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 ABXA9600669Power Supply · defectiveEMERGENCY LIGHTING STAYS ON WHEN POWER IS REMOVED FROM AIRCRAFT. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC-9 SUPP MM 33-53-00.SDR 97ZZZM6Light · damagedDTW - FORWARD WHITE EMERGENCY FLOOR EVACUATION LIGHT CRUSHED. REPLACED BULB AND LENS. OPERATIONAL CHECKED NORMAL IAW MM 33-50-0. (M)SDR 96ZZZX6071Spar · corrodedDURING C-CHECK, FOUND CORROSION IN NR 1 TANK ON AFT SPAR XW58.50 TO XRS111.5.SDR 96ZZZX6059Stringer · corrosionDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE FORWARD CARGO PIT, S29R BETWEEN STA 389 AND STA 408 AROUND NUTPLATES FOR RADIO ALTIMETER NR 1.SDR 96ZZZX6058Longeron · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE AFT CARGO PIT, STA S30 FROM STA 897 TO STA 965. MECHANICALLY REMOVED CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW DC9 SRM 51-01 FIG 1. REMOVED CORRODED AREA OF STR 30 IAW DC9 SRM 51SDR 96ZZZX6057Frame · crackedDURING A SCHEDULED INSPECTION AT AERO CORP, A 1 INCH CRACK WAS FOUND IN THE AFT CARGO PIT FRAME AT STA 897 BETWEEN S28L AND S27L. REMOVED OLD REPAIR CRACKED DOUBLER IAW DC9 SRM 51-30-5. REMOVED CORROSION ON ANGLE FRAME, MATERIAL LOSS LESS THAN .002 INCH IAW SDR 96ZZZX6056Intercostal · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION FOUND IN THE AFT CARGO PIT, S29R FROM STA 870 - STA 897. S29R WAS NOT CORRODED, INTERCOSTAL ON TOP WAS CORRODED AND CRACKED. REMOVED CORROSION, CORROSION WAS OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1, SRM 51-SDR 96ZZZX6055Threshold · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE FWD PIT LOWER THRESHOLD PAN SECTION AND 1 EACH SPLICE.SDR 96ZZZX6054Floor Beam · corrodedDURING A SCHEUDLED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE AFT CARGO PIT CABIN FLOOR BEAM AT STA 996 AT BL 34R. REMOVED CORROSION IAW DC9 SRM 51-10-2. FOUND TO BE OUT OF LIMITS AT LBL 31, 38, 40, 45, AT STA 980 IAW DC9 SRM 53-05 FIG 20A, 50 PERCESDR 96ZZZX6053Stringer · corrosionDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE AFT CARGO PIT AT STA 756 S30 AROUND FASTENERS. REMOVED CORROSION, OUT OF LIMITS IAW DC9 SRM 53-01, WAS .180 INCH, NOW .130 INCH. NDT VERIFIED. REMOVED CORRODED END OF SPLICE IAW DC9 SRM SDR 96ZZZX6052Frame · corrodedDURING A SCHEUDLED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE AFT CARGO PIT, FRAME STA 917 FROM S29L TO S29R. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1 (GAUGE A-0299). RECEIVED DRILLED AND DEBURRED NEW L29L FS 918 - FS 996,SDR 96ZZZX6051Frame · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE FWD CARGO PIT, FRAME STA 522 FROM S28R TO S29L.SDR 96ZZZX6050Seat Track · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE NR 4 SEAT TRACK FS 180 TO FS 218, INBD AND OTBD FLANGES. (X)SDR 96ZZZX6049Seat Track · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE NR 1 SEAT TRACK LEFT FLANGE.SDR 96ZZZX6048Seat Track · corrosionDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE LEFT INBOARD SEAT TRACK BETWEEN STA 579 - STA 756. REMOVED CORROSION IAW DC9 SRM 51-10-3. CORROSION OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1, FABRICATED REPAIR SPLICE (7075 T6 .160 INCH, .18SDR 96ZZZX6046Longeron · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE E/E COMPARTMENT, S28L, S29L, S30, S29R, AND S28R FROM STA 120 TO STA 130. REMOVED AND REPLACED LONGERONS 29L/R AND LONGERON 30 IAW DC9 SRM 53-02. REMOVED CORROSION, WITHIN LIMITS. ALODINSDR 96ZZZX6045Frame · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE E/E COMPARTMENT FRAMES AT STA 130 AND STA 160 BETWEEN S28L TO S28R. REMOVED FRAME STA 130 AND SHEAR CLIP. CORROSION OUT OF LIMITS IAW DC9 SRM 53-01 FIG 1. FABBED NEW SHEAR CLIP IAW DC9 SSDR 9627899618Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING STR 11L FROM WS 58 TO 4 OUTBOARD OF WS 91 WEB. REPAIRED PER EA 99-97715.SDR 9627889618Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING STR 13R FROM WS 58 TO WS 69. REPAIRED PER EA 99-97715.SDR TWAA9614304Power Supply · inoperativeSTL - FLT 608 - DURING PRE-FLIGHT, FOUND EGRESS LIGHTS IN FIRST CLASS INOPERATIVE. FOUND POWER SUPPLY, MFG PN 5822-3, MALFUNCTIONING. REPLACED POWER SUPPLY AND EGRESS LIGHT SYSTEM OPERATION CHECKED NORMAL. CHECK C - 7-25-96 - STL. (X)SDR TWAA9614302Battery Pack · dischargedSTL - FLT 567 - DURING PRE-FLIGHT, FOUND EGRESS LIGHTS INOPERATIVE. FOUND BATTERY PACK, MFG PN 60-117-9LB, WITH LOW VOLTAGE. REPLACED BATTERY PACK AND POWER SUPPLY. EGRESS LIGHT SYSTEM OPERATION THEN CHECKED NORMAL. CHECK C - 9-3-95 - STL. (X)SDR CALA9601783Skin · corrodedINSPECTION FOUND CORROSION BETWEEN RUDDER SKIN AND BONDED DOUBLERS ON LT SIDE AT STA ZR 111. THE SKIN WAS SPLICED TO PRODUCTION SPLICE, A LOWER LEFT SKIN SECTION WAS FABRICATED AND INSTALLED IAW ECRA 5540-01070, SRM 55-03 FIGURE 12 AND SRM 55-40-1.SDR CALA9601705Skin · damagedTHE AIRCRAFT STRUCK A FLOCK OF BIRDS DURING CLIMBOUT BETWEEN 2,500 TO 3,000 FEET. THE AIRCRAFT WAS RETURNED TO CLE. MAINTENANCE DISCOVERED IMPACT DAMAGE TO FUSELAGE SKIN, APPROXIMATELY 2 FEET BY 2 INCHES IN AREA, TWO FEET AFT OF RADOME ON LT FORWARD LOWER SKSDR 9627879614Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING STR 20R FROM WS 58 WEB TO WS 137 WEB. REPAIRED PER EA 99-97708.SDR 9627859614Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE LEFT WING STR 20L, WS 58 WEB. REPAIRED PER EA 99-97708.SDR 9627849614Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE RIGHT WING STR 16R WS 58 WEB TO WS 137 WEB. REPAIRED PER EA 99-97708.SDR 9625109987Compressor · stalledDURING TAKEOFF ROLL, ONE OR MORE ENGINES EXPERIENCED COMPRESSOR STALLS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED BOTH ENGINES, PERFORMED OPERATIONAL CHECK AND CHECKED OK. COULD NOT DUPLICATE STALLS.SDR CALA9601690Tr Unit · failedWHEN CREW ENTERED AIRCRAFT AT GATE, WITH EXTERNAL POWER ON, THEY NOTICED SMOKE IN COCKPIT AND CABIN. THE NR 2 TRANSFORMER RECTIFIER CIRCUIT BREAKER WAS POPPED AND WOULD NOT RESET. EXAMINATION OF THE NR 2 TRANSFORMER RECTIFIER FOUND IT BURNT. THE NR 2 TRANSFSDR 97ZZZX81Skin · crackedDURING A SCHEDULED INSPECTION AT AERO CORP., A 1 INCH CRACK WAS FOUND ON THE RIGHT WING UPPER SKIN PANEL FROM EDGE OF ACCESS PANEL NR 1410 A LANDING, THROUGH FASTENER HOLE AT AFT OUTBOARD QUADRANT OF ACCESS OPENING. STOP DRILLED CRACK, FABRICATED DOUBLER 7075SDR 97ZZZX6225Skin · crackedDURING A SCHEDULED INSPECTION AT AERO CORP., THE LEFT WING UPPER SKIN PANEL WAS FOUND CRACKED (LENGTH OF CRACK .4375 INCH) FROM EDGE TO FASTENER HOLE OF ACCESS PANEL NR 1307A LANDING AT AFT OUTBOARD QUADRANT OF ACCESS OPENING. STOP DRILLED CRACK, FABRICATED DSDR 97ZZZX39Skin · corrosionDURING A SCHEDULED INSPECTION AT AERO CORP, CORROSION WAS FOUND IN THE SKIN AT STA 580, LONGERON 30.SDR 9625049940Pitot Line · blockedRUDDER TRAVEL UNRESTRICTED LIGHT REMAINED ON AFTER TAKEOFF. FLIGHT DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PITOT LINE TO RUDDER LIMITER PROBE BLOCKED WITH ICE. DRAINED WATER FROM TRAP. REPLACED RUDDER TRAVEL UNRESTRICTED LIGHT SWITCHSDR MWEA96634Power Supply · inoperativeDURING SERVICE CHECK FOUND AF FLT ATTEND EMERGENCY LIGHT IN CEILING REMAINED ON WITH PWR OFF. REMOVED AND REPLACED AFT EMERGENCY LIGHT BATTERY PACK.SDR MWEA96633Power Supply · inoperativeDURING A-CHECK, FOUND AFT ACCESSORY COMPARTMENT EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PWR SUPPLY, OPS CHECK GOOD.SDR 9624829923Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE KEEL LONGERON END FITTINGS 29L AND 29.5L, FORWARD END FS 605. REPLACED FITTINGS PER SRM 51-30-5 AND DWG 5911418-505.SDR TWAA9614002Door Switch · out of adjustSTL - FLT 543 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, DOOR OPEN LIGHT REMAINED ILLUMINATED. CYCLED LANDING GEAR. FOUND DOOR SWITCH, MFG PN H14-6, OUT OF ADJUSTMENT. REPLACED DOOR SWITCH. LANDING GEAR DOOR INDICATION THEN CHECKED NORMAL. CHECK C -SDR CA961128031Lanyard Bracket · broken(CAN) GALLEY DOOR CHUTE PACK CAME ADRIFT. UNABLE TO INSTALL DUE TO BROKEN LANYARD ATTACHMENT BRACKET. MAINTENANCE INSTALLED NEW BRACKET CHECKED SERVICEABLE.SDR CA961128030Atc Cntrl Panel · elect short(CAN) AIRCRAFT RETURNED TO GATE DUE TO AIR TRAFFIC CONTROL PANEL ELECTRICAL SHORT AND CIRCUIT BREAKER ATC-1 POPPED. ATC CONTROL PANEL REPLACED AND SYSTEM CHECKED SERVICEABLE.SDR 9624749983Battery · dischargedDURING LINE CHECK, FOUND THAT THE LAST FOUR ROWS OF EMERGENCY SEAT LIGHTS AND THE AFT LEFT LAV EMERGENCY LIGHT WERE INOPERATIVE. REPLACED THE BATTERY PACK (P/N 9133-90368-1) AND POWER SUPPLY (P/N BC5-0447-907, CHECKED OK.SDR 9624709604Power Supply · inoperativeDURING LINE CHECK, FOUND THAT THE CATWALK EMERGENCY LIGHTS AND THE TAILCONE EXIT SIGN LIGHT WERE INOPERATIVE. REPLACED THE POWER SUPPLY, CHECKED OK.SDR 9614749983Battery · dischargedDURING LINE CHECK, FOUND THAT THE LAST FOUR ROWS OF EMERGENCY SEAT LIGHTS AND THE AFT LEFT LAV EMERGENCY LIGHT WERE INOPERATIVE. REPLACED THE BATTERY PACK (P/N 9133-90368-1) AND POWER SUPPLY (P/N BC5-0447-907), CHECKED OK.SDR MWEA96631Beam · crackedDURING C-CHECK, FOUND GALLEY SERVICE DOOR LOWER BEAM CRACKED IN RADIUS AT FWD END. MAINTENANCE INSTALLED REPAIR IAW SRM 52-05 FIG 25.SDR CA961125008Thrust Reverser · intermittent(CAN) LEFT ENGINE REVERSE UNLOCK LIGHT REMAINS ON AFTER DEPLOYMENT. RECYCLED REVERSER SEVERAL TIMES WITH NO CHANGE. MAINTENANCE ACTION INVOLVED ADJUSTING LH THRUST REVERSER LATCH AND SYSTEM CHECKED SERVICEABLE.SDR CA961125007Switch · broken wire(CAN) RIGHT LANDING GREEN LIGHT DID NOT ILLUMINATE ON APPROACH. MAINTENANCE CHECK FOUND BROKEN WIRE AT RH MAIN LANDING DOWN LOCK SWITCH. BROKEN WIRE REPAIRED.SDR 9624809982Vane · crackedDURING LINE CHECK, FOUND A BROKEN CASTING IN THE RIGHT WING AFT MOVEABLE VANE INBOARD END. REPLACED VANE PER MM 27-51-2 PG 505.SDR 9624719987Battery · contaminatedDURING LINE CHECK, FOUND THAT THE EMERGENCY SEAT LIGHTS WERE INOPERATIVE. FOUND THE TAILCONE EMERGENCY BATTERY PACK FILLED WITH DE-ICING FLUID. REPLACED THE BATTERY PACK, CHECKED OK.SDR 97ZZZX1770Hat Section · crackedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND AFT CABIN FLOOR AREA HAS HAT SECTION FLOOR SUPPORT CRACKED AND CORRODED AT STA 965 BL ZERO TO RT BL 24. FABBED NEW ANGLE SPLICE PER DC9 SRM 53-11-3, PAGE 3. ALODINED AND TREATED AREA. INSTALSDR 9624609986Frame · crackedDURING H-CHECK, FOUND A ONE INCH CRACK IN THE FS 617 FRAME FLANGE AT THE RIGHT SIDE FLOORBEAM LUG. REPAIRED FRAME (PSE 53.09.016, P/N 9919613-502) PER EA DC9-53-068 AND SRM 51-30-2, 51-30-5.SDR 9624599986Skin · crackedDURING H-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AT THE FORWARD SERVICE DOOR FORWARD SIDE UPPER AFT ADJUSTOR CUTOUT. REPAIRED SKIN PER EA 99-111057.SDR 97ZZZX1769Door Frame · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, AFT ENTRY DOOR HAS CORROSION ON BOTTOM FRAME. REMOVED CORRODED CHANNEL. INSTALLED NEW CHANNEL IAW DC9 SRM'S 51-30-5, 51-10-4, AND 51-10-3.
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