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 96ZZZM837Radar · malfunctionedFLT 509 - ATL-ATL, AIR RETURN, THE RADAR WAS MALFUNCTIONING AND THE WEATHER PRESENTATION WAS UNUSABLE. REMOVED AND REPLACED RADAR INDICATOR AND RADAR R/T. OPS CHECK NORMAL.SDR 9605699919Switch · dirtyDURING APPROACH INTO SLC, AMBER GEAR DOOR LIGHT CAME ON AFTER GEAR WAS EXTENDED. CREW DID GO-AROUND DURING WHICH GEAR DOOR LIGHT EXTINGUISHED. EMERGENCY EQUIPMENT REQUESTED AS A PRECAUTION. FLIGHT LANDED WITHOUT INCIDENT. CLEANED DOOR SWITCH AND OPERATION SDR 9605679991Coalescer Bag · dirtySHORTLY AFTER TAKEOFF, THE LAVATORY SMOKE DETECTORS WERE ACTIVATED BY SMOKE ENTERING THE CABIN FROM THE AIR CONDITIONING SYSTEM. THE FLIGHT RETURNED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND CHANGED THE AIR CONDITIONING COALESDR MWEA96055Pt 2 Line · ice buildupPILOT REPORTS UPON SPOOLING UP FOR TAKEOFF, THE NR 1 ENGINE EPR WOULD NOT RISE ABOVE 1.4 INDICATED. ALL OTHER PARAMETERS NORMAL. RETURN TO GATE. FOUND ICE IMBEDDED IN PT2 INLET. CLEANED ICE. RAN ENGINE TO TAKEOFF POWER. OPS CHECK GOOD.SDR ABXA9600357Angle · crackedDURING C-CHECK INSPECTION, FOUND A CRACK IN THE UPPER PYLON ATTACH ANGLE AT STA 980. REPAIRED IAW DC-9 SRM 54-04, FIGURE 10.SDR ABXA9600318Link · wornDURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND THE RIGHT MAIN LANDING GEAR OUTBOARD DOOR LINK WORN. REPLACED LINK IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR 96ZZZM683Engine · failedON FLT NR 236 - DFW-DFW - AIR RETURN AFTER TAKEOFF, LEFT ENGINE FAILED.SDR 96ZZZM682Engine · failedON FLT NR 236 - DFW - THE LEFT ENGINE FAILED AFTER TAKEOFF. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL PER MM 73-00, NO HELP. REMOVED AND REPLACED ENGINE PER MM 71-00, OPS CHECK AND LEAK CHECK GOOD. (M)SDR 9607679950Skin · crackedDURING M-CHECK, FOUND A CRACK IN THE MAIN CABIN DOOR CUTOUT SKIN, UPPER AFT CORNER. REPAIRED SKIN (P/N 5911406-5) PER EA 99-108518.SDR 9607669610Control Panel · malfunctionLOSS OF B-PHASE ITEMS ON NR 2 GENERATOR OCCURRED EN ROUTE. FLIGHT DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 GENERATOR CONTROL PANEL, OPERATIONAL CHECK NORMAL.SDR 9605719604Retract Mech · malfunctionedDURING ALTERNATE FUELING PROCEDURE, NOSE GEAR DOORS WERE OPENED ACCORDING TO MANUAL PROCEDURES. AFTER TAKEOFF, THE GEAR DOORS WOULD NOT CLOSE. THE AIRCRAFT RETURNED TO OMA AND LANDED WITHOUT INCIDENT. INSPECTED AND CLOSED NOSE GEAR DOORS MANUALLY. AIRCRAFTSDR MWEA96054Slide Cover · fell offCREW REPORTS, FWD ENTRY DOOR EVAC SLIDE COVER FELL OFF. REINSTALLED EVAC SLIDE COVER.SDR MWEA96052Skin · crackedDURING INSPECTION, FOUND CRACK IN RUDDER SKIN .5 INCH LENGTH ON LT SIDE 4 AFT OF CENTERLINE STA ZR 26.043. MAINTENANCE INSTALLED DOUBLER REPAIR IAW SRM 55-01 FIG 2. RECALCULATED BALANCE AND RETURNED A/C TO SERVICE.SDR MWEA96051Evac Slide Cover · fell offCREW REPORTS, FWD ENTRY DOOR EVACUATION SLIDE COVER FELL OFF. MAINT REINSTALLED EVACUATION SLIDE COVER.SDR 9607999611Chord · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE LEFT HORIZONTAL STABILIZER REAR SPAR AT THE OUTBOARD ELEVATOR HINGE BRACKET MOUNTING HOLES. REPAIRED THE UPPER AND LOWER SPAR CAPS PER EA 12-5510-9-C0794.SDR 9605669611Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE INTERCOSTAL ATTACH FITTING AT FS 996, LONGERON 28R. REPLACED FITTING PER SRM 51-30-02.SDR 9605659611Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN A LEFT ELEVATOR GEARED TAB HINGE FITTING. REPLACED FITTING (P/N 3918075-509) PER SRM 51-30-2.SDR 9605279610Epr Transmitter · malfunctionedNR 2 ENGINE EPR INDICATION DID NOT REACH TARGET ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EPR TRANSMITTER WITH A SERVICEABLE UNIT.SDR CAL960332Blkhd T-Cap · corrodedHOU - INSPECTION FOUND T-CAP CORRODED AT AFT BULKHEAD STATION 110 IN NLG WHEEL WELL RIGHT TUNNEL. THE CORROSION WAS REMOVED AND THE AREA WAS TREATED IAW SRM 51-10-3. (M)SDR 9605109983Pump · malfunctionedDURING CLIMBOUT, COCKPIT LIGHTS BEGAN FLICKERING AND LEFT AC GENERATOR LOAD METER INTERMITTENTLY PEGGED TO MAXIMUM. RIGHT HYDRAULIC PRESSURE WENT TO 3,000 PSI WITH ENGINE PUMPS AT LOW AND AUXILIARY PUMP SWITCH OFF. AUXILIARY PUMP CIRCUIT BREAKER ON LEFT GENESDR MWEA96050Wire · chafedCREW REPORTS, ABOVE ROW 5 C AND D OVERHEAD BIN THERE WAS A FLASH AND SUBSEQUENT SMOKE. REPLACED SIDEWALL LIGHT DISCONNECT DUE TO CHAFED WIRES AND LIGHT OPS CHECKED GOOD.SDR MWEA96049Evac Slide · fell offMAINT REPORTS, WHEN GALLEY SERVICE DOOR WAS OPENED THE EVACUATION SLIDE FELL OFF. REINSTALLED GALLEY DOOR EVAC SLIDE.SDR 96ZZZX2849Retract Mech · malfunctionedATL/ATL - FLT 495 - AIR RETURN, AFTER TAKEOFF, THERE WAS A LOUD WIND NOISE COMING FROM THE NOSE GEAR AREA. RECYCLED GEAR, HAD A RED NOSE GEAR LIGHT ON. LIGHT WENT OUT IN SIXTY SECONDS AND HAD A NORMAL LANDING. JACKED AIRCRAFT, ADJUSTED NOSE GEAR DOORS, CYCLSDR 9607989611Angle · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE MAIN CABIN DOOR UPPER CUSP ANGLE FS 200 AT LONGERON 18L. REPAIRED ANGLE PER EA 12-5310-9-C0733.SDR 9605259611Fitting · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK AND CORROSION IN THE FLOOR SUPPORT CORNER FITTING AT FS 996, LONGERON 18L LBL 50. REPLACED FITTING (P/N 5913100-1), PER SRM 51-30-5.SDR 9605249923Skin · crackedDURING LINE CHECK, FOUND A 3 INCH CRACK IN THE LEFT SIDE WINDOW BELT FS 237 TO 241, 10 O'CLOCK POSITION. REPLACED BELT (P/N 9911531-1), PER SRM 51-01 SEC 1 ITEM C.SDR MWEA96048Power Supply · inoperativeMAINTENANCE REPORTS, SEVERAL A/C INTERIOR EMERGENCY LIGHTS REMAINED ILLUMINATED WHEN A/C WAS POWERED DOWN. REPLACED TWO BATTERY POWER SUPPLIES AND OPS CHECK GOOD.SDR 96ZZZM680Bungee Cylinder · brokenON FLT 101 - ATL - AIR RETURN, AFTER GEAR RETRACTION THE LEFT GEAR UNSAFE LIGHT STAYED ON AND GEAR DOOR OPEN LIGHT STAYED ON, CYCLED ONCE, NO CHANGE. FOUND BUNGEE CYCLE PISTON ROD BROKEN. REPLACED PER MM 32-10. ACCOMPLISHED GEAR SWING. (M)SDR 9607219606Skin · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND A CRACK IN THE SKIN CUTOUT FOR THE LEFT PYLON AFT UPPER SPAR CAP STRAP FS 1038. REPAIRED SKIN (P/N 5952562-7) PER EA 99-109066.SDR 9604889951Uplock Latch · bindingDURING CLIMBOUT, RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FREED MOVEMENT TO RIGHT MAIN GEAR UPLOCK LATCH. OPERATIONAL CHECK NORMAL, AIRCRAFT RETURNED TO SERVICE.SDR CAL960279Skin · crackedHOU - INSPECTION FOUND A 4.5 INCH CRACK IN LEFT UPPER RUDDER SKIN. THE CRACKED AREA WAS ROUTED OUT. A FILLER AND DOUBLER REPAIR WERE FABRICATED AND INSTALLED IAW SRM 55-03. (M)SDR CAL960278Skin · crackedHOU - INSPECTION FOUND A 2 INCH CRACK BETWEEN FOUR RIVETS AT RIVET LINE FOR UPPER CAP AND A .5 INCH CRACK BETWEEN TWO RIVETS AT RIVET LINE FOR UPPER CAP IN RIGHT UPPER RUDDER SKIN. THE CRACKS WERE REPAIRED BY FABRICATING AND INSTALLING A DOUBLER IAW SRM 55-01SDR 9607979611Longeron · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE CENTER WING STR 20 FROM WS 58R TO 91R. REPAIRED THE STRINGER PER EA 12-5710-9-C0783.SDR CA960321511Slats · inoperative(CAN)AFTER TAKEOFF UNABLE TO RETRACT SLATS ALSO SLATS LEVER STIFF. MAINTENANCE ACTION INVOLVED LUBRICATING PEDESTAL MECHANISM AND WHEEL WELL CABLES. SLATS SYSTEM OPERATED SEVERAL TIMES.SDR 96ZZZM312Grd Sense Mech · out of adjustON FLT NR 550, ATL-ATL, AIR RETURN, AFTER TAKEOFF THE TAKEOFF WARNING HORN SOUNDED DURING FLAP RETRACTION. THE FLAP SLAT WERE RE-EXTENDED TO 5 DEGREES, DID NOT GET AIR MODE. AUTO SPOILER ' DO NOT USE' LIGHT WAS ON FOR LANDING. MAINTENANCE FOUND THE GROUND SSDR 9604799942Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND MID TO AFT CABIN EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERY PACKS AND OPERATIONAL CHECK NORMAL.SDR 96ZZZX2846Circuit Breaker · trippedWHILE SITTING AT GATE IN MCO MAKING PA ANNOUNCEMENTS, THE CIRCUIT BREAKER'S FOR PA, INTERPHONE, 'NO SMOKING' AND 'FASTEN SEAT BELT' LIGHTED SIGNS TRIPPED. SMOKE SMELL IN THE CABIN. ACCOMPLISHED VALUJET AIRLINES EO DC-9-3396005, SEAT BELT, NO SMOKING SIGN, PASDR 96ZZZX2541Pax Warn Sign · smokingWHILE SITTING AT GATE IN MCO MAKING PA ANNOUNCEMENTS, THE CIRCUIT BREAKER'S FOR PA INTERPHONE, 'NO SMOKING' AND 'FASTEN SEAT BELT' LIGHTED SIGNS TRIPPED. SMOKE SMELL IN THE CABIN. ACCOMPLISHED VALUJET AIRLINES EO DC-9-3396005, SEAT BELT, NO SMOKING SIGN, PASSDR 96ZZZM321Control Wheel · stuck openON FLT NR 363 - BOS-RDU, CAPTAIN COULD NOT PRESSURIZE THE CABIN IN MANUAL OR AUTO. MAINTENANCE FOUND THE OUTFLOW VALVE CONTROL WHEEL STUCK IN FULL OPEN POSITION. MAINTENANCE FREED WHEEL AND OPS CHECKED OK. (M)SDR CAL960189Retract Mech · malfunctionedFLT NR 1047 - CLE - THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF FROM CLE. THE GEAR WAS CYCLED AND THE NOSE GEAR GREEN LIGHT ILLUMINATED IMMEDIATELY. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. THE GEAR WAS SWUNG SEVERAL TIMES IAW MM 3SDR 96ZZZM645Seal · failedON FLT NR 183 - ATL-MSY - DIVERTED TO MGM, EN ROUTE TO MSY NR 2 ENGINE OIL QUANTITY WENT TO ZERO THEN OIL PRESSURE DROPPED TO 35 PSI, SHUT DOWN NR 2 ENGINE AND LANDED IN MGM. MAINTENANCE FOUND OIL LEAKING FROM THE STARTER OIL SEAL ON GEAR BOX. REMOVED STARTESDR 96ZZZX1464Generator · failedRDU/RDU - FLT 790 - AIR RETURN, AFTER TAKEOFF, RIGHT GENERATOR FAIL/CROSS TIE LOCK-OUT WARNING. C/W QRH PROCEDURES, DISCONNECTED RIGHT GENERATOR/CSD. ASSIGNED MEL 24-01-01 CONTROL NR DM7319.SDR 96ZZZX1451Dnlock Sw · malfunctionedBOS/RDU - FLT 361 - NO GREEN LIGHT ON LEFT MAIN GEAR WHEN LOWERED IN RDU. APPROPRIATE PROCEDURES WERE FOLLOWED AND EVENTUALLY LIGHT CAME ON STEADY. GEAR PINNED FOR TAXI. INSPECTED AND PINNED GEAR DOWN AND LOCKED FOR MAINTENANCE FERRY TO 31J. REPAIRED LEFTSDR 96ZZZM829Windshield · failedON FLT 229 - ATL-ATL, AIR RETURN, CAPTAINS WINDSHIELD SHATTERED (OUTER PANE) NO IMPACT. REMOVED AND REPLACED CAPTAINS SIDE WINDSHIELD IAW 56-10-2. NO DEFECTS NOTED.SDR 9607209606Doubler · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION IN THE FORWARD CARGO DOOR JAMB DOUBLER BETWEEN FS 389 TO 408. REPAIRED DOUBLER (P/N 9912455) PER EA 99-108777.SDR CA960321505Press.Controller · failed(CAN)AFTER TRAKEOFF AT FL.290, MASTER CAUTION LIGHT ILLUMINATED INDICATING A PRESSURIZATION PROBLEM. QRH DRILL CARRIED OUT, INITIATED EMERGENCY DESCENT AND MANUALLY DEPLOYED OXYGEN MASKS. ON RETURN MAINTEN ANCE ACTION INVOLVED CHANGING #1 AND #2 PRESSURIZATIONSDR 96ZZZX2339Engine · malfunctionedDFW/DFW - FLT 234 - AIR RETURN, THE RIGHT ENGINE WAS SLOW TO SPOOL UP ON TAKEOFF, DID NOT PRODUCE FULL POWER. INSPECTED INTAKE, EXHAUST, AND AIR RETURN FOR DAMAGE. FOUND NORMAL. RAN ENGINE AND TRIMMED WITHIN PARAMETERS OF TRIM CHART MM 71-00. (X)SDR 9606549605Bulkhead · corrodedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON THE FS 1046 CANTED BULKHEAD UPPER CAP BETWEEN LONGERONS 3L TO 6L. REPAIRED CAP PER EA 99-108995.SDR 9604969919Guide Pins · wornDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE TAIL CONE HANDLE AND THAT THE TAIL CONE DID NOT DROP. ALSO, FOUND 16 WORN GUIDE PINS AND 7 WORN PLATES. REPLACED THE PINS, PLATES AND ACCOMPLISHED EO 5350-01049, CHECKED OK.SDR 9604769924Fuel Control · failedNR 1 ENGINE EPR INDICATION WAS BELOW TARGET ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL CONTROL UNIT WITH A SERVICEABLE COMPONENT. SUBSEQUENT RUNUP WAS SATISFACTORY.
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