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 9624439612Fuel Cap · brokenON TAKEOFF, TOWER NOTICED FUEL VENTING FROM RIGHT WING. TAKEOFF WAS ABORTED AT 90 KTS. MAINTENANCE FOUND OVERWING FUEL CAP BROKEN AND POPPED OFF. INSPECTED CAP FLANGE AND REPLACED CAP. AIRCRAFT REFUELED AND APPROVED SERVICE.SDR 9624269618Retainer · corrodedDURING M-CHECK, FOUND CORROSION IN ONE OF THE FIRST OFFICER'S WINDSHIELD RETAINERS. REPLACED RETAINER (P/N 9957862-506) PER SRM 51-10-03.SDR MWEA96627Power Supply · inoperativeDURING C-CHECK, FOUND AFT SECTION OF EMERGENCY LIGHTS IN CABIN CEILING WERE DIM DURING TEST. MAINTENANCE REPLACED BATTERY POWER SUPPLIES. OPS CHECK GOOD, RETURNED A/C TO SERVICE.SDR 9624369920Light · inoperativeDURING LINE CHECK, FOUND FORWARD INTERIOR OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERIES AND POWER SUPPLY. OPERATIONAL CHECK OK.SDR 9624079920Battery · dischargedDURING LINE CHECK, FOUND THAT THE INTERIOR OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. REPLACED THE BATTERY PACK/POWER SUPPLY. CHECKED OK.SDR MWEA96624Pan · corrodedDURING C-CHECK, MAINT SPLICED IN NEW LOWER DOOR JAMB PAN SECTION IN AFT CARGO DOOR CUTOUT WHICH HAD AREA OF CORROSION IAW SRM 53-05, FIG 44.SDR ABXA9700675Vane · dentedTHE RIGHT INBOARD FLAP VANE WAS DEEPLY DENTED AND DELAMINATED ON THE UPPER SIDE AT THE CENTER RUBSTRIPS. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKINS IAW DC-9 SRM.SDR 9623589986Floor Beam · crackedDURING H-CHECK, FOUND A 4 INCH CRACK IN THE FS 680 FLOOR BEAM AT THE RIGHT FRAME ATTACH POINT. REPLACED FLOOR BEAM (P/N 9915527-506, PSE 53.09.016) PER SRM 51-30-2, 51-30-5.SDR 97ZZZX1780Stringer · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, FOUND STR 29R CORRODED, STA 945 TO STA 965. MECHANICALLY REMOVED CORROSION FROM STRINGER AND INTERCOSTAL, P/N 99582339. STRINGER WITHIN LIMITS, INTERCOSTAL REPLACED IAW DC9 SRM'S 51-10-3, 51-10-4, AND 51-30-5.SDR 9625079601Clamp · brokenLOSS OF PRESSURIZATION OCCURRED AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND FLIGHT WAS RETURNED TO DTW. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BROKEN CLAMP ON LEFT AIR CYCLE MACHINE OUTLET DUCT. REPLACED CLAMP, OPERATIONAL CHECK NORMAL.SDR 9623689606Wire · brokenDURING PERIODIC CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE. OPERATIONAL CHECK NORMAL.SDR ABXA9700227Arm · looseDURING COMPLIANCE OF AD 91-22-07; ASB 32-244, FOUND RIGHT HAND MAIN LANDING GEAR OUTBOARD DOOR LINKAGE ARM LOOSE/WORN. REMOVED AND REPLACED BOLT AND SHIMMED LINKAGE ARM IAW DC-9 M/M 20-16-0.SDR ABXA9700225Arm · looseDURING COMPLIANCE WITH AD 91-22-07; ASB 32-244, FOUND LEFT HAND MAIN LANDING GEAR OUTBOARD DOOR ARTICULATING DOOR TO HAVE EXCESSIVE PLAY. REMOVED AND REPLACED BOLT AND SHIMMED LINKAGE ARM IAW DC-9 M/M 20-16-0.SDR 97ZZZX1782Floor Beam · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, AT FS 218 TO FS 237 BL ZERO THE FLOOR BEAM WAS FOUND WITH CORROSION. REMOVED CORRODED T-CAP, FABBED AND INSTALLED H-CHANNEL, L-ANGLE, 2 EACH IAW DC9 SRM'S 53-01 FIG 2, 51-30-2 AND 51-10-3.SDR 97ZZZX1781Longeron · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP, FOUND LONGERON 29L CORRODED BETWEEN STA 389 - STA 408 AROUND NUTPLATES FOR RADIO ALTIMETER NR 1. REMOVED LONGERON 29L AND 30 FOR ACCESS TO CORROSION. UPON REMOVAL OF LONGERON 30, A 5 INCH CRACK WAS FOUND IN THE FACSDR 96NK215Light Assy · inopLOG PAGE 027664. FWD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY. OPS NORMAL IAW MM 33-53. (X)SDR 9624249951Frame · corrodedDURING H-CHECK, FOUND CORROSION ON THE FS 218 FRAME LOWER CHORD AT LONGERON 30. REPAIRED FRAME (P/N S 2777930-5) PER EA 99-109580.SDR 9623859924Frame · crackedDURING H-CHECK, FOUND A 2.5 INCH CRACK IN THE FS 658L FRAME LOWER OUTBOARD LEG. REPAIRED FRAME (PSE 53.09.013) PER SRM 51-30, 53-03.SDR 9623849924Frame · crackedDURING H-CHECK, FOUND A 2 INCH CRACK IN THE FS 639R FRAME LOWER OUTBOARD LEG. REPAIRED FRAME (PSE 53.04.014) PER SRM 51-10, 51-30, 53-03.SDR 9623749922Press Amplifier · malfunctionedLOSS OF CABIN PRESSURIZATION OCCURRED DURING FLIGHT AT 35,000 FEET. CABIN ALTITUDE REACHED 10,000 FEET WITH MASTER WARNING/CABIN PRESSURE ANNUNCIATOR LIGHTS ILLUMINATED. CAPTAIN DECLARED AN EMERGENCY AND SUCCESSFUL DESCENT WAS MADE TO 16,000 FEET. FLIGHT COSDR 9623739984Hsi · malfunctionedCAPTAIN'S HORIZONTAL SITUATION INDICATOR BEGAN STICKING ON HEADINGS DURING TURNS. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CAPTAIN'S HORIZONTAL SITUATION INDICATOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR 9623719985Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL.SDR 9623709940Wire · misinstalledDURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND WIRES AT CANNON PLUG RECEPTACLES R5-4009 PINS L AND M REVERSED. CORRECTED WIRING AT RECEPTACLE. OPERATIONAL CHECK NORMAL.SDR 9623699918Wire · misinstalledDURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND WIRES AT FLIGHT ATTENDANT SWITCH REVERSED. OPERATIONAL CHECK NORMAL.SDR GTIA96NK217Trapezoidal Pnl · crackedDURING INSPECTION OF LEFT AND RIGHT TRAPEZOIDAL PANEL PER SERVICE BULLETIN 53-182 RIGHT TRAP PANEL CRACKED EXTENDING FROM LEADING EDGE OF PANEL TO SECOND FASTENER. EDDY CURRENT BOLT HOLE INSPECTION CONFIRMS CRACK IS ONLY FROM FIRST HOLE TO FRONT EDGE OF PANELSDR GTIA96NK216Trapezoidal Pnl · crackedDURING INSPECTION OF LEFT AND RIGHT TRAPEZOIDAL PANEL PER S/B 53-182. LEFT TRAP PANEL CRACKED EXTENDED BEYOND EXISTING APPROVED SRM 57-09 FIGURE 6 SHEET 4 REPAIR IT RUNS PAST 4 FASTENER. DAC NOTIFIED ROUTED OUT CRACKED AREA .090 PAST AFT EDGE OF 4TH HOLE. ESDR 9624239951Skin · corrodedDURING H-CHECK, FOUND CORROSION ON THE FUSELGE SKIN AND FINGER DOUBLER AT FS 510 FROM LONGERON 29L TO 29R. REPAIRED SKIN (P/N 5911412-191, -55).SDR 9624229951Longeron · corrodedDURING H-CHECK, FOUND CORROSION AT LONGERONS 29L AND 29R AT FS 579. REPAIRED LONGERONS (P/N 3920596-1) PER EA 99-120176, 99-120174.SDR 9623469922Relay · malfunctionedDURING DESCENT INTO EWR, THE LANDING GEAR WARNING CIRCUIT BREAKER TRIPPED. NO GREEN GEAR DOWNLOCK LIGHTS WERE ILLUMINATED AFTER GEAR WAS EXTENDED FOR LANDING. CREW VISUALLY CONFIRMED GEARS TO BE DOWN AND LOCKED THROUGH PERISCOPES. EMERGENCY EQUIPMENT WAS CASDR 9623449941Downlock Switch · malfunctionedDURING APPROACH, THE RIGHT MAIN LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE ON GEAR EXTENSION. RECYCLED GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT MAIN GEAR DOWNLOCK SWITCH AND LANDING GEAR LEVERSDR CA961118010Actuator · failed(CAN) ON APPROACH LOST RIGHT HYDRAULIC SYSTEM (QUANTITY AND PRESSURE). MANUAL GEAR EXTENSION CARRIED OUT AND AIRCRAFT LANDED SAFELY. MAINTENANCE ACTION INVOLVED REPLACING RH MAIN LANDING GEAR RETRACT ACTUATOR, ENGINE DRIVEN HYDRAULIC PUMP P/N 314195, CASE DRAISDR CA961118009Strut · collapsed(CAN) AFTER GEAR SELECTED UP NOSE GEAR UNSAFE LIGHT ILLUMINATED AND LOUD NOISE HEARD COMING FROM VICINITY OF NOSE GEAR AREA. GEAR RECYCLED TWICE, NO CHANGE. MAINTENANCE CHECK REVEALED NOSE GEAR OLEO COLLAPSED. NOSE GEAR OLEO SERVICED AND SYSTEM CHECKED SERVICESDR 9623339985Roller Bracket · looseDURING CLIMBOUT, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. FLIGHT CONTINUED TO DESTINATION AT REDUCED SPEED AND AIRCRAFT LANDED WITHOUT INCIDENT. NO VIBRATION WAS EVER ENCOUNTERED DURING FLIGHT. MAINTENANCE FOUND LEFT MAIN GEAR DOORSDR MWEA96620Battery Pack · dischargedFWD OVERWING EMERGENCY EXIT LIGHT ON LT AND RT SIDES VERY DIM. FOUND BATTERY PACK NOT CHARGING. REMOVED AND REPLACED BATTERIES AND BATTERY PACK FOR FWD OVERWING EXIT LIGHT.SDR 9623349919Indication Bulbs · failedDURING APPROACH, NOSE GEAR DOWNLOCK GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. CREW EXECUTED GO-AROUND PROCEDURES AND TOWER REPORTED THAT GEAR APPEARED TO BE DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR GREEN ISDR CALA9601562Skin · crackedINSPECTION FOUND A .8750 INCH CRACK IN SKIN COMING FROM FASTENER HOLE AT STA 200, FOUR INCHES ABOVE L21L. A .1250 INCH CRACK WAS ALSO FOUND IN SKIN AT STA 200, APPROXIMATELY FOUR INCHES ABOVE L20L. THE CRACKS WERE STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLSDR CALA9601541Duct · crackedTHE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED SHORTLY AFTER TAKEOFF. THE FIRE WARNING CEASED AFTER THE ENGINE THROTTLE WAS RETARDED LESS THAN TEN PERCENT. BOTH FIRE LOOPS TESTED NORMAL AND ALL ENGINE INDICATIONS WERE NORMAL. THE FLIGHT CONTINUED AT SDR 96NK214Window · delaminatedLOG PAGE NR 028273, ITEM NR P782. CLIMBING THROUGH 10,000 FEET, HEARD LOUD BANG. RT DV WINDOW APPEARED TO DELAMINATE AT FWD EDGE. RETURNED TO DTW. INSP F/O'S (CAPT) CLEARVIEW WINDOW AND FOUND ROUGH EDGE DELAMINATED ON FWD EDGE OF WINDOW, NO CORRECTIVE ACTISDR 9624209951Fitting · corrodedDURING H-CHECK, FOUND CORROSION ON THE NR 2 PYLON LOWER FORWARD SURFACE BEAVER TAIL FITTING AND LOWER SPAR CHORD. REPLACED FITTING AND REMOVED SPAR CORROSION PER EA 99-120169.SDR 9623809924Fitting · corrodedDURING H-CHECK, FOUND CORROSION IN THE FUEL TANK TO FUSELAGE ATTACH FITTING BETWEEN FS 598 TO 617. REPLACED FITTING PER SRM 51-10, 51-30.SDR 9623329941Downlock Bulb · failedDURING APPROACH, THE RIGHT MAIN GEAR DOWNLOCK GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR WAS EXTENDED. RECYCLED GEAR TWO TIMES AND NORMAL INDICATIONS WERE ACHIEVED. CREW REPLACED ONE RIGHT MAIN GEAR GREEN INDICATION BULB. AIRCRAFT LANDED WITHOUT INCIDENT. DSDR 9623269987Latch Arm · wornDURING LINE CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE EXTERIOR TAILCONE HANDLE FROM THE CLIPS. ALSO, FOUND A WORN UPPER LEFT LATCH ARM AND AN INCORRECT LOWER RIGHT LATCH HOUSING. ADJUSTED THE CLIPS AND REPLACED THE LATCH ARM AND LATCH HOUSINSDR CA961112034Coalescer Bag · saturated(CAN) DURIG DEPARTURE CHECK WITH APU RUNNING SUPPLYING PRESSURE ON LEFT HAND AIR CONDITIONING PACK A STRONG ODOUR WITH LIGHT SMOKE WAS NOTED IN THE CABIN AND DUCT TEMPERATURE AROUND 70 DEGREES. LEFT HAND COALESCER BAG CHANGED. ALSO CHECKED AIR CYLING MACHINE FSDR 9623169923Power Supply · malfunctionedDURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EXIT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL.SDR 9623159917Uplock Switch · malfunctionedDURING CLIMBOUT FROM ORD, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. COCKPIT OPERATING MANUAL PROCEDURES WERE FOLLOWED AND LIGHT STAYED ON. FLIGHT WAS CONTINUED TO DESTINATION (MSP) AT REDUCED SPEED AND LANDED WITHOUT INCIDENT. MASDR CALA9601528Ckt Breaker · failedTHE B-PHASE CIRCUIT BREAKER ON LEFT AC BUS POPPED FOLLOWED BY ALL FORWARD LT, RT AND CENTER FUEL BOOST PUMP CB. THE A-PHASE CIRCUIT BREAKER ON RADIO RACK COOLING FAN POPPED AND LIGHTS ON RT SIDE IN CABIN WENT OUT AS WELL AS CAPT'S INSTRUMENT LIGHTS, VOR AND RSDR 9624189951Frame · corrodedDURING H-CHECK, FOUND CORROSION ON THE FS 756 BULKHEAD FRAME T-CHORD AT LONGERON 29L. REPAIRED FRAME (P/N 9958212-3) PER EA 99-109572.SDR 9623559618Fitting · corrodedDURING M-CHECK, FOUND CORROSION IN THE FS 935 LEFT SIDE CUSP WEB. REPLACED FRAME END FITTING AND WEB PER SRM 51-10-2, 51-30-2, AND 53-01.SDR 9624169951Skin · delaminatedDURING H-CHECK, FOUND DELAMINATION IN THE LEFT WING FLAP TRAILING EDGE UPPER SKIN AT XFLS 187-235. REPAIRED SKIN (P/N 9957578-503) PER EA 99-120171.SDR 9623539618Fitting · corrodedDURING M-CHECK, FOUND CORROSION IN THE FIRST OFFICER'S SLIDING WINDOW LOWER AFT FITTING AND STOP PLATE. REPLACED BOTH PER SRM 51-30-00.
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