MR.SDR 9509149976Fitting · crackedDURING PERIODIC CHECK, FOUND A CRACK IN THE AFT CABIN DOOR UPPER HINGE FITTING. REPLACED FITTING PER SRM 51-30.SDR 9509139976Fitting · crackedDURING PERIODIC CHECK, FOUND A CRACK IN THE LONGERON 27L END FITTING AT FS 590. REPLACED FITTING PER SRM 51-30-2.SDR 9508959964Heat Exchanger · inoperativeAIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. CABIN ALTITUDE WAS CLIMBING AT AN EXCESSIVE RATE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED HEAT EXCHANGER. LEAK AND OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.SDR USAA950670Angle · corrodedPIT - DURING Q-3 CHECK INSPECTION, FOUND LEVEL 1 CORROSION CPCP TASK NR C58-53300, LT LAV THRESHOLD ANGLE, STA 983, PREVIOUS REWORK. INSTALLED DOUBLER REPAIR PER SRM 53-01. (X)SDR USAA950669Pan · corrodedPIT - DURING Q-3 CHECK INSPECTION FOUND LEVEL 1 CORROSION AT GALLEY FLOOR PAN, STA 180 TO STA 205, RT SIDE, PREVIOUS REWORK. REF: CRCP TASK C46-53303. INSTALLED NEW SECTION OF FLOOR SUB-PAN PER SRM 53-01. (X)SDR USAA950668Angle · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK IN LEFT PYLON TOP ATTACH ANGLE AT STA 980. CUT OUT DAMAGED AREA AND INSTALLED FILLER AND DOUBLER REPAIR PER SRM 54-04, FIGURE 10. (X)SDR USAA950667Membrane · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND 1.50 INCH CRACK IN CUSP MEMBRANE, STA 596, LONGERON 18R. MFG NEW SECTION OF WEB MEMBRANE AND INSTALLED PER SRM 53-01. (X)SDR USAA950666Clip · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK IN FORWARD CARGO FLOOR SUPPORT CLIP, STA 598, LONGERON 27L. MFG NEW CLIP AND INSTALLED PER SRM 53-01. (X)SDR USAA950665Support · corrodedPIT - DURING Q-3 CHECK INSPECTION, FOUND CORROSION, STA 237, FLOOR SUPPORT CENTER, LT SIDE. FABRICATED NEW SUPPORT AND SPLICED IN ANGLE REPAIR PER USAIR TYPICAL REPAIR 53-10-21A. (X)SDR USAA950664Longeron · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK IN LONGERON 4L, STA 160. INSTALLED SPLICE REPAIR OF LONGERON PER SRM 53-02, FIGURE 2, VIEW BB. (X)SDR USAA950663Membrane · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND 2 INCH CRACK IN CUSP MEMBRANE, STA 617, LONGERON 18L. MFG NEW SECTION OF WEB MEMBRANE AND INSTALLED PER SRM 53-01. (X)SDR USAA950662Belt Beam · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND 2 CRACKS, .1250 INCH EACH, IN STA 207, LT SIDE TOP OF BOTTOM WINDOW BELT BEAM. INSTALLED DOUBLER TYPE REPAIR PER SRM 53-03, FIGURE 36. (X)SDR USAA950661Web · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND 12 INCH CRACK IN STA 180 WEB 9923484-7. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER DAC DWG 9923484. (X)SDR USAA950660Blkhd Angle · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK TOP C/L ANGLE ABOVE AFT PAX ENTRY DOOR ON FWD SIDE OF PRESSURE DOME, STA 996. INSTALLED ANGLE AND DOUBLER REPAIR PER SRM 53-01, FIGURE 2. (X)SDR USAA950659Longeron · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK IN LONGERON 4L AT STA 637. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIGURE 2. (X)SDR USAA950658Rib · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND .1250 INCH CRACK AT VERTICAL STAB L.E. BOTTOM 7TH RIB. INSTALLED NESTED DOUBLER REPAIR PER SRM 55-01. (X)SDR USAA950657Longeron · crackedPIT - DURING Q-3 CHECK INSPECTION FOUND .1250 INCH CRACK IN RIGHT NAV LONGERON 17R STA 965. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02. (X)SDR USAA950547Eel · inoperativePHL - FLT 0059 - THE EMERGENCY LOW LEVEL LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHECKED THE OPERATION OF THE EMERGENCY LIGHTS FROM THE FLIGHT ATTENDANT AND COCKPIT POSITIONS. OPERATIONS CHECKED NORMAL. (M)SDR ABXA9500551Doubler · crackedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 56-11, REV 3, FOUND CRACKED DOUBLER AROUND RIGHT CLEARVIEW WINDOW FRAME UPPER AFT CORNER. REPAIRED BY REPLACING DOUBLER IAW DC-9 SRM 51-30-2 AND 51-30-1.SDR 9509229996Skin · corrodedDURING LINE CHECK, FOUND CORROSION AND SHEARED FASTENERS IN THE FUSELAGE SKIN FS 332 AT LONGERON 29L TO 30. REPAIRED PER EA 99-98462.SDR 9508899988Switch · out of adjustAFTER TAKEOFF MSP-DFW AT APPROXIMATELY 6000 FEET MSL, THE FORWARD STAIRWAY DOOR WARNING LIGHT ILLUMINATED. RETURNED TO MSP WITHOUT FURTHER INCIDENT. ADJUSTED THE SWITCH PER MM 52-62-0 PG 501, OPERATIONAL CHECK OK.SDR USAA950542Trim · loosePIT - FLT 0728 - AFTER TAKEOFF, THE TOWER NOTICED A PIECE OF THE MED TRIM FLAPPING. FLIGHT RETURNED TO PIT. MAINTENANCE CUT THE LOOSE INTERIOR TRIM THAT WAS HANGING OUTSIDE OF THE DOOR. OPERATIONAL GOOD. (M)SDR ABXA9600503Switch · defectiveDURING SERVICE CHECK, WHEN SELECTING EMERGENCY LIGHTS TO OFF, THE LIGHTS REMAINED ILLUMINATED. REPLACED THE EMERGENCY LIGHT SWITCH.SDR ABXA9500614Jamb · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL 1 CORROSION AND A REPAIR TO THE LOWER JAMB OF THE FORWARD LOWER CARGO DOOR . REPAIRED IAW ABX REA D953-11672-MR.SDR ABXA9500592Tr Fairing · crackedDURING COMPLIANCE OF A.D. 92-22-08, FOUND CRACKED FAIRING ON LOWER THRUST REVERSER BUCKET, INBOARD SIDE, LEFT ENGINE. REPAIRED IAW DC-9 OVERHAUL MANUAL 78-30-1.SDR 9510889995Bulkhead · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE AFT CARGO, AFT BULKHEAD BETWEEN RBL 12 - RBL 36. REPAIRED PER EA 99-192235.SDR USAA950635Skin · dentedPIT - DURING Q-t/CX-5 INSPECTION, FOUND 2 , 20 INCH BY 6 INCH BY .375 INCH DEEP DENTS AND 1.5 INCH CRACK BETWEEN STA 256 TO 294 AND LONGERON 20R AND 21R APPROX STA 280. CUT OUT DAMAGED AREA AND INSTALLED FILLER DOUBLER AND TAPERED SHIMS PER USAIR EA NR 30552.SDR USAA950540Oil Tank Assy · leakingDAY - FLT NR 0152 - FLIGHT DIVERTED TO DAY DUE TO THE NR 2 ENGINE OIL PRESSURE DECREASING. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE OIL TANK DUE TO LEAKAGE. LEAK CHECKED GOOD. (M)SDR USAA950539Mixer Assy · lack of lubePIT - FLIGHT 0856 - AIRCRAFT RETURNED TO PIT DUE TO THE LEFT AILERON BINDING. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY. MAINTENANCE LUBED THE LATCHED CONTROL MIXER ASSEMBLY AND RECHECKED THE AILERON TAB DEFLECTION FORCE LEFT AND RIGHT WING. SDR ABXA9500625Longeron · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 29L CRACKED AT STA 313 - STA 389. REPLACED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9500624Splice · crackedDURING C-CHECK INSPECTION, FOUND TWO LONGERON SPLICES AT LONGERONS 29L AND 30L CRACKED AT STA. 237 AND 256. REPLACED SPLICES IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9500623Longeron · crackedDURING C-CHECK INSPECTION, FOUND LONGERON 30 CRACKED AT STA 294 AND STA 370. REPLACED LONGERON IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR ABXA9500539Skin · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL I CORROSION AROUND THE NR 1 AND NR 2 ADF LOOP ANTENNAS ON THE UPPER FUSELAGE SKIN. REPAIRED IAW ABX REA D953-11673-MR.SDR 95ZZZX4156Longeron · crackedSTL - DURING OP-15, FOUND .1250 INCH CRACK IN LONGERON 29R, STA 218. REPAIRED BY REPLACING LONGERON PER SRM 51-10-0, PAGES 1 AND 2, AND STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 66,307 HOURS; 81,239 CYCLES.SDR 9508829995Studs · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE,FOUND CORROSION ON THE LEFT WING AILERON A BRACKET ATTACH STUDS FOR HINGES NR 1 TO NR 4. REPLACED STUDS PER MM 20-16-0.SDR 9508819915Fitting · crackedDURING PERIODIC CHECK, FOUND A CRACK IN THE LONGERON 30 END FITTING IN THE KEEL AREA. REPLACED FITTING PER SRM 51-30-5.SDR USAA950545Eel Wire · damagedCLT - FLT NR 1287 - THE EMERGENCY FLOOR PATH LIGHTING BETWEEN ROWS 6 AND 11 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A DAMAGED WIRE ON THE FLOOR TRACK LIGHT. OPERATIONS CHECKED GOOD. (M)SDR USAA950535Fuel Pump · failedROC - FLT NR 0581 - THE LEFT ENGINE FAILED AS THE GEAR WAS RETRACTED. THE CREW RETURNED TO ROC. FLIGHT LANDED WITHOUT FURTHER INCIDENT. REPLACED FUEL PUMP. (M)SDR USAA950533Conduit · inoperativeCLT - FLT NR 0424 - WHILE EXTENDING THE GEAR FOR LANDING, THE NOSE GEAR UNSAFE LIGHT AND NOSE GEAR DOOR OPEN LIGHT ILLUMINATED. CAPTAIN FLEW BY THE TOWER TO CONFIRM THAT THE GEAR WAS DOWN. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY. MAINTENANCE
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