Douglas DC-9-32
Service difficulty reports · 12,755
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 = 'DC932' 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 = 'DC932' 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 ABXA9500307Floorbeam · gougedDURING C-CHECK, INSPECTION FOUND FLOORBEAM AT STA 945 GOUGED ON FORWARD FACE, RBL 1. REPAIRED IAW ABX REA D953-11238-MR.SDR ABXA9500306Jamb · crackedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 94-03-01, FOUND THE UPPER FORWARD CORNER OF SERVICE DOOR JAMB HAD A CRACK IN THE EXTERIOR SKIN AT RIVET STA 160. TO GAIN ACCESS TO REPAIR SKIN THE WEB WAS CUT AT STA 184.375. REPAIRED CRACKED SKIN IAW DC-9 SRMSDR AENA131C1Bracket Assy · brokenON APPROACH INTO LAS, PILOT SELECTED 40 DEGREE FLAP DOWN AND HAD 30 DEGREE SPLIT ON FLAP INDICATOR L20 DEGREEES, R50 DEGREES. PILOT INDICATED NO CONTROL PROBLEMS AND ACFT LANDED WITHOUT INCIDENT. ON INSPECTION BY MAINTENANCE AT LAS, FOUND RT INBD FLAP HINGE SDR AENA131CBracket Assy · crackedINSPECTION FOUND BRACKET ASSY CRACKED AT THE RT CENTER FLAP HINGE, WS 251.683. (X)SDR ABXA9500295T Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING LOWER T-CAP AT FORWARD AND AFT FLANGES ON STRINGER NR 20. BLENDED IAW DC-9 SB 57-98.SDR ABXA9500294T Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING T-CAP BETWEEN STRINGERS 21 TO 22. BLENDED IAW DC-9 SB 57-98.SDR ABXA9500293T Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LOWER T-CAP ON LEFT WING BETWEEN STRINGERS 20 TO 21. BLENDED IAW DC-9 SB 57-98.SDR ABXA9500292T Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING LOWER T-CAP BETWEEN STRINGERS 19 TO 20. BLENDED IAW DC-9 SB 57-98.SDR ABXA9500291Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING UPPER SURFACE OF STRINGER NR 17. BLENDED IAW DC-9 SRM 51-10-3.SDR ABXA9500305Frame · corrodedDURING C-CHECK, INSPECTION FOUND LEVEL II CORROSION ON FUSELAGE FRAME AT STA 110, RIGHT NOSE WHEEL TUNNEL, LOWER AFT CORNER. REPAIRED FRAME IAW ABX REA D953-11209-MR.SDR ABXA9500304Skin · corrodedDURING C-CHECK, INSPECTION FOUND LEVEL I CORROSION ON INSIDE OF OUTER SKIN, JUST AFT OF ALC DOOR JAMB AT STA 937. REPAIRED IAW ABX REA D953-11223-MR.SDR ABXA9500268Cap · corrodedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP BETWEEN STRINGERS 22-23. BLENDED IAW DC-9 SB 57-98.SDR 95ZZZX1629Cofeemaker · overheatATL/PBI - FLT 501 - RETURNED TO ATL BECAUSE ON CLIMB-OUT CAPTAIN REPORTED SMOKE IN THE COCKPIT COMING FROM THE GALLEY AREA BEHIND THE FIRST OFFICER'S SEAT, AND DECLARED AN IN-FLIGHT EMERGENCY. ON FINAL APPROACH, CAPTAIN PULLED FORWARD GALLEY CIRCUIT BREAKER ASDR ABXA9500308Skin · buckledDURING C-CHECK, INSPECTION FOUND SKIN JUST ABOVE LEFT FORWARD CORNER OF FORWARD NOSE GEAR DOOR BUCKLED. REPAIRED SKIN IAW ABX REA D953-11207-MR.SDR ABXA9500298Rod End · wornDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ACTUATING ROD OUTBOARD END HAD EXCESSIVE PLAY. REPLACED ROD END IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9500303Rib · gougedDURING C-CHECK, INSPECTION FOUND DEEP GOUGE ON RIGHT WING ADJACENT TO TELESCOPIC SLAT BLEED AIR DUCT. REPAIRED IAW ABX REA D957-11203-MR.SDR ABXA9500286Cap · crackedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND RIGHT WING LOWER T-CAP CRACKED IN THE RADIUS JUST AFT OF STRINGER NR 16. BLENDED IAW DC-9 SRM 51-10-3.SDR ABXA9500287Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP, AFT OF STRINGER NR 11. BLENDED IAW DC-9 SRM 51-10-3.SDR ABXA9500285Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP, BETWEEN STRINGERS 11-12. BLENDED IAW DC-9 SB 57-98.SDR ABXA9500282Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 11, RIGHT WING. BLENDED CORROSION IAW DC-9 SRM 51-22-1 AND 57-01.SDR ABXA9500281Stringer · gougedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 11, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.SDR ABXA9500280Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 12, RIGHT WING. BLENDED IAW DC-9 SRM 51-22-1 AND 57-01.SDR ABXA9500279Stringer · gougedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 12, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.SDR ABXA9500278Stringer · corrodedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 13, RIGHT WING. BLENDED IAW DC-9 SRM 51-00-1 AND 57-01.SDR ABXA9500277Stringer · gougedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03; SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 13, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.SDR ABXA9500276Stringer · gougedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 14, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.SDR ABXA9500275Stringer · gougedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 15, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.SDR ABXA9500274Stringer · corrodedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 16, RIGHT WING. BLENDED IAW DC-9 SRM 51-22-1 AND 57-01.SDR ABXA9500273Stringer · gougedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 16, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.SDR ABXA9500272Stringer · corrodedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER NR 17, RIGHT WING. BLENDED IAW DC-9 SRM 51-22-1 AND 57-01.SDR ABXA9500271Stringer · gougedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03; SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 17, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.SDR ABXA9500270Stringer · gougedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 18, RIGHT WING. BLENDED IAW DC-9 SRM 57-01.SDR ABXA9500269Stringer · corrodedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING ON TOP OF STRINGER NR 20. BLENDED IAW DC-9 SRM 51-10-3 AND 57-01.SDR ABXA9500266Stringer · gougedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN STRINGER NR 23R. BLENDED IAW DC-9 SRM 57-01.SDR ABXA9500265Stringer · corrodedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 23R. BLENDED IAW DC-9 SRM 51-10-3 AND 57-01.SDR ABXA9500264Stringer · gougedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND BARREL NUT HOLE GOUGED IN RIGHT WING STRINGER NR 20. BLENDED IAW DC-9 SRM 57-01.SDR MWEA95150Evac Slide · fell offPILOT REPORTS MAIN CABIN DOOR EVACUATION SLIDE FELL OFF DOOR. RESECURED SLIDE, RETURNED A/C TO SERVICE.SDR ABXA9500284Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON STRINGER NR 22, LOWER FORWARD LEG. BLENDED IAW DC-9 SB 57-98.SDR ABXA9500283Cap · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 57-98, FOUND LEVEL I CORROSION ON LEFT WING LOWER T-CAP HORIZONTAL FLANGE INSIDE BARREL NUT HOLES IN STRINGERS 11, 14, 16, 18, 20 AND 21. BLENDED IAW DC-9 SB 57-98.SDR ABXA9500267Cap · corrodedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON RIGHT WING LOWER T-CAP, INSIDE BARREL NUT HOLES IN STRINGERS NR 12, 13, 14, 15, 16, 17, 18, 19 AND 21. BLENDED IAW DC-9 SRM 51-10-3 AND SB 57-98.SDR ABXA9500299Hinge · gougedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR HINGE DEEPLY GOUGED. REPLACE DOOR HINGE IAW DC-9 SRM 51-30-2 AND 51-30-5.SDR 95ZZZX1628Door · malfunctionDTW/ATL - FLT 441 - RETURNED TO DTW DUE TO A VIBRATION FROM NOSE GEAR WHEELWELL AREA AFTER GEAR RETRACTION. FOUND NOSE GEAR DOORS OPEN. CLOSED DOORS AND INSPECTED NOSE GEAR AREA PER MM 32.SDR EISA95053Duct · rupturedDURING CLIMB-OUT FROM HSA GOT FIRE INDICATION ON LEFT ENGINE, DIVERTED TO GPT. FOUND 13TH STAGE BLEED AIR DUCT RUPTURED, REPLACED DUCT. (Z)SDR ABXA9500300Arm Assy · wornDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR FORWARD LINKAGE CONNECTING POINT HAD EXCESSIVE PLAY. REPLACED ARM ASSEMBLY IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR ABXA9500297Door · delaminatedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR AFT EDGE LOWER CORNER DELAMINATED. SEALED LEFT MAIN LANDING GEAR OUTBOARD DOOR AFT EDGE LOWER CORNER IAW DC-9 SRM 51-20-0. REPLACED RIVETS IAW DSDR 95ZZZX1627Csd · failedIAD/ATL - FLT 173 - EXPERIENCED NR 2 ENGINE CSD OVERTEMP AND FOUND THE CSD WOULD NOT DISCONNECT. CREW WAS INFORMED TO SHUT DOWN NR 2 ENGINE AND AIR TURNED BACK TO IAD. CREW DECLARED AN EMERGENCY AND LANDED WITH NO OTHER PROBLEMS.SDR ABXA9500296Hinge · wornDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 91-22-07, ASB 32-244, FOUND LEFT MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR HINGE HAD EXCESSIVE PLAY. REPLACED HINGE IAW DC-9 SRM 51-30-2 AND DC-9 OVERHAUL MANUAL 32-10-6.SDR MWEA95145Slide Cover · fell offCREW REPORTS, GALLEY SERVICE DOOR EVACUATION SLIDE COVER CAME OFF. REINSTALLED GALLEY DOOR EVACUATION SLIDE COVER AND RETURNED A/C TO SERVICE.SDR MWEA95144Eel Battery Pack · dischargedDURING ROUTINE INSPECTION, FOUND THAT THE EMERGENCY LIGHTS IN TAIL COMPARTMENT WOULD NOT EXTINGUISH. REPLACED EMERGENCY LIGHT BATTERY PACK.SDR 95ZZZX1663Pack Unit · malfunctionATL/DFW - FLT 231 - RETURNED TO ATL DUE TO RT AND LT AIR CONDITIONING PACKS AIRFLOW WENT TO ZERO. RESET CIRCUIT BREAKER FOR GROUND COOLING FAN FOR RT AIR CONDITION PACK. ON LT AIR CONDITION PACK, FOUND DUCT TEMP INDICATOR STUCK AND PACK THERMAL TRIPPED. PAC
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