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 9502519928Beam · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK AND CORROSION IN VERTICAL STABILIZER BEAM ACROSS THE LOWER RUDDER 'A' BRACKET. REPAIRED SPAR ASSEMBLY PER EA 99-0924422.SDR 9502509928Rib · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON VERTICAL STABILIZER RIB ZRS 19. REPAIRED PER EA 99-092433.SDR 9502039909Compressor · stalledAS POWER WAS BROUGHT UP FOR TAKEOFF, COMPRESSOR STALLS OCCURRED ON NR 2 ENGINE APPROXIMATELY 85 PERCENT N2. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED A SMALL PIECE OF CARDBOARD FROM THE INLET AND INSPECTED FOR DAMAGE, NONSDR USAA950322Seat Track · corrodedPIT - DURING Q-4 CHECK INSPECTION, FOUND LEVEL I CORROSION FORWARD END OF LEFT OUTBOARD SEAT TRACK STATION 200. SPLICED IN SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. (W)SDR USAA950292Angle · crackedPIT - DURING SCHEDULED Q-1 INSPECTION, FOUND 1 INCH CRACK RIGHT UPPER PYLON ATTACH ANGLE STATION 1019. INSTALLED DOUBLER REPAIR PER SRM 54-04 FIG 10. (W)SDR ABXA9500134Stop Bolt · deformedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND FORWARD SERVICE DOOR AFT UPPER STOP BOLT DEFORMED. REPLACED DOOR STOP IAW DC-9 M.M. 20-16-0.SDR ABXA9500110Drain Boss · crackedDURING COMPLIANCE OF AD 87-11-07, PRATT AND WHITNEY ASB 5676, FOUND CRACK INDICATION ON FORWARD LOWER COMBUSTION CHAMBER OUTER CASE DRAIN BOSS. REPLACED ENGINE IAW ABX WORKCARD RJT 7001.SDR ABXA9500086Eel Power Supply · defectiveCOCKPIT EMERGENCY LIGHTS INTERMITTENTLY GO DIM TO BRIGHT. REPLACED EMERGENCY POWER SUPPLY. OPS CHECKED GOOD IAW DC-9 MM 33-53-0.SDR 95ZZZX1730Skin · crackedSTL - DURING CHECK-C, FOUND A .50 INCH AND A .25 INCH LONG SKIN CRACK AT TWO FASTENERS, STA 68.5. REPAIRED PER ARA 8823, USING SRO 9530239. AIRCRAFT TOTAL TIME: 60,099 HOURS; 71,912 CYCLES.SDR USAA950289Membrane · corrodedPIT - DURING SCHEDULED Q-1 INSPECTION, FOUND LEVEL I CORROSION AT CUSP MEMBRANE AT STATION 945 RT SIDE. REMOVED CORRODED SECTION OF MEMBRANE AND INSTALLED SPLICE REPAIR PER SRM 53-05 FIG 96. (W)SDR USAA950100Nlg Strut · faultyPIT - FLT 1297 - ON CLIMB-OUT, THE CAPTAIN PULLED THE GEAR HANDLE BUT IT WOULD NOT GO INTO THE 'UP' POSITION. CREW DECIDED TO RETURN TO PIT. MAINTENANCE DRAINED FLUID FROM THE NOSE LANDING GEAR LOWER LEG, REINSTALLED THE LOWER LEG AND SERVICED. NUMEROUS GEASDR ABXA9500140Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03 AND S.B. 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 19, NEAR BARREL NUT HOLES IN RIGHT WING. REMOVED CORROSION IAW DC-9 SRM 51-22-1 AND 51-10-3BSDR ABXA9500139Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03 AND S.B. 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 17, NEAR BARREL NUT HOLES IN RIGHT WING. REMOVED CORROSION IAW DC-9 SRM 51-22-1 AND 51-10-3B.SDR ABXA9500138Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03 AND S.B. 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 15, NEAR BARREL NUT HOLES IN RIGHT WING. REMOVED CORROSION IAW DC-9 SRM 51-22-1 AND 51-10-3B.SDR ABXA9500137Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03 AND S.B. 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 13, NEAR BARREL NUT HOLES IN RIGHT WING. REMOVED CORROSION IAW DC-9 SRM 51-22-1 AND 51-10-3B.SDR ABXA9500136Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03 AND S.B. 57-98, FOUND LEVEL I CORROSION ON TOP OF STRINGER 12, NEAR BARREL NUT HOLES IN RIGHT WING. REMOVED CORROSION IAW DC-9 SRM 51-22-1 AND 51-10-3B.SDR ABXA9500133Seal Depressor · damagedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND FORWARD LOWER SERVICE DOOR SEAL DEPRESSOR GOUGED AND BENT. BLENDED AND STRAIGHTENED SEAL DEPRESSOR IAW DC-9 SRM 53-01 AND 51-10-3.SDR ABXA9500132Seal Depressor · damagedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 94-03-01, FOUND AFT LOWER SERVICE DOOR SEAL DEPRESSOR GOUGED AND BENT. BLENDED AND STRAIGHTENED SEAL DEPRESSOR IAW DC-9 SRM 53-01 AND 51-410-3.SDR ABXA9500131Web · deformedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 78-07-05 AND S.B. 53-131, FOUND LEFT CUSP WEB OVER FRAMES 699, 718 AND 737 DEFORMED AND PARTS MISSING. REPLACED CUSP WEB IAW E.A. NR FS-53-03689-MA.SDR ABXA9500130Web · deformedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 78-07-05 AND S.B. 53-131, FOUND RIGHT CUSP WEB OVER FRAMES 669, 718 AND 737 DEFORMED AND MISSING PARTS. REPLACED CUSP WEB IAW E.A. NR FS-53-03689-MA.SDR 9502789914Switch Wires · brokenNOSE GEAR UNSAFE LIGHT FLICKERED ON AND OFF DURING GEAR EXTENSION. PERFORMED GO-AROUND OF TOWER AND LIGHT EXTINGUISHED DURING SECOND APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND BAD WIRING IN NOSE GEAR DOWNLOCK SWITCH. REPAIRED BROKEN WIRES. OPERATIOSDR 9502029930Slip Joint · out of positionAIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED WITH WING AIRFOIL SYSTEM ANTI-ICE ACTIVATED. LIGHT EXTINGUISHED WITH TAIL ANTI-ICE ACTIVATED. AFTER CYCLE OF TAIL SYSTEM, THE LIGHT REILLUMINATED. FLIGHT DIVERTED TO ORD AND LANDED WITHOUT INCIDENT.SDR USAA950316Longeron · crackedPIT - DURING Q-4 CHECK INSPECTION, FOUND .25 INCH CRACK IN LONGERON 30 AT SPLICE BETWEEN BELTFRAMES AT STATION 465 AND 484. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02 FIG 14. (W)SDR USAA950101Temp Contl Vlv · stuckCLT - FLT 0881 - DURING CLIMB, BOTH PACKS FAILED. THE RIGHT PACK RETURNED FOR 15 SECONDS THEN FAILED AGAIN. CREW RETURNED CLT. MAINTENANCE FOUND THE LEFT TEMPERATURE CONTROL VALVE STUCK OPEN CAUSING THERMOL TRIP ON LEFT PACK. THE LEFT PACK TEMPERATURE CONTSDR 9502729944Csd Oil Cooler · rupturedTAXIING FOR TAKEOFF, THE NR 2 ENGINE CSD OIL PRESSURE LOW LIGHT STARTED FLICKERING. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE FOUND THE CSD OIL COOLER RUPTURED. THE COOLER WAS REPLACED AND THE OIL WAS SERVICED. ACCOMPLISHESDR 9502249945Studs · corrodedDURING PERIODIC CHECK, FOUND CORROSION ON NR 2 FLAP HINGE ATTACH STUDS. REPAIRED PER XEA X9-27-9.SDR 9501979997Prbc Valve · malfunctionedON TAKEOFF, A COMPRESSOR STALL OCCURRED ON NR 1 ENGINE. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. ENGINE WAS INSPECTED FOR DAMAGE, NON FOUND. MAINTENANCE REPLACED THE PRBC AND P/D VALVES. ENGINE WAS RUN UP AND CHECKED OK. AIRCRAFT RETURNESDR USAA950102Strut · inoperativeSYR - FLT 0545 - AFTER TAKEOFF, CREW RECEIVED A NOSE GEAR UNSAFE LIGHT. THE GEAR WAS CYCLED TWO MORE TIMES AND THE LIGHT REMAINED ON. THE FLIGHT DIVERETED TO SYR AND LANDED SAFELY. MAINTENANCE SERVICED THE NOSE STRUT. A GEAR SWING WAS PERFORMED WITH NO DISSDR USAA950104Strut · flatPIT - FLT NR 1576 - THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM PIT. MAINTENANCE FOUND THE NOSE GEAR STRUT FLAT ON ARRIVAL AT THE GATE. THE STRUT WAS SERVICED WITH NITROGEN AND THE STRUT INFLATED TO THE PROPER HEIGHT. (W)SDR 9502199992Frame · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND PIT MARKS IN THE RIGHT SIDE WINDOW CUTOUTS AT FS 884 AND FS 903. REPAIRED PER EA 99-95751.SDR 9502189992Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACK IN FS 639 FRAME FITTING 'DINOSAUR RIB', LEFT SIDE JUST ABOVE CENTER TANK. REPAIRED PER EA 99-093477.SDR 9502179988Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON LONGERON 18L LOWER SPLICE FITTING AT FS 229. REPLACED FITTING PER SRM 51-30-5.SDR 9502169988Skin · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON INNER FUSELAGE SKIN FS 897 - 917 BETWEEN LONGERONS 22L - 23L. REPAIRED PER XEA X9-53-57.SDR USAA950105Uplatch Roller · looseCAE - FLT 0253 - ON LANDING IN CAE, THE GEAR DOOR OPEN LIGHT WOULD NOT GO OUT. THE GEAR WAS RECYCLED THREE TIMES BUT THE LIGHT REMAINED ON. MAINTENANCE SECURED A LOOSE ROLLER ON THE RIGHT MAIN LANDING GEAR UPLATCH. CHECKED OTHER PORTIONS OF THE DOOR INDICATSDR ABXA9500067Eel Switch · intermittentCABIN EMERGENCY LIGHTS ILLUMINATE INTERMITTENTLY IN FLIGHT. REPLACED CABIN EMERGENCY LIGHT SWITCH PER DC-9 MM. OPS CHECKED NORMAL.SDR 9502119945Hinge · corrodedDURING PERIODIC CHECK, FOUND CORROSION IN NR 3 FLAP HINGE MOUNTING HOLES, WS 251. REPLACED HINGE FITTING PER CITEXT 09-5740-1-9800.SDR 9501949971T Duct · bindingSLAT DISAGREEMENT LIGHT ILLUMINATED WHEN SLATS WERE SELECTED FOR LANDING INTO SRQ. AIRCRAFT EXPERIENCED A ROLL TO THE RIGHT. RECYCLED HANDLE THREE TIMES BEFORE LIGHT EXTENDED. NORMAL LANDING WAS ACCOMPLISHED. FOUND LEFT SLAT 'T' DUCT BINDING. ADJUSTED GUISDR ABXA9500092Fitting · crackedDURING C-CHECK INSPECTION WHILE ACCOMPLISHING AD 80-02-16, THE AFT PRESSURE DOME PLUG DOOR LUG SHOWED A CRACK INDICATION ON THE X-RAY. FITTING WAS REPLACED IAW DC-9 SRM 51-30-5.SDR 95ZZZX851Downlock Switch · failedSTL - FLT 641 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, RIGHT MLG UNSAFE LIGHT REMAINED ILLUMINATED; CYCLED LANDING GEAR. REPLACED RIGHT MLG DOWNLOCK SWITCH, MFG PN H14-6. LANDING GEAR OPERATION AND POSITION AND WARNING SYSTEM CHECKED NORMAL. CHECK SDR 9505259988Fitting · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON RIGHT WING NR 3 FLAP HINGE FASTENER BORES. REPLACED HINGE FITTING PER MM 57-40-1.SDR 9502089981Blkhd Web · oil cannedDURING PERIODIC CHECK, FOUND OIL CANNING IN THE LEFT LAVATORY BULKHEAD WEB AT THE INBOARD LIGHTENING HOLE. REPAIRED PER EA 99-096894.SDR 9501859968Rectifier · malfunctionedLOSS OF RIGHT TRANSFORMER RECTIFIER OCCURRED AFTER TAKEOFF. DC LOAD WAS INDICATING ZERO. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT TRANSFORMER RECTIFIER. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR ABXA9500085Tr Link · nickedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 75-14-06, A.D.90-18-03, S.B.'S 78-36, 78-38, 78-40, 78-66, FOUND BY EDDY CURRENT INSPECTION TWO EACH CRACK INDICATIONS ON THE INBOARD LOWER THRUST REVERSER LINK ON THE NR 2 ENGINE. BLENDED NICKS ON THRUST RESDR USAA950085Retract Mech · malfunctionedPIT - FLT 1005 - AFTER TAKEOFF, THE CAPTAIN RAISED THE GEAR, BUT GOT AN UNSAFE NOSE GEAR INDICATION LIGHT. THE GEAR WAS LOWERED, BUT THE UNSAFE NOSE GEAR LIGHT REMAINED. THE CAPTAIN THEN USED ABNORMAL PROCEDURES TO LOWER THE NOSE GEAR, AND RECEIVED A GREEN LSDR USAA950062Intercostal · crackedIND - ACCOMPLISHED SCHEDULED SID INSPECTION PSE 53.09.001A FORWARD CARGO DOOR JAMB AREA. FOUND 1.25 INCH CRACK IN FRAME STATION 389 LONGERON 18R (VISUAL INSPECTION). REMOVED AND REPLACED INTERCOSTAL. (Z)SDR 95ZZZX714Connector · dirtyCVG - FLT 698 - DURING APPROACH, LT MLG UNSAFE LIGHT REMAINED ON AFTER LANDING GEAR EXTENSION. CYCLED LANDING GEAR AND VISUALLY CHECKED LOCK. CLEANED ELECTRICAL CONNECTOR ON DOWNLOCK SWITCH. LANDING GEAR INDICATION SYSTEM OPERATION CHECKED NORMAL. CHECK OPSDR 9501599988Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND ONE INCH CRACK IN THE FORWARD CARGO DOOR NR 4 BEAM AFT END FITTING. REPLACED FITTING PER SRM 51-30-5.SDR ABXA9500084Stringer · gougedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D.90-18-03, S.B. 57-98, FOUND GOUGES ON TOP OF STRINGER NR 13 NEAR BARREL NUT HOLE. REMOVED GOUGES ON TOP OF STRINGER NR 13 IAW DC-9 SRM 57-03.SDR ABXA9500083Stringer · gougedDURING C-CHECK INSPECTION WHILE COMPLYING WITH A.D. 90-18-03, S.B. 57-98, FOUND GOUGES IN STRINGER NR 11 BARREL NUT HOLE IN RIGHT WING. REMOVED GOUGES IN STRINGER NR 11 BARREL NUT HOLE IAW DC-9 SRM 57-03.SDR 95ZZZX715Switch · malfunctionSTL - FLT 106 - DURING APPROACH WHEN LANDING GEAR WAS EXTENDED, LT MLG UNSAFE LIGHT REMAINED ON. RECYCLED LANDING GEAR AND VISUALLY CHECKED LOCK. REPLACED LT MLG UPLOCK SWITCH, MFG P/N H14-6. LANDING GEAR POSITION AND WARNING SYTEM CHECKED NORMAL. CHECK OP
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