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 MWEA95143Eel Battery · dischargedCREW REPORTS THE LAST 4 TO 6 EMERGENCY FLOOR TRACK LIGHTS IN CABIN BLINKED ON IN CRUISE. PERFORMED OPS CHECK IAW MM 33-50-00. REPLACED D-CELL NICAD BATTERY IN AFT PACK AS PRECAUTION. OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVICE.SDR ABXA9500234Vane · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE LEFT WING UPPER MOVEABLE VANE. REPLACED VANE IAW DC-9 M.M. 27-51-2.SDR 95ZZZX1662Pump · failedPHL/ATL - FLT 225 - EXPERIENCED A LOSS OF HYDRAULIC PUMP PRESSURE ON THE RIGHT ENGINE. CREW TURNED ON THE AUXILIARY HYDRAULIC PUMP AND HAD SUFFICIENT PUMP PRESSURE AND NO LOSS OF HYDRAULIC FLUID. PLACED RIGHT HYDRAULIC PUMP ON MEL 29-5.SDR 9503779983Dnlock Switch · failedDURING CLIMB-OUT FROM MSP, LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR WAS RETRACTED. RECYCLED GEAR AND LIGHT EXTINGUISHED. FLIGHT CONTINUED TO DESTINATION (ORD) AND LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN GEAR DOWNLOCK SWITCH. OPERATIONSDR MWEA95142Nose Cowl · crackedDURING ROUTINE INSPECTION, THE LEFT ENGINE NOSE COWL WAS FOUND TO HAVE A 2 INCH CRACK ON LIP OF INLET BETWEEN TWO FASTENERS AT THE 4 O'CLOCK POSITION. REMOVED AND REPLACED WITH SERVICEABLE NOSE COWL. RETURNED A/C TO SERVICE.SDR 95ZZZW269Duct · failedSTL - FLT 658 - DURING CLIMB, THE NR 1 ENGINE (S/N 2107) WAS SHUTDOWN DUE TO OIL FILTER BYPASS LIGHT ILLUMINATION AND A DECREASE IN OIL QUANTITY. FOUND NOSE COWL ANTI-ICE DUCT, (P/N 7958591-501), RUPTURED, BLOWING HOT AIR ON BYPASS LIGHT SWITCH, MELTING SOLDSDR CAL950178Eel Batt · dischargedIAH - FLT 1859 - BOTH COCKPIT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. THE BATTERIES IN THE BATTERY PACK FOR THE COCKPIT EMERGENCY LIGHTS WERE REPLACED. OPERATION OF THE COCKPIT EMERGENCY LIGHTS WERE RESTORED. (W)SDR ABXA9500237Vane · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE LEFT WING INBOARD FLAP FIXED VANE. REPLACED VANE IAW DC-9 M.M. 27-51-3.SDR ABXA9500236Vane · corrodedDURING C-CHECK INSPECTION, FOUND LEVEL II CORROSION ON THE LEFT WING OUTBOARD FLAP FIXED VANE. REPLACED VANE IAW DC-9 M.M. 27-51-3.SDR ABXA9500235Vane · crackedDURING C-CHECK INSPECTION, FOUND THE LEFT WING CENTER FIXED VANE CRACKED AT THE CENTER SUPPORT. REPLACED VANE IAW DC-9 M.M. 27-51-3.SDR 9503519940Wire · chafedTAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED DURING CRUISE FLIGHT AT 33,000 FEET. FLIGHT DIVERTED TO BIS AND LANDED WITHOUT INCIDENT. FOUND WIRING TO RIGHT TEMPERATURE SENSOR CHAFED AND GROUNDING ON TUBING. REPLACED THE RIGHT TEMPERATURE SENSOR AND ISDR 9503579926Le Spar · crackedDURING "A" CHECK, FOUND 9.5 INCH CRACK IN THE RIGHT INBOARD FLIGHT SPOILER LEADING EDGE SPAR. REPLACED SPOILER PER CITEXT 90-2760-1-9901.SDR MWEA95140Door Pan · crackedDURING ROUTINE INSP THE AFT CARGO DOOR PAN WAS FOUND TO BE CRACKED AT A PREVIOUS REPAIR ON FWD LOWER SIDE. REPAIRED AFT CARGO DOOR IAW SRM 52-05, FIG 50. RETURNED A/C TO SERVICE.SDR 96ZZZM1404Tee Cap · crackedRIGHT WING LOWER TEE CAP CRACKED IN THE RADIUS AFT OF STRINGER 16 EXTENDING UNDERNEATH STRINGER 15 (AD90-18-03 UPDATED TO 96-10-11). REMOVED AND REPLACED STA XCW 58.5 RIGHT AND LEFT TEE CAPS IAW MDC SERVICE BULLETING 57-98 REV 8 DATED 3-15-91 AND WORKORDER NRSDR ABXA9500146Bushing · missingDURING COMPLIANCE OF A.D. 91-22-07; A.S.B. 32-244, FOUND BUSHING MISSING IN RIGHT MAIN LANDING GEAR OUTBOARD DOOR WING MOUNTED HINGE. REPLACED BUSHING IAW DC-9 OVERHAUL MANUAL 32-10-6.SDR 95ZZZW258Harness · shortedSTL - AFTER TAKEOFF VERY LOUD BANG, AND ELECTRICAL SMOKE ENTERED COCKPIT. SHUT-OFF ELECTRICAL POWER TO GALLEY. FOUND ELECTRICAL CONNECTOR FOR NR 2 COFFEEMAKER SHORTED. REPLACED NR 2 COFFEEMAKER AND ELECTRICAL HARNESS (P/N WK6-236318). OPERATION OF NR 2 COFSDR 95ZZZW228Connector · shortedSTL - AFTER TAKEOFF VERY LOUD BANG, AND ELECTRICAL SMOKE ENTERED COCKPIT. SHUT OFF ELECTRICAL POWER TO GALLEY. FOUND ELECTRICAL CONNECTOR FOR NR 2 COFFEEMAKER SHORTED. REPLACED NR 2 COFFEEMAKER AND ELECTRICAL HARNESS, MFG P/N WK-236318. OPERATION OF NR 2 COFSDR 9503349962Dnlock Switch · malfunctionedLEFT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION IN DSM. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT MAIN GEAR DOWNLOCK SWITCH. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR ABXA9500121Retainer · crackedDURING D-CHECK ACCEPTANCE INSPECTION WHILE COMPLYING WITH AD 90-18-03; SB 56-11 REV 3, FOUND THE RIGHT CLEARVIEW WINDOW FRAME CRACKED IN THE UPPER AFT CORNER. REPLACED DOUBLER IAW DC-9 SRM 56-01 AND ABX REA D956-13036-SB.SDR CAL950153Bungee Cyl · inoperativeFLT NR 1647 - CLE - THE LEFT MLG RED UNSAFE LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND BOTH RED LIGHTS EXTINGUISHED WITH THREE GREEN GEAR LIGHTS INDICATED. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDESDR 9503179945Strut · deflatedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF DUE TO GROUND SHIFT FAILURE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. INSPECTED GROUND SHIFT LINKAGE AND CABLES WITH NO PROBLEMS FOUND. PERFORMED FULL SERVICE OF NOSE LANDING GEAR STRUT. AIRCRAFT RETUSDR 9503089923Clips · out of adjustDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL BOTH THE INTERIOR AND EXTERIOR HANDLES FROM THE CLIPS. ADJUSTED THE CLIPS. CHECKED OK.SDR 95ZZZX2283Regulator · failedFLL/ATL - FLT 128 - EXPERIENCED AN ELECTRICAL MALFUNCTION WHEN THE RIGHT GENERATOR DROPPED OFF-LINE AFTER THE AIRCRAFT STARTED ITS ROLL FOR TAKEOFF. PILOT POWERED BACK AND PROCEEDED BACK TO THE GATE. CREW RESET CIRCUIT BREAKERS AND GENERATOR RESET TO NORMAL SDR CAL950148Eel Batt · dischargedJAX - FLT 1521 - THE FWD OVERWING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING A PREFLIGHT CHECK. THE BATTERIES FOR THE FWD OVERWING EMERGENCY EXIT LIGHT WERE REMOVED AND REPLACED. OPERATION OF THE EMERGENCY EXIT LIGHT WAS RESTORED. (W)SDR ABXA95107Bushing · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND SECONDARY LINKAGE CLEVIS ON RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVE ROD WORN. REPLACED BUSHING ON LINK ASSEMBLY IAW DC-9 MM 32-10-0.SDR CAL950157Press Panel · crackedHOU - INSPECTION FOUND A 4 INCH CRACK IN NOSE WHEEL WELL UPPER PRESSURE PANEL AT STATION 83.55. THE PRESSURE PANEL WAS REPAIRED IAW ECRA 5310-03031. (Z)SDR ABXA9500335Stringer · corrodedDURING C-CHECK INSPECTION WHILE COMPLYING WITH AD 90-18-03, SB 57-98, FOUND LEVEL I CORROSION ON STRINGER NR 12 NEAR T-CAP. REMOVED CORROSION IAW DC-9 SRM 57-03.SDR MWEA95132Skin · puncturedDURING ROUTINE MAINTENANCE, FOUND 1 INCH BY .75 INCH PUNCTURE IN AFT CARGO DOOR OUTER SKIN. REMOVED DAMAGED AREA, INSTALLED DOUBLER IAW DAC SRM 52-01, FIG 2, SHEET 3. AIRCRAFT RETURNED TO SERVICE.SDR ABXA95106Rod End · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVE ROD END WORN. REPLACED ROD END ARM ASSEMBLY IAW DC-9 MM 32-10-0.SDR ABXA95104Bolt · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND SECONDARY LINKAGE CLEVIS ON LEFT MAIN OUTBOARD GEAR DOOR DRIVE ROD WORN. REPLACED BOLT ON LINK ASSEMBLY IAW DC-9 MM 32-10-0.SDR ABXA9500108Bolt · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND SECONDARY LINKAGE CLEVIS ON RIGHT MAIN LANDING GEAR OUTBOARD DOOR DRIVE ROD WORN. REPLACED BOLT ON LINK ASSEMBLY IAW DC-9 MM 32-10-0.SDR ABXA9500105Bushing · wornDURING COMPLIANCE OF AD 91-22-07, ASB 32-244, FOUND SECONDARY LINKAGE CLEVIS ON LEFT MAIN OUTBOARD GEAR DOOR DRIVE ROD WORN. REPLACED BUSHING ON LINK ASSEMBLY ON LEFT MAIN GEAR OUBOARD DRIVE ROD IAW DC-9 MM 32-10-0.SDR MWEA95137Engine · failedPILOT REPORTS WITH CLIMB POWER THE EPR AND N1 ON LEFT ENGINE DROPPED SIGNIFICANTLY. ALL OTHER INDICATIONS ON LEFT ENGINE NORMAL AND EQUAL TO RIGHT ENGINE. ADVANCING LEFT THROTTLE CLIMB POWER ON EPR GAUGE INCREASED LT ENGINE EGT & N2 TO NEAR LIMITS. IN CRUISSDR MWEA95131Hinge · crackedDURING C-CHECK INSP, ON THE LEFT MAIN LANDING GEAR OUTBOARD DOOR HINGE, FOUND 1 HINGE LOBE CRACKED. REPLACED HINGE PER DAC SB 32-244 AND SRM 51-30. A/C RETURNED TO SERVICE.SDR 9504769982Skin · loose fastenersDURING LINE CHECK, FOUND APPROXIMATELY 40 LOOSE FASTENERS ON BOTH SIDES OF THE RUDDER. REPLACED FASTENERS.SDR 9502859984Duct · tornFLIGHT ATTENDANT REPORTED SMOKE IN CABIN DURING CLIMB-OUT THROUGH 12,000 FEET. AIRFLOW WAS VERY LOW AND TEMPERATURES IN COCKPIT AND CABIN WERE HIGH. MIX VALVE ON LEFT SIDE WAS NOTED AS BEING FULL COLD. SELECTED MANUAL POSITION AND MOVED IT SLIGHTLY TOWARD HSDR MWEA95134Evac Slide · slow to inflateDURING A TIME CHANGE FOR A TAIL SLIDE (3 YR INTERVAL), A FUNCTIONAL TEST OF THE SLIDE REVEALED A 20 SECOND HESITATION BEFORE THE SLIDE STARTED TO INFLATE. SLIDE SENT TO VENDOR FOR BENCH CHECK.SDR ABXA9500203Door Jamb · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND LEVEL II CORROSION ON FORWARD LOWER CARGO COMPARTMENT DOOR JAMB AT LONGERON 29R FS 370 TO FS 427. REPLACED DOOR JAMB AND U-CHANNEL IAW DC-9 SRM CHAPTER 51-30-2.SDR ABXA9500152Doubler · damagedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE INNER DOUBLER CUT OUT AT BOTTOM OF LOWER CARGO DOOR JAMB AT FS 408. REPAIRED INNER DOUBLER IAW ABX REA D953-10895-MR.SDR 95ZZZZ131Air Distr · odorFLT 462 - TPA-IAD - FLIGHT ATTENDANT REPORTED FAINT SMELL OF SMOKE IN CABIN ON APPROACH AT 8000 FEET. PRESSURE DUMPED AT SAME TIME. BOTH AIRFOIL AND ENGINE ANTI-ICE WERE ON. DUCT TEMP AND DUCT PRESSURE WERE OK. NO AIRFOIL TEMP HIGH LIGHTS ON. OPERATIONS CSDR ABXA9500322Fitting · corrodedDURING D-CHECK ACCEPTANCE INSPECTION WHILE PERFORMING DC-9 RUDDER OFF WING INSPECTION FOUND LEVEL II CORROSION ON FITTING. REPLACED FITTING IAW DC-9 OVERHAUL MANUAL 27-20-1.SDR ABXA9500222Floor Beam · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON THE L0WER FLANGE OF THE FLOOR BEAM AT STA 935, RBL 15. REPAIRED FLOOR BEAM IAW ABX REA D953-10973-MR.SDR 95ZZZX1625Position Switch · malfunctionATL - FLT 134 - DURING APPROACH, LEFT GEAR UNSAFE LIGHT INITIATED A GO-AROUND. LANDED IN ATL, NO TROUBLE REPORTED. REMOVED AND REPLACED THE LEFT GEAR DOWNLOCK SWITCH AND CONNECTOR.SDR 95ZZZX1624Engine · power lossIAD/PBI - FLIGHT 477 - RUNWAY CONDITIONS, STANDING SLUSH. DURING TAKEOFF, NR 2 ENGINE EXPERIENCED A LOUD BANG ACCOMPANIED BY DECAYING OF THE NR 2 ENGINE INSTRUMENTS. INITIATED A REJECTED TAKEOFF AT 110 KNOTS. ACCOMPLISHED A VISUAL INSPECTION OF NR 2 ENGINE SDR 9502839985Hyd Pump · malfunctionedLOSS OF LEFT HYDRAULIC SYSTEM PRESSURE OCCURRED AFTER TAKEOFF. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP. LEAK AND OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR ABXA9500153Door · damagedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE FORWARD AIRSTAIR DOOR HAD A REPAIR ON A CRACK AT THE INNER RIB THAT WAS NOT IAW THE SRM. REPAIRED IAW ABX REA D952-10953-MR.SDR ABXA9500150Doubler · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE STEEL PLATE ALONG THE CENTER WINDSHIELD LOWER FRAME RUSTED AND HAD POPPED RIVETS. CLEANED AND TREATED PLATE IAW DC-9 SRM CHAPTER 51-10-3 AND REPLACED FASTENERS IAW DC-9 SRM CHAPTERS 51-30-2, 51-30-5 AND ABX REA SDR MWEA95128Water Line · leakingPILOT REPORTS LANDING GEAR HANDLE TOOK MORE THAN NORMAL FORCE TO PUT IN DOWN POSITION PRIOR TO LANDING. ALSO, PILOT REPORTED DURING LANDING AS BRAKES WERE APPLIED THERE WAS LITTLE BRAKING AND THE PEDAL PRESSURE FELT ERRATIC. PEDAL PRESSURE FELT ERRATIC DURINSDR CAL950119Hyd Line · leakingFLT NR 1688 - JAX - THE RT HYDRAULIC SYSTEM FLUID QUANTITY WAS LOST WHILE EN ROUTE TO JAX. 'ABNORMAL' PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED IN JAX WITHOUT INCIDENT. MAINTENANCE FOUND THE ELECTRIC PUMP HYDRAULIC PRESSURE LINE TO FILTER LINE LESDR 9502609951Cable · frayedDURING PERIODIC CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE THE TAILCONE USING THE INTERIOR HANDLE. ALSO, FOUND THE TAILCONE CABLE FRAYED BETWEEN THE RIGHT SIDE LATCHES AT THE LOWER PULLEY. REPLACED THE CABLE AND RERIGGED THE TAILCONE.
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